Module 07.Maintenance Practice
01. Safety Precautions Aircraft and Workshop.
Question Number. 1 A dry powder extinguisher is coloured.
Option A. green.
Option B. red.
Option C. blue.
Correct Answer is. blue.
Explanation. BS EN3.
Question Number. 2. Acetylene gas forms an explosive
compound with.
Option A. tin
and silver.
Option B. tin
and copper.
Option C. copper
and silver.
Correct Answer is. copper
and silver.
Explanation. NIL.
Question Number. 3. When mixing acid and water.
Option A. the
acid should always be added to the water.
Option B. it
does not matter which way the two are mixed.
Option C. the
water should always be added to the acid.
Correct Answer is. the
acid should always be added to the water.
Explanation. NIL.
Question Number. 4. You are involved with a fire caused by
titanium swarf. What type of extinguishant should you use to deal with the
fire?.
Option A. Dry
asbestos wool and chalk powder.
Option B. CO2.
Option C. Chemical
foam.
Correct Answer is. Dry
asbestos wool and chalk powder.
Explanation. BL/6-18
12.5.
Question Number. 5. An aircraft should not be refueled
when.
Option A. the
APU is running.
Option B. navigation
and landing light in operation.
Option C. within
10 metres (30 feet) of radar operating.
Correct Answer is. within
10 metres (30 feet) of radar operating.
Explanation. AL/3-8
2.1.6, GOL/1-1 7.3.2.
Question Number. 6. The minimum 'no smoking' zone around an
aircraft when refuelling is.
Option A. 15m.
Option B. 10m.
Option C. 6m.
Correct Answer is. 6m.
Explanation. Leaflet
5-1 2.2.2.
Question Number. 7. A CO2 extinguisher is used
on.
Option A. solid,
liquid, hot metal and electrical fires.
Option B. solid,
liquid and electrical fires.
Option C. solid
and liquid fires.
Correct Answer is. solid,
liquid and electrical fires.
Explanation. Hot
metal and liquid fires would be extinguished with foam.
Question Number. 8. In an oxygen system, if the pressure
drops to 500 PSI, it.
Option A. causes
anoxia.
Option B. begins
to overheat.
Option C. blocks
the oxygen system regulator.
Correct Answer is. blocks
the oxygen system regulator.
Explanation. At low
pressure, air can mix with the oxygen. The moisture in the air freezes as the
gas expands on exit of the system and blocks the regulator. Jeppesen A&P
Airframe Technician Page 14-17.
Question Number. 9. After working with epoxy resins, how is
natural oil returned to the skin?.
Option A. Epoxy
removing cream.
Option B. Refatting
cream.
Option C. Acetone/lanolin
mixture.
Correct Answer is. Acetone/lanolin
mixture.
Explanation. Acetone
is used to remove epoxy resin, but it dries the skin, so it is mixed with
lanolin to prevent this (same mixture as nail varnish remover).
Question Number. 10. Neither oil nor grease should be used as
a lubricant on couplings or pipelines carrying.
Option A. Oxygen.
Option B. Kerosene.
Option C. Nitrogen.
Correct Answer is. Oxygen.
Explanation. AL/3-25
5.4 (vi).
Question Number. 11. Which type of extinguisher can be used
for an electric fire?.
Option A. Foam.
Option B. Water.
Option C. CO2.
Correct Answer is. CO2.
Explanation. AL/3-10
3.3.
Question Number. 12. The colour of CO2 type fire
extinguisher is.
Option A. red.
Option B. black.
Option C. green.
Correct Answer is. black.
Explanation. NIL.
Question Number. 13. Which type of extinguisher can be used
for engine fire?.
Option A. CO2.
Option B. BCF.
Option C. Water.
Correct Answer is. CO2.
Explanation.
Leaflet 5-1 4.2.4 (a).
Question Number. 14. Fire on landing gear brake should be
extinguished with.
Option A. dry
powder extinguisher.
Option B. carbon
dioxide extinguisher.
Option C. water
extinguisher.
Correct Answer is. dry
powder extinguisher.
Explanation. AL/3-19
10.4. Jeppesen A&P Mechanics Handbook Page 503, CAAIP S Leaflet 5-8 10.4.
Question Number. 15. Which type of fire extinguishers can be
used in the cabin?.
Option A. C.T.C.
Option B. water
or B.C.F.
Option C. M.B.
Correct Answer is. water
or B.C.F.
Explanation. Methyl
Bromide and CTC extinguishers are toxic. Jeppesen A&P Mechanics Handbook
Page 502 and 504.
Question Number. 16. Risk assessments should only be carried
out on.
Option A. all
tasks and processes that are performed.
Option B. tasks
using hazardous chemicals.
Option C. tasks
carried out above the height of 6 foot.
Correct Answer is. all
tasks and processes that are performed.
Explanation. NIL.
Question Number. 17. The most appropriate fire extinguisher
for an aircraft wheel and brake fire would be.
Option A. carbon
dioxide.
Option B. dry
powder.
Option C. water.
Correct Answer is. dry
powder.
Explanation. AL/3-19
10.4.
Question Number. 18. Once a person has been disconnected from
the source of an electrical shock the next step should be.
Option A. seek
assistance immediately.
Option B. check
for breathing start AR if necessary.
Option C. check
for pulse start cardiac massage if necessary.
Correct Answer is. check
for breathing start AR if necessary.
Explanation. NIL.
Question Number. 19. What can cause dermatitis?.
Option A. Washing
hands in solvents.
Option B. Not
wearing eye protection when using solvents.
Option C. Inhalation
of paint fumes.
Correct Answer is. Washing
hands in solvents.
Explanation. NIL.
Question Number. 20. If an oxygen cylinder pressure falls
below 500 PSI.
Option A. the
diluter stick will stick.
Option B. the
oxygen will degrade and cause anoxia.
Option C. condensation
will cause corrosion.
Correct Answer is. condensation
will cause corrosion.
Explanation. NIL.
02. Workshop Practices.
Question Number. 1. On a hollow tube where would a small
indentation normally be unacceptable?.
Option A. Nowhere
on the tube is an indentation acceptable.
Option B. In the
mid 1/3 section.
Option C. In
either of the outer 1/3 portion of the tube.
Correct Answer is. In
the mid 1/3 section.
Explanation. CAAIP s
Leaflet 6-4 Para 7.2.
Question Number. 2. What type of grinding wheel would you
sharpen an HSS drill bit on?.
Option A. A
green wheel.
Option B. A
course wheel.
Option C. A fine
wheel.
Correct Answer is. A
fine wheel.
Explanation. A Green
Grit (Silicon Carbide) wheel is used for Tungsten Carbide bit tools
(Non-steel). For HSS you need a fine Grey Aluminium Oxide wheel.
Question Number. 3. When using a reamer.
Option A. use no
lubricant.
Option B. use
the same lubricant as was used on the drill bit.
Option C. use
lard oil.
Correct Answer is. use
the same lubricant as was used on the drill bit.
Explanation. NIL.
Question Number. 4. How many teeth per inch are used on a
hacksaw blade for cutting hard metal?.
Option A. 54.
Option B. 36.
Option C. 26.
Correct Answer is. 26.
Explanation. Blades
are available 18 - 32 TPI. Greatest TPI is for hard metals.
Question Number. 5. How many strokes per minute are used on
a hacksaw when cutting thick metal?.
Option A. 30.
Option B. 65.
Option C. 55.
Correct Answer is. 55.
Explanation. NIL.
Question Number. 6. When lifting a bulky component with a
wire rope sling, the component can be protected from damage by the sling by.
Option A. fabricating
alternative lifting points.
Option B. using
a suitably shaped sling.
Option C. using
spreader bars and packing.
Correct Answer is. using
spreader bars and packing.
Explanation. NIL.
Question Number. 7. Gas bottles for CO2 air and
acetylene are coloured.
Option A. grey,
maroon, green.
Option B. black,
grey, maroon.
Option C. green,
grey, maroon.
Correct Answer is. black,
grey, maroon.
Explanation. NIL.
Question Number. 8. To drill a 1/4 inch hole in titanium,
the correct starting procedure would be.
Option A. to
centre drill.
Option B. to
centre punch.
Option C. to
drill 1/4 inch hole direct.
Correct Answer is. to
centre drill.
Explanation. CAIP S
EL/3-3 Para. 3.2.
Question Number. 9. In a torque wrench of handle length, L
= 12 in. and an extension E = 3 in, the desired torque value is 300 lbs.in. the
dial should read.
Option A. 240
lb.ins.
Option B. 375
lb.ins.
Option C. 280
lb.ins.
Correct Answer is. 240
lb.ins.
Explanation. CAAIP S
Leaflet 2-11 4.4.
Question Number. 10. When a torque loading is specified for a
castellated or slotted nut on an undrilled new bolt.
Option A. the
bolt should be pre-drilled, the torque applied and the nut eased back, if
necessary, to allow the split pin to be fitted.
Option B. the
bolt should be pre-drilled and the torque increased if necessary to allow the
split pin to be fitted.
Option C. the
torque should be applied and the bolt suitably drilled for the split pin.
Correct Answer is. the
torque should be applied and the bolt suitably drilled for the split pin.
Explanation. NIL.
Question Number. 11. A reamer with spiral flutes is removed.
Option A. clockwise.
Option B. straight.
Option C. anticlockwise.
Correct Answer is. clockwise.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-19.
Question Number. 12. The difference between high and low
limits of a size for a dimension is known as the.
Option A. deviation.
Option B. tolerance.
Option C. fit.
Correct Answer is. tolerance.
Explanation. NIL.
Question Number. 13. Rubber components should be stored.
Option A. in
warm and humid conditions.
Option B. in a
well lit room.
Option C. in a
cool dark area.
Correct Answer is. in
a cool dark area.
Explanation. CAAIP S
Leaflet 1-8 3.3.
Question Number. 14. When comparing the machining techniques
for stainless steel sheet material to those for aluminium alloy sheet, it is
normally considered good practice to drill the stainless steel at a.
Option A. higher
speed with less pressure applied to the drill.
Option B. lower
speed with more pressure applied to the drill.
Option C. lower
speed with less pressure applied to the drill.
Correct Answer is. lower
speed with more pressure applied to the drill.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-27.
Question Number. 15. When drilling stainless steel, the drill
used should have an included angle of.
Option A. 140°
and turn at a low speed.
Option B. 90°
and turn at a low speed.
Option C. 118°
and turn at a high speed.
Correct Answer is. 140°
and turn at a low speed.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-27.
Question Number. 16. When stop drilling a crack, what is the
typical drill size used?.
Option A. 0.025
inch.
Option B. 0.250
inch.
Option C. 0.125
inch.
Correct Answer is. 0.125
inch.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-6.
Question Number. 17. When degreasing aluminium alloys, and no
trichloroethylene is available, a suitable alternative is.
Option A. dilute
sulphuric acid.
Option B. M.E.K.
Option C. white
spirit and naphtha.
Correct Answer is. white
spirit and naphtha.
Explanation. NIL.
Question Number. 18. A grinding wheel is normally refaced by.
Option A. dressing
with a special tool.
Option B. grinding
through using another grinding wheel.
Option C. holding
a hard wood scraper against the rotating wheel.
Correct Answer is. dressing
with a special tool.
Explanation. NIL.
Question Number. 19. When checking a torque wrench 15 inches
long, the load required to give torque of 120 lbs.in. is.
Option A. 6 lbs.
Option B. 8 lbs.
Option C. 10
lbs.
Correct Answer is. 8
lbs.
Explanation. NIL.
Question Number. 20. How would you check the setting of an
adjustable reamer?.
Option A. Ring
gauge.
Option B. Dial
test indicator and 'V' blocks.
Option C. External
calipers.
Correct Answer is. Ring
gauge.
Explanation. NIL.
Question Number. 21. What is the specified lubricant for
drilling brass?.
Option A. None.
Option B. Paraffin.
Option C. Lard
oil.
Correct Answer is. None.
Explanation. NIL.
Question Number. 22. In the Limit System, the term 'allowance'
is the.
Option A. difference
between shaft and hole diameters.
Option B. hole
diameter variation.
Option C. shaft
diameter variation.
Correct Answer is. difference
between shaft and hole diameters.
Explanation. NIL.
Question Number. 23. Which is correct concerning the use of a
file?.
Option A. The
terms 'double-cut' and 'second-cut' have the same meaning in reference to
files.
Option B. Apply
pressure on the forward stroke, only, except when filing very soft metals such
as lead or aluminium.
Option C. A
smoother finish can be obtained by using a double-cut file than by using a
single-cut file.
Correct Answer is. Apply
pressure on the forward stroke, only, except when filing very soft metals such
as lead or aluminium.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-11.
Question Number. 24. Which procedure is correct when using a reamer
to finish a drilled hole to the correct size?.
Option A. Turn
the reamer only in the cutting direction.
Option B. Turn
the reamer in the cutting direction when enlarging the hole and in the opposite
direction to remove from the hole.
Option C. Apply
considerable pressure on the reamer when starting the cut and reduce the
pressure when finishing the cut.
Correct Answer is. Turn
the reamer only in the cutting direction.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-19.
Question Number. 25. Of what tolerance is the following an
example? 1 in. + 0.002-0.001.
Option A. Bilateral.
Option B. Multilateral.
Option C. Unilateral.
Correct Answer is. Bilateral.
Explanation. NIL.
Question Number. 26. How should a scraper be finally sharpened?.
Option A. By
draw filing.
Option B. On a
grindstone.
Option C. On an
oil-stone.
Correct Answer is. On
an oil-stone.
Explanation. NIL.
Question Number. 27. How is a D.T.I. initially set up?.
Option A. The
gauge plunger should be fully extended and the needle zeroed.
Option B. The
gauge plunger should be partly depressed and the needle zeroed.
Option C. The
needle zeroed, then the plunger fully extended.
Correct Answer is. The
gauge plunger should be partly depressed and the needle zeroed.
Explanation. NIL.
Question Number. 28. Nickel alloy chisels should be sharpened.
Option A. by
filing.
Option B. on a
grindstone.
Option C. on an
oilstone.
Correct Answer is. on
an oilstone.
Explanation. NIL.
Question Number. 29. What type of lubricant should be used
when drilling aluminium?.
Option A. Vegetable
oil.
Option B. Paraffin.
Option C. None.
Correct Answer is. Paraffin.
Explanation. Paraffin
is the lubricant for aluminium.
Question Number. 30. How are spring dividers sharpened?.
Option A. By
filing the outside of the points.
Option B. By
stoning the outside of the points.
Option C. By
grinding the inside of the points.
Correct Answer is. By
stoning the outside of the points.
Explanation. NIL.
Question Number. 31. What would be the result of an
insufficient clearance angle on a twist drill?.
Option A. It
would cut slowly, if at all.
Option B. It
would produce an oversize hole.
Option C. It
would tend to pull through the hole
Correct Answer is. It
would cut slowly, if at all.
Explanation. External
website. http://www.unionbutterfield.com/tech/drills/trouble_shooting.asp
Question Number. 32. A tolerance given on a dimension is
indicated.
Option A. by a
plus and minus sign preceding the permitted tolerance.
Option B. by the
prefix TOL with the permitted tolerance.
Option C. by
enclosing the permitted tolerance within a triangle.
Correct Answer is. by
a plus and minus sign preceding the permitted tolerance.
Explanation. NIL.
Question Number. 33. How much material should be allowed for
reaming?.
Option A. 0.001
in.
Option B. 0.003
in.
Option C. 0.010
in.
Correct Answer is. 0.003
in.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-19.
Question Number. 34. After cutting a 3/8 inch BSF internal
thread and stud, it is found that the stud is too large. How is a fit
achieved?.
Option A. Remove
the male thread crests with a fine emery cloth.
Option B. Grind
a taper on the end of the bolt.
Option C. Re-adjust
the die and re-cut the male thread.
Correct Answer is. Re-adjust
the die and re-cut the male thread.
Explanation. NIL.
Question Number. 35. You have reamed out a hole in a piece of
titanium. How should you remove the reamer safely to prevent unnecessary
damage?.
Option A. Allow the
reamer to pass right through the hole.
Option B. Remove
it, but in the same rotation as if cutting.
Option C. Anti-clockwise.
Correct Answer is. Remove
it, but in the same rotation as if cutting.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-19.
Question Number. 36. Why are some components torque loaded?.
Option A. To
ensure that their elastic limit is not exceeded.
Option B. To
ensure they do not vibrate loose.
Option C. To
ensure that they are tightened to their yield point.
Correct Answer is. To
ensure that their elastic limit is not exceeded.
Explanation. NIL.
Question Number. 37. When using a reamer, in which direction
should it be turned?.
Option A.
Anti-clockwise when Cutting and removing.
Option B. Clockwise
when cutting and anti-clockwise when removing.
Option C. Clockwise
when cutting and removing.
Correct Answer is. Clockwise
when cutting and removing.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-19.
Question Number. 38. Draw filing produces.
Option A. a
course finish.
Option B. a fine
finish.
Option C. a
mottled finish.
Correct Answer is. a
fine finish.
Explanation. NIL.
Question Number. 39. A safe edge of a file is used.
Option A. against
a finished surface.
Option B. to
give a fine polished finish to a smooth surface.
Option C. against
a rough unfinished surface.
Correct Answer is. against
a finished surface.
Explanation. NIL.
Question Number. 40. What is the minimum number of hacksaw
blade teeth that should be in contact with the material being cut?.
Option A. 2.
Option B. 4.
Option C. 3.
Correct Answer is. 3.
Explanation. NIL.
Question Number. 41. When reading a blueprint, a dimension is
given as 4.387 inches + 0.005-0.002. Which statement is true?.
Option A. The maximum
acceptable size is 4.385 inches.
Option B. The
minimum acceptable size is 4.385 inches.
Option C. The
maximum acceptable size is 4.389 inches.
Correct Answer is. The
minimum acceptable size is 4.385 inches.
Explanation. NIL.
Question Number. 42. Chalk when used with a fine file
produces.
Option A. a
finer finish.
Option B. a
milled type surface.
Option C. a
ground type surface.
Correct Answer is. a
finer finish.
Explanation. NIL.
Question Number. 43. When using a hand file correctly, the
downward pressure should be used only.
Option A. on a
return stroke.
Option B. on the
forward stroke.
Option C. on the
forward and return stroke.
Correct Answer is. on
the forward stroke.
Explanation. NIL.
Question Number. 44. The size of the nibs of vernier calipers
can be ascertained by.
Option A. using
the standard of 0.693 inches.
Option B. measuring
the steel rule.
Option C. noting
the dimension engraved on the instrument.
Correct Answer is. noting
the dimension engraved on the instrument.
Explanation. BL/3-4
3.5.
Question Number. 45. A shaft dimension given as 1.225 inches
+/- 0.003 inches followed by 'MMC' should be manufactured to what size?.
Option A. 1.228
Inches.
Option B. 1.222
Inches.
Option C. 1.225
Inches.
Correct Answer is. 1.228
Inches.
Explanation. Leaflet
2-1 5.11.3.
Question Number. 46. 2 microns is.
Option A. 0.002
mm.
Option B. 0.002
inch.
Option C. 0.000
002 inch.
Correct Answer is. 0.002
mm.
Explanation. 1
micron = 0.001 mm.
Question Number. 47. The edge or surface of a part from which
dimensions are measured from is called the.
Option A. water
line.
Option B. reference
plane.
Option C. datum.
Correct Answer is. datum.
Explanation. Leaflet
2-1 5.5.1.
Question Number. 48. Water Lines are.
Option A. front
to rear measurements on the fuselage.
Option B. vertical
measurements on the fuselage.
Option C. left
and right measurements on the fuselage.
Correct Answer is. vertical
measurements on the fuselage.
Explanation. AL/7-2
fig 15.
Question Number. 49. When clamping cable looms containing
co-axial cables.
Option A. distortion
of the outer sheath is allowed providing the inner cable is not affected.
Option B. the
clamps must be no more than 1 metre apart.
Option C. avoid
distortion to the co-axial cable to maintain the dielectric constant.
Correct Answer is. avoid
distortion to the co-axial cable to maintain the dielectric constant.
Explanation. NIL.
Question Number. 50. If a test or inspection instrument has no
calibration data supplied by the manufacturer, you would use the calibration
data provided by.
Option A. the
British Standards Quality Assurance documentation referring to calibration of
instrumentation and test equipment.
Option B. CAAIP
S.
Option C. the
Maintenance Manual.
Correct Answer is. the
British Standards Quality Assurance documentation referring to calibration of
instrumentation and test equipment.
Explanation. Leaflet
2-14 2.2.
Question Number. 51. Why are test or inspection instruments
regularly calibrated and certified?.
Option A. To
ensure they will perform within the required limits of operation.
Option B. To
ensure they can handle the range of measurements required of them.
Option C. To
ensure they are being used regularly.
Correct Answer is. To
ensure they will perform within the required limits of operation.
Explanation. Leaflet
2-14 1.2.
Question Number. 52. Who is responsible for ensuring that
weight and balance instrumentation is serviceable before use?.
Option A. An
engineer holding a license in the instrument category.
Option B. The
manufacturer of the equipment.
Option C. The
person responsible for carrying out the weight and balance procedure.
Correct Answer is. The
person responsible for carrying out the weight and balance procedure.
Explanation. NIL.
Question Number. 53. At which frequency is the calibration of
frequently used crimping tools carried out?.
Option A. Bi-annually.
Option B. Annually.
Option C. Every
1000 crimps.
Correct Answer is. Every
1000 crimps.
Explanation. Or
every 3 months, whichever comes first.
Question Number. 54. When using the trepanning tool, the hole
to be drilled should be.
Option A. 1/32
inch larger than the guide pin.
Option B. same
diameter as the guide pin.
Option C. 1/32
inch smaller than the guide pin.
Correct Answer is. same
diameter as the guide pin.
Explanation. NIL.
Question Number. 55. When using a strip-board, the tracks on a
PCB are etched.
Option A. before
component fitment.
Option B. after
fitment but before soldering the components.
Option C. after
fitment and soldering of components.
Correct Answer is. before
component fitment.
Explanation. MMC/1-1
7.
Question Number. 56. A 'light drive' fit for a 3/8 inch
diameter bolt has a maximum allowance of.
Option A. 0.005
inch.
Option B. 0.0025
inch.
Option C. 0.0006
inch.
Correct Answer is. 0.0006
inch.
Explanation. AC43.13-1B
Page 7-5 Para.7-39.
Question Number. 57. The intervals for calibration of test
equipment.
Option A. are
every year.
Option B. are
different from one appliance to another.
Option C. are as
specified in EASA Part-145.
Correct Answer is. are
different from one appliance to another.
Explanation. EASA
Part-145 is not specific.
Question Number. 58. What drill angle is used to drill
titanium?.
Option A. 130-140
degrees.
Option B. 105-120
degrees.
Option C. 90-100
degrees.
Correct Answer is. 105-120
degrees.
Explanation. BL/6-18
Para. 6.
Question Number. 59. When tightening a nut on a bolt the
torque loading applied is.
Option A. inversely
proportional to the force applied to the spanner.
Option B. the
tangential application of the force times the perpendicular distance from the
point of application to the centre of the bolt.
Option C. independent
of whether the threads are wet or dry.
Correct Answer is. the
tangential application of the force times the perpendicular distance from the
point of application to the centre of the bolt.
Explanation. Torque
= force * distance of force from centre of bolt.
Question Number. 60. The UK standard of limits and fits is.
Option A. BS4500.
Option B. BS8888.
Option C. BS308.
Correct Answer is. BS4500.
Explanation. BS4500
is Limits and Fits.
Question Number. 61. When using a Pacific tensiometer the
correct tension is found by.
Option A. reading
dial, provided the correct riser is used for the cable diameter.
Option B. comparing
reading to chart provided.
Option C. adding
reading to riser number.
Correct Answer is. comparing
reading to chart provided.
Explanation. The
Pacific Tensiometer is NOT a direct reading type. See Pacific Tensiometer
instructions.
Question Number. 62. What temperature should the heat gun be
set for shrinking heat shrink sleeve?.
Option A. At the
rated temperature.
Option B. 100°C
below rated temperature.
Option C. 100°C
above rated temperature.
Correct Answer is. 100°C
above rated temperature.
Explanation. Rated
temperature is the normal working temperature of the heat-shrink material. The
shrink at approximately 100°C above that.
Question Number. 63. Calibration of aircraft hydrostatic
weighing equipment is.
Option A. done
once a year.
Option B. carried
out every time before an aircraft is weighed and adjusted by operator.
Option C. not
required.
Correct Answer is. done
once a year.
Explanation. Hydrostatic
weighing equipment should be calibrated every year.
Question Number. 64. When drilling light alloy.
Option A. lard
oil should be used.
Option B. use
the specified lubricant.
Option C. no
lubricant is required.
Correct Answer is. use
the specified lubricant.
Explanation. Since
the question is not specific as to which light alloy is to be drilled, the
'specified' lubricant is used (even if the 'specified' lubricant is 'nothing').
Question Number. 65. The picture shows a torque wrench with an
extension. To apply a torque of 350 lb.in. the reading on the dial should be.
Option A. 350
lb.in.
Option B. 280
lb.in.
Option C. 245
lb.in.
Correct Answer is. 280
lb.in.
Explanation. BL/6-30
4.4.1.
Question Number. 66. Reaming light alloy tube is done with.
Option A. no
lubricant.
Option B. the
same oil and lubrication as used for cutting.
Option C. hard
base lubricant.
Correct Answer is. the
same oil and lubrication as used for cutting.
Explanation. Reaming
is lubricated with the same fluid as cutting (drilling).
Question Number. 67. Tolerance is the.
Option A. the
difference between a hole and shaft size.
Option B. allowable
error due to faulty workmanship and tools.
Option C. difference
between worn and new tools.
Correct Answer is. allowable
error due to faulty workmanship and tools.
Explanation. Tolerance
is allowable error due to faulty workmanship and tools.
Question Number. 68. What should be done if a tool is found
not to be working to its calibrated requirements?.
Option A. It
should be removed from service, marked as unserviceable and sent away for
overhaul.
Option B. It
should be placed back into stores and kept in service until the next
calibration is due.
Option C. A
mechanic should adjust it to restore it to the correct operation.
Correct Answer is. It
should be removed from service, marked as unserviceable and sent away for
overhaul.
Explanation. Tool
should be removed from service, marked as unserviceable and sent away for
overhaul.
Question Number. 69. When carrying out soldering to an end
termination and a wire, you should tin.
Option A. only
the end of the wire.
Option B. neither
the wire or the termination as tinning is not required.
Option C. both
the end of the wire and the termination.
Correct Answer is. both
the end of the wire and the termination.
Explanation. BL/6-1
13.2.
Question Number. 70. Run-out of a rod is measured using.
Option A. DTI,
surface plate and V-blocks.
Option B. micrometer
and V-blocks.
Option C. vernier
and V-blocks.
Correct Answer is. DTI,
surface plate and V-blocks.
Explanation. EL/3-3
Page 2 fig 1.
Question Number. 71. How would you mark a defect on an exhaust
system?.
Option A. Pencil.
Option B. Chalk.
Option C. Special
zinc/copper tipped marking tool.
Correct Answer is. Chalk.
Explanation. AC43
Para. 8-49. Jeppesen Aircraft Gas Turbine Powerplants 5-31.
Question Number. 72. Which of the following is the most
appropriate filing technique?.
Option A. Pressure
backwards, relieve pressure forwards.
Option B. Even
pressure forward and backwards.
Option C. Pressure
forwards, relieve pressure backwards.
Correct Answer is. Pressure
forwards, relieve pressure backwards.
Explanation. Jeppesen
A&P Mechanics Handbook Page 537.
Question Number. 73. Stubborn pins in file teeth should be
removed by.
Option A. tapping
file gently on workbench.
Option B. using
file card.
Option C. pricking
out with sharp point.
Correct Answer is. pricking
out with sharp point.
Explanation. Jeppesen
A&P Mechanics Handbook Page 538.
Question Number. 74. When using low tungsten hacksaw blades it
is recommended to use.
Option A. 60
strokes per minute.
Option B. 50
stroke per minute.
Option C. 40
strokes per minute.
Correct Answer is. 50
stroke per minute.
Explanation. Jeppesen
A&P Mechanics Handbook Page 535.
Question Number. 75. Units of torque are.
Option A. lbs/ft2
and lbs/in2.
Option B. Lbs
and Kg.
Option C. lbs.ft
and lbs.in.
Correct Answer is. lbs.ft
and lbs.in.
Explanation. NIL.
Question Number. 76. The calibration of a piece of test
equipment is suspect. Your actions would be.
Option A. calibrate/rectify
immediately.
Option B. note
and rectify later.
Option C. remove
from service and annotate accordingly.
Correct Answer is. remove
from service and annotate accordingly.
Explanation. NIL.
Question Number. 77. What should you check before using a set
of V blocks?.
Option A. That
both blocks have the same identification stamps.
Option B. It
doesn't matter.
Option C. The
calibration date.
Correct Answer is. That
both blocks have the same identification stamps.
Explanation. NIL.
Question Number. 78. When turning the handle on a megger with
the probes kept apart.
Option A. the
needle stays at infinity.
Option B. the
needle deflects to infinity.
Option C. the
needle moves to zero.
Correct Answer is. the
needle stays at infinity.
Explanation. The
needle of a Megger rests on infinity and is deflected to Zero.
03. Tools.
Question Number. 1. How many strokes per minute should
generally be used with a hacksaw?.
Option A. 60.
Option B. 30.
Option C. 55.
Correct Answer is. 55.
Explanation. NIL.
Question Number. 2. What type of drill would you use on
carbon fibre?.
Option A. Diamond
tipped.
Option B. Carborundum.
Option C. Tungsten
carbide.
Correct Answer is. Tungsten
carbide.
Explanation. Airbus
A340-600 SRM.
Question Number. 3. A micro-shaver is used to.
Option A. cut
rivets to length prior to forming.
Option B. mill
the rivet head after forming.
Option C. trim
the shank diameter prior to forming.
Correct Answer is. mill
the rivet head after forming.
Explanation. A&P
Technician Airframe Textbook 2-37 and 2-68.
Question Number. 4. How many teeth per inch are there on a
fine hacksaw blade?.
Option A. 64.
Option B. 16.
Option C. 32.
Correct Answer is. 32.
Explanation. Jeppesen
A&P Technician General Textbook Page 13.
Question Number. 5. What is the normal cutting angle of a
drill?.
Option A. 59°.
Option B. 130°.
Option C. 12°.
Correct Answer is. 59°.
Explanation. Jeppesen
A&P Technician General Textbook Page 15.
Question Number. 6. When using a moving coil as an ammeter
the greatest amount of current flows through the.
Option A. bushes.
Option B. coil.
Option C. shunt.
Correct Answer is. shunt.
Explanation. Jeppesen
A&P Technician General Textbook Page 3-89.
Question Number. 7. When using the old style vernier
caliper for taking internal measurements.
Option A. add
the nib measurements.
Option B. subtract
the nib measurements.
Option C. the
nib size has no relevance and can be ignored.
Correct Answer is. add
the nib measurements.
Explanation. Jeppesen
A&P General Textbook 9-39.
Question Number. 8. To carry out an insulation test on a
wire rated at 115 volts you would use.
Option A. a 250
volt megger.
Option B. a 115
volt megger.
Option C. a 500
volt megger.
Correct Answer is. a
250 volt megger.
Explanation. CAAIP S
Leaflet 9-1, 4.4.2 As a rule of thumb, the megger should be twice the voltage
of the system under test.
Question Number. 9. The normal drill angles are.
Option A. cutting
angle 59°, web angle 130° and clearance angle 12°.
Option B. cutting
angle 130°, web angle 59° and clearance angle 12°.
Option C. cutting
angle 12°, web angle 130° and clearance angle 130°.
Correct Answer is. cutting
angle 59°, web angle 130° and clearance angle 12°.
Explanation. NIL.
Question Number. 10. The abbreviation 'A/F' means.
Option A. American
Fine.
Option B. Across
Flats.
Option C. Associated
Fine.
Correct Answer is. Across
Flats.
Explanation. CAAIP S
Leaflet 9-3 Pg.7.
Question Number. 11. A rivet shaver is used to.
Option A. mill
the head flush.
Option B. mill
the tail after cutting.
Option C. mill
the tail after setting.
Correct Answer is. mill
the head flush.
Explanation. Jeppesen
A&P Airframe Textbook 2-68.
Question Number. 12. A drill and wire gauge has holes
numbered.
Option A. 10 to
60.
Option B. 1 to
80.
Option C. 1 to
50.
Correct Answer is. 1
to 80.
Explanation. Jeppesen
A&P Airframe Textbook Fig.2-47.
Question Number. 13. A 250 volt megger should not be used.
Option A. on
electronic equipment.
Option B. in
fuel tanks.
Option C. on
radio aerials.
Correct Answer is. on
electronic equipment.
Explanation. Leaflet
9-1 4.4.4.
Question Number. 14. If the leads of a megger are held apart.
Option A. the
spring will return the needle to infinity.
Option B. the
spring will return the needle to the zero stop.
Option C. if the
handle was turned the meter would read infinity.
Correct Answer is. if
the handle was turned the meter would read infinity.
Explanation. A
megger has no spring.
Question Number. 15. One megohm is equal to.
Option A. 1,000
ohms.
Option B. 1,000,000
ohms.
Option C. 100,000
ohms.
Correct Answer is. 1,000,000
ohms.
Explanation. NIL.
Question Number. 16. Reamers are used to.
Option A. drill
accurate holes.
Option B. to
make holes oversize.
Option C. enlarge
holes to accurate dimensions.
Correct Answer is. enlarge
holes to accurate dimensions.
Explanation. Jeppesen
A&P General Textbook 9-19.
Question Number. 17. The pitch of a hacksaw blade is.
Option A. its
length.
Option B. the
number of teeth on the blade.
Option C. the
number of teeth per inch.
Correct Answer is. the
number of teeth per inch.
Explanation. NIL.
Question Number. 18. The web angle of a normal twist drill is.
Option A. 59°.
Option B. 12°.
Option C. 130°.
Correct Answer is. 130°.
Explanation. Jeppesen
A&P Airframe Textbook 2-27.
Question Number. 19. The leads of a bonding tester.
Option A. are
interchangeable, one 60 foot long having two prongs and a 6 foot one with a
single prong.
Option B. have
critical lengths and the resistance of the leads is accounted for.
Option C. are
supplied in 60 foot and 6 foot lengths but can be varied due to wear.
Correct Answer is. have
critical lengths and the resistance of the leads is accounted for.
Explanation. CAIP S
EEL/1-6 Para 3-11-2 & CAAIP S Leaflet 9.1 3.10.2(b).
Question Number. 20. Expanding reamers are used to.
Option A. ream
holes of different diameters by adjusting the position of the blades.
Option B. ream
tapered holes.
Option C. ream
holes in metal that has been heated.
Correct Answer is. ream
holes of different diameters by adjusting the position of the blades.
Explanation. Jeppesen
A&P Technician General Textbook Page 9-19.
Question Number. 21. The main scale on a 24/25 vernier caliper
is divided into.
Option A. inches,
tenths and twentieths.
Option B. inches,
tenths and fortieths.
Option C. inches,
tenths and thousandths.
Correct Answer is. inches,
tenths and fortieths.
Explanation. CAIP S
BL/3-4 2.
Question Number. 22. The vernier height gauge uses the same
principle as the.
Option A. vernier
caliper.
Option B. bevel
protractor.
Option C. micrometer.
Correct Answer is. vernier
caliper.
Explanation. CAIP S
BL/3-4 4.
Question Number. 23. One revolution of the thimble of the
English micrometer produces a linear movement of the spindle of.
