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CHƯƠNG 1: BẢO DƯỠNG HỆ THỐNG 1

Total questions: 77

Worksheet time: 39mins

Name
Class
Date
1.
The loops are connected in parallel to a Fire Detection Unit (FDU). The connection is made through an AND logic to avoid spurious FIRE warnings. If one loop fails, the AND becomes an OR logic. The aircraft can be released in this configuration. (khó)
a)

A. two sets of loops avoid false warnings

b)

B. normally, both loops must detect a fire simultaneously

c)

C. the aircraft cannot depart with only one loop operative

2.
Remove the QAD bolt and retain its and the ball seat washer. (trung bình)
a)

A. packing

b)

B. coating

c)

C. cowling

3.
Apply common grease to the of the drive shaft.
a)

A. elbows

b)

B. looms

c)

C. splines

4.
Removal of the THS front center box access panel.
a)

A. tip

b)

B. spar

c)

C. spare

5.
Install the call on its support.
a)

A. jack

b)

B. horn

c)

C. worn

6.
On the instrument panel, set the BRT/DIM _ to OFF. (trung bình)
a)

A. notch

b)

B. B. probe

c)

C. C. knob

7.

the safety pin

a)

A. Insert

b)

B. Introduce

c)

C. Enter

8.

Drain and refill the gearbox.

a)

A. spray

b)

B. B. de-ice

c)

C. C. flush

9.

Before performing the test C/B 6XX.

a)

A. trigger

b)

B. B. trip

c)

C. C. dump

10.

the panel with Dzus fasteners. (trung bình)

a)

A. Stow

b)

B. B. Secure

c)

C. C. Slide

11.

The oxygen cylinder disc has .

a)

A. popped out

b)

B. tripped

c)

C. jacked up

12.

Cold weather causes metal shrink.

a)

A. down

b)

B. into

c)

C. to

13.

If the cargo door is not locked, indicators protrude the bottom of the door. (khó)

a)

A. from

b)

B. through

c)

C. under

14.

You can revolve the pallets the ball mat. (trung bình)

a)

A. with

b)

B. on

c)

C. by

15.

The flaps are extended 25o landing.

a)

A. for

b)

B. as

c)

C. in

16.

The window runs _ a groove or track. (trung bình)

a)

A. by

b)

B. in

c)

C. on

17.
ADF sense antenna 1 is on the left lower fuselage____________No 2 is on the right (trung bình)
a)

A. whereas

b)

B. thus

c)

C. since

18.
The HUD enables landing _________visibility is poor.
a)

A. provided

b)

B. because

c)

C. though

19.
The needle is in the green range__________the nitrogen pressure is low. (trung bình)
a)

A. as a result,

b)

B. thus

c)

C. unless

20.
The glide scale is displayed on the ADI__________it is repeated on the HSI. (Trung bình)
a)

A. in order to

b)

B. B. moreover

c)

C. C. so

21.
The shut-off valve is electrically controlled_________pneumatically operated. (trung bình)
a)

A. but

b)

B. if

c)

C. because

22.
The wing anti-ice system is (deactivate) __________when the a/c is on the ground (khó)
a)

A. deactivating

b)

B. B. making deactivate

c)

C. C. deactivated

23.
An overheat thermostat (de-energize) __________the resistance when a window overheat condition exists. (khó)
a)

A. de-energizes

b)

B. de-energized

c)

C. is de-energized

24.