Option A. 0.001
inch.
Option B. 0.025
inch.
Option C. 0.040
inch.
Correct Answer is. 0.025
inch.
Explanation. CAIP S
BL/3-5.
Question Number. 24. The pitch of a metric micrometer screw
thread is.
Option A. 0.02
mm.
Option B. 1.0
mm.
Option C. 0.5
mm.
Correct Answer is. 0.5
mm.
Explanation. NIL.
Question Number. 25. When torque loading, a wrench should be
selected where the required value falls.
Option A. at the
top end of the range.
Option B. in the
middle of the range.
Option C. at the
bottom end of the range.
Correct Answer is. at
the top end of the range.
Explanation. CAIP S
BL/6-30 4.5.1.
Question Number. 26. The test equipment normally used to carry
out a continuity test on an electrical cable is.
Option A. a high
tension circuit tester.
Option B. an
ammeter.
Option C. a low
reading ohmmeter.
Correct Answer is. a
low reading ohmmeter.
Explanation. CAIP
EEL/1-6 4.2.1 & CAAIP S Leaflet 9-1 4.2.1.
Question Number. 27. If all three prongs on a bonding tester
were shorted together, the metre would read.
Option A. FSD.
Option B. zero.
Option C. off-scale
high.
Correct Answer is. zero.
Explanation. CAIP
EEL/1-6 3.10.2b.
Question Number. 28. The pitch of the screw thread on an
English micrometer is.
Option A. 0.0001
inches.
Option B. 0.050
inches.
Option C. 0.025
inches.
Correct Answer is. 0.025
inches.
Explanation. Jeppesen
A&P General Textbook 9-36.
Question Number. 29. The vernier scale on an English caliper
is divided into.
Option A. 50
equal divisions.
Option B. 40
equal divisions.
Option C. 25
equal divisions.
Correct Answer is. 25
equal divisions.
Explanation. Jeppesen
A&P General Textbook 9-36.
Question Number. 30. The thimble of a metric micrometer is
divided into.
Option A. 50
equal divisions.
Option B. 40 equal
divisions.
Option C. 25
equal divisions.
Correct Answer is. 50
equal divisions.
Explanation. NIL.
Question Number. 31. The measuring capacity of a Vernier
Caliper is.
Option A. the
length of the graduated scale less the length of the vernier scale.
Option B. the
length of the graduated scale.
Option C. the
length of the graduated scale plus the width of the nibs.
Correct Answer is. the
length of the graduated scale less the length of the vernier scale.
Explanation. NIL.
Question Number. 32. Vee-blocks are manufactured.
Option A. as
single items and may be paired with any other vee-block.
Option B. in
sets of two and identified for use as a set.
Option C. in
sets of three and identified for use as a set.
Correct Answer is. in
sets of two and identified for use as a set.
Explanation. NIL.
Question Number. 33. The metric micrometer reading shown is.
Option A. 13.87
mm.
Option B. 13.37
mm.
Option C. 10.337
mm.
Correct Answer is. 13.37
mm.
Explanation. NIL.
Question Number. 34. A ketts saw is used because.
Option A. it can
cut thicker metal than is required by most repair schemes.
Option B. it is
available both pneumatic and electric.
Option C. its
low torque allows single handed use.
Correct Answer is. it
can cut thicker metal than is required by most repair schemes.
Explanation. Jeppesen
A&P Airframe Textbook. It describes it as electrical, with the advantage of
being able to cut sheet to 3/16 inch thick. Care to be taken to prevent blade
from 'grabbing and kicking back'.
Question Number. 35. The gears used in a pistol windy are.
Option A. gears
in a gearbox.
Option B. gyrator
type gears.
Option C. spur
gears.
Correct Answer is. spur
gears.
Explanation. Sun and
planet gear reduction, using spur gears.
Question Number. 36. Cross cut files.
Option A. cut on
the backward stroke only.
Option B. cut in
both directions.
Option C. cut on
the forward stroke only.
Correct Answer is. cut
on the forward stroke only.
Explanation. NIL.
Question Number. 37. The correct size spanner for use on a
unified 5/16 in. threaded hexagon headed bolt is.
Option A. 5/16
in A/F.
Option B. 1/2 in
A/F.
Option C. 1/4 in
A/F.
Correct Answer is. 1/2
in A/F.
Explanation. NIL.
Question Number. 38. The length of the Vernier Scale in a 24/25
Vernier Caliper is.
Option A. 0.6
in.
Option B. 1.2
in.
Option C. 2.45
in.
Correct Answer is. 0.6
in.
Explanation. NIL.
Question Number. 39. What is used to measure the depth of a
blend after a corrosion repair?.
Option A. Dial
Test Indicator.
Option B. Straight
edge and slip gauges.
Option C. Vernier
caliper.
Correct Answer is. Dial
Test Indicator.
Explanation. AL/7-14
Page 12. BL/4-20 Page 9.
Question Number. 40. Vacu-blast beads re-used on a steel
component, after being used on an aluminium component will.
Option A. cause
clogging of the vacu-blast machine.
Option B. be
ineffective in abrasion.
Option C. cause
corrosion to the steel component.
Correct Answer is. cause
corrosion to the steel component.
Explanation. NIL.
Question Number. 41. The main scale on a 49/50 Vernier caliper
is divided into.
Option A. inches,
tenths and thousandths.
Option B. inches,
tenths and twentieths.
Option C. inches,
tenths and fortieths.
Correct Answer is. inches,
tenths and twentieths.
Explanation. NIL.
Question Number. 42. Centre punches are made of.
Option A. high
carbon steel with the tip hardened and tempered.
Option B. case
hardened mild steel.
Option C. high
carbon steel hardened and tempered.
Correct Answer is. high
carbon steel hardened and tempered.
Explanation. The
whole centre punch is hardened and tempered.
Question Number. 43. What type of flutes should be used in a
reamer for cutting titanium?.
Option A. Spiral
flutes.
Option B. Straight
flutes.
Option C. Tapered
flutes.
Correct Answer is. Spiral
flutes.
Explanation. BL/6-18
7.1.
Question Number. 44. The depth micrometer reading shown is.
Option A. 0.261
ins.
Option B. 0.361
ins.
Option C. 0.336
ins.
Correct Answer is. 0.261
ins.
Explanation. NIL.
Question Number. 45. What should be the included angle of a
twist drill for soft metals?.
Option A. 118
degrees.
Option B. 65
degrees.
Option C. 90
degrees.
Correct Answer is. 90
degrees.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-27.
Question Number. 46. What should the point angle of a drill be
if it is to be used for drilling titanium (drill size below 1/4 inch diameter)?
Option A. 90° to
105°.
Option B. 105 to
120°.
Option C. 90°.
Correct Answer is. 105
to 120°.
Explanation. BL/6-18
6.
Question Number. 47. How are pin punches classified?.
Option A. By
length and diameter of the small end.
Option B. By
overall length and type.
Option C. By
type and diameter of the small end.
Correct Answer is. By
type and diameter of the small end.
Explanation. How are
spring dividers classified?.
Question Number. 48. The length of the legs.
Option A. The
length of the legs.
Option B. The
diameter of a circle scribed with the legs at 600.
Option C. The
diameter of the largest circle that can be scribed.
Correct Answer is. The
length of the legs.
Explanation. NIL.
Question Number. 49. The purpose of a taper tap is to.
Option A. produce
a fine thread.
Option B. start
a thread.
Option C. form a
tapered thread.
Correct Answer is. start
a thread.
Explanation. NIL.
Question Number. 50. Why is the Vee cut in the base of a
scribing block?.
Option A. to
reduce the contact area with the marking off table and reduce friction.
Option B. to
allow the scribing block to be used on the edge of the marking off table.
Option C. to
trap any dirt that may be adhering to the surface of the marking off table.
Correct Answer is. to
trap any dirt that may be adhering to the surface of the marking off table.
Explanation. NIL.
Question Number. 51. An inside micrometers normal measurement
range is.
Option A. ½ in.
to 10in.
Option B. 2in.
to 10in.
Option C. 2in.
to 12in.
Correct Answer is. 2in.
to 12in.
Explanation. BL/3-5
para 3.2 under Note.
Question Number. 52. What is the purpose of Target Points on a
Vernier caliper?.
Option A. To
enable spring dividers to be accurately set.
Option B. To
zero the caliper.
Option C. For
scribing lines inside tubes.
Correct Answer is. To
enable spring dividers to be accurately set.
Explanation. BL/3-4
3.6.
Question Number. 53. Die Nuts are used to.
Option A. form
internal threads.
Option B. form
external threads.
Option C. clean
up damaged threads.
Correct Answer is. clean
up damaged threads.
Explanation. NIL.
Question Number. 54. A Dial Test Indicator may be used for.
Option A. checking
a round bar for bow.
Option B. checking
dimensions to within 0.125''.
Option C. checking
any known depth.
Correct Answer is. checking
a round bar for bow.
Explanation. EL/3-3
fig 1.
Question Number. 55. Which cut of a file should be used on
mild steel?.
Option A. Single
cut.
Option B. Double
cut.
Option C. Second
cut.
Correct Answer is. Double
cut.
Explanation. NIL.
Question Number. 56. Which of the following statements is
correct?.
Option A. To cut
thin mild steel plate use a coarse blade.
Option B. To cut
an aluminium block use a fine hacksaw blade.
Option C. To cut
thin sheet metal use a fine blade.
Correct Answer is. To
cut thin sheet metal use a fine blade.
Explanation. AC65-9A
Chapt 12-Metal Cutting Tools.
Question Number. 57. A power meter indicates that a circuit
has a power of 4 kW. Separate readings of the voltage and current are 400 V and
20 A respectively. The Power factor is.
Option A. 2.
Option B. ½.
Option C. 20.
Correct Answer is. ½.
Explanation. PF =
TP/AP TP = 4,000 AP = 20 * 400 = 8000 4000/8000 = 1/2.
Question Number. 58. What is a key-seat rule used for?.
Option A. Marking
lines which are parallel to a true edge.
Option B. Marking
lines parallel to an axis of a round bar.
Option C. Providing
a positive driving force.
Correct Answer is. Marking
lines parallel to an axis of a round bar.
Explanation. NIL.
Question Number. 59. When measuring current in a circuit, the
ammeter is placed.
Option A. in series
with the circuit.
Option B. in
series with the shunt.
Option C. in
parallel with the circuit.
Correct Answer is. in
series with the circuit.
Explanation. NIL.
Question Number. 60. A 3 ½ bit multimeter will indicate
readings up-to.
Option A. 9999.
Option B. 999 ½.
Option C. 1999.
Correct Answer is. 1999.
Explanation. A&P
General Textbook CH3-109 PG 167 Para 2A, and Eismin Aircraft Electricity and
Electronics 5th edition P171.
Question Number. 61. The resolution a bevel protractor can be
read to is.
Option A. 50'
minutes.
Option B. 5'
minutes.
Option C. 1 º.
Correct Answer is. 5'
minutes.
Explanation. BL/3-4
5.2.
Question Number. 62. If an English micrometer is showing 4
main divisions, 3 sub-divisions and the 25th thimble division was in line, what
would the reading be?.
Option A. 0.475
in.
Option B. 0.175
in.
Option C. 0.555
in.
Correct Answer is. 0.475
in.
Explanation. BL/3-5
Para 2.3, 4.1.2.
Question Number. 63. An open circuit on an ohmmeter would be
indicated by a reading of.
Option A. infinite
resistance.
Option B. zero
resistance.
Option C. a
negative resistance.
Correct Answer is. infinite
resistance.
Explanation. Eismin
Aircraft Electricity and Electronics P165/166.
Question Number. 64. The leads of an ohmmeter should be
replaced if their resistance is greater than.
Option A. 0.5
ohms.
Option B. 1 ohm.
Option C. 0.05
ohms.
Correct Answer is. 1
ohm.
Explanation. NIL.
Question Number. 65. Torque loading is determined by
multiplying the tangent force applied at the free end of the spanner.
Option A. by the
dia. of the bolt and the distance of its point of application.
Option B. by the
distance moved by the point of application.
Option C. by its
distance of application from the axis of the bolt.
Correct Answer is. by
its distance of application from the axis of the bolt.
Explanation. Leaflet
2-11 pg 3 para 4.2.
Question Number. 66. Which electrical measuring device needs a
power source?.
Option A. A
voltmeter.
Option B. An
ohmmeter.
Option C. An ammeter.
Correct Answer is. An
ohmmeter.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 165.
Question Number. 67. When measuring voltage or current with a
digital multimeter, the indication is.
Option A. Average
values.
Option B. peak
values.
Option C. RMS
values.
Correct Answer is. RMS
values.
Explanation. A&P
General Textbook Page 3-94. DMMs are 'Average-Responding' meaning they read RMS
if AC.
Question Number. 68. On a multimeter, what colour lead is
connected to the Common socket?.
Option A. Green.
Option B. Red.
Option C. Black.
Correct Answer is. Black.
Explanation. Jeppesen
A&P General Technician Textbook Page 3-94 fig 3-201 and fig 3-202.
Question Number. 69. The Vernier scale of a Bevel Protractor
is shown below. What is the reading?.
Option A. 38º
45’minutes.
Option B. 86º
15’minutes.
Option C. 63º
15’ minutes.
Correct Answer is. 63º
15’ minutes.
Explanation. NIL.
Question Number. 70. Three point micrometers are for
measuring.
Option A. internal
dimensions.
Option B. external
dimensions.
Option C. linear
dimensions.
Correct Answer is. internal
dimensions.
Explanation. BL/3-5
3.4.
Question Number. 71. When is a coarse hacksaw blade used?.
Option A. When
cutting material of thick cross section.
Option B. When
cutting ferrous metals only.
Option C. When
cutting material of thin cross section.
Correct Answer is. When
cutting material of thick cross section.
Explanation. Jeppesen
A&P General Technician Textbook Page 9-13.
Question Number. 72. A voltage drop across a component is
measured by placing the meter in.
Option A. parallel
with the component.
Option B. series
with he component.
Option C. series
with the power source.
Correct Answer is. parallel
with the component.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 164 and CAAIP S Leaflet
9-1, 4.3.
Question Number. 73. Which of the following reamers would you
use in a hole having a keyway?.
Option A. Expanding
reamer.
Option B. Spiral
fluted reamer.
Option C. Parallel
reamer.
Correct Answer is. Spiral
fluted reamer.
Explanation. NIL.
Question Number. 74. What is the purpose of a Morse taper on
large sizes of twist drills?.
Option A. To
allow the drills to be fitted to a drilling machine.
Option B. To
ensure that the drill is fitted correctly.
Option C. To
give a positive drive when fitted into a tapered chuck.
Correct Answer is. To
give a positive drive when fitted into a tapered chuck.
Explanation. NIL.
Question Number. 75. What should be the included angle of a
twist drill for hard metal?.
Option A. 90
degrees.
Option B. 100
degrees.
Option C. 118
degrees.
Correct Answer is. 118
degrees.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-27.
Question Number. 76. The threads per inch on the spindle of an
English micrometer are.
Option A. 40
t.p.i.
Option B. 50
t.p.i.
Option C. 25
t.p.i.
Correct Answer is. 40
t.p.i.
Explanation. BL/3-5
4.1.
Question Number. 77. The spring loaded ratchet attached to the
spindle of a standard external micrometer produces.
Option A. a
pre-set feel during use.
Option B. a
means for controlling thread binding.
Option C. a
smooth free run during use.
Correct Answer is. a
pre-set feel during use.
Explanation. BL/3-5
2.2.
Question Number. 78. The purpose of the land on a twist drill
is to.
Option A. to
allow clearance for swarf.
Option B. reduce
friction.
Option C. present
the cutting edge at the required angle.
Correct Answer is. reduce
friction.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-27.
Question Number. 79. The name given to the moving scale on the
Vernier caliper is.
Option A. the
main scale.
Option B. the
vernier scale.
Option C. the
cursor.
Correct Answer is. the
vernier scale.
Explanation. BL/3-4
fig 2 (although the whole moving frame - which has the scale - is called the
cursor).
Question Number. 80. What is the reading of the Vernier
caliper scale in inches shown below?.
Option A. 0.1816.
Option B. 1.816.
Option C. 1.8016.
Correct Answer is. 1.816.
Explanation. BL/3-4
2.5 and fig 1.
Question Number. 81. What does the cut of a file refer to?.
Option A. Arrangement
of the teeth.
Option B. Number
of teeth per inch.
Option C. Grade.
Correct Answer is. Arrangement
of the teeth.
Explanation. A&P
Technician Airframe Textbook Page 220.
Question Number. 82. Why are teeth of hacksaw blades off-set?.
Option A. To
allow a quick cutting positive action.
Option B. To
provide greater strength.
Option C. To
provide clearance for non-cutting part of the blade.
Correct Answer is. To
provide clearance for non-cutting part of the blade.
Explanation. NIL.
Question Number. 83. How are files classified?.
Option A. By
length, grade and material.
Option B. By
length, grade, cut and section.
Option C. By
length, grade, cut, section and material.
Correct Answer is. By
length, grade, cut and section.
Explanation. NIL.
Question Number. 84. Hammers are classified by.
Option A. shape
of head and length of shaft.
Option B. weight
and length of shaft.
Option C. weight
and type of head.
Correct Answer is. weight
and type of head.
Explanation. NIL.
Question Number. 85. What does the term 'second cut' indicate
as applied to hand files?.
Option A. The
grade of the file.
Option B. The section
of the file.
Option C. A
reconditioned file.
Correct Answer is. The
grade of the file.
Explanation. NIL.
Question Number. 86. What comprises a full set of BA taps?.
Option A. A
taper, second and plug tap.
Option B. A
taper and second tap.
Option C. A
taper and plug tap.
Correct Answer is. A
taper and plug tap.
Explanation. Most
tap sets are sets of 3. Except BA tap sets which do not have a second tap.
Question Number. 87. The teeth on a hacksaw blade.
Option A. does
not matter which way they point.
Option B. should
point away from the handle.
Option C. should
point towards the handle.
Correct Answer is. should
point away from the handle.
Explanation. NIL.
Question Number. 88. What is the clearance angle on a normal
twist drill?.
Option A. 130
degrees.
Option B. 59
degrees.
Option C. 12
degrees.
Correct Answer is. 12
degrees.
Explanation. NIL.
Question Number. 89. When tapping blind holes.
Option A. a set
of three taps is used.
Option B. a set
of two taps is used.
Option C. a
single tap is used.
Correct Answer is. a
set of three taps is used.
Explanation. NIL.
Question Number. 90. On a torque wrench the torque loading is.
Option A. the
tangential application of the force divided by the perpendicular distance to
the centre of the bolt.
Option B. the
tangential application of the force times the perpendicular distance to the
centre of the bolt.
Option C. the
tangential application of the force plus the perpendicular distance to the
centre of the bolt.
Correct Answer is. the
tangential application of the force times the perpendicular distance to the
centre of the bolt.
Explanation. Leaflet
2-11 pg 3 para 4.2.
Question Number. 91. Surface Plates are used.
Option A. for
marking out work and testing flat surfaces.
Option B. for
filing flat surfaces.
Option C. only
on surface tables.
Correct Answer is. for
marking out work and testing flat surfaces.
Explanation. NIL.
Question Number. 92. The main scale of a Metric Vernier
Caliper is calibrated in.
Option A. millimetres.
Option B. micro-meters.
Option C. millimetres
and half millimetres.
Correct Answer is. millimetres
and half millimetres.
Explanation. BL/3-4
2.5.1
Question Number. 93. For a drill to cut properly it is
essential that the point angle be the same on each side, for general use the
angle is.
Option A. 12°.
Option B. 130°.
Option C. 59°.
Correct Answer is. 59°.
Explanation. Jeppesen
A & P Technician Airframe page 2-27.
Question Number. 94. The pitch of a hacksaw blade is.
Option A. the
number of teeth per inch.
Option B. its
length.
Option C. the
number of teeth on the blade.
Correct Answer is. the
number of teeth per inch.
Explanation. NIL.
Question Number. 95. When using a bench grinding machine the
wheel rotates.
Option A. from
the top down towards the work piece.
Option B. either
direction as selected on starting the machine.
Option C. from
the bottom upwards past the work piece.
Correct Answer is. from
the top down towards the work piece.
Explanation. NIL.
Question Number. 96. The thimble of an English micrometer is
divided into.
Option A. 50
equal divisions.
Option B. 40
equal divisions.
Option C. 25
equal divisions.
Correct Answer is. 25
equal divisions.
Explanation. BL/3-5
fig 1.
Question Number. 97. The reading on the inch micrometer scale
shown is.
Option A. 0.483
ins.
Option B. 0.488
ins.
Option C. 4.758
ins.
Correct Answer is. 0.483
ins.
Explanation. BL/3-5.
Question Number. 98. The vernier height gauge uses the same
principle as.
Option A. the vernier
caliper.
Option B. the
micrometer.
Option C. the
bevel protractor.
Correct Answer is. the
vernier caliper.
Explanation. BL/3-4
4.
Question Number. 99. The pitch of the screw thread on an
English micrometer is.
Option A. 0.050
in.
Option B. 0.001
in.
Option C. 0.025
in.
Correct Answer is. 0.025
in.
Explanation. BL/3-5
4.1.
Question Number. 100. An avometer can measure alternating current
because it has a.
Option A. moving
coil.
Option B. bridge
rectifier circuit.
Option C. moving
iron.
Correct Answer is. bridge
rectifier circuit.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 113 and 167 read together.
Question Number. 101. Taper reamers are classified by.
Option A. a type
number (1 to 10).
Option B. the
diameter of the small end.
Option C. the
diameter of the large end.
Correct Answer is. a
type number (1 to 10).
Explanation. Taper
reamers are classified by a type number 1- 10.
Question Number. 102. A crimped electrical connection is
suspected to be high resistance. How would you verify this without
disconnecting the circuit?.
Option A. Measure
the millivolt drop across the connection with a millivolt meter.
Option B. Measure
the resistance with an ohmmeter.
Option C. Measure
the resistance with a 250 volt megger.
Correct Answer is. Measure
the millivolt drop across the connection with a millivolt meter.
Explanation. EEL/1-6
4.3.
Question Number. 103. How would you measure continuity of a
coaxial cable?.
Option A. With a
safety ohmmeter.
Option B. With a
reflectometer.
Option C. With a
250 volt megger.
Correct Answer is. With
a reflectometer.
Explanation. Other
versions of this question say Time Domain Reflectometer, or Time Delay
Reflectometer.
Question Number. 104. On a long coaxial cable how would you check
for discontinuities and shorts in situ?.
Option A. Continuity
tester.
Option B. Safety
ohmmeter.
Option C. Time
Domain Reflectometer.
Correct Answer is. Time
Domain Reflectometer.
Explanation. A TDR
will find damaged bits of long coax runs. One version of this question says
Time 'Delay' Reflectometer - which means the same thing.
Question Number. 105. If the leads of a bonding tester are
damaged, what is the procedure?.
Option A. The
damaged leads and the tester should be returned to the manufacturer for repair
and calibration.
Option B. Provided
that the damage is situated close to the end of the leads the cable may be
shortened.
Option C. A new
lead may be manufactured using the correct current rated cable.
Correct Answer is. The
damaged leads and the tester should be returned to the manufacturer for repair
and calibration.
Explanation. Leaflet
9-1 3.1.1. & EEL/1-6 Para 3.11.2.
Question Number. 106. When carrying out a continuity test on a
circuit when a known resistance exists, what instrument would you use?.
Option A. A lamp
and battery.
Option B. A high
resistance insulation tester.
Option C. A
multimeter.
Correct Answer is. A
multimeter.
Explanation. NIL.
Question Number. 107. Taper pins are classified by.
Option A. length
and diameter of large end.
Option B. length
and diameter of small end.
Option C. length
and taper.
Correct Answer is. length
and diameter of small end.
Explanation. Leaflet
2-5 11. BL/6-13 11.
Question Number. 108. Live AC circuits are to be checked for open
circuits by the use of.
Option A. multimeter
set to AC volts.
Option B. ammeter
set to amps.
Option C. ohmmeter
set to megohms.
Correct Answer is. multimeter
set to AC volts.
Explanation. A
voltmeter would be used because it does not require the breaking of the
circuit.
Question Number. 109. A multiplier resistance is used to extend
the working range of the.
Option A. ammeter.
Option B. voltmeter.
Option C. ohmmeter.
Correct Answer is. voltmeter.
Explanation. Multipliers
are used with voltmeters. A&P Airframe Technician Textbook.
Question Number. 110. On twist drill chart, small drills have.
Option A. smallest
numbers.
Option B. largest
numbers.
Option C. their
sizes in fractions, in inches.
Correct Answer is. largest
numbers.
Explanation. Numbered
drill go from 80 (0.0135 inches - smallest) to 1 (0.228 inches - largest) and
are then lettered.
Question Number. 111. The Sine Bar is used to.
Option A. check
accuracy of slip gauges.
Option B. produce
angles using slip gauges.
Option C. by
itself to calculate angles.
Correct Answer is. produce
angles using slip gauges.
Explanation. Workshop
Technology Part 2 WAJ Chapman Pg.57.
Question Number. 112. On a vernier micrometer, what will three
turns of the barrel represent?.
Option A. 0.075
inch.
Option B. 0.100
inch.
Option C. 0.050
inch.
Correct Answer is. 0.075
inch.
Explanation. One
full turn of a vernier micrometer thimble is 0.025 inch.
Question Number. 113. How does a windy drill get its power?
Option A. Spur
gears.
Option B. Impeller.
Option C. Bevel
gears.
Correct Answer is. Impeller.
Explanation. Windy
drills have an impeller to derive power from the air pressure.
Question Number. 114. How are taper reamers classified?.
Option A. Length,
diameter of large end, and diameter of small end.
Option B. Taper
and diameter of small end.
Option C. Length
and diameter of large end.
Correct Answer is. Length
and diameter of large end.
Explanation. Taper
reamers are normally classified by a number 1-10, but if not, by diameter of
large end.
Question Number. 115. An AC voltmeter reads.
Option A. peak
value.
Option B. peak
to peak value.
Option C. average
value.
Correct Answer is. average
value.
Explanation. An AC
voltmeter (known as Average Responding) measures RMS.
Question Number. 116. A hydrometer is used to.
Option A. check
battery electrolyte specific gravity.
Option B. check
battery electrolyte density.
Option C. take
humidity reading.
Correct Answer is. check
battery electrolyte specific gravity.
Explanation. Specific
gravity is the density relative to water at 4 degrees C.
Question Number. 117. A pyrometer is a.
Option A. thermometer
for use at high temperature.
Option B. pyramid
shaped altimeter.
Option C. foam/granule
fire extinguisher.
Correct Answer is. thermometer
for use at high temperature.
Explanation. A
pyrometer measures high temperature.
Question Number. 118. A hygrometer is used to.
Option A. check
battery electrolyte relative density.
Option B. take
humidity reading.
Option C. check
battery electrolyte specific gravity.
Correct Answer is. take
humidity reading.
Explanation. A
hygrometer measures humidity.
Question Number. 120. To measure AC with a moving coil, it.
Option A. can be
directly connected.
Option B. is
rectified and measures peak value.
Option C. is
rectified and measures average value.
Correct Answer is. is
rectified and measures average value.
Explanation. Also
known as a D'Arsonval meter. See Jeppesen A&P General Textbook Section 3.
Note that the word 'Average' is incorrect because the meter reads RMS, but
average is the closest of the three answers.
Question Number. 121. What is a countersink tool used for?.
Option A. To
prevent damage to pipework in a blind hole.
Option B. To
adjust the depth of a countersink.
Option C. To
adjust the angle of a countersink.
Correct Answer is. To
adjust the depth of a countersink.
Explanation. The
countersink tool is to cut and adjust depths of the countersink.
Question Number. 122. PIDG crimp tools are marked by.
Option A. wire
crimp size on tool only.
Option B. coloured
handles and wire crimp size on tool.
Option C. coloured
handles only.
Correct Answer is. coloured
handles and wire crimp size on tool.
Explanation. Leaflet
9-3 fig 2. Handles are red, blue or yellow and the AWG is stamped on the jaws.
Question Number. 123. When measuring a square waveform with a
multimeter, what voltage does it display?.
Option A. Less
than RMS value.
Option B. More
than RMS value.
Option C. Equal
to RMS value.
Correct Answer is. Equal
to RMS value.
Explanation. A
multimeter measures RMS of whatever waveform it is measuring.
Question Number. 124. If an ammeter reads 0 - 1mA FSD, what would
you be required to do to enable it to read 10mA FSD?.
Option A. Place
a 5.8 ohm resistor as a shunt in parallel with the meter.
Option B. Place
a 9.9 ohm resistor across the coils.
Option C. Place
a 9 ohm resistor in series with the meter.
Correct Answer is. Place
a 5.8 ohm resistor as a shunt in parallel with the meter.
Explanation. No
calculation necessary (nor possible, with information given). A shunt is used
with an ammeter to bypass unwanted current.
Question Number. 125. The internal resistance of a voltmeter is.
Option A. no
more than 0.05 ohms.
Option B. low.
Option C. high.
Correct Answer is. high.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 164.
Question Number. 126. The internal resistance of an ammeter is.
Option A. low.
Option B. 1 ohm.
Option C. high.
Correct Answer is. low.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 162.
Question Number. 127. A drill bit of 0.250 inch would be.
Option A. 7/32
and letter G.
Option B. 8/32
and letter E.
Option C. 6/32
and letter F.
Correct Answer is. 8/32
and letter E.
Explanation. See a
drill chart.
Question Number. 128. Needle grease points are used on.
Option A. items
with gland seals.
Option B. small
pivoted joints.
Option C. large
pivoted joints.
Correct Answer is. small
pivoted joints.
Explanation. Needle
grease points are flush grease nipples which require a pointed adapter on the
grease gun.
Question Number. 129. A flat chisel being used for aluminium
should have a point angle of.
Option A. 65
degrees.
Option B. 30
degrees.
Option C. 55
degrees.
Correct Answer is. 30
degrees.
Explanation. NIL.
Question Number. 130. A mill file can be used for.
Option A. corners
less than 60 degrees.
Option B. saw
sharpening.
Option C. general
purpose.
Correct Answer is. saw
sharpening.
Explanation. External
document. http://www.rockler.com/tech/12369.pdf
Question Number. 131. A rawhide mallet is.
Option A. available
with copper inserts.
Option B. less
expensive than bossing mallet.
Option C. used
for giving softer blows than boxwood mallet.
Correct Answer is. used
for giving softer blows than boxwood mallet.
Explanation. NIL.
Question Number. 132. Tension files.
Option A. can be
used to cut in one direction only.
Option B. clog
easily.
Option C. can
cut in either direction.
Correct Answer is. can
cut in either direction.
Explanation. Also
known as an ABRAFILE.
Question Number. 133. The scale on an ohmmeter is.
Option A. cramped
at high resistance.
Option B. linear.
Option C. cramped
at low resistance.
Correct Answer is. cramped
at high resistance.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 169 photo, fig 8-26.
Question Number. 134. Three revolutions of a 40 T.P.l. micrometer
will show.
Option A. 0.03
inch.
Option B. 0.075
inch.
Option C. 0.003
inch.
Correct Answer is. 0.075
inch.
Explanation. 0.025
inch * 3 = 0.075.
Question Number. 135. To carry out a continuity test you would
use.
Option A. ammeter.
Option B. an HT
circuit tester.
Option C. a low
reading ohmmeter.
Correct Answer is. a
low reading ohmmeter.
Explanation. NIL.
Question Number. 136. What is the resolution of a standard DTI?.
Option A. 0.020
mm.
Option B. 0.050
mm.
Option C. 0.010
mm.
Correct Answer is. 0.010
mm.
Explanation. Some
modern DTIs can do 1/10th of that.
Question Number. 137. In a moving coil meter the deflecting force
is provided by.
Option A. a soft
iron permanent magnet.
Option B. a
current carrying coil pivoted in a permanent magnet field.
Option C. hairsprings
which move the pointer towards full scale.
Correct Answer is. a
current carrying coil pivoted in a permanent magnet field.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 159.
Question Number. 138. The force acting on a meter which returns
the pointer to zero is called the.
Option A. turning
force.
Option B. deflecting
force.
Option C. controlling
force.
Correct Answer is. controlling
force.
Explanation. NIL.
Question Number. 139. The forces acting on a meter which moves
the pointer over the scale is called.
Option A. the
controlling force.
Option B. the
turning force.
Option C. the
deflecting force.
Correct Answer is. the
deflecting force.
Explanation. NIL.
Question Number. 140. The resistance of an ammeter must be.
Option A. high
to create a large volts drop across it.
Option B. low to
prevent volts drop across it.
Option C. low
because the ammeter is in parallel with the circuit.
Correct Answer is. low
to prevent volts drop across it.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 162/3.
Question Number. 141. The resistance of a voltmeter must be.
Option A. high
so that little current passes through it.
Option B. low to
prevent overloading the circuit.
Option C. low to
provide a parallel path for the circuit current.
Correct Answer is. high
so that little current passes through it.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 164.
Question Number. 142. When operating a grease gun, you.
Option A. verify
grease fitting can accept grease by hand feel.
Option B. apply
a pressure of 50 - 80 psi.
Option C. clean
grease fitting with clean dry cloth beforehand.
Correct Answer is. clean
grease fitting with clean dry cloth beforehand.
Explanation. NIL.
04. Avionic General Test Equipment.
Question Number. 1. A fuel quantity test set has an
externally adjustable.
Option A. capacitor.
Option B. inductor.
Option C. resistor.
Correct Answer is. resistor.
Explanation. AL/10-3
8.2.6.
Question Number. 2. How would you test a mach switch
in-situ?.
Option A. Use
built in test equipment.
Option B. Use an
external test kit.
Option C. It is
not possible to test a mach switch in situ.
Correct Answer is. Use
built in test equipment.
Explanation. NIL.
Question Number. 3. The maximum value of bonding of a
secondary structure is.
Option A. 1
megohm.
Option B. 1 ohm.
Option C. 1
kilohm.
Correct Answer is. 1
ohm.
Explanation. CAIP S
EEL/1-6 Para 3-8.
Question Number. 4. Circuit tests on aircraft should be
carried out in the following order:
Option A. bonding,
continuity, insulation, functional.
Option B. continuity,
bonding, functional, insulation.
Option C. functional,
bonding, continuity, insulation.
Correct Answer is. bonding,
continuity, insulation, functional.
Explanation. Code to
remember, B C I F.
Question Number. 5. Before using a dead weight tester you
would.
Option A. calibrate
the tester using a standard weight.
Option B. pressurize
the tester to the required pressure.
Option C. replace
the oil.
Correct Answer is. pressurize
the tester to the required pressure.
Explanation. The
dead weight tester is first pumped up to the required pressure
(platform/weights floating) then gauge under test is connected.
Question Number. 6. How should a dead weight tester be
used?.
Option A. The
pressure increasing handle should be screwed in before the addition of fluid
and screwed out when fluid is added.
Option B. The
outlet should not be connected to the instrument until the required weights are
raised by the platform.
Option C. The
platform should be removed and fluid poured into the hole.
Correct Answer is. The
outlet should not be connected to the instrument until the required weights are
raised by the platform.
Explanation. Handle
is wound in until the weights are floating, then the outlet pressure is slowly
released to the gauge under test.
Question Number. 7. When testing thermocouples using a test
set the ambient temperature.
Option A. never
needs to be considered.
Option B. is
considered every time.
Option C. is
only considered when temperatures of 20°C or above.
Correct Answer is. is
considered every time.
Explanation. AL/10-3
11.11.1. To test the system the test set has to be trimmed for ambient
temperature, as the system when in operation is adjusted for ambient
temperature by the compensating resistor. This is clearly stated in the B 737
AMM.
Question Number. 8. Electronic test equipment for fuel tank
contents systems usually incorporate variable.
Option A. resistors.
Option B. inductors.
Option C. capacitors.
Correct Answer is. capacitors.
Explanation. NIL.
Question Number. 9. Before using a bonding tester, the 6 foot
lead has the two prongs shorted together with a piece of metal. What would the
indicator read?.
Option A. Full
scale left.
Option B. Full
scale right.
Option C. Zero
at the centre.
Correct Answer is. Full
scale right.
Explanation. Leaflet
9-1 3.10.2 a Infinity is full scale to the right.
Question Number. 10. When using a megger to test insulation
resistance, capacitive filters should be disconnected for what reason?.
Option A. Remove
the risk of damage to the megger.
Option B. Remove
the spurious readings caused by the capacitors charging and discharging.
Option C. Prevent
damage to the filters.
Correct Answer is. Prevent
damage to the filters.
Explanation. Leaflet
9-1 4.4.4 e AandP Mechanics General Handbook Pg 351.
Question Number. 11. When carrying out a serviceability check
on a bonding tester - short together the three prongs of both probes and ensure
which of the following?.
Option A. The
meter reads 0.1 ohm.
Option B. A zero
reading.
Option C. A full
scale reading is obtained.
Correct Answer is. A
zero reading.
Explanation. Leaflet
9-1 3.10.2 (b).
Question Number. 12. If an insulation resistance tester is
operated and the leads are suspended in free air, what will the meter read?.
Option A. Zero.
Option B. Mid
scale - it is a ratiometer movement and there is no current flowing in the
external circuit.
Option C. Infinity.
Correct Answer is. Infinity.
Explanation. NIL.
Question Number. 13. When using a digital meter to test a
diode, a correct operation of the diode is indicated by a volt drop of.
Option A. 0.3V
to 0.7V.
Option B. 2.5V
to 2.8V.
Option C. 1.5V
to 2V.
Correct Answer is. 0.3V
to 0.7V.
Explanation. Forward
voltage drop of a diode is 0.2V (germanium) or 0.6V (silicon).
Question Number. 14. To check that the ident pulse is being
generated from an ATC transponder,.
Option A. select
an ATC channel and check the morse code.
Option B. select
ident and check the indication on the instrument panel.
Option C. press
the ident and monitor the indication on the ramp test set.
Correct Answer is. press
the ident and monitor the indication on the ramp test set.
Explanation. The
ident is a button on the transponder panel, which, when pressed, causes the
indication on the ATCs radar screen to 'bloom'.
Question Number. 15. A pressure gauge is fitted to a Dead
Weight Tester. The piston area is 0.25 sq.in. and the total mass of the mass
carrier and masses is 5lb. If the pressure gauge is accurate what pressure in
pounds per square inch (PSI) will it read?.
Option A. 1.25
psi.
Option B. 20
psi.
Option C. 200
psi.
Correct Answer is. 20
psi.
Explanation. Pressure
= Force / Area = 5/0.25 = 20 PSI.
Question Number. 16. When testing a fuel metering unit, how is
it checked?.
Option A. With
the meter in series with the unit.
Option B. With
the unit disconnected.
Option C. With
the meter in parallel with the unit.
Correct Answer is. With
the meter in series with the unit.
Explanation. A fuel
metering unit is checked with the fuel meter in series with the meter under
test. No reference found.
Question Number. 17. When using a bonding tester.
Option A. ensure
prongs penetrate anodised layer.
Option B. ensure
prongs do not penetrate anodising layer.
Option C. an
anodised component cannot be tested.
Correct Answer is. ensure
prongs penetrate anodised layer.
Explanation. Leaflet
9-1 Para.3.10.6.
Question Number. 18. On a static leak tester, pressure is
released by.
Option A. an
internal balance valve in the tester.
Option B. slowly
opening the release knob for 3 minutes.
Option C. a
bleed valve in the tester.
Correct Answer is. slowly
opening the release knob for 3 minutes.
Explanation. The
pressure in the pitot/static leak tester must be released slowly.
Question Number. 19. A fuel calibration test set when used to
check an aircraft with half a fuel load is connected.
Option A. to
gauge with fuel level in parallel.
Option B. to
gauge with fuel level capacitance.
Option C. to
gauge with fuel level in series.
Correct Answer is. to
gauge with fuel level in series.
Explanation. The
test set is connected in series with the fuel level conditioner.
Question Number. 20. A capacitive fuel contents system should
be tested with.
Option A. a
ratiometer.
Option B. a
Wheatstone bridge.
Option C. a
decade box.
Correct Answer is. a
Wheatstone bridge.
Explanation. By
elimination.
Question Number. 21. Continuity of a fibreoptic cable is
tested with a.
Option A. light
source and optometer.
Option B. multimeter.
Option C. calibrated
light generator and opto-power meter.
Correct Answer is. calibrated
light generator and opto-power meter.
Explanation. External
website. http://www.tpub.com/neets/tm/109-13.htm
Question Number. 22. When using transistorized test equipment,
what should the output be?.
Option A. Not
affected by impedance.
Option B. High
impedance.
Option C. Low
impedance.
Correct Answer is. Low
impedance.
Explanation. Transistorised
equipment generally has a high input impedance and a low output impedance.
Question Number. 23. To read the transponder coding from an
aircraft's transponder you.
Option A. use
the code signal and a chart to determine the signal.
Option B. use a
ATC600 test set.
Option C. use
the output on the flight deck.
Correct Answer is. use
a ATC600 test set.
Explanation. Jeppesen
Aircraft Radio Systems - Powell Page 136/7.
Question Number. 24. Bonding lead testers are attached with.
Option A. a 60
feet lead is connected to the main earth and a 6 foot test lead is connected to
check the resistance between selected points.
Option B. a 6
feet test lead is connected to the main earth and a 60 feet lead is connected
to check the resistance between selected points.
Option C. either
of the leads can be connected anywhere.
Correct Answer is. a
60 feet lead is connected to the main earth and a 6 foot test lead is connected
to check the resistance between selected points.
Explanation. Leaflet
9-1 3.10.3.
Question Number. 25. On a Bonding Tester the number of probes
on the 60 ft and 6ft leads respectively are.
Option A. 1 and
2.
Option B. 2 and
2.
Option C. 2 and
1.
Correct Answer is. 1
and 2.
Explanation. Leaflet
9-1 3.10.
Question Number. 26. The damping force in a meter.
Option A. prevents
oscillation of the pointer.
Option B. returns
the pointer to zero.
Option C. assists
the pointer to move over the scale.
Correct Answer is. prevents
oscillation of the pointer.
Explanation. NIL.
Question Number. 27. On a VOR/ILS test set the 'Tone Delete'
function.
Option A. functionally
checks that the glideslope pointer moves down-scale.
Option B. functionally
checks that the glideslope failure flag operates.
Option C. functionally
checks that the glideslope pointer moves up-scale.
Correct Answer is. functionally
checks that the glideslope failure flag operates.
Explanation. The
Tone Delete tests the flag.
05. Engineering Drawings, Diagrams and Standards.
Question Number. 1. What is third angle projection?.
Option A. each
view represents the side of the object furthest from the adjacent view.
Option B. each
view represents the side of the object nearest to it in the adjacent view.
Option C. each
view is at an angle of 30 degrees to the plane of projection.
Correct Answer is. each
view represents the side of the object nearest to it in the adjacent view.
Explanation. CAAIP S
leaflet 2.1 page 7 para 5.3.1.
Question Number. 2. This drawing indicates.
Option A. a
countersunk hole.
Option B. a
blind tapped hole.
Option C. a
counterbored hole.
Correct Answer is. a
blind tapped hole.
Explanation. CAAIP S
Leaflet 2-1 Table 3.
Question Number. 3. The width of a visible outline on a
drawing is.
Option A. 0.3
mm.
Option B. 0.7
mm.
Option C. 0.5
mm.
Correct Answer is. 0.7
mm.
Explanation. CAAIP S
Leaflet 2-1 5.2.
Question Number. 4. What does GA stand for on a drawing?.
Option A. General
assembly.
Option B. General
arrangement.
Option C. Gradient
Axis.
Correct Answer is. General
arrangement.
Explanation. NIL.
Question Number. 5. Design drawings of aircraft components
are produced by organizations approved by.
Option A. SBAC.
Option B. British
Standards Institute.
Option C. CAA in
accordance with the BCARs.
Correct Answer is. CAA
in accordance with the BCARs.
Explanation. NIL.
Question Number. 7. Which pictorial projection shows one
face in true elevation and line of depth normally draw at 30° or 45° to the
horizontal?.
Option A. Oblique.
Option B. Perspective.
Option C. Isometric.
Correct Answer is. Oblique.
Explanation. NIL.
Question Number. 8. If a design amendment is made on a
drawing.
Option A. a new
issue number and date must be allocated to the drawing.
Option B. the
old issue number is retained, with the amendment date added.
Option C. no
change in issue number or date is necessary.
Correct Answer is. a
new issue number and date must be allocated to the drawing.
Explanation. Leaflet
2-1 4.2.
Question Number. 9. The British Standard for Engineering
Drawings is.
Option A. BS
308.
Option B. BS
306.
Option C. BS
307.
Correct Answer is. BS
308.
Explanation. Leaflet
2-1 1.3.
Question Number. 10. P.C.D. is an abbreviation for.
Option A. Pitch
Circle Diameter.
Option B. Pitch
Cord Diameter.
Option C. Precision
Circle Dimension.
Correct Answer is. Pitch
Circle Diameter.
Explanation. Leaflet
2-1 table 3.
. Question Number. 13. Drawing numbers are.
Option A. the
same as serial numbers.
Option B. changed
after each drawing amended after May 28, 1999.
Option C. unique
to each drawing.
Correct Answer is. unique
to each drawing.
Explanation. Leaflet
2-1 4.1.
Question Number. 14. Hatching lines are usually drawn at:.
Option A. 60°.
Option B. 30°.
Option C. 45°.
Correct Answer is. 45°.
Explanation. Jeppesen
A&P General Textbook fig 5-20 and Leaflet 2-1 5.4.1a.
Question Number. 15. The scale of an engineering drawing is shown
as 1 : 4. This indicates it is.
Option A. drawn
to a quarter.
Option B. drawn
to scale.
Option C. drawn
four times larger.
Correct Answer is. drawn
to a quarter.
Explanation. Leaflet
2-1 5.1.
Question Number. 16. An orthographic projection usually shows.
Option A. one,
three-dimensional view of an object.
Option B. a
pictorial view of the object.
Option C. three,
two-dimensional views of an object.
Correct Answer is. three,
two-dimensional views of an object.
Explanation. Leaflet
2-1 5.3.
Question Number. 17. When dimensioning a drawing, the
dimension lines should be.
Option A. the
minimum number of dimensions necessary to enable the component to be
manufactured.
Option B. as
many dimensions as possible.
Option C. only
size dimensions.
Correct Answer is. the
minimum number of dimensions necessary to enable the component to be
manufactured.
Explanation. Leaflet
2-1 5.5.
Question Number. 18. PFD' on an engineering drawing would
indicate.
Option A. dye
penetrant check.
Option B. ultra-sonic
test.
Option C. repair
and recondition.
Correct Answer is. dye
penetrant check.
Explanation. CAAIP S
Leaflet 2-1 Table 4.
Question Number. 19. S.W.G. is an abbreviation for.
Option A. Standard
Wire Gauge.
Option B. Screw
Width Gauge.
Option C. Standard
Water Gauge.
Correct Answer is. Standard
Wire Gauge.
Explanation. CAAIP S
Leaflet 2-1 Table 3.
Question Number. 20. If you are unable to identify a structure
'classification' as either primary or secondary, what action should you adopt?.
Option A. Grade
it as 'secondary'.
Option B. Upgrade
it to ‘primary’.
Option C. Paint
it red and stamp it as 'tertiary'.
Correct Answer is. Upgrade
it to ‘primary’.
Explanation. NIL.
Question Number. 21. What colour is used to indicate a tertiary
structure on a diagram or drawing?.
Option A. Red.
Option B. Green.
Option C. Yellow.
Correct Answer is. Green.
Explanation. NIL.
Question Number. 22. Which parts of the aircraft are
classified secondary structures?.
Option A. Highly
stressed parts but if damaged will not cause failure of the aircraft.
Option B. Highly
stressed parts and if damaged may cause failure of the aircraft and loss of
life.
Option C. Lightly
stressed parts such as fairings, wheel shields and minor component brackets etc.
Correct Answer is. Highly
stressed parts but if damaged will not cause failure of the aircraft.
Explanation. NIL.
Question Number. 25. The abbreviation B.A. means.
Option A. British
Assembly.
Option B. British
Association.
Option C. British
Arrangement.
Correct Answer is. British
Association.
Explanation. Leaflet
3-3.
Question Number. 27. Where are correct layout, dimensioning,
numbering and reference procedures for engineering drawing are to be found?.
Option A. BS 31.
Option B. BS
1916.
Option C. BS
308.
Correct Answer is. BS
308.
Explanation. Leaflet
2-1 1.1.
Question Number. 28. 10 : 1 on an engineering drawing
indicates.
Option A. the
drawing is full size.
Option B. the
drawing is one tenth full size.
Option C. the
drawing is ten times full size.
Correct Answer is. the
drawing is ten times full size.
Explanation. Aircraft
Instruments and Integrated Systems, Pallett Page 1 5.1.
Question Number. 30. Lines known as short dashes (thin) are
used on drawings to indicate.
Option A. hidden
detail.
Option B. visible
outlines.
Option C. cutting
revolved.
Correct Answer is. hidden
detail.
Explanation. Leaflet
2-1 table 1.
Question Number. 32. Any change to a drawing.
Option A. must
be notified to the S.B.A.C.
Option B. must
be accompanied by the new issue number and date.
Option C. requires
a new drawing number.
Correct Answer is. must
be accompanied by the new issue number and date.
Explanation. Leaflet
2-1 4.2.
Question Number. 35. Break lines are used.
Option A. to
show where components are expected to break.
Option B. in
sectional drawing.
Option C. where
it would be inconvenient (because of limited space) to draw long lengths of the
same section.
Correct Answer is. where
it would be inconvenient (because of limited space) to draw long lengths of the
same section.
Explanation. Leaflet
2-1 5.45.
Question Number. 36. An oblique projection.
Option A. is the
same as an isometric projection.
Option B. has
one view looking directly at one face with the lines representing depth drawn
at 90°.
Option C. has
one view looking directly at one face with the lines representing depth drawn
at a constant angle.
Correct Answer is. has
one view looking directly at one face with the lines representing depth drawn
at a constant angle.
Explanation. NIL.
Question Number. 37. A drawing in which the subassemblies or
parts are shown as brought together on the aircraft is called.
Option A. an
installation drawing.
Option B. a
detail drawing.
Option C. a
sectional drawing.
Correct Answer is. an
installation drawing.
Explanation. NIL.
Question Number. 38. A thread on a drawing is labeled ½-20 UNF
– 1B. The thread is
Option A. either
external or internal, depending on the application.
Option B. external.
Option C. internal.
Correct Answer is. internal.
Explanation.
Question Number. 39. NTS on a drawing stands for.
Option A. Not
True Scale.
Option B. No
Tolerance System.
Option C. Not To
Scale.
Correct Answer is. Not
To Scale.
Explanation. Leaflet
2-1 table 3.
Question Number. 40. A hydraulic system schematic drawing
would indicate the.
Option A. type
and quantity of the hydraulic fluid.
Option B. specific
location of the individual components within the aircraft.
Option C. direction
of fluid flow through the system.
Correct Answer is. direction
of fluid flow through the system.
Explanation. NIL.
Question Number. 41. Which statement is true regarding an
orthographic projection?.
Option A. There
are always at least two views.
Option B. It
could have as many as eight views.
Option C. One-view,
two-view, and three-view drawings are the most common.
Correct Answer is. One-view,
two-view, and three-view drawings are the most common.
Explanation. NIL.
Question Number. 42. A line used to show an edge which is not
visible is a.
Option A. break
line.
Option B. phantom
line.
Option C. hidden
line.
Correct Answer is. hidden
line.
Explanation. Leaflet
2-1 5.2 table 1.
Question Number. 43. One purpose for schematic diagrams is to
show the.
Option A. size
and shape of components within a system.
Option B. functional
location of components within a system.
Option C. physical
location of components within a system.
Correct Answer is. functional
location of components within a system.
Explanation. NIL.
Question Number. 45. What type of line is normally used in a
mechanical drawing or blueprint to represent an edge or object not visible to
the viewer?.
Option A. Alternate
short and long light dashes.
Option B. Medium-weight
dashed line.
Option C. Light
solid line.
Correct Answer is. Medium-weight
dashed line.
Explanation. Leaflet
2-1 5.2 table 1.
Question Number. 46. A specific measured distance from the datum
or some other point identified by the manufacturer, to a point in or on the
aircraft is called a.
Option A. zone
number.
Option B. station
number.
Option C. specification
number.
Correct Answer is. station
number.
Explanation. AL/7-2
6.
Question Number. 50. In a first angle orthographic projection
the plan view is placed.
Option A. above
the front elevation.
Option B. below
the side elevation.
Option C. below
the front elevation.
Correct Answer is. below
the front elevation.
Explanation. Leaflet
2-1 Figure 3.
Question Number. 51. When a cutting plane on a drawing cuts a
web longitudinally, the web is.
Option A. sectioned
the same as the rest of the view.
Option B. not
sectioned.
Option C. sectioned
with different direction of hatch.
Correct Answer is. not
sectioned.
Explanation. BS 308.
Question Number. 54. When a cutting plane goes through a bush
and bolt assembly, on the sectioned view.
Option A. both
the bush and the bolt will be hatched.
Option B. the
bush will be hatched but the bolt will not.
Option C. neither
the bush nor the bolt will be hatched.
Correct Answer is. the
bush will be hatched but the bolt will not.
Explanation. Leaflet
2-1 fig 5 5.4.1 (b).
Question Number. 58. The letter A.F.D. in a circle stamped on
a material indicates that it has.
Option A. been
anodic flaw detected.
Option B. been annealed
fired and doped.
Option C. an
across flats diameter bolt.
Correct Answer is. been
anodic flaw detected.
Explanation. Leaflet
2-1 Table 4.
Question Number. 59. Where would Zone 324 be found in ATA
100?.
Option A. Between
rear spar of wing and trailing edge of wing.
Option B. Tip of
horizontal stabilizer.
Option C. Fwd of
the wing rear spar.
Correct Answer is. Tip
of horizontal stabilizer
Explanation. Zone
3xx is empennage.
Question Number. 61. The latest drawing is identified by the.
Option A. issue
number.
Option B. amendment
number.
Option C. date.
Correct Answer is. issue
number.
Explanation. CAAIP\'s
leaflet 2-1 pg 4 para 4.2.
06. Fits and Clearances.
Question Number. 1. Tolerances are classified in two ways,
these are.
Option A. Dimensional
and isometric.
Option B. Upper
and lower.
Option C. Dimensional
and geometric.
Correct Answer is. Dimensional
and geometric.
Explanation. CAAIP S
leaflet 2-1 p16 para 5.11.
Question Number. 2. The maximum permissible bow in a steel
tube is.
Option A. 1 :
400.
Option B. 1 :
200.
Option C. 1 :
600.
Correct Answer is. 1
: 600.
Explanation. CAAIP S
Leaflet 6-4.
Question Number. 3. The equipment required to carry out a
run-out check on a shaft would be.
Option A. a DTI
and 'V' blocks.
Option B. a ball
bearing and a micrometer.
Option C. a
surface plate and a three leg trammel.
Correct Answer is. a
DTI and 'V' blocks.
Explanation. AC43.13-1B
Page 4-20.
Question Number. 4. What is the maximum bow allowed in a
strut?.
Option A. 1 in
200.
Option B. 1 in
500.
Option C. 1 in
600.
Correct Answer is. 1
in 600.
Explanation. CAAIP S
Leaflet 2-10.
Question Number. 5. Which of the following shafts would you
use to obtain a clearance fit in a bush 0.750 inch diameter?.
Option A. 0.752
inch.
Option B. 0.748
inch.
Option C. 750
inch.
Correct Answer is. 0.748
inch.
Explanation. NIL.
Question Number. 6. Which of the following is checked when
using a 'GO / NO -GO' gauge?.
Option A. Clearance.
Option B. Tolerance.
Option C. Allowance.
Correct Answer is. Tolerance.
Explanation. NIL.
Question Number. 7. Which of the following is a 'Bilateral
Tolerance'?.
Option A. 2
inches -0.002.
Option B. 2
inches +0.002.
Option C. 2
inches ±0.002.
Correct Answer is. 2
inches ±0.002.
Explanation. NIL.
Question Number. 8. A tolerance is.
Option A. a
permitted difference between new and worn dimensions.
Option B. a
permitted variation on a dimension to allow for inaccuracy of equipment.
Option C. a
required difference in dimension between mating parts to obtain a certain class
of fit.
Correct Answer is. a
permitted variation on a dimension to allow for inaccuracy of equipment.
Explanation. NIL.
Question Number. 9. A transition fit is one in which the
shaft is.
Option A. larger
than the hole.
Option B. smaller
than the hole.
Option C. the
same size as the hole.
Correct Answer is. the
same size as the hole.
Explanation. BS 4500
Datasheet 4500A., External document. www.tech.plym.ac.uk/sme/disnotes/tola.pdf
Question Number. 10. The length of a blended repair of
corrosion should be no less than.
Option A. 10
times its depth.
Option B. 20
times its depth.
Option C. 5
times its depth.
Correct Answer is. 20
times its depth.
Explanation. NIL.
Question Number. 11. If there is a positive allowance between
the smallest possible hole and the largest possible shaft, the fit is known as.
Option A. a
transition fit.
Option B. a
clearance fit.
Option C. an
interference fit.
Correct Answer is. a
clearance fit.
Explanation. NIL.
Question Number. 12. After mechanical removal of corrosion on
an aluminium alloy casting, the length of the blended recess should be.
Option A. no
less than ten times the depth.
Option B. no
less than twenty times the depth.
Option C. no
more than twenty times the depth.
Correct Answer is. no
less than twenty times the depth.
Explanation. AC43
6.118 6-23.
Question Number. 13. A press fit requires.
Option A. some
sort of driving force.
Option B. the
shaft to be shrunk by cooling.
Option C. the
hole to be expanded by heat.
Correct Answer is. some
sort of driving force.
Explanation. A press
fit is a small interference only.
Question Number. 14. What is the typical acceptable limit of a
dent on a frame member?.
Option A. One
and a half times the skin thickness.
Option B. Twice
the skin gauge and 0.75 inch diameter.
Option C. One
gauge depth and 0.75 inch diameter.
Correct Answer is. One
gauge depth and 0.75 inch diameter.
Explanation. NIL.
Question Number. 15. A light drive clearance between 3/4 inch
diameter bolt and hole, on a drawing would be shown as.
Option A. 0.005
Inches.
Option B. 0.0015
Inches.
Option C. 0.0025
Inches.
Correct Answer is. 0.0015
Inches.
Explanation. AC43
says 0.0006 for a 3/8 in. bolt, so 0.0015 is the closest (and reasonable for a
3/4 in. bolt).
07. Electrical Cables and Connectors.
Question Number. 1. In a front release connector the pin
will be.
Option A. released
from rear and extracted from the front.
Option B. released
from the front and extracted from the front.
Option C. released
from the front and extracted from the rear.
Correct Answer is. released
from the front and extracted from the rear.
Explanation. CAAIP S
Leaflet 9-3 8.3.2.
Question Number. 2. A wire clamped vertically at one end
and horizontally at the other end should have a bend radius of no less than.
Option A. 3
times the diameter of the wire.
Option B. 5
times the diameter of the wire.
Option C. 10
times the diameter of the wire.
Correct Answer is. 3
times the diameter of the wire.
Explanation. CAIP S
AL/3-2 6.4.
Question Number. 3. Glycol deicer fluid in contact with a
silver cable can cause.
Option A. a
fire.
Option B. disintegration
of the cable insulation.
Option C. corrosion.
Correct Answer is. a
fire.
Explanation. CAAIP S
Leaflet 11-5 Para.8.8.
Question Number. 4. With a rear release connector, the pin
will be.
Option A. released
from the front and extracted from the rear.
Option B. released
from the rear and extracted from the front.
Option C. released
from the rear and extracted from the rear.
Correct Answer is. released
from the rear and extracted from the rear.
Explanation. CAAIP S
Leaflet 9-3, 8.3.2 (b) (i).
Question Number. 5. The maximum operating temperature for a
nickel plated copper or aluminium connector is.
Option A. 260°C.
Option B. 135°C.
Option C. 200°C.
Correct Answer is. 260°C.
Explanation. CAAIP S
leaflet 11-5 para 7.2.1.
Question Number. 6. What gauge of pin would a yellow
plastic insert/extract tool be used on?.
Option A. 16 - 14.
Option B. 12 -
10.
Option C. 22 -
18.
Correct Answer is. 12
- 10.
Explanation. NIL.
Question Number. 7. Can the insulation grip be adjusted on
a PIDG crimp tool?.
Option A. No.
Option B. Yes by
turning a knob.
Option C. Yes by
adjusting the pins.
Correct Answer is. Yes
by adjusting the pins.
Explanation. NIL.
Question Number. 8. What gauge of pin would a red plastic
insert/extract tool be used on?.
Option A. 12 -
10.
Option B. 22 -
18.
Option C. 16 -
14.
Correct Answer is. 22
- 18.
Explanation. Boeing
Standard Wiring Practices, External website. http://www.cheifaircraft.com/Aircraft/InstallationSupply/Terminals.html
Question Number. 9. What cable would you use where
temperatures are going to exceed 200°C?.
Option A. Tinned
copper or aluminium.
Option B. Silver
plated copper or aluminium.
Option C. Nickel
plated copper or aluminium.
Correct Answer is. Nickel
plated copper or aluminium.
Explanation. CAAIP S
Leaflet 11-5, 7.2.1.
Question Number. 10. How long should a fireproof cable last in
a fire?.
Option A. 5
minutes.
Option B. 50
minutes.
Option C. 15
minutes.
Correct Answer is. 15
minutes.
Explanation. NIL.
Question Number. 11. What gauge of pin would a blue plastic
insert / extract tool be used on?.
Option A. 12 -
10.
Option B. 16 -
14.
Option C. 22 -
18.
Correct Answer is. 16
- 14.
Explanation. NIL.
Question Number. 12. The insulation resistance for wiring in
undercarriage wheel-wells should normally be not less than.
Option A. 10
megohms.
Option B. 5
megohms.
Option C. 2
megohms.
Correct Answer is. 2
megohms.
Explanation. CAIP S
EEL/1-6 Para 4-5-4 (a).
Question Number. 13. What causes knuckling on older type
electrical cables?.
Option A. Over-temperature
soldering.
Option B. Applying
cable ties too tightly.
Option C. Excessive
pull through forces.
Correct Answer is. Excessive
pull through forces.
Explanation. Leaflet
1l-5 8.6.
Question Number. 14. To find a high resistance or open
circuit, carry out.
Option A. a
milli-volt drop test.
Option B. a
continuity check.
Option C. a
bonding check.
Correct Answer is. a
continuity check.
Explanation. CAAIP S
Leaflet 9-1, 4.2.1.
Question Number. 15. The maximum bonding resistance on an
aircraft primary structure should be.
Option A. 0.01
ohms.
Option B. 0.001
ohms.
Option C. 0.05
ohms.
Correct Answer is. 0.05
ohms.
Explanation. CAAIP S
Leaflet 9-1, 3.8.
Question Number. 16. Before effecting a crimp, the bare ends
of a cable should be.
Option A. tightly
twisted.
Option B. twisted
lightly in the direction of the lay.
Option C. straightened
out.
Correct Answer is. twisted
lightly in the direction of the lay.
Explanation. CAAIP S
Leaflet 9-3, 7.5.3.
Question Number. 17. The number of the dots impressed on the
insulation of the pre-insulated connectors during crimping indicates that.
Option A. the
correct connector has been used.
Option B. the
correct tool was used to effect the connection.
Option C. the
crimp is properly formed.
Correct Answer is. the
correct tool was used to effect the connection.
Explanation. NIL.
Question Number. 18. The pressure of the insulation crimp jaws
on the PIDG crimping tool can be changed by.
Option A. varying
the torque applied to the handles.
Option B. using
different coloured crimping pliers and terminations.
Option C. changing
the position of the pins.
Correct Answer is. changing
the position of the pins.
Explanation. CAAIP S
Leaflet 9-3 fig 2.
Question Number. 19. When referring to fuses, HRC means.
Option A. high rupture
capacity.
Option B. hot
running capacity.
Option C. high
running current.
Correct Answer is. high
rupture capacity.
Explanation. High
Rupturing Capacity.
Question Number. 20. When wiring an electrical component to a
plug, the live wire is coloured.
Option A. blue.
Option B. green
and yellow.
Option C. brown.
Correct Answer is. brown.
Explanation. NIL.
Question Number. 21. A hole is placed in the lowest point of
electrical cable conduit.
Option A. to
allow for pull-through of the cables.
Option B. to
secure the conduit to a piece of aircraft structure.
Option C. to
allow for drainage of moisture.
Correct Answer is. to
allow for drainage of moisture.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 65.
Question Number. 22. The minimum distance between electrical
cable splices is.
Option A. 3
feet.
Option B. 12
inches.
Option C. 500
mm.
Correct Answer is. 500
mm.
Explanation. NIL.
Question Number. 23. A fire resistant cable is proof tested by
exposure to a standard fire for.
Option A. 30
minutes.
Option B. 5
minutes.
Option C. 15
minutes.
Correct Answer is. 5
minutes.
Explanation. CAAIP S
Leaflet 11-5 4.5 and EASA CS-1 Pg.6.
Question Number. 24. When fitting coaxial cable connectors it
is important to.
Option A. fit
the correct lock nuts.
Option B. make
sure the outer cup is fitted the correct way round.
Option C. not
damage any seals fitted.
Correct Answer is. not
damage any seals fitted.
Explanation. NIL.
Question Number. 25. When inserting pins into a front release
connector the inserting tool should be used with the gap facing which
direction?.
Option A. The
centre of the connector.
Option B. Either
direction.
Option C. The
outside of the connector.
Correct Answer is. The
outside of the connector.
Explanation. Leaflet
9-3 Para.8.3.2.
Question Number. 26. When using a hydraulic crimping tool,
after completing the crimping operation, the crimp is formed when when.
Option A. the
bypass valve opens and the ram returns to neutral.
Option B. the
foot pedal force is at maximum.
Option C. the
bypass valve closes and the ram returns to neutral.
Correct Answer is. the
bypass valve opens and the ram returns to neutral.
Explanation. NIL.
Question Number. 27. The type of binding tape used for cables
in temperatures above 260°C is which of the following?.
Option A. Nomex.
Option B. Teflon.
Option C. Nylon.
Correct Answer is. Teflon.
Explanation. This is
probably referring to the Teflon tape referred to in Aircraft Electricity and
Electronics by Eismin 5th Edition Page 69. Also AC43 Para.11.96 z and Appendix
1 (Teflon is Dupont trade-name for PTFE).
Question Number. 28. What is the minimum bend radius of a loom
adequately supported at a terminal block?.
Option A. 10 *
diameter.
Option B. 8 *
diameter.
Option C. 3 *
diameter.
Correct Answer is. 3
* diameter.
Explanation. Leaflet
9-3 7.3.
Question Number. 29. How are front release pins removed?.
Option A. The
tool is inserted from the front and the pin is removed from the front.
Option B. The
tool is inserted from the rear and the pin Is removed from the front.
Option C. The
tool is inserted from the front and the pin is removed from the rear.
Correct Answer is. The
tool is inserted from the front and the pin is removed from the rear.
Explanation. Leaflet
9-3 8.3.2 (b)(ii).
Question Number. 30. If a co-axial cable clamp is over
tightened so as to compress the dielectric, how will the capacitance change?.
Option A. Stay
the same.
Option B. Increase.
Option C. Decrease.
Correct Answer is. Increase.
Explanation. AC43
11-117. Decreasing dielectric thickness (of a capacitor) increases its
capacitance.
Question Number. 31. What is the minimum bend radius of a
single co-axial cable?.
Option A. 10 *
diameter.
Option B. 8 *
diameter.
Option C. 6 *
diameter.
Correct Answer is. 6
* diameter.
Explanation. AC43.13-1B
Page 11-45 Para.11-96 bb. No British reference found.
Question Number. 32. What is wet arc tracking?.
Option A. A
fault caused by hot stamp printing.
Option B. A
fault caused by insulation damage.
Option C. A
fault caused by 'knuckling through'.
Correct Answer is. A
fault caused by hot stamp printing.
Explanation. AC43.13-1B,
11-210 and CAAIP S Leaflet 11-5 Para.8.2.
Question Number. 33. When using a heat shrink gun, what should
the temperature of the gun be set to?.
Option A. 100°
below the heat shrink temperature.
Option B. 15°
below the heat shrink temperature.
Option C. 100°
above the heat shrink temperature.
Correct Answer is. 100°
above the heat shrink temperature.
Explanation. A trick
question. The 'Heat shrink temperature' is the normal 'room' temperature of
about 20-25°C. Most heat shrink materials shrink at around 125°C.
Question Number. 34. In an electrical cable 1EF6B22NMS, what
does the letter E represent?.
Option A. Circuit
function.
Option B. Cable
size.
Option C. Segment
letter.
Correct Answer is. Circuit
function.
Explanation. Leaflet
9-3 Para.9.1.1.
Question Number. 35. On a coaxial cable, cable impedance is.
Option A. proportional
to length.
Option B. not
effected by length.
Option C. inversely
proportional to length.
Correct Answer is. not
effected by length.
Explanation. The
length has nothing to do with a coaxial cable impedance. External website. http://www.epanorama.net/documents/wiring/cable_impedance.html
Question Number. 36. A secondary earth is.
Option A. not
less than 0.5mm cross sectional area.
Option B. 18
AWG.
Option C. 22
AWG.
Correct Answer is. 18
AWG.
Explanation. Leaflet
9-1 para.3.3 & EEL/1-6 3.3.1 (a) ii.
Question Number. 37. E' on a wire, under ATA 100 is a.
Option A. phase
indication.
Option B. system
ID code.
Option C. cable
size.
Correct Answer is. system
ID code.
Explanation. Leaflet
9-3 para.9.1.1.
Question Number. 38. To prevent wet arc tracking.
Option A. cable
grips should be tight.
Option B. ensure
hot stamp printing is controlled.
Option C. cables
should not be stretched.
Correct Answer is. ensure
hot stamp printing is controlled.
Explanation. Leaflet
11-5 8.2 and 6.7.
Question Number. 39. When splicing a cable with a soldered
joint, the operation is finished when.
Option A. the
solder has melted.
Option B. the
solder sleeve disappears.
Option C. the
solder and insulation have formed.
Correct Answer is. the
solder and insulation have formed.
Explanation. The
solder sleeve is a plastic cylinder with two rings of plastic at each end and a
solder ring in the middle. When heated the cylinder first melts on to the
wires, then the plastic rings melt, sealing the ends of the cylinder.
Question Number. 40. When manufacturing an electrical
connector the unused holes are.
Option A. filled
with connectors.
Option B. filled
with connectors and blanked.
Option C. covered
with blanks.
Correct Answer is. filled
with connectors and blanked.
Explanation. Leaflet
9-3 para 8.3.2 f)iii) and AC 43.13B 11-234.
Question Number. 41. Co-axial cable is preferred to airframe
cable in which application?.