(Depress) the LOOPS push-button tests the continuity of the fire detection loops. (trung bình)

a)

A. Depression

b)

B. B. Depressive

c)

C. C. Depressing

25.
The water tank is (fill)_________during turnaround.
a)

A. being filled

b)

B. filled

c)

C. filling

26.
The engine mount bolts are (ease)__________into position.
a)

A. eased

b)

B. eased down

c)

C. being eased

27.
A fuel crossfeed valve is usually in.
a)

A. the closed position.

b)

B. the open position.

c)

C. its last position.

28.
Sliding couplings in fuel systems are used on.
a)

A. low pressure systems.

b)

B. high pressure systems.

c)

C. air or vapour systems.

29.
A fuel cross-feed valve is lubricated.
a)

A. by internal cooling.

b)

B. by air.

c)

C. by the fuel.

30.
Fuel cross feed valves are operated by the.
a)

A. 28 V DC bus.

b)

B. 115 V AC.

c)

C. battery.

31.
Fuel systems that are interconnected must have.
a)

A. separate venting for each tank.

b)

B. no airspace.

c)

C. air spaces interconnected.

32.
As fuel level increases, system capacitance.
a)

A. decreases.

b)

B. no change.

c)

C. increases.

33.
When refuelling.
a)

A. the fuel nozzle will automatically cut off the supply when the tank is full.

b)

B. it is important not to fill the expansion space in the tank.

c)

C. it is important to fill the expansion space in the tank.

34.
When using Biopor microbial fuel growth treatment.
a)

A. it is added to the fuel and burnt.

b)

B. it is applied dry and left.

c)

C. it is applied wet and flushed out.

35.
Microbial growth is.
a)

A. red dots.

b)

B. brown, black slime.

c)

C. green sludge.

36.
Bladder type fuel tanks are secured by.
a)

A. bolts.

b)

B. contact adhesive.

c)

C. press type rivets.

37.
Spongy brakes are usually a result of.
a)

A. internal leakage.

b)

B. air in the system.

c)

C. external leakage.

38.
Over inflated tyres may cause damage to the.
a)

A. brake drum.

b)

B. wheel hub.

c)

C. wheel flange.

39.
A brake debooster valve is provided for.
a)

A. applying brake pressure slowly and releasing the the brakes quickly.

b)

B. increasing the pressure and applying the brakes rapidly.

c)

C. decreasing the pressure and slowly releasing the brakes.

40.
Tubeless tyres are stored.
a)

A. at 15 to 20 P.S.I.

b)

B. horizontally maximum of four high with smallest diameter tyre on top.

c)

C. vertically.

41.
On a wheel bogie unit, positive camber is when the.
a)

A. bottom of the wheels are closer together.

b)

B. top of the wheels are closer together.

c)

C. front of the wheels are closer together.

42.
A badly corroded and pitted brake disk will.
a)

A. wear brake pads too quickly, and should be replaced.

b)

B. be serviceable, and provide better grip.

c)

C. produce a loss of fluid.

43.
How much oxygen is in a tyre (as a maximum)?.
a)

A. 5% by pressure.

b)

B. 15% by volume.

c)

C. 5% by volume

44.
A tyre specification 32 x 10.75-14. What does the 10.75 refer to.
a)

A. Section Width.

b)

B. Bead diameter.

c)

C. Overall diameter.

45.
When servicing an oleo, fluid comes out of the air valve when the leg is depressurised?.
a)

A. The leg is serviceable - the separator has bottomed.

b)

B. Leaking air/oil seals.

c)

C. Separator plate stuck open.

46.
The type of fluid in an oleo strut will depend upon.
a)

A. type of fluid most readily available.

b)

B. the type of seal material.

c)

C. heat generated in operation of the system.

47.
A restrictor valve.
a)

A. speed up the flow in one direction.

b)

B. may be used to slow down undercarriage extension.

c)

C. restrict the extent of travel of the undercarriage.

48.
The function of the oil in a shock absorber is to.
a)

A. ensure the separator does not bottom.

b)

B. damp the rebound.

c)

C. absorb the landing shock.

49.
The purpose of the flutter plate in a shock absorber is to.
a)

A. permit free flow of oil during compression and restriction of oil during extension.

b)

B. restrict the compression of the air.

c)

C. separate the oil from the air.

50.
Made up wheels should be stored.
a)

A. vertical at working pressure.

b)