Option A. Where
the diameter of cable is not important.
Option B. High
frequency interference.
Option C. Low
frequency interference.
Correct Answer is. Where
the diameter of cable is not important.
Explanation. Cable
is susceptible to all frequencies of interference. Co-axial cable is reasonably
well protected from all frequencies of interference but is much thicker overall
than airframe cable.
Question Number. 42. Forward release electrical connectors are
removed by the wire being.
Option A. pushed
forwards.
Option B. twisted
to the right.
Option C. pulled
backwards.
Correct Answer is. pulled
backwards.
Explanation. Leaflet
9-3 8.32 II.
Question Number. 43. When crimping wires, the wires should be.
Option A. straight.
Option B. lightly
twisted.
Option C. twisted.
Correct Answer is. lightly
twisted.
Explanation. Leaflet
9-3 7.5.5 ©.
Question Number. 44. Why are copper wires used in electrical
systems?.
Option A. They
have high permeability.
Option B. They
do not give off a magnetic field.
Option C. They
have a low resistance to current.
Correct Answer is. They
have a low resistance to current.
Explanation. Copper
has a low resistance to current.
Question Number. 45. When crimping wires, the wire should.
Option A. be
flush with the crimp.
Option B. extend
0.8 mm beyond the crimp.
Option C. be
beneath the crimp.
Correct Answer is. extend
0.8 mm beyond the crimp.
Explanation. NIL.
Question Number. 46. 1EF6B22 NMSV. What does the B mean?.
Option A. Segment
letter.
Option B. Cable
number.
Option C. Circuit
function.
Correct Answer is. Segment
letter.
Explanation. Leaflet
9-3 9.1.1.
Question Number. 47. A white/blue insertion-extraction tool
would be used on a cable of what size?.
Option A. 10.
Option B. 22.
Option C. 16.
Correct Answer is. 16.
Explanation. NIL.
Question Number. 48. The value of the insulation resistance of
an electric motor compared to its supply leads is.
Option A. greater.
Option B. same.
Option C. smaller.
Correct Answer is. smaller.
Explanation. Leaflet
9-1 4.5.4 (c) 'Rated voltage / 150' whereas supply leads must take the supply
voltage at least.
Question Number. 49. According to ATA 100, a symbol code 'X'
on a wiring number denotes.
Option A. a
warning circuit.
Option B. a
ground circuit.
Option C. AC
power.
Correct Answer is. AC
power.
Explanation. Aircraft
Electricity and Electronics. Eismin 5th Edition page 79.
Question Number. 50. When securing wire after it leaves an
LRU, cable bundle bends should be not less than?.
Option A. minimum
radius of five times the outside diameter of the cable, or cable bundle.
Option B. minimum
radius of three times the outside diameter of the cable, or cable bundle.
Option C. minimum
radius of eight times the outside diameter of the cable, or cable bundle.
Correct Answer is. minimum
radius of eight times the outside diameter of the cable, or cable bundle.
Explanation. CAAIP
9-3, 7.4 states 8 times the diameter (not 3 times, because it is not at a
terminal block).
Question Number. 51. When terminating an aluminium cable, what
preparations would be carried out before crimping?.
Option A. Degrease
stripped cable.
Option B. Just
terminate.
Option C. Apply
a mixture of 50% petroleum jelly and zinc oxide.
Correct Answer is. Apply
a mixture of 50% petroleum jelly and zinc oxide.
Explanation. CAAIP S
Leaflet 9-1 3.5.4.
Question Number. 52. An in-line splice should be positioned on
the.
Option A. terminal
of the loom.
Option B. outside
of the loom.
Option C. outer
surface of the loom for easy inspection.
Correct Answer is. outer
surface of the loom for easy inspection.
Explanation. NIL.
Question Number. 53. A conductor after being crimped. The
maximum amount of conductor which protrudes from the terminal end should be
Option A. 1/32 inch.
Option B. 1/8
inch.
Option C. 1/16
inch.
Correct Answer is. 1/32
inch.
Explanation. Leaflet
9-1 Fig 1 (0.8 mm = 1/32 in.).
Question Number. 54. Two or more operations should be
performed to strip wire with hand operated wire stripper if the total stripping
length exceeds.
Option A. 0.50
in.
Option B. 0.75
inch.
Option C. 0.25
in.
Correct Answer is. 0.75
inch.
Explanation. Leaflet
9-3 7.5.5 (d).
Question Number. 55. A cable loom should be protected by
conduit when fed through the.
Option A. main
equipment centre.
Option B. wheelwell
door.
Option C. cargo
compartment ceiling.
Correct Answer is. wheelwell
door.
Explanation. NIL.
Question Number. 56. The size of proper conduit for electrical
wires must be.
Option A. 75%
larger than the maximum diameter of wires.
Option B. 25%
larger than the maximum diameter of wires.
Option C. 100%
larger than the average diameter of wires.
Correct Answer is. 25%
larger than the maximum diameter of wires.
Explanation. AC43
11-249.
Question Number. 57. Blue metal extract tool would be used
with contacts sized.
Option A. 16.
Option B. 12.
Option C. 22.
Correct Answer is. 16.
Explanation. NIL.
Question Number. 58. A Silver coated conductor in an
unpresurised area is subject to moisture and has a damaged coating would be
likely to cause.
Option A. Wet
Arc Tracking.
Option B. Knuckling
Through.
Option C. Red
Plague.
Correct Answer is. Red
Plague.
Explanation. NIL.
08. Riveting.
Question Number. 1. When riveting, the distance from the
edge to the rivet (land) should not be less than.
Option A. 1D.
Option B. 2D.
Option C. 4D.
Correct Answer is. 2D.
Explanation. A&P
Technician Airframe Textbook 2-53.
Question Number. 2. The strength of a riveted joint
compared to that of the original metal is.
Option A. 75%.
Option B. 100%.
Option C. 125%.
Correct Answer is. 75%.
Explanation. NIL.
Question Number. 3. A repair has a double riveted joint.
The shear strength would be.
Option A. 125%.
Option B. 75%.
Option C. 100%.
Correct Answer is. 75%.
Explanation. NIL.
Question Number. 4. The standard minimum rivet row spacing
is.
Option A. 2 1/4
D.
Option B. 3 D.
Option C. 4 D.
Correct Answer is. 4
D.
Explanation. NIL.
Question Number. 5. What is the normal spacing between
rivets?.
Option A. 2 D.
Option B. 4 D.
Option C. 3 D.
Correct Answer is. 4
D.
Explanation. NIL.
Question Number. 6. In British rivets (solid) what is the
length grading unit?.
Option A. 1/16.
Option B. 1/10.
Option C. 1/32.
Correct Answer is. 1/16.
Explanation. CAIP S
BL/6-1, 4.2.
Question Number. 7. If the thickness of a single sheet of
material, about to be joined by riveting was 1/16 of an inch thick what would
be the approximate diameter of the rivets to be used?.
Option A. 1/16
inch.
Option B. 3/16
inch.
Option C. 1/8
inch.
Correct Answer is. 3/16
inch.
Explanation. CAIP S
BL/6-29 Para 3.
Question Number. 8. Regarding riveting, which of the
following is correct?.
Option A. Both
of the above are correct.
Option B. The
length of a countersunk rivet (flush head) is measured from the end of the
rivet to the top of the countersunk head.
Option C. The
length of a round head or flat head is measured from the end of the rivet to
underside of rivet head.
Correct Answer is. Both
of the above are correct.
Explanation. Jeppesen
A&P Airframe Textbook 2-36 and AC43 page 4.16.
Question Number. 9. When riveting, a certain clearance must
exist between the rivet and the hole in which it is fitted, to allow for shank
expansion. If the clearance is too large, what could be the result?.
Option A. Indentations
by rivet head on the material.
Option B. Separation
of the sheets may occur.
Option C. Sheet
may tend to buckle.
Correct Answer is. Separation
of the sheets may occur.
Explanation. CAIP S
BL/6-29 Para 9.3.1 -Fig 4, Too small a hole causes buckling, too large causes
separation.
Question Number. 10. To replace one 1/8 inch rivet.
Option A. three
1/16 inch rivets would be required.
Option B. two
1/16 inch rivets would be required.
Option C. four
1/16 inch rivets would be required.
Correct Answer is. four
1/16 inch rivets would be required.
Explanation. CAIP
BL/6-27 in the NOTE below para 5.3.
Question Number. 11. If treated rivets have not been used
within the prescribed time they can be re-treated. What is the maximum number
of times that they can be heat-treated?.
Option A. If no
more in Stores, as many times as required.
Option B. Twice
only.
Option C. Three
times.
Correct Answer is. Three
times.
Explanation. CAIP S
BL/6-27 Para 6-3.
Question Number. 12. Rivets kept at a temperature of between
–15°C and –20°C are usable for.
Option A. 150
days.
Option B. 150
minutes.
Option C. 150
hours.
Correct Answer is. 150
hours.
Explanation. CAIP S
BL/6-27 Para 6-2.
Question Number. 13. Avdel rivets are closed by.
Option A. a
broaching process.
Option B. a
tapered mandrel.
Option C. a
squeezing process.
Correct Answer is. a
broaching process.
Explanation. CAIP S
BL/6-28 Para 3.2 Fig 2.
Question Number. 14. What is the purpose of the Avdel pin
tester?.
Option A. To
test the tightness of the pin in the rivet.
Option B. To
test the tightness of the rivet in the hole.
Option C. To
test the shear strength of the pin.
Correct Answer is. To
test the tightness of the pin in the rivet.
Explanation. Inspection
after Installation of AVDEL rivets. The security of the mandrel must be
tested.Use the AVDEL PIN TESTER (Part Number 79/95-0700) set to 35 Lbs. No
movement of the mandrel is permitted. Ref. SRM A300-600.Chapter 51-40-21.
Question Number. 15. The stems of an Avdel rivet are.
Option A. removed
with the riveting tool.
Option B. nipped
off and milled flush with the head.
Option C. removed
with a taper punch.
Correct Answer is. nipped
off and milled flush with the head.
Explanation. NIL.
Question Number. 16. What is the pressure range for the Avdel
Riveter Type F?.
Option A. 40 to
60 lbs per sq. in.
Option B. 20 to
60 lbs per sq. in.
Option C. 60 to
80 lbs per sq. in.
Correct Answer is. 60
to 80 lbs per sq. in.
Explanation. NIL.
Question Number. 17. When countersinking rivet holes in a
material.
Option A. a
special countersinking bit with a pad to prevent drilling too deep should be
used.
Option B. a
plain countersinking bit should be used.
Option C. the
rivet head should stand 1/32 of an inch above the surface.
Correct Answer is. a
special countersinking bit with a pad to prevent drilling too deep should be
used.
Explanation. NIL.
Question Number. 18. The riveting defect in the figure shown
is.
Option A. too
much hammering.
Option B. the
dolly was not square.
Option C. the
snap was not square.
Correct Answer is. the
snap was not square.
Explanation. BL/6-29
Para 9-3-1 Fig 4.
Question Number. 19. Rivet allowance is.
Option A. the
distance the rivet is positioned from the edge of the repair plate.
Option B. the
amount of material required to form the rivet on installation.
Option C. the
distance between rivets in the same row.
Correct Answer is. the
amount of material required to form the rivet on installation.
Explanation. BL/6-29
8.1.
Question Number. 20. What is the approximate distance of the
sphere of influence of a rivet?.
Option A. 4 D.
Option B. 2 D.
Option C. 5 D.
Correct Answer is. 5
D.
Explanation. NIL.
Question Number. 21. Rivet clearance is.
Option A. the
distance between rivets in the same row.
Option B. the
amount that the rivet hole diameter exceeds the rivet diameter.
Option C. the distance
between rows of rivets.
Correct Answer is. the
amount that the rivet hole diameter exceeds the rivet diameter.
Explanation. BL/6-29
4.2.
Question Number. 22. The minimum rivet pitch is.
Option A. 2 1/2
* the rivet diameter.
Option B. 3 *
the rivet diameter.
Option C. 2 *
the rivet diameter.
Correct Answer is. 3
* the rivet diameter.
Explanation. A&P
Airframe Textbook CH12-37 Fig 12-57. (BL/6-29 3.1 - staggered double row only).
Question Number. 23. The riveting defect in the figure shown
is.
Option A. the
snap was not square.
Option B. the
hole was too small.
Option C. an
incorrect snap has been used.
Correct Answer is. the
hole was too small.
Explanation. CAIP S
BL/6-29 Para 9.3.1 Fig 4. AC43 21.
Question Number. 24. The ‘grip’ of a rivet is.
Option A. the
length of rivet left to form the head.
Option B. the
thickness of plates which can be fastened.
Option C. the
area of the plates held firmly together.
Correct Answer is. the
thickness of plates which can be fastened.
Explanation. NIL.
Question Number. 25. The strength of a riveted joint is
determined by.
Option A. shear
strength and pitch of rivet.
Option B. pitch
and tensile strength of rivet.
Option C. shear
strength of rivet and material it is made of.
Correct Answer is. shear
strength and pitch of rivet.
Explanation. BL/6-27
5.2 The shear strength of the rivet is determined by the material it is made
of. All rivets are under shear.
Question Number. 26. If the bearing strength of a metal is
greater than the shear strength of the rivet, what will occur?.
Option A. Rivet
will joggle.
Option B. Rivet
will show incorrectly installed.
Option C. Rivet
will pull through the metal.
Correct Answer is. Rivet
will joggle.
Explanation. NIL.
09. Pipes and Hoses.
Question Number. 1. When carrying out a pressure test on a
pipe it should be.
Option A. twice
the working pressure for two minutes.
Option B. 1.5
times the working pressure.
Option C. three
times the working pressure for five minutes.
Correct Answer is. 1.5
times the working pressure.
Explanation. Leaflet
5-5 8.5.
Question Number. 2. When checking a hose after installation
it should be checked for freedom of movement.
Option A. by flexing
through the normal operating range plus 15°.
Option B. by
flexing through the normal operating range only.
Option C. by
flexing +/-15° either side of the neutral position.
Correct Answer is. by
flexing through the normal operating range plus 15°.
Explanation. Leaflet
5-5 8.4.2.
Question Number. 3. If the outer cover of a flexible hose
is found to be cracked.
Option A. it is
unserviceable since it may have a restricted flow.
Option B. it may
still be serviceable.
Option C. it is
unserviceable since it may leak.
Correct Answer is. it
may still be serviceable.
Explanation. Leaflet
5-5 7.2.2.
Question Number. 4. A rigid hydraulic pipe requires
shaping. It should be carried out.
Option A. after
annealing.
Option B. after
age hardening.
Option C. as
supplied.
Correct Answer is. as
supplied.
Explanation. CAIP S
BL/6-15 3.3 and 4.4.4 (iii).
Question Number. 5. Fretting corrosion on a braided pipe
would mean it was.
Option A. unserviceable
and should be replaced.
Option B. not
necessarily unserviceable.
Option C. only
unserviceable if the corrosion penetrates the braids.
Correct Answer is. unserviceable
and should be replaced.
Explanation. NIL.
Question Number. 6. Pipe flaring is carried out.
Option A. as
supplied.
Option B. in the
annealed state.
Option C. after
normalizing.
Correct Answer is. as
supplied.
Explanation. BL/6-15.
Question Number. 7. To allow for shrinkage, vibration and
whip all straight hoses must be.
Option A. 5%
longer than the distance between the fittings.
Option B. 2%
longer than the distance between the fittings.
Option C. 3%
longer than the distance between the fittings.
Correct Answer is. 3%
longer than the distance between the fittings.
Explanation. CAAIP S
Leaflet 5-5 6.5.
Question Number. 8. A flexible hose that cannot be
internally inspected by eye or introscope can be ball tested by suspending from
one end at a time to check.
Option A. a ball
of 95% of bore of hose can be pushed through with a metal rod.
Option B. a ball
of 98% of bore of end fittings passes freely under own weight.
Option C. ball
of 90% of bore of end fittings passes freely under own weight.
Correct Answer is. ball
of 90% of bore of end fittings passes freely under own weight.
Explanation. CAAIP S
Leaflet 5-5 9.5.3 a.
Question Number. 9. Hoses are normally pressure tested to.
Option A. maximum
working pressure.
Option B. 2
times maximum working pressure.
Option C. 1½
times maximum working pressure.
Correct Answer is. 1½
times maximum working pressure.
Explanation. CAAIP S
Leaflet 5-5 8.5.
Question Number. 10. A fluid line marker with a skull &
crossbones is.
Option A. fluid
line carries toilet waste.
Option B. warning
symbol.
Option C. radioactive
symbol.
Correct Answer is. warning
symbol.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 10-13.
Question Number. 11. The international marking for a water
injection pipeline is a series of.
Option A. chevrons.
Option B. squares.
Option C. dots.
Correct Answer is. chevrons.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 10-13.
Question Number. 12. The international marking for a fire
protection pipe line is a series of.
Option A. circles.
Option B. squares.
Option C. diamonds.
Correct Answer is. diamonds.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 10-13.
Question Number. 13. To prevent corrosion where aluminium
alloy pipelines are supported by rubber cleats, the pipe should be treated over
the area of contact with.
Option A. french
chalk.
Option B. varnish.
Option C. petroleum
jelly.
Correct Answer is. varnish.
Explanation. NIL.
Question Number. 14. The international marking for an
instrument air pipe line is a.
Option A. series
of dots.
Option B. zig
zag line.
Option C. wavy
band.
Correct Answer is. zig
zag line.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 10-13, A&P Technician General
page 10-13 figure 10-28.
Question Number. 15. The maximum distance between end fittings
to which a straight hose assembly is to be connected is 50 inches. The minimum
hose length should be.
Option A. 51
inches.
Option B. 51½
inches.
Option C. 3
inches.
Correct Answer is. 51½
inches.
Explanation. CAAIP S
Leaflet 5-5 6.5.
Question Number. 16. The length of a hose assembly with
elbowed end fittings is taken from.
Option A. the
maximum length of the straight portion of hose.
Option B. the
centre of the bore at the nipple extremity.
Option C. the
extreme overall length.
Correct Answer is. the
centre of the bore at the nipple extremity.
Explanation. CAIP S
AL/ 3-13 Para 2-3.
Question Number. 17. The international marking for a breathing
oxygen pipe line is a series of.
Option A. dots.
Option B. diamonds.
Option C. rectangles.
Correct Answer is. rectangles.
Explanation. Jeppesen
A&P General Technician Textbook Page 10-13.
Question Number. 18. The resistance between a flexible hose
and a component should not exceed.
Option A. 1 ohm.
Option B. 0.5
ohm.
Option C. 0.05
ohm.
Correct Answer is. 0.05
ohm.
Explanation. Leaflet
5-5 9.5.5.
Question Number. 19. Bore tests of flexible hoses are carried
out using a suitable ball or bobbin of.
Option A. 90% of
the diameter of the end fittings.
Option B. 85% of
the diameter of the end fittings.
Option C. 25% of
the diameter of the end fittings.
Correct Answer is. 90%
of the diameter of the end fittings.
Explanation. Leaflet
5-5 9.5.3 (a) (ii).
Question Number. 20. The 'Lay Line' on a flexible hose is.
Option A. an
arrow painted on the hose to show the direction of fluid flow.
Option B. a
white line painted the full length of the hose to indicate any twist in the
hose.
Option C. a
white line painted the full length of the hose to indicate any stretch in the
hose.
Correct Answer is. a
white line painted the full length of the hose to indicate any twist in the
hose.
Explanation. AL/3-13
4.2 figure 4.
Question Number. 21. Aluminium alloy pipe used for hydraulics
systems is flared.
Option A. normalized.
Option B. as
supplied.
Option C. annealed.
Correct Answer is. as
supplied.
Explanation. BL/6-15
6.2.
Question Number. 22. Identify the parts required to make up a
flared-tube fitting?.
Option A. Sleeve
and nut.
Option B. Ferrule
and nut.
Option C. Body,
sleeve and nut.
Correct Answer is. Sleeve
and nut.
Explanation. BL/6-15
6.2.2. A&P Mechanic General Handbook Pg.103.
Question Number. 23. The flare angle on an AGS pipe is.
Option A. 90
degrees.
Option B. 45
degrees.
Option C. 32
degrees.
Correct Answer is. 32
degrees.
Explanation. BL/6-15
6.1.
Question Number. 24. Repair to aluminium pipe can be done
using burnishing.
Option A. if
damage is surface only.
Option B. if
damage is no more than 5%.
Option C. if
damage is no more than 10%.
Correct Answer is. if
damage is no more than 10%.
Explanation. AC43
Pg.9-18 Para.9.30 c.
Question Number. 25. Rigid pipes are designed with bends to.
Option A. allow
for expansion and contraction due to heat and absorb vibration.
Option B. absorb
vibration.
Option C. fit to
the aircraft structure.
Correct Answer is. allow
for expansion and contraction due to heat and absorb vibration.
Explanation. Answer
b is just too obvious.
Question Number. 26. You find a pipe with a flare end fitting
of 74°. What specification has it been manufactured to?.
Option A. A.G.S.
Option B. A.N.
Option C. S.A.E.
Correct Answer is. A.N.
Explanation. BL/6-15
6.1.
Question Number. 27. Bonding connections between flexible and
rigid pipes are achieved by.
Option A. ti-wrapping
the bonding lead to the pipes.
Option B. using
a corrugated strip.
Option C. tucking
the bonding leads between the flexible and rigid pipes.
Correct Answer is. using
a corrugated strip.
Explanation. CAAIP S
9-1, 3.6.1.
10. Springs.
Question Number. 1. Springs are manufactured from.
Option A. high
carbon alloy steel with high strength requirements.
Option B. low
carbon alloy steel with high strength requirements.
Option C. high
carbon alloy steel with low strength requirements.
Correct Answer is. high
carbon alloy steel with high strength requirements.
Explanation. Springs
are made from high carbon steel with high strength requirements.
Question Number. 2. A wear check on a cylinder head valve
spring should include.
Option A. length
under load.
Option B. diameter
and length.
Option C. length
off-load.
Correct Answer is. length
under load.
Explanation. EL/3-2
para 4.4 and Aircraft Reciprocating Engines, Jeppesen. Page 88.
Question Number. 3. Material used for springs is.
Option A. High
carbon or alloy steel with low working stresses.
Option B. Low
carbon steel or alloy steel with high working stresses.
Option C. Low
carbon steel or alloy steel with low working stresses.
Correct Answer is. High
carbon or alloy steel with low working stresses.
Explanation. Springs
are made from hardened (high carbon) or alloy steel, and work under low stress
to keep them within the elastic range.
11. Bearings.
Question Number. 1. Needle roller bearings.
Option A. are
susceptible to brinelling.
Option B. can
accept a small amount of misalignment.
Option C. are
designed to carry axial loads.
Correct Answer is. are
susceptible to brinelling.
Explanation. CAIP
BL/6-14 para 2.3.1 ii.
Question Number. 2. When rotating a ball bearing by hand, a
regular click indicates.
Option A. damage
to the balls.
Option B. intergranular
corrosion in the outer ring.
Option C. a
cracked ring.
Correct Answer is. a
cracked ring.
Explanation. NIL.
Question Number. 3. Brinelling of a wheel bearing could be
caused by.
Option A. rotation
of the outer race in the wheel housing.
Option B. heavy
landing.
Option C. overheating
of the brakes.
Correct Answer is. heavy
landing.
Explanation. NIL.
Question Number. 4. Brinelling of a bearing is.
Option A. bluing
of the bearing due to overheating.
Option B. shallow
smooth depressions caused by the rollers being forced against the cup, due to
overtorquing.
Option C. indentations
in the race surface caused by continual static vibration.
Correct Answer is. shallow
smooth depressions caused by the rollers being forced against the cup, due to
overtorquing.
Explanation. NIL.
Question Number. 5. A tapered roller bearing is designed to
take.
Option A. radial
loads only.
Option B. both
radial and axial loads.
Option C. axial
loads only.
Correct Answer is. both
radial and axial loads.
Explanation. NIL.
Question Number. 6. Small indentations in the race of a
ball bearing indicate.
Option A. overtorquing.
Option B. corrosion.
Option C. brinelling.
Correct Answer is. brinelling.
Explanation. Jeppesen
A&P Airframe Textbook 1-46.
Question Number. 7. When fitting a ball bearing to a shaft
it should be carefully positioned using.
Option A. a
steel drift with light blows.
Option B. a
copper or aluminium tube drift.
Option C. a soft
steel or brass tube drift.
Correct Answer is. a
soft steel or brass tube drift.
Explanation. CAIP
BL/6-14 5.4.
Question Number. 8. Graphite prevents seizure and conducts
heat. It is normally used in.
Option A. lithium
based greases.
Option B. sodium
based greases.
Option C. copper
based greases.
Correct Answer is. sodium
based greases.
Explanation. Graphite
is added to sodium based greases.
Question Number. 9. False Brinelling of a bearing is.
Option A. movement
of the outer ring relative to its housing.
Option B. indentations
on the race-way due to load transferred through the bearing when static.
Option C. a
scoring of the race-way surfaces due to ball or roller skidding.
Correct Answer is. indentations
on the race-way due to load transferred through the bearing when static.
Explanation. NIL.
Question Number. 10. On completion of assembly the bearing
housing.
Option A. should
be examined for end float.
Option B. packed
fully with grease.
Option C. lightly
packed with grease.
Correct Answer is. lightly
packed with grease.
Explanation. NIL.
Question Number. 11. When checking a ball bearing for
corrosion and foreign matter.
Option A. rotate
at operational speed and check for roughness.
Option B. make a
strip down inspection.
Option C. oscillate
and rotate slowly to listen for roughness.
Correct Answer is. oscillate
and rotate slowly to listen for roughness.
Explanation. NIL.
Question Number. 12. What type of load is a journal load?.
Option A. Radial.
Option B. Axial.
Option C. Centrifugal.
Correct Answer is. Radial.
Explanation. NIL.
Question Number. 13. Bearings to be cleaned for further
examination should be wiped free of all grease on outer surfaces with the aid
of dry compressed air for cages and rolling parts. The bearings should then be
soaked in.
Option A. M.E.K.
Option B. lead
free gasoline.
Option C. white
spirit.
Correct Answer is. white
spirit.
Explanation. CAIPa
BL/6-14 8.1.
Question Number. 14. After cleaning a bearing should be dried
with.
Option A. left
in free air to dry naturally.
Option B. clean,
warm, dry compressed air.
Option C. lint
free rags.
Correct Answer is. clean,
warm, dry compressed air.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 9-8.
Question Number. 15. Thrust bearings transmit.
Option A. thrust
loads, thus limiting axial movement.
Option B. radial
loads, thus limiting axial movement.
Option C. thrust
loads, thus limiting radial movement.
Correct Answer is. thrust
loads, thus limiting axial movement.
Explanation. BL/6-14
2.2.3 and 3.1.
Question Number. 16. Chipping of a ball bearing indicates.
Option A. brinelling.
Option B. chattering.
Option C. spalling.
Correct Answer is. spalling.
Explanation. NIL.
Question Number. 17. A Hardy Spicer coupling has what type of
bearings?.
Option A. Ball
Bearings.
Option B. Needle
bearings.
Option C. Plain
bearings.
Correct Answer is. Needle
bearings.
Explanation. BL/6-14
2.3.1 (ii).
Question Number. 18. Graphite greases are used for.
Option A. medium
temperature applications.
Option B. high
temperature applications.
Option C. low
temperature applications.
Correct Answer is. high
temperature applications.
Explanation. Graphite
greases are used in high temperature applications.
Question Number. 19. If during an engine overhaul, ball or
roller bearings are found to have magnetised but otherwise have no defects,
they.
Option A. are in
an acceptable service condition.
Option B. must
be degaussed before use.
Option C. cannot
be used again.
Correct Answer is. must
be degaussed before use.
Explanation. Leaflet
4-7 4.9.
Question Number. 20. Ball and roller bearings are made from a
combination of low carbon steel and a percentage of.
Option A. Chromium.
Option B. Nickel.
Option C. Nickel
chrome.
Correct Answer is. Nickel.
Explanation. Outer
rings are made from high carbon chromium alloy steel. Inner rings are made from
low carbon nickel alloy steel and deep case carborized.
Question Number. 21. On inspection a bearing is found to have
distortion, what action should be taken?.
Option A. Reject
bearing.
Option B. No
action required. Some distortion is normal.
Option C. Blend
out distortion and re-grease bearing.
Correct Answer is. Reject
bearing.
Explanation. NIL.
Question Number. 22. On inspection a bearing is found to show
signs of overheating, what action should be taken?.
Option A. Reject
bearing.
Option B. No
action required. Some overheating is normal.
Option C. clean
up bearing and repack with grease.
Correct Answer is. Reject
bearing.
Explanation. NIL.
Question Number. 23. When a bearing has 2 parts and the inner
ring and outer ring is installed.
Option A. neither
of the practices are allowed.
Option B. the
inner ring can be removed from its inner shaft for cleaning.
Option C. the
outer ring can be removed from its housing for inspection.
Correct Answer is. the
outer ring can be removed from its housing for inspection.
Explanation. NIL.
12. Transmissions.
Question Number. 1. A chain removed for routine inspection,
it.
Option A. does
not need proof loading.
Option B. must
be proof loaded to 50%.
Option C. must
be proof loaded to 150%.
Correct Answer is. does
not need proof loading.
Explanation. Leaflet
5-4 6.6.
Question Number. 2. An aircraft control chain is connected
using.
Option A. nuts
and bolts.
Option B. quick
release pins.
Option C. a
split link and spring clip.
Correct Answer is. nuts
and bolts.
Explanation. Leaflet
5-4 3.4.
Question Number. 3. If a control chain can be lifted clear
of a tooth, it should be.
Option A. rejected
as unserviceable.
Option B. removed
and an elongation check carried out.
Option C. cleaned,
re-tensioned and inspected after a period of time.
Correct Answer is. removed
and an elongation check carried out.
Explanation. Leaflet
5-4 5.3.
Question Number. 4. To check a chain for articulation.
Option A. it
should be run over the finger through 180° and checked for smoothness and
kinks.
Option B. move
each link individually and check for tightness.
Option C. lay on
a flat surface and check for kinks.
Correct Answer is. it
should be run over the finger through 180° and checked for smoothness and
kinks.
Explanation. Jeppesen
A&P Airframe Textbook 2-27.
Question Number. 5. How do you remove a tight link from a
chain which is to be used on an aircraft control system?.
Option A. Dismantle,
inspect, rectify and re-assemble the chain.
Option B. If the
chain has a tight link, the chain has to be removed from service.
Option C. You
may be able to remove the tight link by applying a light tap with a hammer.
Correct Answer is. You
may be able to remove the tight link by applying a light tap with a hammer.
Explanation. Leaflet
5-4 6.4.
Question Number. 6. The initial lubricant on a new chain.
Option A. must
be replaced with grade altitude grease.
Option B. should
be removed and replaced with the approved oil.
Option C. should
not be removed.
Correct Answer is. should
not be removed.
Explanation. Leaflet
5-4 4.4.5.
Question Number. 7. Control chains should be fitted in an
aircraft.
Option A. with the
minimum of slack in the chain.
Option B. so
that the chain can be removed easily.
Option C. with
as much slack as possible to allow for contraction.
Correct Answer is. with
the minimum of slack in the chain.
Explanation. NIL.
Question Number. 8. Backlash is a type of wear associated
with.
Option A. gears.
Option B. rivets.
Option C. bearings.
Correct Answer is. gears.
Explanation. NIL.
Question Number. 9. After a chain has been cleaned in
paraffin it should be.
Option A. hung
up to drip dry.
Option B. dried
in hot air.
Option C. washed
in soapy water then hung to drip dry.
Correct Answer is. dried
in hot air.
Explanation. AL/3-2
6.3.1 a.
Question Number. 10. What fraction of the minimum breaking
load should be the proof load for a chain?.
Option A. 0.1.
Option B. 1/3.
Option C. 0.1%.
Correct Answer is. 1/3.
Explanation. Leaflet
5-4 3.3. AL/3-2 Para 6-6.
Question Number. 11. If corrosion is found on a chain.
Option A. replace
the chain.
Option B. clean
off the corrosion and if acceptable re-fit the chain.
Option C. lubricate
the chain.
Correct Answer is. replace
the chain.
Explanation. Leaflet
5-4 5.4. AL/3-2 Para 5-4.
Question Number. 12. The three principle dimensions specified
for a chain is the diameter of the rollers and.
Option A. pitch
and chain length.
Option B. the
pitch and width between the inner plates.
Option C. the
pitch and width across the outside of the plates.
Correct Answer is. the
pitch and width between the inner plates.
Explanation. Leaflet
5-4 Para.3.1. AL/3-2 3.1.
Question Number. 13. The distance between the centres of the
rollers of a chain is called.
Option A. pitch.
Option B. crest.
Option C. length.
Correct Answer is. pitch.
Explanation. Leaflet
5-4 3.3. AL/3-2 3.1.
Question Number. 14. Which of the following formulas should be
used to calculate the percentage extension of an aircraft control chain? Note:
M = Measured length under load in inches X = Number of pitches measured P =
Pitch of chain in inches.
Option A. M + (X
* X) * 100 / P * M.
Option B. X-(M *
P) * 100 / M * P.
Option C. M-(X *
P) * 100 / X * P.
Correct Answer is. M-(X
* P) * 100 / X * P.
Explanation. AL/3-2
6.3.1 ©.
Question Number. 15. The maximum allowable extension of a
chain assembly over a nominal length is.
Option A. 3%.
Option B. 5%.
Option C. 2%.
Correct Answer is. 2%.
Explanation. Leaflet
5-4 6.3.2. AL/3-2 Para 6.3.2.
Question Number. 16. A feather key locates a gear on a shaft
and permits.
Option A. a
positive drive with the gear firmly locked.
Option B. a
positive and strong drive transmission.
Option C. a
positive drive and axial movement.
Correct Answer is. a
positive drive and axial movement.
Explanation. A
feather key allows axial movement.
Question Number. 17. A chain is removed by.
Option A. nuts
and bolts.
Option B. spring
clips.
Option C. removing
chain links on an endless chain.
Correct Answer is. nuts
and bolts.
Explanation. Leaflet
5-4 3.4 & 6.
Question Number. 18. The box unit in a Teleflex control run
which is not suitable for heavily loaded controls is called.
Option A. Double
entry.
Option B. Single
entry.
Option C. Straight
lead.
Correct Answer is. Straight
lead.
Explanation. Both
single and double entry boxes are wrapped lead. External website. http://saywell.co.uk/pages/morseCon.htm
Question Number. 19. How do you check a chain for elongation?.
Option A. Hang
chain up, check sight line and measure.
Option B. Adjust
the end fittings.
Option C. Lay
flat on a table, apply tensile load and measure.
Correct Answer is. Lay
flat on a table, apply tensile load and measure.
Explanation. Leaflet
5-4 6.3.2. AL/3-2 Para 6.3.2.
13. Control Cables.
Question Number. 1. Proof testing after cable installation
is.
Option A. sometimes
required.
Option B. not
required.
Option C. always
required.
Correct Answer is. not
required.
Explanation. NIL.
Question Number. 2. A control cable that has been
contaminated with acid should be.
Option A. cleaned.
Option B. rejected.
Option C. cleaned,
inspected, and reinspected after a period of time.
Correct Answer is. rejected.
Explanation. NIL.
Question Number. 3. A balance cable is installed in a
control system to.
Option A. allow
the aircraft to be flown 'hands off'.
Option B. correct
for wing heaviness.
Option C. enable
the cable to be tensioned.
Correct Answer is. enable
the cable to be tensioned.
Explanation. A&P
Technician Airframe Textbook 2-27.
Question Number. 4. How would you use a Pacific T5
tensiometer?.
Option A. Use
correct chart and correct riser.
Option B. Use a
standard riser and use the chart to correct for different sized cables.
Option C. Use a
load meter to apply the correct load.
Correct Answer is. Use
correct chart and correct riser.
Explanation. NIL.
Question Number. 5. What is the purpose of an aileron
balance cable?.
Option A. Allows
for hands off flying.
Option B. Equalizes
control cable tension.
Option C. Relieves
pilot loads.
Correct Answer is. Equalizes
control cable tension.
Explanation.
Jeppesen A&P Airframe Textbook 1-27.
Question Number. 6. How would you inspect a cable for
fraying?.
Option A. Run
your fingers the full length of the cable.
Option B. Operate
the controls and feel for stiffness.
Option C. Run a
rag the full length of the cable.
Correct Answer is. Run
a rag the full length of the cable.
Explanation. Jeppesen
A&P Airframe Textbook 1-43.
Question Number. 7. When manufacturing aircraft control
cables, the cable can be cut by.
Option A. using
a hacksaw with the cable under tension.
Option B. using
an oxy-acetylene torch.
Option C. using
a chisel on a flat metal surface.
Correct Answer is. using
a chisel on a flat metal surface.
Explanation. CAAIP S
Leaflet 2-12 3.6.
Question Number. 8. The check for a cable pulling out of a
swaged fitting is by.
Option A. seeing
that the cable is still past the safety holes in the swage.
Option B. looking
for a shiny surface on the cable near the fitting.
Option C. seeing
that there are no broken wires near the fitting.
Correct Answer is. looking
for a shiny surface on the cable near the fitting.
Explanation. NIL.
Question Number. 9. A 'Reel' used to hold an aircraft cable
in storage should have a minimum diameter of.
Option A. at
least 25 times that of the cable diameter.
Option B. at
least 50 times that of the cable.
Option C. at
least 40 times that of the cable diameter.
Correct Answer is. at
least 40 times that of the cable diameter.
Explanation. Leaflet
2-12 page 2 para 3.1.
Question Number. 10. Large control cables (45 to 120 cwt) may
have tension loads that can break the locking wire or lease lock nuts. How is
this overcome?.
Option A. The
cable is kept slightly slack.
Option B. Duplicating
the number of cables to cut down on individual tensile loads.
Option C. A tube
is fitted over the turnbuckle assembly and drilled to take up to 3 bolts, to
prevent independent rotation of any part.
Correct Answer is. A
tube is fitted over the turnbuckle assembly and drilled to take up to 3 bolts,
to prevent independent rotation of any part.
Explanation. CAIP S
AL/3-7 Para. 9.5.8.
Question Number. 11. To correctly tension cables it can help.
Option A. to use
a cable with turnbuckles at least every eight feet.
Option B. to
take up initial slack by additional pulleys.
Option C. to
have control surface locks in to support weight and adjust turnbuckles equally.
Correct Answer is. to
have control surface locks in to support weight and adjust turnbuckles equally.
Explanation. NIL.
Question Number. 12. A cable is replaced.
Option A. when a
shiny portion is found.
Option B. when
each strand is worn to limits.
Option C. if a
chemical spillage is suspected.
Correct Answer is. if
a chemical spillage is suspected.
Explanation. NIL.
Question Number. 13. What is the proof loading for cables after
swaging?.
Option A. 1/3
minimum breaking strain.
Option B. 2/3
minimum breaking strain.
Option C. 50%
minimum breaking strain.
Correct Answer is. 50%
minimum breaking strain.
Explanation. CAAIP S
Leaflet 2-12 8.1.
Question Number. 14. The best way to check control cables for
broken wires is to.
Option A. run a
rag along the cable in both directions.
Option B. examine
them visually.
Option C. increase
the tension and check with a magnifying glass.
Correct Answer is. run
a rag along the cable in both directions.
Explanation. AC43
7-149 (d).
Question Number. 15. If the turnbuckles in a control system
are tightened excessively the result will be.
Option A. the
cable will break.
Option B. the
cables will vibrate excessively and cause failure of controls.
Option C. the
aircraft will be heavy on controls.
Correct Answer is. the
aircraft will be heavy on controls.
Explanation. AC43
7-149 (j).
Question Number. 16. A control cable is proof loaded to ensure
that.
Option A. the
end fittings on the cable are secure.
Option B. it
will not stretch after fitting in an aircraft.
Option C. it
will not break after fitting in an aircraft.
Correct Answer is. the
end fittings on the cable are secure.
Explanation. Leaflet
2-12 8.
Question Number. 17. British turnbuckles are checked for
safety by.
Option A. looking
through the hole and checking for threads showing.
Option B. attempting
to pass a hardened pin probe through the inspection hole.
Option C. attempting
to push locking wire through the hole.
Correct Answer is. attempting
to pass a hardened pin probe through the inspection hole.
Explanation. AL/3-7
9.5.7.
Question Number. 18. A suspected chemical spillage on a cable,
you should.
Option A. clean,
inspect and refit immediately.
Option B. replace
the cable.
Option C. clean
the cable and inspect 24 hours later.
Correct Answer is. replace
the cable.
Explanation. NIL.
Question Number. 19. HTS aircraft control cables are protected
from corrosion by.
Option A. Galvanising.
Option B. cadmium
coating.
Option C. zinc
plating.
Correct Answer is. Galvanising.
Explanation. Leaflet
2-12 2.3.
Question Number. 20. What is the purpose of the hole in the
swaged end fitting on a swaged cable?.
Option A. To
ensure the cable end passes the inspection hole on drilled through type
fittings but leaves the locking wire hole clear.
Option B. To
allow trapped air to escape.
Option C. To
allow a split pin to be inserted.
Correct Answer is. To
ensure the cable end passes the inspection hole on drilled through type
fittings but leaves the locking wire hole clear.
Explanation. Leaflet
2-12 5.2 (d). CAIP S BL/6-24 5.2 (d).
Question Number. 21. The inspection hole in a turnbuckle is.
Option A. to
allow the locking wire to pass through for the purpose of locking.
Option B. to
ensure that the locknuts are adequately tightened.
Option C. to
ensure that the turnbuckle is in safety.
Correct Answer is. to
ensure that the turnbuckle is in safety.
Explanation. Leaflet
2-12 9.5.7. CAIP S AL/3-7 9.5.7.
Question Number. 22. Swaging of a cable end fitting is checked
by.
Option A. measuring
the length of the barrel before and after swaging.
Option B. using
a go / no-go gauge on the barrel.
Option C. looking
for cracks on the swage indicating poor swaging.
Correct Answer is. using
a go / no-go gauge on the barrel.
Explanation. Leaflet
2-12 5.3 (b) Jeppesen A&P Airframe Technician Textbook 1-43.
Question Number. 23. A flight control cable is replaced if.
Option A. single
wires are blended together.
Option B. a wire
is 20% worn.
Option C. the
protective fluid coating is missing.
Correct Answer is. single
wires are blended together.
Explanation. AC43
7-149 g.
Question Number. 24. In aircraft control cables, when a lock
is fitted to the control surface.
Option A. it
will prevent the control surface movement but not the control column movement.
Option B. it
will prevent the control surface and the control column movement.
Option C. it
will not prevent the control surface movement but will lock the control column.
Correct Answer is. it
will prevent the control surface and the control column movement.
Explanation. NIL.
Question Number. 25. When checking cable tensions you are
looking for.
Option A. free
movement only.
Option B. full
and free movement.
Option C. artificial
feel.
Correct Answer is. full
and free movement.
Explanation. NIL.
Question Number. 26. A cable should be replaced when
individual wires are worn greater than.
Option A. 40%.
Option B. 60%.
Option C. 20%.
Correct Answer is. 40%.
Explanation. AC43
Para 7-149 g.
14.1. Material Handling - Sheet metal.
Question Number. 1. The purpose of a joggle is.
Option A. to act
as a tear stopper.
Option B. to
make the holes for a rivet line up.
Option C. to
produce a flush fit at a metal joint.
Correct Answer is. to
produce a flush fit at a metal joint.
Explanation. A&P
Technician Airframe Textbook 2-8.
Question Number. 2. Caustic soda applied to a metal turns
black. This would indicate the metal is.
Option A. magnesium
alloy.
Option B. duralumin.
Option C. aluminium.
Correct Answer is. duralumin.
Explanation. NIL.
Question Number. 3. Removal of a scratch from a sheet of
metal requires.
Option A. polishing.
Option B. blending.
Option C. burnishing.
Correct Answer is. burnishing.
Explanation. A&P
Mechanics Airframe Textbook Page 130.
Question Number. 4. When dimpling a sheet of metal you
would require.
Option A. an
oversized rivet and special reaction block.
Option B. a male
and female die.
Option C. a male
die only.
Correct Answer is. a
male and female die.
Explanation. A&P
Technician Airframe Textbook 2-59.
Question Number. 5. The skin on an aircraft is normally
manufactured from.
Option A. 2024
aluminium alloy.
Option B. 7075
aluminium alloy.
Option C. 2117
aluminium alloy.
Correct Answer is. 2024
aluminium alloy.
Explanation. A&P
Technician Airframe Textbook 2-7.
Question Number. 6. The mold point is.
Option A. the
mid point in the thickness of a sheet of metal to which the radius dimension is
calculated.
Option B. the
centre of curvature of a radiused corner in a metal fabricated component.
Option C. an
imaginary point from which real base measurements are provided.
Correct Answer is. an
imaginary point from which real base measurements are provided.
Explanation. A&P
Technician Airframe Textbook 2-71.
Question Number. 7. Relief holes are.
Option A. holes
drilled in a battery container to provide drainage.
Option B. holes
drilled in the corner of a metal box to prevent cracking.
Option C. holes
drilled to stop a crack.
Correct Answer is. holes
drilled in the corner of a metal box to prevent cracking.
Explanation. A&P
Technician Airframe Textbook 2-77.
Question Number. 8. The 'setback' is.
Option A. the
distance from the edge of the metal to the bend tangent line.
Option B. the
distance from the mold point to the bend tangent line.
Option C. the
distance from the bend tangent line to the setback line.
Correct Answer is. the
distance from the mold point to the bend tangent line.
Explanation. A&P
Technician Airframe Textbook 2-71.
Question Number. 9. Faying surfaces are.
Option A. surfaces
that are in contact with each other.
Option B. surfaces
that are stressed.
Option C. surfaces
that have been treated with anti-corrosion compound.
Correct Answer is. surfaces
that are in contact with each other.
Explanation. NIL.
Question Number. 10. In sheet metal bending, how would you
measure the bend radius to calculate the bend allowance?.
Option A. Measure
to the inside of the bend radius.
Option B. Measure
to the outside of the bend radius.
Option C. Measure
to the inside of the bend radius plus half the metal thickness.
Correct Answer is. Measure
to the inside of the bend radius.
Explanation. Jeppesen
A & P Tecnician Airframe Textbook pg 2-70.
Question Number. 11. When dimpling sheet with a squeeze
dimpling tool.
Option A. the
jaws are not adjustable.
Option B. adjust
the jaws to accommodate different material gauges.
Option C. use a
lubricant.
Correct Answer is. adjust
the jaws to accommodate different material gauges.
Explanation. Jeppesen
A&P Airframe Textbook 2-59.
Question Number. 12. Bend radius on sheet metal is.
Option A. inside
radius + ½ thickness.
Option B. inside
radius.
Option C. outside
radius.
Correct Answer is. inside
radius.
Explanation. Jeppesen
A&P Airframe Textbook 2-70.
Question Number. 13. Aircraft skin is joggled to.
Option A. Provide
smooth airflow at faying surfaces.
Option B. Make a
frame lighter but stronger.
Option C. Conform
with the 'Area Rule'.
Correct Answer is. Provide
smooth airflow at faying surfaces.
Explanation. Jeppesen
A & P Tecnician Airframe Textbook pg 2-82.
Question Number. 14. DZinc Chromate applied between faying
surfaces will.
Option A. improve
adhesion thus relieving the amount of riveting necessary.
Option B. improve
bonding between them.
Option C. inhibit
dissimilar metal (electrolytic) corrosion.
Correct Answer is. inhibit
dissimilar metal (electrolytic) corrosion.
Explanation. NIL.
Question Number. 15. If a non-ferrous metal being examined by
chemical test turns black when caustic soda is applied to the surface, the
metal is.
Option A. duralumin.
Option B. alclad.
Option C. aluminium.
Correct Answer is. duralumin.
Explanation. NIL.
Question Number. 16. To aid marking out on Fe metals use.
Option A. graphite
grease.
Option B. copper
sulphate solution.
Option C. engineer's
blue.
Correct Answer is. copper
sulphate solution.
Explanation. Fe
means Ferrous. Copper sulphate solution should be used.
Question Number. 17. The sight line on a sheet metal flat
layout to be bent in a cornice or box brake is measured and marked.
Option A. one-half
radius from either bend tangent line.
Option B. one
radius from the bend tangent line that is placed under the brake.
Option C. one
radius from either bend tangent line.
Correct Answer is. one
radius from the bend tangent line that is placed under the brake.
Explanation. A&P
Airframe Textbook 5-60 Pg 232 Fig 5-118.
Question Number. 18. If copper sulphate is used on magnesium
alloy it will.
Option A. effervesce
to a copper colour.
Option B. have
no effect.
Option C. effervesce
to a black colour.
Correct Answer is. effervesce
to a black colour.
Explanation. NIL.
Question Number. 19. If it is necessary to compute a bend
allowance problem and bend allowance tables are not available, the neutral axis
of the bend can be.
Option A. found
by adding approximately one-half of the stock thickness to the bend radius.
Option B. found
by subtracting the stock thickness from the bend radius.
Option C. represented
by the actual length of the required material for the bend.
Correct Answer is. found
by adding approximately one-half of the stock thickness to the bend radius.
Explanation. Jeppesen
A & P Technician Airframe pg 2-73 fig 2-131.
Question Number. 20. The formula for setback for a 90° bend
is.
Option A. (½R +
T).
Option B. (R +
T).
Option C. (R +
½T).
Correct Answer is. (R
+ T).
Explanation. A&P
Airframe Textbook 5-55 Pg 227 Fig 5-112.
Question Number. 21. Caustic soda placed on the edge of alclad
will turn.
Option A. white
– black – white.
Option B. all
white.
Option C. black
– white – black.
Correct Answer is. white
– black – white.
Explanation. NIL.
Question Number. 22. In marking a light alloy.
Option A. the
scriber must be held at an angle to give a smooth line where bending is
required.
Option B. caustic
soda is used.
Option C. a
pencil is used to mark the material and all marks removed after bending.
Correct Answer is. a
pencil is used to mark the material and all marks removed after bending.
Explanation. BL/6-29
4.1A&P General Textbook 9-33 Pg 32.
Question Number. 23. When assembling metals of different
potential, corrosion may be inhibited by application of.
Option A. zinc
or chromic acid & assemble while wet.
Option B. zinc
or barium chromate & assemble while wet.
Option C. nothing
- assemble bare.
Correct Answer is. zinc
or barium chromate & assemble while wet.
Explanation. BL/4-2
4.4.6.
Question Number. 24. Steel wire brushes or steel wool should.
Option A. be
used to clean magnesium alloys.
Option B. be
used to clean aluminium sheet.
Option C. never
be used on light alloys.
Correct Answer is. never
be used on light alloys.
Explanation. NIL.
Question Number. 25. When a piece of metal is bent, the
surface of the metal on the outside of the bend is.
Option A. in
compression.
Option B. neither
in tension or in compression.
Option C. in
tension.
Correct Answer is. in
tension.
Explanation. NIL.
Question Number. 26. The sight line of a bend is.
Option A. at the
tangent line.
Option B. half a
radius from the tangent line.
Option C. one
radius from the tangent line.
Correct Answer is. one
radius from the tangent line.
Explanation. NIL.
Question Number. 27. The sharpest bend that can be placed in a
piece of metal without critically weakening the part is called the.
Option A. maximum
radius of bend.
Option B. minimum
radius of bend.
Option C. bend
allowance.
Correct Answer is. minimum
radius of bend.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-70.
Question Number. 28. Scribers are used to.
Option A. produce
an accurate finish.
Option B. make
centre pop marks for drilling.
Option C. mark
guide lines on material.
Correct Answer is. mark
guide lines on material.
Explanation. NIL.
Question Number. 29. A hole drilled at the intersection of two
bends in a fabricated sheet metal component is called.
Option A. a
drain hole.
Option B. a
crack stopper.
Option C. a
relief hole.
Correct Answer is. a
relief hole.
Explanation. BL/6-14
2.2.3 and 3.1.
Question Number. 30. Dissimilar metal diffusion bonding gives.
Option A. high
strength and ductility.
Option B. high
strength and stiffness.
Option C. high
strength and brittleness.
Correct Answer is. high
strength and stiffness.
Explanation. NIL.
Question Number. 31. Marking out on stainless steel can be
clarified by application of.
Option A. ammonia.
Option B. copper
sulphate.
Option C. sal
ammoniac.
Correct Answer is. copper
sulphate.
Explanation. Copper
sulphate is used to aid marking out of steel.
Question Number. 32. When drawing lines on aluminium alloy
sheet prior to bending.
Option A. a thin
coat of zinc chromate primer should be used, ready for pencil lines.
Option B. a
scriber should be used.
Option C. a wax
pencil should be used.
Correct Answer is. a
thin coat of zinc chromate primer should be used, ready for pencil lines.
Explanation. CAIP
BL/6-29 4.1.
Question Number. 33. After solution treatment of aluminium
alloy, the effect of immediate refrigeration at a temperature with the range
-15°C to -20°C is.
Option A. to
suspend natural ageing for a limited period.
Option B. to
permanently soften the metal to retard the onset of fatigue.
Option C. to
increase the rate of artificial ageing.
Correct Answer is. to
suspend natural ageing for a limited period.
Explanation. BL/9-1
9. BL/6-27 6.2.
Question Number. 34. Diffusion bonding and superplastic
forming provides.
Option A. high strength
and high ductility.
Option B. high
strength and high stiffness.
Option C. high
stiffness and high ductility.
Correct Answer is. high
stiffness and high ductility.
Explanation. NIL.
14.2. Material Handling - Composite and non-metallic.
Question Number. 1. In a composite repair lay-up, how much
should each layer extend beyond the layer below it?.
Option A. 2 - 3
inches.
Option B. 1 - 2
inches.
Option C. 3 - 4
inches.
Correct Answer is. 1
- 2 inches.
Explanation. AC43
Page 3-5.
Question Number. 2. To enable a composite panel to
dissipate static charge it would be sprayed with.
Option A. polyurethane
paint.
Option B. ferrous
paint.
Option C. aluminium
paint.
Correct Answer is. aluminium
paint.
Explanation. NIL.
Question Number. 3. A mechanic has completed a bonded
honeycomb repair using the potted compound repair technique. What
non-destructive testing method is used to determine the soundness of the repair
after the repair has cured?.
Option A. Eddy
current test.
Option B. Metallic
ring test.
Option C. Ultrasonic
test.
Correct Answer is. Metallic
ring test.
Explanation. NIL.
Question Number. 4. A non-destructive testing technique
which is suitable for inspecting for delamination in Redux bonded structure of
light aluminium alloys is.
Option A. ultrasonic.
Option B. eddy-current.
Option C. magnetic
flow.
Correct Answer is. ultrasonic.
Explanation. NIL.
Question Number. 5. Why is an extra layer of fibreglass
added to a composite repair?.
Option A. To
provide additional flexibility.
Option B. For
sacrificial sanding.
Option C. To
increase the strength of the repair.
Correct Answer is. To
increase the strength of the repair.
Explanation. AC43
3-3(3) page 3-5.
Question Number. 6. How do you reduce or remove electrostatic
charges which may build up on fibreglass surfaces?.
Option A. No
special treatment is necessary because fibre glass is an insulator.
Option B. The
surface is treated with a special conductive paint.
Option C. The
surface is impregnated with copper strips.
Correct Answer is. The
surface is treated with a special conductive paint.
Explanation. Leaflet
9-1 3.4.4.
Question Number. 7. Prior to aluminium alloy bonding we
use.
Option A. alkaline
etch.
Option B. acid
etch.
Option C. solvent
wipe.
Correct Answer is. acid
etch.
Explanation. Phosphoric
acid and chromic acid wash.
Question Number. 8. Glass reinforced panels are bonded by.
Option A. special
conductive paint.
Option B. wire
mesh.
Option C. bonding
strips to conductors.
Correct Answer is. special
conductive paint.
Explanation. Leaflet
9-1 para.3.4.4.
Question Number. 9. What solvents could you use to clean
tools used for fibreglass repairs?.
Option A. Trichloroethylene
or acetone.
Option B. Lead
free petrol/kerosene.
Option C. acetone
or MEK.
Correct Answer is. acetone
or MEK.
Explanation. CAIP S
AL/7-6 6.6.
Question Number. 10. Chopped strand mat is a good general
purpose mat because.
Option A. it has
short fibres.
Option B. it
gives equal properties in all directions.
Option C. it is
a stiffer than woven cloth.
Correct Answer is. it
gives equal properties in all directions.
Explanation. NIL.
15a. Welding, Brazing, Soldering and Bonding.
Question Number. 1. Before soldering stainless steel it
must be.
Option A. pickled.
Option B. cleaned
with emery cloth.
Option C. sand
papered.
Correct Answer is. pickled.
Explanation. BL/6-1
5.3.
Question Number. 2. Insufficient heat used in soldering
will cause.
Option A. the
joint to oxidize.
Option B. a high
resistance joint potential.
Option C. contamination
of the joint.
Correct Answer is. a
high resistance joint potential.
Explanation. NIL.
Question Number. 3. A dry joint when soldering is caused
by.
Option A. too
large an iron.
Option B. too
much flux.
Option C. too
little heat.
Correct Answer is. too
little heat.
Explanation. NIL.
Question Number. 4. The oxyacetylene flame for silver
soldering should be.
Option A. oxidizing.
Option B. carbonising.
Option C. neutral.
Correct Answer is. neutral.
Explanation. BL/6-2
12.2.4 (Silver soldering is also known as low temperature brazing).
Question Number. 5. A flux is used in soldering to.
Option A. to
dissolve oxides.
Option B. etch
the metals surface for more adhesion.
Option C. to
prevent solder spikes.
Correct Answer is. to
dissolve oxides.
Explanation. NIL.BL/6-1
4.2.
Question Number. 6. Plumbers solder is grade.
Option A. C.
Option B. D.
Option C. B.
Correct Answer is. D.
Explanation. NIL.BL/6-1
4.1 table 2.
Question Number. 7. Why is it necessary to use flux in all
silver soldering operations?.
Option A. To
increase heat conductivity.
Option B. To
prevent overheating of the base metal.
Option C. To
chemically clean the base metal of oxide film.
Correct Answer is. To
chemically clean the base metal of oxide film.
Explanation. BL/ 6-2
Para 5-2.
Question Number. 8. When making a small soldered electrical
connection, using flux-cored solder.
Option A. the
connection should be heated first and then solder applied.
Option B. the
soldering iron and solder should be applied simultaneously to the connection.
Option C. the
soldering iron should be loaded with solder and then applied to the connection.
Correct Answer is. the
soldering iron and solder should be applied simultaneously to the connection.
Explanation. NIL.
Question Number. 9. The type of flux to be used when soft
soldering on aircraft is.
Option A. active.
Option B. non-active.
Option C. either
active or non-active.
Correct Answer is. non-active.
Explanation. BL/6-1
4.2.8.
Question Number. 10. The operational temperature of soldering
irons is.
Option A. fjust
above the melting point of solder.
Option B. below
the melting point of the base metal.
Option C. 60°C
above the melting point of solder.
Correct Answer is. 60°C
above the melting point of solder.
Explanation. NIL.
Question Number. 11. What elements is solder made from?.
Option A. Tin,
lead and copper.
Option B. Tin
and lead only.
Option C. Tin,
lead and silver.
Correct Answer is. Tin
and lead only.
Explanation. BL/6-1.
Question Number. 12. General purpose solders are graded by.
Option A. a
colour coding.
Option B. a
letter coding.
Option C. a
numerical coding.
Correct Answer is. a
letter coding.
Explanation. BL/6-1
table 2.
Question Number. 13. What solder should be used to solder
aluminium?.
Option A. D.T.D.
685 lead-silver-tin solder.
Option B. 90%
tin and 10% zinc.
Option C. wire
flux cored solder.
Correct Answer is. wire
flux cored solder.
Explanation. CAIP S
BL/6-1, 14.
Question Number. 14. Solder can be used to join.
Option A. some
dissimilar metals.
Option B. only
copper based metals.
Option C. similar
metals only.
Correct Answer is. some
dissimilar metals.
Explanation. NIL.
Question Number. 15. A flux is used in soldering to.
Option A. dissolve
oxides.
Option B. prevent
solder spikes.
Option C. etch
the metal surface for more adhesion.
Correct Answer is. dissolve
oxides.
Explanation. NIL.
Question Number. 16. On completion of soldering a
non-activated flux.
Option A. must
be cleaned off with an acid solution.
Option B. need
not be cleaned off.
Option C. must
be cleaned off with a selected solvent.
Correct Answer is. must
be cleaned off with a selected solvent.
Explanation. CAIP
BL/6-1 para 4.2.3.
Question Number. 17. A dry joint in soldering is most likely
to be caused by.
Option A. flux
not used.
Option B. components
not hot enough.
Option C. wrong
solder used.
Correct Answer is. components
not hot enough.
Explanation. All are
possibly correct, but the iron not being hot enough is sure to produce a dry
joint.
Question Number. 18. What action is taken when soldering flux
residue may have lodged in deep crevices of an assembly?.
Option A. It
must be immersed in a weak solution of hydrochloric acid and rinsed thoroughly
in running water.
Option B. It
must be immersed in a weak solution of phosphoric acid and rinsed in water.
Option C. It
must be thoroughly rinsed with a weak solution of sulphuric acid and washed in
cold water.
Correct Answer is. It
must be immersed in a weak solution of hydrochloric acid and rinsed thoroughly
in running water.
Explanation. BL/6-1
8.6.
Question Number. 19. A phosphate based flux paste is for
soldering.
Option A. aluminium.
Option B. brass.
Option C. stainless
steel.
Correct Answer is. stainless
steel.
Explanation. BL/6-1
4.2.5.
Question Number. 20. The soldering method where molten solder
is pumped from the bottom of a bath through a slot so that a stationary wave of
solder appears on the surface is known as the.
Option A. rotary
bath method.
Option B. stationary
wave method.
Option C. standing
wave bath method.
Correct Answer is. standing
wave bath method.
Explanation. CAIP S
BL/6-1, 9.2.
Question Number. 21. Solders are available in two forms:.
Option A. stick
solder with a rosin core and solder in a wire form having a rosin core.
Option B. Solder
in a wire form needing a separate flux and stick solder needing no flux at all.
Option C. stick
solder needing a separate flux and solder in wire form having a rosin core.
Correct Answer is. stick
solder needing a separate flux and solder in wire form having a rosin core.
Explanation. BL/6-1
4.1.
Question Number. 22. A resurfaced soldering iron cannot be
used effectively until after the working face has been.
Option A. fluxed.
Option B. polished.
Option C. tinned.
Correct Answer is. tinned.
Explanation. CAIP S
BL/6-1, 6.1.1.
Question Number. 23. High temperature solder is used where the
operating temperature is high. It is an alloy of.
Option A. lead /
copper / antimony.
Option B. tin /
zinc / antimony / silver.
Option C. tin /
lead / antimony / silver.
Correct Answer is. tin
/ lead / antimony / silver.
Explanation. CAIP S
BL/6-1, 4.1.2.
Question Number. 24. Soft solder is suited for joints, which
are.
Option A. subjected
to fatigue.
Option B. subjected
to strong forces.
Option C. subjected
to small forces.
Correct Answer is. subjected
to small forces.
Explanation. AC43
page 4061 para 4. BL/6-1.
Question Number. 25. Silver solder melts within the range.
Option A. 400°C
- 550°C.
Option B. 200°C
- 400°C.
Option C. 600°C
- 850°C.
Correct Answer is. 600°C
- 850°C.
Explanation. BL/6-2,
Para 1.1.
Question Number. 26. The term 'dry joint' is usually applied
to.
Option A. a
metal being lightly heated.
Option B. a
defect associated with a soldered joint.
Option C. a
water tight joint.
Correct Answer is. a
defect associated with a soldered joint.
Explanation. NIL.
Question Number. 27. Silver soldering is suited for.
Option A. electronic
component soldering.
Option B. high
temperature applications.
Option C. general
soldering work.
Correct Answer is. high
temperature applications.
Explanation. BL/6-1
Para.4.1.2.
Question Number. 28. Silver solder is made from.
Option A. tin,
copper and zinc.
Option B. copper,
tin and silver.
Option C. copper,
zinc and silver.
Correct Answer is. copper,
zinc and silver.
Explanation. Workshop
Technology WAJ Chapman Page 105.
Question Number. 29. The materials most commonly soldered in
soft soldering are.
Option A. brass
and mild steel.
Option B. stainless
steel and titanium.
Option C. aluminium
and magnesium.
Correct Answer is. brass
and mild steel.
Explanation. NIL.
15b. Welding, Brazing, Soldering and Bonding.
Question Number. 1. What purpose does flux serve in welding
aluminium?.
Option A. Ensures
proper distribution of the filler rod.
Option B. Removes
dirt, grease, and oil.
Option C. Minimises
or prevents oxidation.
Correct Answer is. Minimises
or prevents oxidation.
Explanation. NIL.
Question Number. 2. The shielding gases generally used in
the Tungsten Inert Gas (TIG) welding of aluminium consist of.
Option A. nitrogen
or hydrogen, or a mixture of nitrogen and hydrogen.
Option B. a
mixture of nitrogen and carbon dioxide.
Option C. helium
or argon, or a mixture of helium and argon.
Correct Answer is. helium
or argon, or a mixture of helium and argon.
Explanation. NIL.
Question Number. 3. Which items listed below is the most
important consideration when selecting a welding rod?.
Option A. Thickness
of the metal to be welded only.
Option B. Type
of torch.
Option C. Type
and thickness of the metal to be welded.
Correct Answer is. Type
and thickness of the metal to be welded.
Explanation. BL/6-4
2 & 4.1.
Question Number. 4. What is a good weld?.
Option A. Build
up by 1/8 inch in the middle of the weld.
Option B. An
oxide coating on the base metals.
Option C. Sides
sloping to the base metals.
Correct Answer is. Sides
sloping to the base metals.
Explanation. Jeppesen
A & P airframe technician textbook p 4-9.
Question Number. 5. Brazing material is made from.
Option A. copper
zinc and silver.
Option B. copper
and tin and lead.
Option C. copper,
silver and tin.
Correct Answer is. copper
zinc and silver.
Explanation. Workshop
Technology WAJ Chapman Page 103.
Question Number. 6. Filing or grinding a weld bead.
Option A. may be
necessary to avoid adding excess weight or to achieve uniform material
thickness.
Option B. may be
performed to achieve a smoother surface.
Option C. reduces
the strength of the joint.
Correct Answer is. reduces
the strength of the joint.
Explanation. CAAIP S
Leaflet 2-10 3.
Question Number. 7. The primary reason for using flux when
welding aluminium is to.
Option A. prevent
oxides from forming ahead of the weld.
Option B. prevent
molten metal from flowing too widely.
Option C. promote
better fusion of the base metal at a lower temperature.
Correct Answer is. prevent
oxides from forming ahead of the weld.
Explanation. BL/6-4
2.
Question Number. 8. In Gas Tungsten Arc (GTA) welding, a
stream of inert gas is used to.
Option A. lower
the temperature required to properly fuse the metal.
Option B. prevent
the formation of oxides in the puddle.
Option C. concentrate
the heat of the arc and prevent its dissipation.
Correct Answer is. prevent
the formation of oxides in the puddle.
Explanation. NIL.
Question Number. 9. After welding you would normalise to.
Option A. remove
oxidation from the welded joint.
Option B. remove
carbon build up from the welded joint.
Option C. release
the stresses from the material.
Correct Answer is. release
the stresses from the material.
Explanation. Normalising
removes local stresses set up by the heat, and in turn prevents corrosion.
Question Number. 10. The flux used during brazing is a
mixture of water and.
Option A. zinc
chloride.
Option B. hydrochloric
acid.
Option C. borax
powder.
Correct Answer is. borax
powder.
Explanation. NIL.
Question Number. 11. Oxides form very rapidly when alloys or
metals are hot. It is important, therefore, when welding aluminium to use a.
Option A. solvent.
Option B. filler.
Option C. flux.
Correct Answer is. flux.
Explanation. BL6-4
8.2.2.
Question Number. 12. Which statement concerning a welding
process is true?.
Option A. In the
oxyacetylene welding process, the filler rod used for steel is covered with a
thin coating of flux.
Option B. In
the metallic-arc welding process, filler material, if needed, is provided by a
separate metal rod of the proper material held in the arc.
Option C. The
inert-arc welding process uses an inert gas to protect the weld zone from the
atmosphere.
Correct Answer is. The
inert-arc welding process uses an inert gas to protect the weld zone from the
atmosphere.
Explanation. Jeppesen
A & P airframe technician textbook pg 4-4 Gas Metal Arc Welding paragraph.
Question Number. 13. When inspecting a butt-welded joint by
visual means.
Option A. the
penetration should be 100 percent of the thickness of the base metal.
Option B. the
penetration should be 25 to 50 percent of the thickness of the base metal.
Option C. look
for evidence of excessive heat in the form of a very high bead.
Correct Answer is. the
penetration should be 100 percent of the thickness of the base metal.
Explanation. Jeppesen
A&P General Textbook 11-4 and Jeppesen A&P Airframe Textbook
4-2.Jeppesen A&P General Textbook 11-4 and Jeppesen A&P Airframe
Textbook 4-2.
Question Number. 14. What is undesirable in a good weld?.
Option A. oxides
mixed in with the filler material.
Option B. fusing
the edges of materials to be joined.
Option C. 100%
penetration by filler material.
Correct Answer is. oxides
mixed in with the filler material.
Explanation. NIL.
Question Number. 15. In selecting a torch tip size to use in
welding, the size of the tip opening determines the.
Option A. temperature
of the flame.
Option B. melting
point of the filler metal.
Option C. amount
of heat applied to the work.
Correct Answer is. amount
of heat applied to the work.
Explanation. NIL.
Question Number. 16. The most important consideration(s) when
selecting welding rod is/are.
Option A. material
compatibility.
Option B. current
setting or flame temperature.
Option C. ambient
conditions.
Correct Answer is. material
compatibility.
Explanation. NIL.
Question Number. 17. When inspecting a weld, you should make
sure that.
Option A. the
parent (or basis) materials are fully fused together.
Option B. the
weld has inclusions inside the bead.
Option C. there
are voids either side of the weld.
Correct Answer is. the
parent (or basis) materials are fully fused together.
Explanation. BL/6-4
13.1 (a) and BL/6-5 8.4 (a) and AC43.13-1B Page 4-54 Para.4-48.
16a. Aircraft Weight and Balance.
Question Number. 1. Fore and aft limits of the CG.
Option A. are
determined by the pilot when calculating the loading data.
Option B. are
specified by the manufacturer.
Option C. are
determined by the licensed engineer after a major check and weighing.
Correct Answer is. are
specified by the manufacturer.
Explanation. Leaflet
1-4 3.3.2.
Question Number. 2. What angle of turn will double the
weight of the aircraft?.
Option A. 30°.
Option B. 60°.
Option C. 45°.
Correct Answer is. 60°.
Explanation. NIL.
Question Number. 3. The basic equipment of an aircraft is.
Option A. that
equipment which is required for every role of the aircraft for which the
aircraft is operated plus unusable fuel.
Option B. all
equipment including fuel and oil necessary for a particular flight.
Option C. the
crew equipment, and other equipment including fuel and oil necessary for a
particular flight.
Correct Answer is. that
equipment which is required for every role of the aircraft for which the
aircraft is operated plus unusable fuel.
Explanation. Leaflet
1-4 1.2 a.
Question Number. 4. Aircraft measurements aft of the datum
are.
Option A. either
positive or negative.
Option B. positive.
Option C. negative.
Correct Answer is. positive.
Explanation. Leaflet
1-4 3.2.1.
Question Number. 5. A Weight and Centre of Gravity Schedule
is required by.
Option A. all
aircraft above 2730 kg MTWA.
Option B. all
aircraft not exceeding 2730 kg MTWA.
Option C. all
aircraft regardless of weight.
Correct Answer is. all
aircraft above 2730 kg MTWA.
Explanation. Leaflet
1-4 2.9.1 (a).
Question Number. 6. Aircraft below 5700kg not used for
commercial air transport purposes are required to be reweighed.
Option A. every
2 years.
Option B. every
5 years.
Option C. as
required by the CAA.
Correct Answer is. as
required by the CAA.
Explanation. CAIP S
BL/6-3 6.4.
Question Number. 7. Variable load is weight of.
Option A. crew,
their baggage and equipment relevant to role.
Option B. fuel,
oil and non-expendable equipment relevant to role.
Option C. basic
weight plus operating weight.
Correct Answer is. crew,
their baggage and equipment relevant to role.
Explanation. BL/
1-11 Para 1-2 (c).
Question Number. 8. The term 'reaction' used in weighing an
aircraft refers to.
Option A. the
sum of the loads on the main landing gear only.
Option B. the
individual loads on each landing gear.
Option C. the
sum of the loads on all of the landing gear.
Correct Answer is. the
individual loads on each landing gear.
Explanation. Leaflet
1-4 1.2 (f).
Question Number. 9. Aircraft must be reweighed.
Option A. after
two years from manufacture only.
Option B. after
two years from manufacture then at periods not exceeding five years.
Option C. at
periods not exceeding five years.
Correct Answer is. after
two years from manufacture then at periods not exceeding five years.
Explanation. Leaflet
1-4 2.2.
Question Number. 10. For purposes of calculating weight and C
of G position, an adult male (with baggage) is considered to have a mass of.
Option A. 85 kg.
Option B. 65 kg.
Option C. 75 kg.
Correct Answer is. 85
kg.
Explanation. JAR OPS
(with baggage) and AN(G)R Para 4 refers to Flight Crew mass of 85 kg. (Cabin
crew 75 kG).
Question Number. 11. Points forward of the datum point are.
Option A. negative.
Option B. neutral.
Option C. positive.
Correct Answer is. negative.
Explanation. Leaflet
1-4 3.2.1.
Question Number. 12. Where would you find documented, the fore
and aft limits of the C of G position?.
Option A. In the
aircraft Maintenance Manual.
Option B. In the
Flight Manual (or the documentation associated with the C of A).
Option C. In the
technical log.
Correct Answer is. In
the Flight Manual (or the documentation associated with the C of A).
Explanation. Leaflet
1-4 2.9.4 and 3.3.2.
Question Number. 13. Previous weighing records are.
Option A. retained
for 2 yrs only.
Option B. are
kept with aircraft records.
Option C. destroyed
after 5 yrs.
Correct Answer is. are
kept with aircraft records.
Explanation. Leaflet
1-4 2.7.
Question Number. 14. A Load Sheet is compiled in the order of.
Option A. Variable
Load, Fuel Load, Disposable Load, Basic Weight.
Option B. Basic
Weight, Variable Load, Disposable Load, Fuel Load.
Option C. Basic
Weight, Variable Load, Fuel Load, Disposable Load.
Correct Answer is. Basic
Weight, Variable Load, Disposable Load, Fuel Load.
Explanation. Leaflet
1-4 Page 24.
Question Number. 15. A Weight and Centre of Gravity Schedule
must be signed by.
Option A. the
CAA.
Option B. the
pilot.
Option C. a
Licensed aircraft engineer.
Correct Answer is. a
Licensed aircraft engineer.
Explanation. Leaflet
1-4 2.9.
Question Number. 16. An aircraft which has its C of G forward
of the Forward Limit.
Option A. the take-off
run will not be affected.
Option B. will
have a longer take-off run.
Option C. will
have a shorter take-off run.
Correct Answer is. will
have a longer take-off run.
Explanation. Leaflet
1-4 3.3.1.
Question Number. 17. The basic weight of an aircraft is.
Option A. the
pilot, flight crew and their luggage.
Option B. the
passengers, baggage and fuel.
Option C. the
aircraft, minimum equipment, unusable fuel and oil.
Correct Answer is. the
aircraft, minimum equipment, unusable fuel and oil.
Explanation. CAIP S
BL/ 1-11 Para 1-2 (b).
Question Number. 18. When an aircraft has been reweighed under
JAR OPS, what should be done to the old Weight and Balance Report?.
Option A. Kept
in the aircraft logbook.
Option B. Destroyed
after 3 months.
Option C. Kept
in the weight and balance schedule.
Correct Answer is. Destroyed
after 3 months.
Explanation. JAR OPS
Subpart P.
Question Number. 19. If the C of G of an aircraft with a full
complement of fuel is calculated. Then.
Option A. the C
of G will always be within limits if it was within limits with full fuel tanks.
Option B. the C
of G must be recalculated with zero fuel to ensure it will still be within
limits.
Option C. the C
of G will only need to be recalculated if the fuel weight is behind the
aircraft C of G position.
Correct Answer is. the
C of G must be recalculated with zero fuel to ensure it will still be within
limits.
Explanation. NIL.
Question Number. 20. Cargo placed aft of the datum will
produce a.
Option A. neutral
moment.
Option B. negative
moment.
Option C. positive
moment.
Correct Answer is. positive
moment.
Explanation. Leaflet
1-4 5.4.4 (a).
Question Number. 21. A load sheet.
Option A. need
not be carried on the aircraft if one remains at base.
Option B. is always
carried on the aircraft.
Option C. is
never carried on the aircraft.
Correct Answer is. is
always carried on the aircraft.
Explanation. NIL.
Question Number. 22. The Datum point on an aircraft, for
measuring C of G position could be.
Option A. the
front bulkhead.
Option B. anywhere
on the aircraft.
Option C. the
nose of the aircraft.
Correct Answer is. anywhere
on the aircraft.
Explanation. AC43
Page 10-1 para F, and A&P general textbook 6-4 Pg 250 'Datum'.
Question Number. 23. Increasing the weight of an aircraft.
Option A. increases
the glide range.
Option B. has no
affect on the glide range.
Option C. decreases
the glide range.
Correct Answer is. has
no affect on the glide range.
Explanation. Mechanics
of Flight Kermode Page 194.
Question Number. 24. A load Sheet must be signed by.
Option A. a
licensed aircraft engineer.
Option B. the
Commander of the aircraft.
Option C. the
Loading Officer.
Correct Answer is. the
Commander of the aircraft.
Explanation. NIL.
Question Number. 25. What is meant by empty weight?.
Option A. Basic
weight only.
Option B. Basic
weight minus unusable fuel plus oil.
Option C. Basic
weight plus unusable fuel plus oil.
Correct Answer is. Basic
weight plus unusable fuel plus oil.
Explanation. Jeppesen
A&P General Textbook 6-2.
Question Number. 26. A Weight and Centre of Gravity Schedule
is to be raised.
Option A. in
triplicate, for the CAA, the operator and the maintenance organisation.
Option B. in
duplicate, for the CAA and the operator.
Option C. once
only, for the CAA.
Correct Answer is. in
duplicate, for the CAA and the operator.
Explanation. Leaflet
1-4 2.9.4.
Question Number. 27. Where would you find the information on
the conditions for weighing the aircraft?.
Option A. Maintenance
Manual.
Option B. Technical
Log.
Option C. Flight
Manual in conjunction with the documents associated with the CofA.
Correct Answer is. Maintenance
Manual.
Explanation. The
information is in both Flight Manual and AMM. However the Flight Manual is for
the loaded aircraft, and the AMM is for the Basic Aircraft, the latter being
most relevant to the aircraft engineer.
Question Number. 28. In aeronautical weighing terms.
Option A. all
arms for forward of the reference datum are positive (+) and all arms aft of
the reference datum are negative (-).
Option B. all
reference datum are as per company procedures.
Option C. all
arms for forward of the reference datum are negative (-) and all arms aft of
the reference datum are positive (+).
Correct Answer is. all
arms for forward of the reference datum are negative (-) and all arms aft of
the reference datum are positive (+).
Explanation. NIL.
Question Number. 29. Details on recording of weight and C of G
position can be found in.
Option A. BCAR section
A.
Option B. Air
Navigation Order.
Option C. Airworthiness
Notices.
Correct Answer is. BCAR
section A.
Explanation. Leaflet
1-4 2.1.
Question Number. 30. If a new Weight and Centre of Gravity
Schedule is issued, the old one must be retained for.
Option A. one
year.
Option B. two
years.
Option C. six
months.
Correct Answer is. six
months.
Explanation. JAR OPS
1.920.
16b. Aircraft Weight and Balance.
Question Number. 1. A weighing cell is based on the
variation of.
Option A. induced
voltage with displacement.
Option B. resistance
with strain.
Option C. differential
currents with stress.
Correct Answer is. resistance
with strain.
Explanation. NIL.
Question Number. 2. When weighing an aircraft using elastic
load cells, the load cells go.
Option A. as a
single unit or combination of units under the aircraft wheels.
Option B. between
undercarriage and aircraft.
Option C. between
top of jack and the aircraft.
Correct Answer is. as
a single unit or combination of units under the aircraft wheels.
Explanation. Leaflet
1-4 4.5.1.
Question Number. 3. When weighing an aircraft with load
cells.
Option A. only
the main wheels are weighed.
Option B. the
aircraft is jacked.
Option C. a load
cell should be placed under each set of wheels.
Correct Answer is. the
aircraft is jacked.
Explanation. Leaflet
1-4 4.4.
Question Number. 4. When weighing an aircraft, the
hydrostatic weighing units are positioned.
Option A. either
under or on top of each jack.
Option B. one
under each jack.
Option C. one on
top of each jack.
Correct Answer is. one
on top of each jack.
Explanation. NIL.
Question Number. 5. When weighing an aircraft, the
hydraulic system should be.
Option A. empty.
Option B. completely
full.
Option C. filled
to 'maximum level' mark.
Correct Answer is. filled
to 'maximum level' mark.
Explanation. Leaflet
1-4 1.2 (b).
Question Number. 6. When weighing an aircraft by the
weighbridge method, the aircraft is.
Option A. only
levelled laterally.
Option B. jacked
and levelled.
Option C. resting
on the wheels.
Correct Answer is. resting
on the wheels.
Explanation. Leaflet
1-4 4.2.
17. Aircraft Handling and Storage.
Question Number. 1. When mooring an aircraft what type of
rope should be used?.
Option A. Nylon.
Option B. Fibre,
tied tight due to stretch when wet.
Option C. Fibre,
with some slack due to shrinkage when wet.
Correct Answer is. Nylon.
Explanation. Leaflet
10-1 4.3.1. Although fibre (manila) rope can be used (with some slack) the
A&P Mechanic General Handbook says Nylon is preferred (Pg.510). Also, fibre
rope does not shrink when wet, it shrinks when it dries.
Question Number. 2. Removal of ice by the use of deicing
fluid on the aircraft, before flight.
Option A. must
be 1 hour before flight to enable fluid to be cleaned from aircraft.
Option B. will
provide sufficient prevention of ice formation until take off.
Option C. may
remove ice for a period of time depending on the airfield conditions.
Correct Answer is. may
remove ice for a period of time depending on the airfield conditions.
Explanation. AL/11-3
3.1.4.
Question Number. 3. When deicing an aircraft with pressure
deicing fluid, the sensors on the outside of the aircraft should.
Option A. have
their heating switched on.
Option B. be fitted
with blanks or bungs.
Option C. not be
blanked.
Correct Answer is. be
fitted with blanks or bungs.
Explanation. AL/11-3
5.3.1.
Question Number. 4. When Ground Power is connected to
aircraft, the generators are.
Option A. paralleled
to supply.
Option B. paralleled
to supply for ground starting only.
Option C. never
paralleled.
Correct Answer is. never
paralleled.
Explanation. NIL.
Question Number. 5. If ice and snow is found on the wings
of an aircraft. Before flight the.
Option A. snow should
be removed but ice can remain because it has no appreciable affect on the
airflow.
Option B. all
snow and ice must be removed.
Option C. ice
should be removed but snow can remain because the airflow will remove it.
Correct Answer is. all
snow and ice must be removed.
Explanation. GOL/1-1
7.9.2. AL/11-3 3.1.
Question Number. 6. There is ice and snow on a helicopter
blade. You.
Option A. wipe
off excess snow and leave ice.
Option B. leave
a layer of ice.
Option C. remove
all traces of ice and snow.
Correct Answer is. remove
all traces of ice and snow.
Explanation. AL/11-3
2.2.
Question Number. 7. Why is the last part of towing an
aircraft, done in a straight line?.
Option A. To
relieve side pressure from the main wheels.
Option B. To relieve
hydraulic pressure from the steering mechanism.
Option C. To
allow nose wheel chocks to be placed at 90 degrees to the aircraft.
Correct Answer is. To
relieve side pressure from the main wheels.
Explanation. NIL.
Question Number. 8. Aluminium clad alloy sheet should not
be polished with mechanical buffing wheels as this.
Option A. will
cause large static charges to build up.
Option B. may
remove the aluminium coating.
Option C. may
remove the alloy coating.
Correct Answer is. may
remove the aluminium coating.
Explanation. NIL.
Question Number. 9. An aircraft should be cleared of snow.
Option A. using
air blast.
Option B. using
cold fluid.
Option C. using
hot fluid.
Correct Answer is. using
air blast.
Explanation. CAIP S
AL/11-3 Para 5.
Question Number. 10. When refueling an aircraft from a tanker,
why are the aircraft and tanker bonded together?.
Option A. To
discharge static electricity from the aircraft to the tanker.
Option B. To
maintain the aircraft and tanker at the same electrical potential.
Option C. To
enable the aircraft re-fuel pumps to be operated from the tanker electrical
supply.
Correct Answer is. To
maintain the aircraft and tanker at the same electrical potential.
Explanation. Pallett
- Aircraft Electrical Systems Pg.95.
Question Number. 11. When turning and towing an aircraft, why
should sharp radiuses be avoided?.
Option A. Power
steering leaks could occur.
Option B. Scrubbing
of main-wheel tyres could occur.
Option C. Scrubbing
of nose-wheel tyres could occur.
Correct Answer is. Scrubbing
of main-wheel tyres could occur.
Explanation. Leaflet
10-1 3.2.4.
Question Number. 12. When an aircraft is pulled out of soft
ground, the equipment should be attached to.
Option A. the
tail cone.
Option B. the
main gear.
Option C. the
nose gear.
Correct Answer is. the
main gear.
Explanation. CAIP S
GOL/ 1-1 Para 3-1-6.
Question Number. 13. When a helicopter lands, how does the
pilot signal to ground staff when it is safe to approach the aircraft?.
Option A. Turn
the anti collision lights off.
Option B. Flash
the landing lights.
Option C. Flash
the Nav lights.
Correct Answer is. Turn
the anti collision lights off.
Explanation. ANO
Section 2 Rule 9.
Question Number. 14. When the park brake has been applied on
an aircraft which has a pressurized hydraulic system and is reading maximum
system pressure, the brake gauges to the left and right main wheels will read.
Option A. no
indication.
Option B. full
system pressure.
Option C. full
scale deflection.
Correct Answer is. full
system pressure.
Explanation. NIL.
Question Number. 15. De-icing fluid Type 1 is used.
Option A. for
short holdover times.
Option B. where
the ambient temperature is below -10degrees Centigrade.
Option C. where
holdover times are long.
Correct Answer is. for
short holdover times.
Explanation. AL/11-3
2.6. Jeppesen A&P Airframe Technician Textbook Page 13-14.
Question Number. 16. When picketing a helicopter you.
Option A. tie
down one blade.
Option B. fit
sleeves to the blades to protect them if they strike the ground.
Option C. fit
sleeves and tie off all blades.
Correct Answer is. fit
sleeves and tie off all blades.
Explanation. Leaflet
10-1 4.4.1.
Question Number. 17. Which is bad practice for removing the
ice and snow in the cold weather?.
Option A. Dry
snow by hot air.
Option B. Deep
ice by de-icing fluid.
Option C. Use
brush for deep wet snow.
Correct Answer is. Dry
snow by hot air.
Explanation. AL/11-3
5.0.
18a. Disassembly, Inspection, repair and Assembly
Techniques.
Question Number. 1. Taper pins resist what loads.
Option A. compression.
Option B. shear.
Option C. tension.
Correct Answer is. shear.
Explanation. A&P
Technician General Textbook 8-29.
Question Number. 2. What test do you do on a bonded join?.
Option A. Shear.
Option B. Peel.
Option C. Tension.
Correct Answer is. Peel.
Explanation. NIL.
Question Number. 3. What would you use to check the run-out
on a control rod?.
Option A. Micrometer
+ ball bearing.
Option B. DTI +
V blocks.
Option C. 3 leg
trammel + feeler gauge.
Correct Answer is. DTI
+ V blocks.
Explanation. NIL.
Question Number. 4. Taper pins are used in which of the
following applications?.
Option A. To
take compression loads.
Option B. To
take shear loads.
Option C. To
take compression and shear loads.
Correct Answer is. To
take shear loads.
Explanation. Jeppesen
A&P Airframe Textbook 1-27.
Question Number. 5. When using a D.T.I. to check the
run-out of a shaft, readings of -15 to +25 would indicate a run-out of.
Option A. 0.025
inches.
Option B. 0.020
inches.
Option C. 0.040
inches.
Correct Answer is. 0.020
inches.
Explanation. CAIP S
EL/3-3 Para. 3.2.
Question Number. 6. A dent is measured in a tubular
push-pull rod by.
Option A. passing
a ball down its bore.
Option B. callipers
and feeler gauges.
Option C. a
steel ball and micrometer.
Correct Answer is. a
steel ball and micrometer.
Explanation. NIL.
Question Number. 7. What is used on Magnesium to re-protect
it?.
Option A. Selenious
Acid.
Option B. Deoxidine.
Option C. Chromic
Acid.
Correct Answer is. Selenious
Acid.
Explanation. NIL.
Question Number. 8. In the procedure to be followed after
spillage of battery acid, neutralizing is carried out.
Option A. by
washing with distilled water.
Option B. by
applying a coating of Vaseline.
Option C. with a
dilute solution of sodium bicarbonate.
Correct Answer is. with
a dilute solution of sodium bicarbonate.
Explanation. CAAIP S
Leaflet 9-2 5.4.1.
Question Number. 9. After carrying out an identification
test of aluminium alloy with caustic soda, the caustic soda should be
neutralized with.
Option A. Chromic
anhydride solution.
Option B. Copper
sulphate solution.
Option C. Phosphoric
acid.
Correct Answer is. Chromic
anhydride solution.
Explanation. BL/4-2
Para 2-4-5 'Note'.
Question Number. 10. To neutralize spilled battery acid on
aluminium alloy, use.
Option A. sulphuric
acid.
Option B. bicarbonate
of soda.
Option C. caustic
soda.
Correct Answer is. bicarbonate
of soda.
Explanation. BL/4-1
4.1.3.
Question Number. 11. Hydrogen embrittlement of high tensile
steel is caused if it is treated with.
Option A. Zinc
Chromate.
Option B. Nitric
acid.
Option C. Phosphoric
acid.
Correct Answer is. Phosphoric
acid.
Explanation. BL/4-2
3.2.2 (iii) BL/7-4 5.2.
Question Number. 12. Dents in a tubular push-pull rod are not
allowed.
Option A. anywhere
on the rod.
Option B. in the
middle third of the rod.
Option C. in the
end thirds of the rod.
Correct Answer is. in
the middle third of the rod.
Explanation. NIL.
Question Number. 13. When checking a diode forward bias
function, the positive lead of the ohmmeter should be placed on the.
Option A. cathode
and the negative lead to the anode.
Option B. anode
and the negative lead to the cathode.
Option C. cathode
and the negative lead the earth.
Correct Answer is. anode
and the negative lead to the cathode.
Explanation. Positive
to the anode.
Question Number. 14. The bonding resistance of primary
structure must not exceed.
Option A. 0.05
ohms.
Option B. 0.005
ohms.
Option C. 0.5
ohms.
Correct Answer is. 0.05
ohms.
Explanation. Leaflet
9-1 3.8 table 1.
Question Number. 15. What is the maximum resistance between
the main earth system and a metal plate on which the earthing device (tyre) is
resting?.
Option A. 100
megohms.
Option B. 1
megohm.
Option C. 10
megohms.
Correct Answer is. 10
megohms.
Explanation. EEL/1-6
Para 3.10.8 & Leaflet 9-1 3.10.8.
Question Number. 16. The three electrical checks carried out
on aircraft are (1) continuity (2) bonding (3) insulation. What is the order in
which they are executed?.
Option A. 2-3-1.
Option B. 1-2-3.
Option C. 2-1-3.
Correct Answer is. 2-1-3.
Explanation. Bonding
- Continuity, Insulation, Function.
Question Number. 17. When an earth-return terminal assembly
has to be replaced which of the following checks must be carried out?.
Option A. Bonding
and continuity tests.
Option B. Bonding
and millivolt drop tests.
Option C. Bonding
and insulation resistance tests.
Correct Answer is. Bonding
and millivolt drop tests.
Explanation. EEL/1-6
Para 3.7.2 & Leaflet 9-1 3.7.2.
Question Number. 18. When carrying out millivolt drop checks
on a circuit, what is an approximate guide for a correct reading?.
Option A. 10
millivolts for every 15 amps flowing.
Option B. 10
millivolts for every 5 amps flowing.
Option C. 5
millivolts for every 10 amps flowing.
Correct Answer is. 5
millivolts for every 10 amps flowing.
Explanation. Leaflet
9-1 4.3 (b). EEL/1-6.
Question Number. 19. Effective continuity is not possible
unless which of the following conditions exists?.
Option A. All
circuit earths are disconnected.
Option B. The
portion of the circuit under test must constitute a simple series circuit with
no parallel paths.
Option C. All
manually operated switches must be off.
Correct Answer is. The
portion of the circuit under test must constitute a simple series circuit with
no parallel paths.
Explanation. Leaflet
9-1 4.2.3. EEL / 1-6 Para 4-2-3.
Question Number. 20. Why is a low voltage supply used for
continuity testing?.
Option A. To
prevent fuses 'blowing' and lamps burning out.
Option B. To
avoid damage to the wiring.
Option C. To
avoid breaking down a high resistance film that might exist between contacting
surfaces.
Correct Answer is. To
avoid breaking down a high resistance film that might exist between contacting
surfaces.
Explanation. Leaflet
9-1 4.2. A problem of poor continuity could be caused by oxidation at
connectors. Using too high a voltage in a continuity test might 'overlook' the
problem and give a false good reading.
Question Number. 21. When replacing a bonding connection and
the original conductor cannot be matched exactly, which of the following
replacements would you use?.
Option A. One
manufactured from the same type of material, but of greater cross sectional
area should be selected.
Option B. One
manufactured from any piece of Nyvin cable having the correct current capacity
may be used.
Option C. One
manufactured from any conducting material of the same cross sectional area be
used.
Correct Answer is. One
manufactured from the same type of material, but of greater cross sectional
area should be selected.
Explanation. Leaflet
9-1 3.5.2.
Question Number. 22. What is a typical minimum insulation
resistance value for an aircraft undercarriage bay?.
Option A. 10
megohms.
Option B. 5
megohms.
Option C. 2
megohms.
Correct Answer is. 2
megohms.
Explanation. EEL/1-6
Para 4-5-4 (a) & Leaflet 9-1 4.5.4 (a).
Question Number. 23. The recommended insulation resistance of
a DC motor is.
Option A. 2
megohms.
Option B. 0.5
megohms.
Option C. 5
megohms.
Correct Answer is. 0.5
megohms.
Explanation. Leaflet
9-1 Para.4.5.4 (Rotating machinery).
Question Number. 24. Bonding value for secondary structure is
a maximum of.
Option A. 0.05
ohms.
Option B. 1 ohm.
Option C. 0.5
ohms.
Correct Answer is. 1
ohm.
Explanation. Leaflet
9-1 para.3.8. EEL 1-6 3.8.
Question Number. 25. Wrinkling of an aircraft skin will.
Option A. cause rivets
to pull.
Option B. weaken
the skin.
Option C. increase
drag on the aircraft.
Correct Answer is. cause
rivets to pull.
Explanation. All
three are possibly correct, but c is the most probable.
Question Number. 26. You have removed a bolt from a critical
bolted joint for inspection and rectification. What action should you take
prior to inspection?.
Option A. Before
any inspection is carried out, the nut/bolt and hole must be cleaned with a
solvent such as trichloroethylene.
Option B. Clean
the bolt shank and thread and re-grease and replace bolt and check for
side-play.
Option C. A
preliminary inspection should be made before the hole is cleaned.
Correct Answer is. A
preliminary inspection should be made before the hole is cleaned.
Explanation. CAIP
AL/7-5 5.4.
Question Number. 27. On inspection of a critical bolted joint
you witness black or grey dust or paste. What type of corrosion has taken place
and what type of material is involved?.
Option A. Exfoliation
corrosion in magnesium alloys.
Option B. Galvanic
corrosion in magnesium alloys.
Option C. Fretting
corrosion in aluminium alloys.
Correct Answer is. Fretting
corrosion in aluminium alloys.
Explanation. CAIP
BL/4-1 3.1.5.
Question Number. 28. What is indicated by the wrinkling of the
underside of an aircraft skin?.
Option A. Hogging.
Option B. Fretting.
Option C. Sagging.
Correct Answer is. Hogging.
Explanation. Hogging
produces wrinkling on the underside of the wing. Sagging produces wrinkling on
the upper side of the wing.
Question Number. 29. What is used to re-protect magnesium?.
Option A. Selenious
acid.
Option B. Deoxidine.
Option C. Chromic
acid.
Correct Answer is. Selenious
acid.
Explanation. CAIP S
BL/7-5 6.3.1.
Question Number. 30. What is used on magnesium to remove
corrosion?.
Option A. Strontium
chromate.
Option B. Chromic
acid / sulphuric acid solution.
Option C. Selenious
acid.
Correct Answer is. Chromic
acid / sulphuric acid solution.
Explanation. CAIP S
BL/4-2 2.4.4. BL/7-5 9.3.5 (i).
Question Number. 31. Galvanic corrosion refers to a type of.
Option A. corrosion
between two pieces of material.
Option B. plating
process.
Option C. surface
corrosion.
Correct Answer is. corrosion
between two pieces of material.
Explanation. AC43
6-20.
Question Number. 32. Chromating used on magnesium alloys
produces.
Option A. chromium
surface electrochemically.
Option B. a
chromate film surface.
Option C. metal
chromates on the electrochemically.
Correct Answer is. a
chromate film surface.
Explanation. CAIP S
BL/7-5 Para.4.
Question Number. 33. Chromating used on magnesium alloys.
Option A. uses
chromium and converts the surface electrochemically.
Option B. uses
chromates and converts the surface chemically.
Option C. uses
chromium, which is deposited on the surface.
Correct Answer is. uses
chromates and converts the surface chemically.
Explanation. BL/7-3
11. Chromate treatment sometimes called 'chromate conversion'.
Question Number. 34. When carrying out a bonding test in the
presence of an anodic coating, what should you do?.
Option A. Take
account of the resistance of the coating.
Option B. Disregard
the resistance of the coating.
Option C. Penetrate
the coating so a good electrical contact is made.
Correct Answer is. Penetrate
the coating so a good electrical contact is made.
Explanation. CAAIP S
Leaflet 9-1, 3.10.6 and note from 3.6.6.
Question Number. 35. Maximum value of resistance between all
isolated parts which may be subjected to appreciable electrostatic charging and
the main earth.
Option A. 0.5
Megohm or 100 kilohm per sq.ft. of surface area whichever is less.
Option B. 1 ohm.
Option C. 0.05
ohm.
Correct Answer is. 0.5
Megohm or 100 kilohm per sq.ft. of surface area whichever is less.
Explanation. Leaflet
9-1 3.8 Table 1 or EEL/1-6 3.5.
Question Number. 36. Removal of corrosion from aluminium clad
alloy is best done.
Option A. mechanically
by buffing.
Option B. chemically
by trichloroethylene.
Option C. chemically
by sulphuric acid solution.
Correct Answer is. chemically
by sulphuric acid solution.
Explanation. NIL.
Question Number. 37. Control methods for galvanic corrosion
include.
Option A. reducing
cyclic stressing and increasing cross sectional area.
Option B. joining
similar metals and using jointing compounds.
Option C. ensuring
correct heat treatments and correct alloying.
Correct Answer is. joining
similar metals and using jointing compounds.
Explanation. NIL.
Question Number. 38. The treatment for stress corrosion is.
Option A. not the
same as fatigue corrosion.
Option B. the
same as for surface corrosion or surface cracks in sheet metal.
Option C. always
the replacement of the part.
Correct Answer is. always
the replacement of the part.
Explanation. NIL.
Question Number. 39. Very light corrosion on aluminium alloy
can be removed by.
Option A. using
a solvent.
Option B. rubbing
with wire wool.
Option C. using
Alocrom 1200.
Correct Answer is. using
a solvent.
Explanation. NIL.
Question Number. 40. To remove corrosion on Fe metals use.
Option A. selenious
acid rust remover.
Option B. sulphuric
acid rust remover.
Option C. phosphoric
acid rust remover.
Correct Answer is. phosphoric
acid rust remover.
Explanation. NIL.
Question Number. 41. The usual manufacturer's anti corrosive
process to be applied to Fe aircraft parts is.
Option A. cadmium
plating.
Option B. anodising.
Option C. metal
spraying.
Correct Answer is. cadmium
plating.
Explanation. NIL.
Question Number. 42. An intervention defect is one where.
Option A. the
engineer has the discretion on whether to intervene.
Option B. there
is a requirement for the maintenance engineer to intervene.
Option C. the
defect occurred because of some previous maintenance action.
Correct Answer is. the
defect occurred because of some previous maintenance action.
Explanation. NIL.
Question Number. 43. Vapour phase inhibitor should be used.
Option A. when
re-protecting after corrosion.
Option B. when
degreasing a component.
Option C. when
painting an aircraft.
Correct Answer is. when
re-protecting after corrosion.
Explanation. NIL.
Question Number. 44. When carrying out insulation resistance
checks.
Option A. the
measurement is always infinity if the cable is installed correctly.
Option B. the
measurement will also show cable continuity.
Option C. the
measurement varies depending upon the ambient conditions of the aircraft under
test.
Correct Answer is. the
measurement varies depending upon the ambient conditions of the aircraft under
test.
Explanation. EEL/1-6
4.5.3, Leaflet 9-1 4.5.3.
Question Number. 45. How is damage classified on an aircraft
skin?.
Option A. Negligible,
repairable, replacement.
Option B. Negligible,
allowable, replacement.
Option C. Negligible,
allowable, repairable.
Correct Answer is. Negligible,
repairable, replacement.
Explanation. NIL.
Question Number. 46. When carrying out a millivolt drop test
on a terminal, the maximum value should be.
Option A. 50mV/10A.
Option B. 10mV/10A.
Option C. 5mV/10A.
Correct Answer is. 5mV/10A.
Explanation. Leaflet
9-1 4.3 (b). EEL/1-6.
Question Number. 47. A jury strut is used.
Option A. as a
reference when checking the C of G position.
Option B. as a
datum when placing the aircraft in a rigging position.
Option C. to
support the structure during repairs.
Correct Answer is. to
support the structure during repairs.
Explanation. NIL.
Question Number. 48. Run out' on a control rod is measured by.
Option A. micrometer,
surface plate and vee-blocks.
Option B. surface
plate, vernier callipers and vee-blocks.
Option C. dial
test indicator, surface plate and vee-blocks.
Correct Answer is. dial
test indicator, surface plate and vee-blocks.
Explanation. NIL.
Question Number. 49. How do you check the resistance of a fire
bottle cartridge?.
Option A. Use an
insulation tester.
Option B. Use a
multimeter.
Option C. Use a
light and bulb.
Correct Answer is. Use
a multimeter.
Explanation. NIL.
Question Number. 50. If after forming a crimp in an electrical
condutor a high resistance is suspected, how would you carry out a check
without disturbing the connection?.
Option A. Use a
multimeter set to millivolts and carry out a millivolts drop test.
Option B. Carry
out an insulation check.
Option C. Use a
multimeter set to ohms to check the resistance.
Correct Answer is. Use
a multimeter set to millivolts and carry out a millivolts drop test.
Explanation. NIL.
18b. Disassembly, Inspection, repair and Assembly
Techniques.
Question Number. 1. Damaged chromate film should be repaired
by using.
Option A. phosphoric
acid 10% by weight in water.
Option B. selenious
acid 10% by weight in water.
Option C. selenious
acid 20% by weight in water.
Correct Answer is. selenious
acid 10% by weight in water.
Explanation. BL/7-3
5.2.
Question Number. 2. Stop Drilling' is the process of.
Option A. drilling
holes to stop a crack at the crack ends.
Option B. drilling
holes in a metal prior to riveting.
Option C. drilling
a rivet head to remove it from the metal.
Correct Answer is. drilling
holes to stop a crack at the crack ends.
Explanation. NIL.
Question Number. 3. When inserting a helicoil insert, which
way does the tang face?.
Option A. Away
from the hole.
Option B. Towards
the hole.
Option C. Towards
the mandrel.
Correct Answer is. Towards
the hole.
Explanation. Jeppesen
A&P Technician General Textbook Page 8-31.
Question Number. 4. On a patch repair you should use.
Option A. material
one gauge thicker than the original structure.
Option B. the
same rivet spacing as the original structure.
Option C. only
aluminium alloy rivets.
Correct Answer is. the
same rivet spacing as the original structure.
Explanation. AC43
Page 4-32.
Question Number. 5. What tap do you use when fitting a
Helicoil?.
Option A. The
same as the original thread size.
Option B. The
next size up from the original tap size.
Option C. The
tap supplied with the Helicoil kit.
Correct Answer is. The
tap supplied with the Helicoil kit.
Explanation. NIL.
Question Number. 6. When fitting a thread insert.
Option A. the
insert should be tapped in using a hammer.
Option B. the
hole should be expanded using a tap supplied by the insert manufacturer.
Option C. a
thread the next size up from the original should be tapped.
Correct Answer is. the
hole should be expanded using a tap supplied by the insert manufacturer.
Explanation. CAAIP S
Leaflet 2-10 3.2.2.
Question Number. 7. A stud broken off below the surface is
removed by.
Option A. using
a stud box.
Option B. a stud
remover tool fitted into a drilled hole.
Option C. cutting
a slot in it and removing with a screwdriver.
Correct Answer is. a
stud remover tool fitted into a drilled hole.
Explanation. A stud
box could only be used if it is broken above the surface.
Question Number. 8. A thread insert is made from.
Option A. white
metal.
Option B. aluminium
alloy.
Option C. stainless
steel.
Correct Answer is. stainless
steel.
Explanation. NIL.
Question Number. 9. On a composite repair the vacuum should
be.
Option A. above
required level.
Option B. below
required level.
Option C. at the
required level.
Correct Answer is. at
the required level.
Explanation. NIL.
Question Number. 10. If bridging strips or bonding cords are
fractured, what action may be taken?.
Option A. The
broken ends can be repaired with an “in-line” splice.
Option B. A new
conductor should be fitted.
Option C. The
broken ends can be soldered.
Correct Answer is. A
new conductor should be fitted.
Explanation. Leaflet
9-1 3.6.3.
Question Number. 11. A UNF threaded wire thread insert may be
identified.
Option A. by a
black painted tang.
Option B. by a
red painted tang.
Option C. by an
unpainted tang.
Correct Answer is. by
a black painted tang.
Explanation. BL/6-22
3.1.
18c. Disassembly, Inspection, repair and Assembly
Techniques.
Question Number. 1. Transducers used in ultrasonic testing
exhibit which of he following effects?.
Option A. Hyper-acoustic.
Option B. Ferromagnetic.
Option C. Piezoelectric.
Correct Answer is. Piezoelectric.
Explanation. CAAIP S
leaflet 4-5 page 3 para 3.2.
Question Number. 2. The eddy current method of N.D.T. uses.
Option A. AC or
DC.
Option B. Direct
current.
Option C. Alternating
current.
Correct Answer is. Alternating
current.
Explanation. CAAIP S
leaflet 4-5 page 1 para 2.1.
Question Number. 3. To measure the thickness of a paint
finish, what type of NDT inspection is used?.
Option A. A
woodpecker.
Option B. Ultrasonic.
Option C. Radiographic.
Correct Answer is. Ultrasonic.
Explanation. CAAIP S
leaflet 4-5 para 1.4.
Question Number. 4. When carrying out a dye penetrant test,
after the developer has been applied it should be inspected.
Option A. after
30 minutes.
Option B. as
soon as the developer is dry and again after approximately 10 minutes.
Option C. after
1 hour.
Correct Answer is. as
soon as the developer is dry and again after approximately 10 minutes.
Explanation. CAAIP S
Leaflet 4-2 Paras 7-1 and 7-2.
Question Number. 5. During a colour contrast test the
penetrant time should be.
Option A. longer
for a small crack.
Option B. shorter
for a small crack.
Option C. longer
for a wide crack.
Correct Answer is. longer
for a small crack.
Explanation. CAAIP S
Leaflet 4-2 Para 4-1.
Question Number. 6. How should a dye penetrant field kit be
stored?.
Option A. At a
cold temperature in a darkened room.
Option B. In
direct sunlight.
Option C. At
room temperature away from direct sunlight.
Correct Answer is. At
room temperature away from direct sunlight.
Explanation. CAAIP S
Leaflet 4-2 Para 9-1.
Question Number. 7. When carrying out a colour contrast
test on a pressure vessel.
Option A. the
dye should be applied to the outside and the developer to the inside.
Option B. the
dye should be applied to the inside and the developer to the outside.
Option C. both
the dye and the developer should be applied to the outside.
Correct Answer is. the
dye should be applied to the inside and the developer to the outside.
Explanation. CAAIP S
Leaflet 4-2 Para 9-1.
Question Number. 8. When leak testing with a colour
contrast field kit, the soak time for a component less than 1/8 in. (3mm) thick
would be.
Option A. at
least twice the normal soak time.
Option B. at
least 3 times the normal soak time.
Option C. at
least the normal soak time.
Correct Answer is. at
least 3 times the normal soak time.
Explanation. CAAIP S
Leaflet 4-2 Para 9-2.
Question Number. 9. When using a colour contrast dye
penetrant kit, and a small crack is suspected in the material.
Option A. less developer
should be used.
Option B. less
inhibitor should be used.
Option C. a
magnifying glass is recommended.
Correct Answer is. a
magnifying glass is recommended.
Explanation. CAAIP\'s
leaflet 4-2 pg 6 para 7.5.
Question Number. 10. What NDT method would you use to detect
delamination?.
Option A. Colour
contrast dye penetrant.
Option B. Ultrasound.
Option C. Eddy
current.
Correct Answer is. Ultrasound.
Explanation. Leaflet
4-5 1.4.
Question Number. 11. Magnetic particle testing detects faults.
Option A. transverse.
Option B. longitudinally.
Option C. longitudinal
and transverse.
Correct Answer is. transverse.
Explanation. CAAIP
4-7, 2.2 The flaw must be between 45 degrees and 90 degrees to the flux lines.
Question Number. 12. Dye penetrant in a cold climate.
Option A. takes
longer to work.
Option B. is not
affected.
Option C. works
more quickly.
Correct Answer is. takes
longer to work.
Explanation. CAAIP S
Leaflet 4-2 Para 4-2.
Question Number. 13. If after spraying the developer, red
blotches appear, the part.
Option A. has
sub-surface defects.
Option B. was
not cleaned properly.
Option C. is
porous.
Correct Answer is. is
porous.
Explanation. CAAIP S
Leaflet 4-2 Para 7-3.
Question Number. 14. What is the purpose of the developer in a
dye penetrant inspection?.
Option A. It
acts a s a blotter to draw out the penetrant that has seeped into the crack.
Option B. It is
drawn to the crack by electrostatic attraction.
Option C. It
seeps into the crack and makes it show up.
Correct Answer is. It
acts a s a blotter to draw out the penetrant that has seeped into the crack.
Explanation. CAAIP S
Leaflet 4-2 Para.6.
Question Number. 15. The main advantage of dye penetrant
inspection is.
Option A. the
part to be inspected does not require cleaning.
Option B. the
defect must be opened to the surface.
Option C. the
penetrant solution works on any non-porous material.
Correct Answer is. the
penetrant solution works on any non-porous material.
Explanation. NIL.
Question Number. 16. To detect a minute crack using dye
penetrant inspection usually requires.
Option A. the
surface to be highly polished.
Option B. a
longer than normal penetrating time.
Option C. that
the developer be applied to a flat surface.
Correct Answer is. a
longer than normal penetrating time.
Explanation. CAAIP S
Leaflet 4-2 Para 7-1.
Question Number. 17. When checking an item with the magnetic
particle inspection method, circular and longitudinal magnetization should be
used to.
Option A. evenly
magnetize the entire part.
Option B. ensure
uniform current flow.
Option C. reveal
all possible defects.
Correct Answer is. reveal
all possible defects.
Explanation. Leaflet
4-2 2 and leaflet 4-7, 4.5.
Question Number. 18. Which type crack can be detected by
magnetic particle inspection using either circular or longitudinal
magnetisation?.
Option A. 45°.
Option B. longitudinal.
Option C. transverse.
Correct Answer is. 45°.
Explanation. CAAIP S
leaflet 4-7 para 2.2.
Question Number. 19. Surface cracks in aluminium castings and
forgings may usually be detected by.
Option A. submerging
the part in a solution of hydrochloric acid and rinsing with clear water.
Option B. gamma
ray inspection.
Option C. the
use of dye penetrants and suitable developers.
Correct Answer is. the
use of dye penetrants and suitable developers.
Explanation. Leaflet
4-2 1.6.2.
Question Number. 20. Which of these metals is inspected using
the magnetic particle inspection method?.
Option A. Magnesium
alloys.
Option B. Aluminium
alloys.
Option C. Iron
alloys.
Correct Answer is. Iron
alloys.
Explanation. Leaflet
4-7 1.1.
Question Number. 21. One way a part may be demagnetized after
magnetic particle inspection is by.
Option A. slowly
moving the part out of an AC magnetic field of sufficient strength.
Option B. slowly
moving the part into an AC magnetic field of sufficient strength.
Option C. subjecting
the part to high voltage, low amperage AC.
Correct Answer is. slowly
moving the part out of an AC magnetic field of sufficient strength.
Explanation. Leaflet
4-7 4.9.2.
Question Number. 22. The testing medium that is generally used
in magnetic particle inspection utilises a ferromagnetic material that has.
Option A. low
permeability and high retentivity.
Option B. high
permeability and low retentivity.
Option C. high
permeability and high retentivity.
Correct Answer is. high
permeability and low retentivity.
Explanation. NIL.
Question Number. 23. The 'Dwell Time' of a dye-penetrant NDT
inspection is the.
Option A. time
it takes for a defect to develop.
Option B. time
the penetrant is allowed to stand.
Option C. amount
of time the developer is allowed to act.
Correct Answer is. time
the penetrant is allowed to stand.
Explanation. A&P
General Textbook 12-3 Pg 447 Para 2.
Question Number. 24. What non-destructive testing method
requires little or no part preparation, is used to detect surface or
near-surface defects in most metals, and may also be used to separate metals or
alloys and their heat-treat conditions?.
Option A. Eddy
current inspection.
Option B. Magnetic
particle inspection.
Option C. Ultrasonic
inspection.
Correct Answer is. Eddy
current inspection.
Explanation. NIL.
Question Number. 25. Gamma Ray Testing of combustion chambers
will show up.
Option A. grey
on white background.
Option B. black
on lighter background.
Option C. light
grey on black background.
Correct Answer is. light
grey on black background.
Explanation. NIL.
Question Number. 26. Which of these non-destructive testing
methods is suitable for the inspection of most metals, plastics and ceramics
for surface and subsurface defects?.
Option A. Eddy
current inspection.
Option B. Magnetic
particle inspection.
Option C. Ultrasonic
inspection.
Correct Answer is. Ultrasonic
inspection.
Explanation. NIL.
Question Number. 27. Ultrasonic flaw detectors use.
Option A. high
frequency sound waves.
Option B. a
magnetic field.
Option C. x-rays.
Correct Answer is. high
frequency sound waves.
Explanation. NIL.
Question Number. 28. Defects are indicated in the dye
penetrant crack detection test by.
Option A. red
lines on a white background.
Option B. yellowish
green marks.
Option C. green
lines and dots.
Correct Answer is. red
lines on a white background.
Explanation. NIL.
Question Number. 29. NDT using colour dye process at
temperatures below 15°C will.
Option A. not be
affected by the temperature.
Option B. retard
the penetrant action of the dye and penetration time is extended.
Option C. mean
choosing alternative NDT method.
Correct Answer is. retard
the penetrant action of the dye and penetration time is extended.
Explanation. CAAIP S
Leaflet 4-2 Para 4-2.
Question Number. 30. When using dye penetrant NDT on a tank,
the dye penetrant should be applied.
Option A. on the
outside with developer on the outside.
Option B. on the
inside, with developer on the outside.
Option C. on the
inside with the developer on the inside.
Correct Answer is. on
the inside, with developer on the outside.
Explanation. CAAIP S
Leaflet 4-2 Para 9-1.
Question Number. 31. In order for dye penetrant inspection to
be effective, the material being checked must.
Option A. be
non-magnetic.
Option B. be
magnetic.
Option C. have
surface cracks.
Correct Answer is. have
surface cracks.
Explanation. A&P
General Textbook 12-2 Pg 446 (B).
Question Number. 32. Which of the following metals can be
inspected using the magnetic particle inspection method?.
Option A. Aluminium
alloys.
Option B. Iron
alloys.
Option C. Magnesium
alloys.
Correct Answer is. Iron
alloys.
Explanation. NIL.
Question Number. 33. After completion of electromagnetic crack
detection, the test piece must be.
Option A. allowed
to cool to room temperature as slowly as possible.
Option B. de-magnetised
before returning to service.
Option C. allowed
to lose any residual magnetism over as long a period possible.
Correct Answer is. de-magnetised
before returning to service.
Explanation. NIL.
Question Number. 34. Which of the following N.D.T. techniques
cannot be used on a component manufactured from austenitic stainless steel?.
Option A. Magnetic
- particle.
Option B. Penetrant
dye.
Option C. Hot
oil and chalk.
Correct Answer is. Magnetic
- particle.
Explanation. NIL.
Question Number. 35. Fluorescent penetrant processes for the
detection of cracks or material defects are used with.
Option A. a
tungsten light source.
Option B. an
ultra-violet radiation source.
Option C. an
infra-red light source.
Correct Answer is. an
ultra-violet radiation source.
Explanation. CAAIP S
Leaflet 4-3 Para 1-5.
Question Number. 36. What is an isotope the power source of?.
Option A. X-Rays.
Option B. Ultra
Violet Rays.
Option C. Gamma
Rays.
Correct Answer is. Gamma
Rays.
Explanation. CAAIP\'s
leaflet 4-6 para 2.
Question Number. 37. The fluid used in the 'Oil and Chalk'
method of non-destructive testing is a mixture of.
Option A. lubricating
oil and petrol.
Option B. lubricating
oil and lard oil.
Option C. lubricating
oil and paraffin.
Correct Answer is. lubricating
oil and paraffin.
Explanation. CAAIP S
Leaflet 4-1 Para 3-2.
Question Number. 38. Under magnetic particle inspection, a
part will be identified as having a fatigue crack under which condition?.
Option A. The
discontinuity pattern is straight.
Option B. The
discontinuity is found in a highly stressed area of the part.
Option C. The
discontinuity is found in a non-stressed area of the part.
Correct Answer is. The
discontinuity is found in a highly stressed area of the part.
Explanation. NIL.
Question Number. 39. When inspecting a component which is
being subjected to the hot fluid chalk process, the examination for defects
should be carried out.
Option A. whilst
the item is still quite hot.
Option B. immediately
on removal of the item from the chalk cabinet.
Option C. when
the item is quite cool.
Correct Answer is. when
the item is quite cool.
Explanation. CAAIP S
Leaflet 4-1 3.
Question Number. 40. Circular magnetization of a part can be
used to detect defects.
Option A. perpendicular
to the concentric circles of magnetisation.
Option B. parallel
to the long axis of the part.
Option C. perpendicular
to the long axis of the part.
Correct Answer is. perpendicular
to the concentric circles of magnetisation.
Explanation. CAIP
BL/8-5 para 2.1.
Question Number. 41. An indication of porosity when using a
penetrant dye crack detection method is.
Option A. areas
where dye is not showing.
Option B. an
area of scattered dots of dye.
Option C. closely
spaced dots of dye formed in a line.
Correct Answer is. an
area of scattered dots of dye.
Explanation. CAAIP S
Leaflet 4-2 7.3.
Question Number. 42. In a test for adequate demagnetization of
a component after a magnetic particle test, the test compass should not
deflect.
Option A. more
than 1° when standing due east of the component.
Option B. more
than 1° when standing due south of the component.
Option C. more
than 1° when standing north-east of the component.
Correct Answer is. more
than 1° when standing due east of the component.
Explanation. CAAIP S
Leaflet 4-7 4.10.2.
Question Number. 43. If on application of developer it all
turns to a pinkish hue, what has happened?.
Option A. Thin
porosity.
Option B. The
hue has pinked.
Option C. Incorrect
cleaning.
Correct Answer is. Incorrect
cleaning.
Explanation. CAAIP S
Leaflet 4-2 Para 6-6.
Question Number. 44. If dye penetrant inspection indications
are not sharp and clear, the most probable cause is that the part.
Option A. is not
damaged.
Option B. was
not correctly degaussed before the developer was applied.
Option C. was
not thoroughly cleaned before developer was applied.
Correct Answer is. was
not thoroughly cleaned before developer was applied.
Explanation. AC43
5.60 G.
Question Number. 45. The pattern for an inclusion is a
magnetic particle build-up forming.
Option A. a
single line.
Option B. parallel
lines.
Option C. a
fern-like pattern.
Correct Answer is. parallel
lines.
Explanation. AandP
Mechanics General Handbook Pg 474 para 2.
Question Number. 46. When carrying out a penetrant dye crack
test, before the dye is applied the surface being tested should be.
Option A. etch
primed.
Option B. thoroughly
degreased.
Option C. painted
with developer fluid.
Correct Answer is. thoroughly
degreased.
Explanation. Leaflet
4-2 Para 2-4.
Question Number. 47. When carrying out a dye penetrant
inspection, what time should elapse after applying the developer before
inspecting the component?.
Option A. Initial
inspection after 30 seconds followed by a 2nd inspection after 10 minutes.
Option B. After
15 minutes.
Option C. After
10 minutes.
Correct Answer is. Initial
inspection after 30 seconds followed by a 2nd inspection after 10 minutes.
Explanation. Leaflet
4-2 Para 7-2.
Question Number. 48. When should the developer be applied to
the component?.
Option A. After
excess penetrant has been removed and the area completely dried.
Option B. Before
applying penetrant.
Option C. Before
the penetrant dries.
Correct Answer is. After
excess penetrant has been removed and the area completely dried.
Explanation. Leaflet
4-2 Para 1.5, 5.4.1.
Question Number. 49. To check the structure of a wing.
Option A. ultrasound
NDT is used.
Option B. high
voltage X-rays are used.
Option C. low
voltage X-rays are used.
Correct Answer is. high
voltage X-rays are used.
Explanation. BL/8-4
2.1.6.
Question Number. 50. Which of the following NDT methods
requires that the orientation (or direction) of the defect be known before the
test can commence?.
Option A. Ultrasonic
and Dye Penetrant.
Option B. Magnetic
Particle and Ultrasonic.
Option C. X-Ray
and Magnetic Particle.
Correct Answer is. Magnetic
Particle and Ultrasonic.
Explanation. Leaflet
4-5 1.2.
Question Number. 51. Which of the following defects could not
be detected by Eddy Current NDT inspection?.
Option A. A
crack in a glass fibre reinforced plastic cowl.
Option B. A
crack in a magnesium alloy wheel casting.
Option C. Heat
damage of a Haynes Alloy turbine blade.
Correct Answer is. A
crack in a glass fibre reinforced plastic cowl.
Explanation. BL/8-8
2.
Question Number. 52. Which of the following methods could be
used to detect the presence of tiny drops of Mercury in a large area of
aircraft hull structure after an accident with a mercury thermometer?.
Option A. X-Ray.
Option B. Magnetic
Particle.
Option C. Ultrasonic.
Correct Answer is. X-Ray.
Explanation. NIL.
Question Number. 53. Which of the following NDT methods
requires that the surface of the test piece is cleaned down to bare metal?.
Option A. Eddy
Current.
Option B. Magnetic
Particle.
Option C. Dye-penetrant.
Correct Answer is. Dye-penetrant.
Explanation. Leaflet
4-2 2.1.
Question Number. 54. When using the colour contrast NDT.
Option A. the
surface paint should be removed.
Option B. the
surface should be lightly scuffed.
Option C. the
surface should be bead blasted.
Correct Answer is. the
surface paint should be removed.
Explanation. Leaflet
4-2 2.1.
Question Number. 55. When using dye penetrant field kit,
removal of excess penetrant is done by applying the solvent by.
Option A. spraying
once direct on the part.
Option B. spraying
twice direct on the part.
Option C. using
a lint free cloth.
Correct Answer is. using
a lint free cloth.
Explanation. Leaflet
4-2 5.3.
Question Number. 56. Liquid penetrant tests can be used to
detect.
Option A. internal
porosity in castings.
Option B. corrosion
wall thinning in pipes and tubes.
Option C. fatigue
cracks in magnesium alloy parts.
Correct Answer is. fatigue
cracks in magnesium alloy parts.
Explanation. CAAIP
Leaflet 4-2 2.3.
Question Number. 57. Water-washable liquid penetrants differ
from Post-emulsification penetrants in that they.
Option A. do not
need an emulsifier added.
Option B. need
not be removed from surfaces prior to development.
Option C. can
only be used on aluminium alloys.
Correct Answer is. do
not need an emulsifier added.
Explanation. BL/8-2
1.3.
Question Number. 58. When using a post-emulsification
penetrant, the timing is most critical during.
Option A. penetrant
removal.
Option B. emulsification.
Option C. penetration.
Correct Answer is. emulsification.
Explanation. BL/8-7
para 4.2.
Question Number. 59. A liquid penetrant test cannot.
Option A. be
used on porous materials.
Option B. locate
sub-surface discontinuities.
Option C. be
used on non-metallic surfaces.
Correct Answer is. locate
sub-surface discontinuities.
Explanation. Leaflet
4-2, A&P Technician General Textbook 12-4 Pg 448 Para 3 (B).
Question Number. 60. Hot air drying of articles during liquid
penetrant testing is carried out at a temperature of.
Option A. 75°F.
Option B. 250°F.
Option C. 130°F.
Correct Answer is. 130°F.
Explanation. Leaflet
4-2 5.4.3. There is no reference in old CAIP S.
Question Number. 61. To check the structure of a wing, which
NDT is used?.
Option A. Radiographic.
Option B. Dye
penetrant.
Option C. Magnetic
Flaw.
Correct Answer is. Radiographic.
Explanation. NIL.
Question Number. 62. Magnetic Flux detection will show defects
which are.
Option A. transverse
to the flux direction only.
Option B. longitudinal
to the flux direction only.
Option C. longitudinal
and transverse to the flux direction.
Correct Answer is. transverse
to the flux direction only.
Explanation. Leaflet
4-7 2.2.
Question Number. 63. A hairline crack would show up on a dye
penetrant inspection as.
Option A. a
continuous line of small dots.
Option B. a thin
broken line or chain.
Option C. a
group of dots spread over a wide area.
Correct Answer is. a
continuous line of small dots.
Explanation. Leaflet
4-2 7.4.
Question Number. 64. When carrying out an ultrasonic
inspection, what is the gel used for?.
Option A. To
create a good sonic coupling between the the probe and the test piece.
Option B. To
reduce the friction between the probe and the test piece.
Option C. To
prevent the test piece from becoming scratched by the probe.
Correct Answer is. To
create a good sonic coupling between the the probe and the test piece.
Explanation. Leaflet
4-5 3.4.
Question Number. 65. Fluorescent dye penetrant is suited for
what materials?.
Option A. Non
magnetic non-ferrous materials.
Option B. Ferrous
magnetic materials.
Option C. Plastics
and non magnetic materials.
Correct Answer is. Non
magnetic non-ferrous materials.
Explanation. Leaflet
4-3 1.2. CAIP S BL/8-7.
Question Number. 66. In film radiography, image quality
indicators (IQI) are usually placed.
Option A. between
the intensifying screen and the film.
Option B. on the
film side of the object.
Option C. on the
source side of the test object.
Correct Answer is. on
the source side of the test object.
Explanation. BL/8-4
3.3.1.
Question Number. 67. Which type crack will probably cause the
most build-up in the magnetic particle indicating medium?.
Option A. Grinding.
Option B. Shrink.
Option C. Fatigue.
Correct Answer is. Fatigue.
Explanation. A&P
Mechanics General Handbook Pg.473.
Question Number. 68. When using dye penetrant NDT on a tank,
the penetrant should be applied.
Option A. on the
inside, with developer on the inside.
Option B. on the
outside, with developer on the outside.
Option C. on the
inside, with developer on the outside.
Correct Answer is. on
the inside, with developer on the outside.
Explanation. BL/8-2
9.
Question Number. 69. To detect a fault with magnetic particle
flaw detection, the test requires.
Option A. two
passes in any direction.
Option B. one
pass in any direction.
Option C. two
passes at 90 degrees to each other.
Correct Answer is. two
passes at 90 degrees to each other.
Explanation. BL/8-5
2.1.
Question Number. 70. The substance used in ultrasound
inspection is.
Option A. a
couplant to allow sound waves to travel.
Option B. a
cleaning agent to keep the components clean.
Option C. a
developer.
Correct Answer is. a
couplant to allow sound waves to travel.
Explanation. Leaflet
4-5 4.5.2 BL/8-3 3.3.
Question Number. 71. Dye penetrant defects are marked using.
Option A. crayon,
unless used in a highly stresses area.
Option B. pencil.
Option C. chalk.
Correct Answer is. crayon,
unless used in a highly stresses area.
Explanation. Leaflet
4-3 5.4BL/8-2 7.5.
Question Number. 72. A pressure vessel of thickness 1/16 inch
to 1/8 inch is being tested with dye penetrant. The penetrant should be left
for.
Option A. 3
times longer than normal.
Option B. less
than normal.
Option C. the
same length of time as normal.
Correct Answer is. 3
times longer than normal.
Explanation. Leaflet
4-2 9.2.
Question Number. 73. Which of the following NDT techniques
cannot be used on a component manufactured from austenitic stainless steel?.
Option A. Penetrant
dye.
Option B. Magnetic
particle.
Option C. Hot
oil and chalk.
Correct Answer is. Magnetic
particle.
Explanation. Austenitic
Stainless Steel is non-magnetic.
Question Number. 74. The dye penetrant field test kit consists
of cans of.
Option A. penetrant,
cleaner, developer and a brush.
Option B. spray
penetrant, spray cleaner and spray developer.
Option C. penetrant,
cleaner and developer.
Correct Answer is. spray
penetrant, spray cleaner and spray developer.
Explanation. NIL.
Question Number. 75. The liquid applied to a component being
checked by magnetic particle inspection is for.
Option A. acting
as a transmission medium for the test.
Option B. to
prevent corrosion occurring from contact with the probe.
Option C. to
prevent scratching of the surface by the probe.
Correct Answer is. acting
as a transmission medium for the test.
Explanation. NIL.
Question Number. 76. Which is the preferred method of test for
aluminium alloy alloy?.
Option A. Electroflux.
Option B. Magnaflux.
Option C. Ultrasonic.
Correct Answer is. Ultrasonic.
Explanation. NIL.
Question Number. 77. A composite flap panel has corrosion.
What NDT method will you use to detect?.
Option A. Low
voltage x-ray.
Option B. Coin
tap test.
Option C. High
voltage x-ray.
Correct Answer is. Low
voltage x-ray.
Explanation. Leaflet
6-9 Appendix 1 Paragraph 4.
Question Number. 78. The eddy current method of flaw detection
can detect.
Option A. sub
surface flaws only.
Option B. surface
flaws and those just beneath the surface.
Option C. surface
flaws only.
Correct Answer is. surface
flaws and those just beneath the surface.
Explanation. Leaflet
4-8.
Question Number. 79. With dye penetrant how is the developer
applied?.
Option A. Using
a tank.
Option B. As an
even layer of chalk applied over the area.
Option C. At a
distance of 10 to 12 inches with several passes.
Correct Answer is. At
a distance of 10 to 12 inches with several passes.
Explanation. Leaflet
4-2 6.
Question Number. 80. When using the dye penetrant method crack
detection, the indications on a short, deep crack are.
Option A. single
dots.
Option B. circles.
Option C. long
chain.
Correct Answer is. single
dots.
Explanation. Leaflet
4-2 7.
Question Number. 81. A deep internal crack in a structural
steel member is detected by.
Option A. x-ray
or ultrasonic process.
Option B. fluorescent
penetrant method.
Option C. magnetic
flaw method.
Correct Answer is. x-ray
or ultrasonic process.
Explanation. Leaflet
4-6.
Question Number. 82. The ultrasonic method of crack detection
can be used on.
Option A. surface
and subsurface defects on all metals.
Option B. surface
and subsurface defects on ferrous metals only.
Option C. subsurface
defects on all metals.
Correct Answer is. surface
and subsurface defects on all metals.
Explanation. leaflet
4-5 1.1 and 4.2.2.
Question Number. 83. Porosity in cast materials.
Option A. only
occurs on the surface.
Option B. is
only detectable on the surface.
Option C. is
detectable as a surface or sub surface defect.
Correct Answer is. is
detectable as a surface or sub surface defect.
Explanation. NIL.
Question Number. 84. When using the fluorescent ink flaw
detection method, the component should be inspected using an.
Option A. ultraviolet
lamp.
Option B. infrared
lamp.
Option C. ordinary
lamp and special glasses.
Correct Answer is. ultraviolet
lamp.
Explanation. Leaflet
4-3 1.5.
Question Number. 85. When using the dye penetrant method of
crack detection, it should not normally be used at temperatures.
Option A. above
20°C.
Option B. below
0°C.
Option C. above
15°C.
Correct Answer is. below
0°C.
Explanation. Leaflet
4-2 4.2.
Question Number. 86. When using the dye penetrant method, the
part should be kept wet with the penetrant for.
Option A. 5
minutes.
Option B. 15
minutes.
Option C. up to
one hour.
Correct Answer is. up
to one hour.
Explanation. Leaflet
4-2 4.1.
Question Number. 87. What NDT would you carry out on aluminium
alloy?.
Option A. Electroflux.
Option B. Magnetic
flaw.
Option C. Ultrasonic.
Correct Answer is. Ultrasonic.
Explanation. NIL.
18d. Disassembly, Inspection, repair and Assembly
Techniques.
Question Number. 1. Where would you disconnect a chain?.
Option A. At a
bolted joint.
Option B. At an
riveted joint.
Option C. At a
spring clip joint.
Correct Answer is. At
a bolted joint.
Explanation. CAIP S
EEL/ 3-1 Para 8-3-1 (b) & CAAIP S Leaflet 5-4 3.4.
Question Number. 2. How many times can a locking plate be
used?.
Option A. 3
times, then discarded.
Option B. indefinitely
providing it is a good fit around the component to be locked.
Option C. once,
then discarded.
Correct Answer is. indefinitely
providing it is a good fit around the component to be locked.
Explanation. CAAIP S
Leaflet 2-5 5.1.
Question Number. 3. A hi-lock collar should be.
Option A. not
lubed or washed because they are lubed at manufacture.
Option B. washed
in solvent before fitting.
Option C. lubricated
before fitting.
Correct Answer is. not
lubed or washed because they are lubed at manufacture.
Explanation. NIL.
Question Number. 4. When drilling out a rivet, use a drill.
Option A. larger
than the hole.
Option B. same
size as the hole.
Option C. smaller
than the hole.
Correct Answer is. same
size as the hole.
Explanation. CAAIP S
Leaflet 6-4 3.7.1 says 'drill equal in diameter than that of the rivet', but
CAIP S BL/6-29 para 10.1 says 'slightly smaller'. We chose the former, because
it is current. Also A&P Technician Airframe Textbook 2-67.
Question Number. 5. When riveting two dissimilar sheets of
metal together the joint should be protected with.
Option A. jointing
compound.
Option B. paint.
Option C. grease.
Correct Answer is. jointing
compound.
Explanation. NIL.
Question Number. 6. The maximum temperature for Nyloc nuts
is.
Option A. 120°C.
Option B. 100°C.
Option C. 160°C.
Correct Answer is. 120°C.
Explanation. NIL.
Question Number. 7. What type of rivet would you use when
there is access to only one side of the work?.
Option A. Blind.
Option B. Pop.
Option C. Hilok.
Correct Answer is. Blind.
Explanation. CAIP S
BL/6-28.
Question Number. 8. Torque loading is carried out to
provide.
Option A. as
tight a joint as possible.
Option B. sufficient
clamping without over-stressing.
Option C. flexibility.
Correct Answer is. sufficient
clamping without over-stressing.
Explanation. NIL.
Question Number. 9. What is generally the best procedure to
use when removing a solid shank rivet?.
Option A. Drill
through the manufactured head and shank with a drill one size smaller than the
rivet and remove the rivet with a punch.
Option B. Drill
through the manufactured head and shank with a shank size drill and remove the
rivet with a punch.
Option C. Drill
to the base of the manufactured rivet head with a drill one size smaller than
the rivet shank and remove the rivet with a punch.
Correct Answer is. Drill
to the base of the manufactured rivet head with a drill one size smaller than
the rivet shank and remove the rivet with a punch.
Explanation. CAAIP S
Leaflet 6-4 3.7.1 says 'drill equal in diameter than that of the rivet', but
CAIP S BL/6-29 para 10.1 says 'slightly smaller'. Both documents say 'to the
base of the head only'.
Question Number. 10. What action is taken with a common
circlip removed from a component?.
Option A. It is
replaced with a new item on assembly.
Option B. It is
checked for springiness.
Option C. It is
examined for distortion.
Correct Answer is. It
is checked for springiness.
Explanation. NIL.
Question Number. 11. The maximum bolt diameter for which a
1/16 split pin may be used is.
Option A. 7/16.
Option B. 1/4.
Option C. 3/8.
Correct Answer is. 3/8.
Explanation. Leaflet
2-5 table 1.
Question Number. 12. Why is a shouldered stud used?.
Option A. To
provide a rigid assembly.
Option B. To
decrease weight without loss of strength.
Option C. As a
replacement for a damaged stud.
Correct Answer is. To
provide a rigid assembly.
Explanation. NIL.
Question Number. 13. A thread insert is removed by.
Option A. once
fitted, a thread insert must not be removed.
Option B. using
a drill the major diameter of the thread insert.
Option C. a
special drill provided by the thread insert manufacturer.
Correct Answer is. a
special drill provided by the thread insert manufacturer.
Explanation. NIL.
Question Number. 14. When fitting Rivnuts into position, how
are they secured and prevented from rotating?.
Option A. Locknut
at the rear.
Option B. A
locating key.
Option C. Peened.
Correct Answer is. A
locating key.
Explanation. Jeppesen
A&P Airframe Technician Textbook Page 2-48.
Question Number. 15. Hi-loks are installed with the.
Option A. thread
and shank not lubricated.
Option B. shank
lubricated when fitting.
Option C. thread
lubricated when fitting.
Correct Answer is. thread
and shank not lubricated.
Explanation. The
threads are lubricated at manufacture - not during fitting.
Question Number. 16. A jury strut is one giving.
Option A. a
temporary support.
Option B. a part
of the structure that takes only tensile loads.
Option C. additional
support to a stressed area.
Correct Answer is. a
temporary support.
Explanation. CAIP S
AL/7-14 Para 2-3-5.
Question Number. 17. Which type of repair has to be used where
the damage is large and lost strength of the area has to be restored?.
Option A. Filling
plate and patch.
Option B. Patch
repair to the punctured skin.
Option C. Insert
and butt strap.
Correct Answer is. Insert
and butt strap.
Explanation. NIL.
Question Number. 18. Which of the following actions would be
taken to fit a locking device to a nut or bolt, if the correct torque has been
reached but the locking device will not fit?.
Option A. Tighten
further until device fits.
Option B. File
the base of the nut.
Option C. Change
the nut or bolt for one that will achieve the desired condition.
Correct Answer is. Change
the nut or bolt for one that will achieve the desired condition.
Explanation. BL/6-30
para 3.3.
Question Number. 19. In the Push-pull tube linkage used in
aircraft flying control systems, how is the length of the tube adjusted?.
Option A. Fit
anew push-pull tube.
Option B. By
adjusting end fittings at each end of the tube.
Option C. It is
fixed and does not require adjusting.
Correct Answer is. By
adjusting end fittings at each end of the tube.
Explanation. NIL.
Question Number. 20. Spotfacing is done to.
Option A. provide
a flat area on a rough surface.
Option B. compensate
for height in lieu of a spring washer.
Option C. provide
a good surface for welding.
Correct Answer is. provide
a flat area on a rough surface.
Explanation. NIL.
Question Number. 21. When fitting a hydraulic component, the
hydraulic seal should be lubricated with.
Option A. with a
specified hydraulic oil.
Option B. grease.
Option C. the
same fluid that is used in the hydraulic system (e.g. skydrol).
Correct Answer is. the
same fluid that is used in the hydraulic system (e.g. skydrol).
Explanation. Hydraulic
seals are lubricated with the same hydraulic fluid that they are used with.
Question Number. 22. A gap in a firewall can be plugged by.
Option A. an
aluminium plate.
Option B. a
fireproof bung or bush.
Option C. a
plastic bung.
Correct Answer is. a
fireproof bung or bush.
Explanation. A gap
in a firewall must be filled with approved fireproof material.
Question Number. 23. In a critically bolted joint.
Option A. a PLI
washer can be used more than once only with self locking nuts.
Option B. a PLI
washer can be affected by thread lubricant.
Option C. a PLI
washer can only be used once.
Correct Answer is. a
PLI washer can only be used once.
Explanation. CAIP
AL/7-8 4.5.3.
Question Number. 24. Which of the following jointing compounds
should not be used in the vicinity of a joint where the temperature may exceed
200°C?.
Option A. DTD
900.
Option B. DTD
200.
Option C. DTD
369.
Correct Answer is. DTD
369.
Explanation. CAIP S
AL/7-8 3.4.
Question Number. 25. Why is jointing compound applied to the
surfaces of material being joined together prior to riveting?.
Option A. To act
as a sealant and prevent filiform corrosion.
Option B. To
inhibit electrolytic action.
Option C. To
prevent swarf damage.
Correct Answer is. To
inhibit electrolytic action.
Explanation. CAIP S
BL/6-29.
Question Number. 26. A metallic stiff nut.
Option A. cannot
be torque loaded.
Option B. cannot
be used in areas in excess of 250oC.
Option C. is pre
lubricated and does not need lubricating.
Correct Answer is. cannot
be used in areas in excess of 250oC.
Explanation. Leaflet
3-4 4.2.3 (assuming it means HTS cad plated and not CRS, but a and b are not
correct anyway).
Question Number. 27. How do you prevent earth loops forming on
screened cables?.
Option A. Do not
earth the screen.
Option B. Earth
both ends of the screen.
Option C. Earth
one end of the screen.
Correct Answer is. Earth
one end of the screen.
Explanation. Electromagnetic
Compatibility. Earth one end of the screen.
Question Number. 28. When fitting a shackle pin, fit with.
Option A. head
uppermost.
Option B. 0.020.
Option C. a
shake-proof washer under the head.
Correct Answer is. head
uppermost.
Explanation. The
heads of all fasteners should be uppermost where possible.
Question Number. 29. The threads on a stud.
Option A. are of
opposite hand at each end of the plain of portion.
Option B. are of
the same hand at each end of the plain portion.
Option C. are
continuous throughout its length and there is no plain portion.
Correct Answer is. are
of the same hand at each end of the plain portion.
Explanation. The
threads on a stud are the same hand at each end of the plain portion.
Question Number. 30. The angle between starts on a double
start thread is.
Option A. 180
degrees.
Option B. 120
degrees.
Option C. 90
degrees.
Correct Answer is. 180
degrees.
Explanation. NIL.
Question Number. 31. What does 18N and contiguous circles on
the head of a bolt indicate?.
Option A. 1.8
inch threaded portion and plain shank 1/2 inch UNF.
Option B. 1.8
inch nominal length 1/2 inch BSF.
Option C. 1.8
inch plain shank 1/2 inch UNF.
Correct Answer is. 1.8
inch plain shank 1/2 inch UNF.
Explanation. Leaflet
3-3 2.3.4. BL/2-3 2.1.2.
Question Number. 32. A UNF bolt is indicated by.
Option A. a
triangle on the head.
Option B. 2-3
rings on the head.
Option C. green
dye.
Correct Answer is. 2-3
rings on the head.
Explanation. CAAIP
Leaflet 3-3 2.3.4 (a).
18e. Disassembly, Inspection, repair and Assembly
Techniques.
Question Number. 1. Immediately after carrying out an
insulation check, which of the following applies?.
Option A. A
continuity check must be carried out before switching on the circuit for the
first time.
Option B. The
readings observed and the atmospheric conditions at the time should be noted
and compared to previous readings.
Option C. The
observed readings should be noted and an independent check carried out by
another engineer.
Correct Answer is. The
readings observed and the atmospheric conditions at the time should be noted
and compared to previous readings.
Explanation. Leaflet
9-1 4.5.3. EEL / 1-6 Para 4-5-3.
Question Number. 2. An Insulation test is carried out on a
group of cables and a low reading obtained. What action would you take?.
Option A. A low
reading would be expected because the cables are in parallel.
Option B. Change
or renew all the cables involved in the test.
Option C. Break
the circuit down and carry out further checks.
Correct Answer is. Break
the circuit down and carry out further checks.
Explanation. EEL /
1-6 Para 4-4-2 & Leaflet 9-1 4.4.2.
Question Number. 3. BITE systems to be used on the ground
only are deactivated by.
Option A. on
take off.
Option B. the
parking break.
Option C. by the
undercarriage retraction.
Correct Answer is. on
take off.
Explanation. A
proximity switch on the undercarriage will signal a computer (Airbus) or a
Proximity Sensor Control Unit (Boeing). This signal is then sent to all
appropriate units.
Question Number. 4. After the normal function test of an
individual circuit has been completed and the circuit switched off.
Option A. a
second function test must be carried out to verify the first.
Option B. the
fuse should be removed and the circuit again switched on to check the isolation
of the circuit concerned.
Option C. a
duplicate check must be carried out in accordance with AWN 3.
Correct Answer is. the
fuse should be removed and the circuit again switched on to check the isolation
of the circuit concerned.
Explanation. CAIP S
EEL/1-6 Para 4-6-3.
Question Number. 5. A millivolt drop check is to be carried
out on a heavy duty relay. The Millivoltmeter would be connected to the relay.
Option A. when
contacts closed and power is on.
Option B. when
contacts open and power off.
Option C. when
contacts are open and power is on.
Correct Answer is. when
contacts closed and power is on.
Explanation. Leaflet
9-1 Para.4.3.
Question Number. 6. Electrical cables installed on
aircraft. What is used to indicate a fault?.
Option A. Bonding
test.
Option B. Continuity
test.
Option C. Resistance
test.
Correct Answer is. Continuity
test.
Explanation. CAAIP S
Leaflet 9-1, 4.2.1.
Question Number. 7. When checking resistance of a cable to
the starter motor what test is carried out?.
Option A. Millivolt
drop test.
Option B. Safety
Ohmmeter.
Option C. Time
Domain Reflectometer.
Correct Answer is. Millivolt
drop test.
Explanation. NIL.
19a. Abnormal Events.
Question Number. 1. When inspecting an aircraft after a
lightning strike, you should observe.
Option A. entry
damage.
Option B. all
signs of burning.
Option C. entry
and exit damage.
Correct Answer is. all
signs of burning.
Explanation. AL/7-1
5.4.
Question Number. 2. To ensure protection against HIRF
affecting audio and navigation aids.
Option A. ensure
that all audio and navigation equipment is adequately screened.
Option B. inspect
and check all bonding leads to ensure their serviceability and replace if
defective.
Option C. ensure
that the correct number of static wicks are fitted.
Correct Answer is. ensure
that all audio and navigation equipment is adequately screened.
Explanation. Understanding
HIRF By Gerald L. Fuller.
Question Number. 3. Which of the following is a preventive
process against HIRF?.
Option A. Monitoring
HIRF on the communication system.
Option B. Visual
inspections.
Option C. Periodically
checking aircraft bonding.
Correct Answer is. Visual
inspections.
Explanation. Understanding
HIRF By Gerald L. Fuller.
Question Number. 4. How do you prevent aquaplaning during
landing?.
Option A. Reduce
flare.
Option B. Use
reverse thrust.
Option C. Put
flaps up.
Correct Answer is. Use
reverse thrust.
Explanation. Aquaplaning
is caused by excessive speed on a wet runway. Reverse thrust slows the aircraft
and allows the wheels to continue turning (rather than 'planing' which they do
if they are locked by the brakes).
Question Number. 5. Skin wrinkling on the lower surface of
a wing is caused by.
Option A. hogging.
Option B. tension.
Option C. sagging.
Correct Answer is. hogging.
Explanation. NIL.
Question Number. 6. After a report of flight through heavy
turbulence, you would.
Option A. check
the aircraft symmetry.
Option B. carry
out a major overhaul.
Option C. not
carry out any checks.
Correct Answer is. check
the aircraft symmetry.
Explanation. CAAIP S
Leaflet 6-3.
Question Number. 7. After a heavy landing you should check.
Option A. engine
compressor shaft alignment.
Option B. engine
thrust alignment.
Option C. engine
module alignment.
Correct Answer is. engine
thrust alignment.
Explanation. Leaflet
6-3 2.8 (b)©.
Question Number. 8. A lightning strike on an aircraft would
show.
Option A. the
entry and exit point.
Option B. the
entry point only.
Option C. the
exit point only.
Correct Answer is. the
entry and exit point.
Explanation. NIL.
Question Number. 9. When an engine is not in direct
electrical contact with its mounting, how should it be bonded?.
Option A. With
at least one primary conductor.
Option B. With
at least two primary conductors on one side of the engine.
Option C. With
at least two primary conductors, one each side of the engine.
Correct Answer is. With
at least two primary conductors, one each side of the engine.
Explanation. Leaflet
9-1 3.5.9. EEL/1-6 Para 3.5.7.
Question Number. 10. On a composite aircraft, large items are
bonded.
Option A. by use
of large copper strips.
Option B. Don't
need to be bonded because they are made of an insulating material.
Option C. by
primary bonding leads attached to a cage.
Correct Answer is. by
primary bonding leads attached to a cage.
Explanation. Leaflet
9-1 3.4.2.
Question Number. 11. HIRF interference occurs when.
Option A. in use
on mid frequencies.
Option B. in use
on low frequencies.
Option C. in use
on all frequencies.
Correct Answer is. in
use on all frequencies.
Explanation. HIRF is
a problem from 10kHz - 18GHz (Civil-40 GHz Military) Understanding HIRF By
Gerald L. Fuller.
Question Number. 12. Non metallic parts of the aircraft.
Option A. do not
require to be bonded because they are non conductive.
Option B. must
be bonded by bonding leads.
Option C. must
be bonded by application of conductive paint.
Correct Answer is. must
be bonded by application of conductive paint.
Explanation. Leaflet
9-1 Para.3.4.4.
Question Number. 13. Whenever possible a functional test
should be carried out on an aircraft using which power supply?.
Option A. The
aircraft battery.
Option B. The
aircraft generators.
Option C. An
external supply.
Correct Answer is. An
external supply.
Explanation. Leaflet
9-1 4.6.1.
Question Number. 14. How many primary bonding conductors are
required on an engine?.
Option A. 1
only.
Option B. 2 on
one side.
Option C. 1 on
each side.
Correct Answer is. 1
on each side.
Explanation. Leaflet
9-1 Para 3.5.9 and EEL/1-6 Para.3.5.9.
Question Number. 15. What is the primary purpose of bonding of
metallic parts of an aircraft?.
Option A. To
provide a return path for electrical two-wire system.
Option B. To
prevent high potential differences between metallic parts from building up.
Option C. To
prevent lightening strikes.
Correct Answer is. To
prevent high potential differences between metallic parts from building up.
Explanation. Leaflet
9-1 3.2.
Question Number. 16. In order to maintain HIRF protection,
bonding checks between airframe and electrical components carrying voltages
greater than 50V RMS or dc should not exceed.
Option A. 0.05
ohm.
Option B. 1 ohm.
Option C. 1 M
ohm.
Correct Answer is. 1
ohm.
Explanation. Leaflet
9-1 3.8 table 1CAIP S EEL/1-6 Para 3.8 Table 1.
Question Number. 17. Ribbon cables affected by mutual
impedance and current loop leakage should be protected by.
Option A. earthing
each alternate conductor to separate points.
Option B. connecting
all conductors to a common earth.
Option C. shielding
each individual conductor.
Correct Answer is. earthing
each alternate conductor to separate points.
Explanation. NIL.
19b. Abnormal Events.
Question Number. 1. An aircraft with under-wing mounted
engines has a heavy landing, where would you expect to see wrinkling of the
skins?.
Option A. Bottom
skin caused by engine inertia.
Option B. Top
skin only.
Option C. On the
top and bottom skins.
Correct Answer is. On
the top and bottom skins.
Explanation. Leaflet
6-3 2.6 (a) and AL/7-1 Para 2-6 (a).
Question Number. 2. Which of the following could be a
primary cause of HIRF protection failure?.
Option A. Corrosion
on bonding leads.
Option B. Broken
or missing static wicks.
Option C. Unserviceable
radio filters.
Correct Answer is. Unserviceable
radio filters.
Explanation. Understanding
HIRF By Gerald L. Fuller.
Question Number. 3. What is the reason for a primary
bonding connection’s large cross-sectional area?.
Option A. To
carry the static discharge current to the conducting nose wheel.
Option B. To
carry lightening discharge current should the need arise.
Option C. To
maintain the airframe at the same potential throughout.
Correct Answer is. To
carry lightening discharge current should the need arise.
Explanation. CAAIP S
leaflet 9-1 3.3.1 Jeppesen A&P Mechanics Handbook Pg.452.
Question Number. 4. When an aircraft has been struck by
lightning.
Option A. control
surface bearings and hinges should be checked for stiffness in operation.
Option B. control
surface freedom of movement need not be checked provided skin punctures are
less than 3/16 inch diameter.
Option C. control
surface freedom of movement need not be checked providing the bonding is
undamaged.
Correct Answer is. control
surface bearings and hinges should be checked for stiffness in operation.
Explanation. Leaflet
6-3 6.4 CAIP S AL/7-1 5.4.
Question Number. 5. On an aircraft which has had a heavy
landing, on the lower wing you may see.
Option A. sagging.
Option B. hogging.
Option C. wrinkling.
Correct Answer is. wrinkling.
Explanation. Leaflet
6-3 para.2.6.
Question Number. 6. After a reported lightning strike.
Option A. the
flight controls should be checked for full and free movement before the next
flight.
Option B. the
flight controls need to be checked for full and free movement only if a bonding
lead to one of the control surfaces is found to be burned or broken.
Option C. the
aircraft and its systems must have a major overhaul before the next flight.
Correct Answer is. the
flight controls should be checked for full and free movement before the next
flight.
Explanation. NIL.
20. Maintenance Procedures.
Question Number. 1. Mandatory Warning Plaques and symbols.
Option A. must
be displayed on all flights.
Option B. must
be displayed in the cabin only if they are legible.
Option C. need
not be displayed if they are incorporated in the flight manual.
Correct Answer is. must
be displayed on all flights.
Explanation. NIL.
Question Number. 2. Following a major defect the C of A.
Option A. is not
affected, however may run out on a time basis.
Option B. will
be invalidated and needs renewing.
Option C. Nothing
will happen.
Correct Answer is. is
not affected, however may run out on a time basis.
Explanation. NIL.
Question Number. 3. When storing parts you should use.
Option A. monitor
the temperature.
Option B. silica
gel.
Option C. place
in a sealed container.
Correct Answer is. silica
gel.
Explanation. CAAIP S
Leaflet 1-8 2.2.3.
Question Number. 4. ATA specification 100 is.
Option A. the
procedures which must be complied with before an aircraft can be given a
Certificate of Airworthiness in the Transport Category (Passenger).
Option B. the
International standardization of maintenance manuals, illustrated parts
catalogues, overhaul and repair manuals, service bulletins and letters.
Option C. the
American FAA specification controlling the manufacture of aluminium and its
alloys.
Correct Answer is. the
International standardization of maintenance manuals, illustrated parts
catalogues, overhaul and repair manuals, service bulletins and letters.
Explanation. Jeppesen
A&P General Textbook 14-12.
Question Number. 5. An aircraft should carry at least the
following number of spare fuses:.
Option A. 10.
Option B. 3.
Option C. 3 or
10%, whichever is greater.
Correct Answer is. 3
or 10%, whichever is greater.
Explanation. ANO
Schedule 4.
Question Number. 6. Maintenance Schedules are issued.
Option A. in a
folder with the operators name on the cover.
Option B. with
an approval certificate by the CAA.
Option C. by the
operator with CAA approval.
Correct Answer is. by
the operator with CAA approval.
Explanation. BCAR
A/B 6-2 Para. 3.4.
Question Number. 7. After a mandatory inspection has been
carried out by a Licensed Engineer, what is issued.
Option A. a
Certificate of Maintenance Review.
Option B. Certificate
of Release to Service.
Option C. a
Flight Release Certificate.
Correct Answer is. Certificate
of Release to Service.
Explanation. NIL.
Question Number. 8. A hard time engine inspection involves.
Option A. replacement
with a new or overhauled component.
Option B. an
in-situ function test.
Option C. removal
of an engine component, its inspection and refitting.
Correct Answer is. replacement
with a new or overhauled component.
Explanation. Leaflet
1-7 2.2.1.
Question Number. 9. Who approves Maintenance Manuals?.
Option A. The
CAA.
Option B. The
Department of Trade and Industry.
Option C. The
Board of Trade.
Correct Answer is. The
CAA.
Explanation. NIL.
Question Number. 10. A Certificate of Release to Service must
be issued after.
Option A. a
repair has been carried out in accordance with an approved repair scheme.
Option B. a
re-fuel has been done.
Option C. engine
runs.
Correct Answer is. a
repair has been carried out in accordance with an approved repair scheme.
Explanation. NIL.
Question Number. 11. If the operator varies the content of the
maintenance schedule, what action must be taken?.
Option A. Amend
the Maintenance Schedule and seek the CAA approval.
Option B. Await
CAA approval before amending the Maintenance Schedule.
Option C. Amend
the Maintenance Schedule.
Correct Answer is. Await
CAA approval before amending the Maintenance Schedule.
Explanation. NIL.
Question Number. 12. When is an EASA Permit to Fly conditions
required?.
Option A. To
allow an unregistered aircraft to fly for air test.
Option B. To
allow an aircraft to fly on air test to check out a modification.
Option C. After
a Certificate of Maintenance Review has been signed.
Correct Answer is. To
allow an aircraft to fly on air test to check out a modification.
Explanation. NIL.
Question Number. 13. When there is an overlap of
responsibility, how is the CRS signed?.
Option A. Appropriate
Type Rated Licensed Aircraft Engineers must each certify the parts appropriate
to their license coverage.
Option B. Only
one appropriate Type Rated Licensed Aircraft Engineer may sign the CRS as he
assumes responsibility for the operation, the other engineers must sign the
paperwork.
Option C. An
appropriate Type Rated Licensed Aircraft Engineer and an ATPL holder sign the
CRS when the aircraft is away from base.
Correct Answer is. Appropriate
Type Rated Licensed Aircraft Engineers must each certify the parts appropriate
to their license coverage.
Explanation. AWN 3.
Question Number. 14. Information contained in the ANO is.
Option A. of a
legal nature in all sections and is therefore mandatory.
Option B. of a
mandatory nature where safety is concerned.
Option C. written
in compliance of the Civil Aviation Act of 1943 ratifying the ICAO Convention.
Correct Answer is. of
a legal nature in all sections and is therefore mandatory.
Explanation. NIL.
Question Number. 15. An 'On Condition' Inspection involves.
Option A. a
program of inspections used to increase the life of lifed components.
Option B. an
inspection of a component with a view to continued operation if its condition
warrants such action.
Option C. replacement
of life expired components for new ones.
Correct Answer is. an
inspection of a component with a view to continued operation if its condition
warrants such action.
Explanation. CAIP S
BL/ 1-16 Para 2-2-2.
Question Number. 16. Air Navigation General Regulations are to
be found in.
Option A. Airworthiness
Requirements CAP 455.
Option B. British
Civil Airworthiness Requirements Section A.
Option C. CAA
Printed Manual CAP 393.
Correct Answer is. CAA
Printed Manual CAP 393.
Explanation. CAIP S
BL/1-9 Para 8-11.
Question Number. 17. The information in the ANO is given in
the form of.
Option A. Articles
of Law, some of which are further clarified by Schedules.
Option B. Chapters,
each one dealing with a different aspect of Civil Aviation, these chapters
being backed up by the schedules.
Option C. Regulations,
each one covering a different aspect of Civil Aviation and as such is
mandatory.
Correct Answer is. Articles
of Law, some of which are further clarified by Schedules.
Explanation. CAIP S
BL/1-9 Para 4.
Question Number. 18. British Civil Airworthiness Requirements.
Option A. form
the Technical requirements for the design and operation of aircraft and their
equipment.
Option B. interpret
the ANO and form the Technical requirements for the design.
Option C. are
printed by the CAA and are of an advisory nature.
Correct Answer is. interpret
the ANO and form the Technical requirements for the design.
Explanation. CAIP S
BL/1-9 Para 4-4.
Question Number. 19. A CMR is raised after.
Option A. defect
rectification.
Option B. scheduled
servicing at specified intervals.
Option C. major
overhaul.
Correct Answer is. scheduled
servicing at specified intervals.
Explanation. NIL.
Question Number. 20. Compliance with the ANO is restricted to.
Option A. aircraft
and their equipment which are on the UK Civil Register only.
Option B. aircraft
and their equipment which are on the UK & Commonwealth Civil Registers.
Option C. All
civil aircraft and their equipment on the international Civil Register.
Correct Answer is. aircraft
and their equipment which are on the UK Civil Register only.
Explanation. NIL.
Question Number. 21. A Certificate of Release to service
states that.
Option A. a task
has been carried out in accordance with the ANO.
Option B. an
operator has satisfied the CAA of his competence.
Option C. the
aircraft has been maintained to an approved schedule.
Correct Answer is. a
task has been carried out in accordance with the ANO.
Explanation. NIL.
Question Number. 22. Technical and Administrative information
is officially circulated to L.A.M.E.S. in.
Option A. B.C.A.R.s.
Option B. A.W.N.s.
Option C. CAIP.s.
Correct Answer is. A.W.N.s.
Explanation. NIL.
Question Number. 23. Vital point inspections are carried out.
Option A. after
an area is disturbed.
Option B. on a
'C' check.
Option C. on an
'A' Check.
Correct Answer is. after
an area is disturbed.
Explanation. BCAR
A5-3 para 3 states: VITAL POINTS are any point on an aircraft at which single
mal-assembly could lead to catastrophe.
Question Number. 24. What colour is used to identify a
'primary structure' when using the aircraft Maintenance Manual?.
Option A. Yellow.
Option B. Green.
Option C. Red.
Correct Answer is. Red.
Explanation. NIL.
Question Number. 25. Which of the following NDT methods can be
carried out and certified by a mechanic not approved specifically for NDT inspections.
Option A. Ultrasonic.
Option B. Magnetic
Particle.
Option C. Neither
of the above.
Correct Answer is. Neither
of the above.
Explanation. AWN 3
para 1.7.
Question Number. 26. B.C.A.R’s.
Option A. contain
minimum requirements to be met.
Option B. are
issued by Ministry of Trade and Industry.
Option C. detail
mandatory requirements for aircraft design and construction.
Correct Answer is. contain
minimum requirements to be met.
Explanation. CAIP S
BL / 1-9 Para 6-1.
Question Number. 27. The purpose of the CRS is.
Option A. to
ensure that the log book entry is complete.
Option B. to
turn a log book or job card entry into a legal document and to ensure that the
signatory takes full responsibility for the work done.
Option C. to
comply with article 15 of the ANO which states that an aircraft must not fly
unless it is properly equipped for the intended flight.
Correct Answer is. to
turn a log book or job card entry into a legal document and to ensure that the
signatory takes full responsibility for the work done.
Explanation. AWN 3
para 1.5.
Question Number. 28. Duplicate inspections are.
Option A. inspections
which have to be duplicated but which can finally be certified by one LAE or
approved signatory.
Option B. inspections
certified by one approved signatory or LAE and then certified by a second
approved signatory or LAE.
Option C. inspections
signed by a mechanic and countersigned by an approved signatory or licensed
engineer.
Correct Answer is. inspections
certified by one approved signatory or LAE and then certified by a second
approved signatory or LAE.
Explanation. NIL.
Question Number. 29. When related to aeronautical engineering,
the term 'Inspection' is defined in the publication.
Option A. Airworthiness
Notice (AWN) 3.
Option B. ANO
article 11.
Option C. BCAR
Section L.
Correct Answer is. Airworthiness
Notice (AWN) 3.
Explanation. AWN 3
page 2 para 1.2 (d).
Question Number. 30. The technical laws relating to Civil
Aviation are contained in.
Option A. the
Civil Aircraft Inspection Procedures.
Option B. the
Air Navigation Order.
Option C. the
Civil Aviation Act 1971.
Correct Answer is. the
Air Navigation Order.
Explanation. NIL.
Question Number. 31. Civil aircraft manufactured in the UK are
constructed from parts that have been.
Option A. manufactured
to approved drawings.
Option B. manufactured
by British Aerospace.
Option C. tested
to destruction.
Correct Answer is. manufactured
to approved drawings.
Explanation. NIL.
Question Number. 32. Design drawings of aircraft components
are produced by organisations approved by.
Option A. C.A.A.
in accordance with BCAR.
Option B. British
Standards Institute.
Option C. S.B.A.C.
Correct Answer is. C.A.A.
in accordance with BCAR.
Explanation. CAIP S
BL / 1-4 Para 2.
Question Number. 33. Civil Aircraft Airworthiness Information
Procedures.
Option A. contain
information of a mandatory nature.
Option B. contain
approved inspection schedules.
Option C. are a
guide to the general maintenance of aircraft.
Correct Answer is. are
a guide to the general maintenance of aircraft.
Explanation. NIL.
Question Number. 34. British Civil Airworthiness Requirements.
Option A. specify
the minimum qualifications for aircrew and engineers.
Option B. list
the minimum design requirements for aircraft.
Option C. give
General technical information.
Correct Answer is. list
the minimum design requirements for aircraft.
Explanation. CAIP S
BL / 1-9 Para 6-1.
Question Number. 35. What work has to be recorded and signed
for?.
Option A. Only
work which entails a duplicate inspection.
Option B. Only
work involving replacements.
Option C. All
work carried out.
Correct Answer is. All
work carried out.
Explanation. NIL.
Question Number. 36. Are CAAIP. mandatory?.
Option A. Only
selected parts which are in B.C.A.R.
Option B. Yes,
but only for six months at a time.
Option C. No,
nothing in CAAIPs is mandatory.
Correct Answer is. No,
nothing in CAAIPs is mandatory.
Explanation. NIL.
Question Number. 37. With a serviceable chain not required for
use, how should you store it?.
Option A. Lay
the chain flat in full length , lubricate and wrap in brown paper to exclude
all dirt and moisture.
Option B. Clean,
lubricate, wrap the chain in grease proof paper and suspend.
Option C. Carefully
coil, lubricate, lay flat and wrap in grease proof paper.
Correct Answer is. Carefully
coil, lubricate, lay flat and wrap in grease proof paper.
Explanation. DLeaflet
5-4 6.7. CAIP S AL/3-2 Para 6.7.
Question Number. 38. What is the licensed engineer responsible
for when fitting a new component to an aircraft?.
Option A. That
the paperwork is signed by an approved signatory.
Option B. That
is has a green serviceable tag.
Option C. The
correct part number, the modification state and the serviceability of the
component.
Correct Answer is. The
correct part number, the modification state and the serviceability of the
component.
Explanation. NIL.
Question Number. 39. If an aircraft exceeded the RVSM, when
shall the crew report the incident in the appropriate channels.
Option A. 48
hrs.
Option B. 24
hrs.
Option C. 72
hrs.
Correct Answer is. 72
hrs.
Explanation. Reduced
Vertical Separation Minimum excedance is an 'Incident'. JAR OPS Subpart D.
Para.1.420.
Question Number. 40. If the aircraft is away from base who may
certify the second part of the duplicate inspection?.
Option A. a
pilot with a licence for the aircraft type.
Option B. a
pilot with a licence for any similar aircraft type.
Option C. any
licensed engineer.
Correct Answer is. a
pilot with a licence for the aircraft type.
Explanation. BCAR
A/B 6-2 10.3.9.
Question Number. 41. Block cumulative maintenance means that.
Option A. all
the checks require the same man hour input except for the major inspections.
Option B. each
check usually involves an increased aircraft down time.
Option C. all
the maintenance is carried out in blocks.
Correct Answer is. each
check usually involves an increased aircraft down time.
Explanation. NIL.
Question Number. 42. A separate modification record book is
required for.
Option A. passenger
aircraft exceeding 2730 kgs MTWA.
Option B. all
aircraft.
Option C. passenger
aircraft exceeding 3600 kgs MTWA.
Correct Answer is. passenger
aircraft exceeding 2730 kgs MTWA.
Explanation. BCAR
A/B 7-9 Para.1.3.
Question Number. 43. Sector record pages from the Tech Logs,
must be.
Option A. at
least duplicated.
Option B. retained
for two years from the date of issue.
Option C. retained
for four years from the last effective date.
Correct Answer is. at
least duplicated.
Explanation. BCAR
A/B 7-8 Para.4.1.
Question Number. 44. Minimum equipment to be carried is listed
in.
Option A. JAR
145.
Option B. JAR
OPS.
Option C. JAR
25.
Correct Answer is. JAR
OPS.
Explanation. JAR OPS
subpart K.
Question Number. 45. What should be checked before a licensed
engineer signs a CRS?.
Option A. That
he/she has worked for 6 months on the aircraft type within the previous 2
years.
Option B. That
he/she has worked for 4 months on the aircraft type within the previous 2
years.
Option C. That
he/she has had continuation training within the previous 2 years.
Correct Answer is. That
he/she has worked for 6 months on the aircraft type within the previous 2
years.
Explanation. JAR
145.35 and associated IEM.
Question Number. 46. Rubber components should be stored.
Option A. in a
cool dark area.
Option B. in
warm and humid conditions.
Option C. in a
well lit room.
Correct Answer is. in
a cool dark area.
Explanation. Leaflet
1-8 3.13.1 and 3.13.3.
Question Number. 47. Storage of components to prevent
corrosion is helped.
Option A. by
using silica gel.
Option B. by
wrapping in grease proof paper.
Option C. by
placing them in a plastic box.
Correct Answer is. by
using silica gel.
Explanation. BL/1-7
2.2.3Silica gel (silica dioxide) is a 'desiccant' i.e. it absorbs moisture.
Question Number. 48. Dye penetrant kits should be stored.
Option A. out of
sunlight in a dry place.
Option B. in
direct sunlight to keep it dry.
Option C. in a
dark damp cupboard.
Correct Answer is. out
of sunlight in a dry place.
Explanation. NIL.
Question Number. 49. When receiving new parts it is the
responsibility of the engineer to check.
Option A. it has
a green serviceable label attached.
Option B. it is
of the correct modification state and is serviceable.
Option C. it was
designed to acceptable standards.
Correct Answer is. it
is of the correct modification state and is serviceable.
Explanation. AWN 3.
Question Number. 50. For airworthiness purposes, aircraft
structural parts are graded as.
Option A. primary,
secondary and tertiary.
Option B. class
A, B and C.
Option C. 1, 2
and 3.
Correct Answer is. primary,
secondary and tertiary.
Explanation. Primary,
secondary and tertiary are the three 'structure' classifications.
Question Number. 51. If an unauthorized repair is carried out
Option A. the
aircraft can fly with a Certificate of Fitness for Flight.
Option B. the
Cof A is invalidated until an authorized repair has been done.
Option C. the
Cof A is not invalidated providing a CRS is issued.
Correct Answer is. the
Cof A is invalidated until an authorized repair has been done.
Explanation. NIL.
Question Number. 52. A C.of A. for export.
Option A. does
not give authority by it self for the aircraft to fly.
Option B. gives
authority for the aircraft to fly.
Option C. is
required before aircraft registration in a foriegn country.
Correct Answer is. does
not give authority by it self for the aircraft to fly.
Explanation. NIL.
Question Number. 53. A fitness for flight is issued for an
aircraft after a major modification by.
Option A. the
pilot, type rated on that particular aircraft.
Option B. a
appropriate licensed aircraft engineer.
Option C. a CAA
surveyor or person approved within the CAA.
Correct Answer is. a
appropriate licensed aircraft engineer.
Explanation. NIL.
Question Number. 54. An unauthorised repair has been carried
out.
Option A. sign a
CRS for the repair.
Option B. apply
for it as a modification.
Option C. carryout
an approved repair.
Correct Answer is. carryout
an approved repair.
Explanation. NIL.
Question Number. 55. A Part-66 licensed engineer, when signing
a CRS for a non-Part-145 company would need to have.
Option A. maintenance
experience for 6 months within the last 24 months.
Option B. an
aircraft type refresher in the last 24 months.
Option C. maintenance
experience for 4 months within the last 24 months.
Correct Answer is. maintenance
experience for 6 months within the last 24 months.
Explanation. NIL.
Question Number. 56. A National UK licensed engineer, when
signing a CRS would need to have.
Option A. an
aircraft type refresher in the last 24 months.
Option B. maintenance
experience for 4 months within the last 24 months.
Option C. maintenance
experience for 6 months within the last 24 months.
Correct Answer is. maintenance
experience for 6 months within the last 24 months.
Explanation. AWN 3
(issue 20) pg 4 para 1.8.
Question Number. 57. Vital point inspections.
Option A. are
points which require special certifying LAEs.
Option B. are
components which involve duplicate inspections.
Option C. are
lifed components.
Correct Answer is. are
components which involve duplicate inspections.
Explanation. BCAR
A5-3 para 3 states: VITAL POINTS are any point on an aircraft at which single
mal-assembly could lead to catastrophe, ie. result in loss of aircraft and/or
in fatalities. Hence the need for duplicate inspections, AWN 3 pg 3 para 1.6.
Question Number. 58. On a pre flight check you notice an
instrument glass is cracked. You should.
Option A. enter
into technical log.
Option B. check
MEL.
Option C. tell
oncoming captain.
Correct Answer is. check
MEL.
Explanation. NIL.
Question Number. 1. A Category-A licenced engineer can sign
a CRS for what?.
Option A. A task
he has been locally trained for.
Option B. An
aircraft that he has sufficient type ratings for.
Option C. A task
that someone else has completed.
Correct Answer is. A
task he has been locally trained for.
Explanation. NIL.
Question Number. 2. When removing a piece of equipment from
an aircraft that supports the aircraft, what should you do?.
Option A. Go
ahead and remove the part.
Option B. Wait
for the new part to arrive before replacing.
Option C. Fit a
jury strut in place of the removed part.
Correct Answer is. Fit
a jury strut in place of the removed part.
Explanation. NIL.
Question Number. 3. How do you prime a dead weight tester?.
Option A. wind
handle fully out and pour fluid in the reservoir.
Option B. Remove
the weights and pour fluid into the hole.
Option C. wind
handle fully in and pour fluid in the reservoir.
Correct Answer is. wind
handle fully in and pour fluid in the reservoir.
Explanation. It is
normal to wind the handle (and plunger) fully in, fill the reservoir, then wind
the handle out, to draw the fluid.
Question Number. 4. When you change an EGT gauge, you
should.
Option A. do a
test without considering ambient temperature, as it is already accounted for by
the instrument.
Option B. do a
test immediately, taking ambient temperature into consideration.
Option C. do
test letting new gauge 'soak' for 30 minutes then do test taking ambient
temperature into consideration.
Correct Answer is. do
test letting new gauge 'soak' for 30 minutes then do test taking ambient
temperature into consideration.
Explanation. Correction
factors for ambient temperatures are usually found on the inside of teh test
instrument's lid.
Question Number. 5. What is the problem with using a megger
on a piece of equipment containing capacitors.
Option A. Fluctuating
readings will occur while the capacitors charge up.
Option B. Feedback
from the capacitors will blow the megger up.
Option C. Impedance
in the capacitors will give a false high reading.
Correct Answer is. Fluctuating
readings will occur while the capacitors charge up.
Explanation. NIL.
Question Number. 6. Water marks on bearings are indications
of.
Option A. bearing
insufficiently lubricated.
Option B. intergranular
corrosion.
Option C. bearing
been run dry.
Correct Answer is. intergranular
corrosion.
Explanation. Jepperson
A & P Airframe Technician Textbook page 9-9 fig 9-11.
Question Number. 7. What is the allowable reaction on a
rivet?.
Option A. 2D.
Option B. 1D.
Option C. 1.5D.
Correct Answer is. 1D.
Explanation. Allowance
is 1.5D, formed tail is 0.5D, so reaction must be 1.0D.
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