B. vertical at 20/30 PSI charge.

c)

C. horizontal no more than 4 high.

51.
1. "After MLG down and securely locked, a red light is illuminated n the flight deck. The possible causes are."
a)

A. shorted sensor.

b)

B. out of adjustment sensor.

c)

C. wiring problem.

52.
When checking for alignment of a MLG, check.
a)

A. symmetry, tracking, camber.

b)

B. symmetry, splay, tracking.

c)

C. symmetry, twist, tracking.

53.
These markings are found on a tyre32 x 10.45 R 14.What does the number 32 mean?.
a)

A. Outer diameter.

b)

B. qwidth.

c)

C. Inner diameter.

54.
A green/grey dot marking on aircraft tyre casing represents.
a)

A. breather points.

b)

B. the light part of the tyre.

c)

C. military reference.

55.
In detachable flange type wheels, the flange is secured by.
a)

A. a retainer plate.

b)

B. a lock ring.

c)

C. bolts.

56.
Fuse plugs in aircraft tyres are.
a)

A. for over temperature protection.

b)

B. for overpressure protection.

c)

C. to deflate the tyre before removal.

57.
A purpose of a 'cut-out' in a hydraulic system.
a)

A. is to prevent creep in jack operated services which have several selected positions.

b)

B. is to limit loss of fluid in the event of pipe fracture.

c)

C. is to relieve the pump of load when the operation of services is complete and the accumulator charged with fluid.

58.
Hydraulic pressure can be restored by.
a)

A. compressing the air charge in an accumulator.

b)

B. the use of a pressure/heat exchanger.

c)

C. compressing the fluid in a reservoir.

59.
What is the colour of the band on a hydraulic seal?.
a)

A. Yellow.

b)

B. Green.

c)

C. White.

60.
A maintainer valve in an hydraulic system will.
a)

A. allow continued press to essential systems during times of reduced supply.

b)

B. dampen pressure inputs.

c)

C. maintain a high pressure to all systems.

61.
Where is the temperature overheat switch located in a hydraulic pump?.
a)

A. In the pressure line.

b)

B. In the suction line.

c)

C. In the case drain.

62.
What happens if a component has an internal hydraulic leak?.
a)

A. Fluid loss.

b)

B. Increase in fluid pressure.

c)

C. Increase in fluid temperature.

63.
What happens to hydraulic fluid when it is overheated?.
a)

A. Increase acidity.

b)

B. Increase viscosity.

c)

C. Increase alkalinity.

64.
How is the hydraulic pump depressurising solenoid actuated?.
a)

A. Energised both open and closed depending on cockpit selection.

b)

B. Energised Open.

c)

C. Energised Closed for fail-safe.

65.
How do you prevent hydraulic fluid frothing?.
a)

A. By pressurising.

b)

B. Vent Reservoir to atmosphere.

c)

C. Pass over a tray.

66.
Accumulators as fitted to aircraft hydraulic systems.
a)

A. are only ever used in an emergency.

b)

B. store fluid under pressure.

c)

C. provide additional fluid if leaks occur.

67.
How is a serrated rod ice detector bench tested?.
a)

A. Screwdriver torque test.

b)

B. By a motor load test.

c)

C. Motor test and go/no-go gap measurement.

68.
Windshield heating provides.
a)

A. thermal expansion for a tighter fit.

b)

B. impact resistance enhancement.

c)

C. increases strength to resist cabin pressure.

69.
At what pressure and temperature is anti ice fluid applied?.
a)

A. 7°F at 100 PSI.

b)

B. 70°C at 100 PSI.

c)

C. 70°F at 10 PSI.

70.
The advantage of leading edge fluid de-icing is.
a)

A. less of a fire hazard.

b)

B. aerodynamic shape is not disturbed.

c)

C. more efficient.

71.
On large transport aircraft, the windshield wiper system is.
a)

A. one system for both sides but with the same power source.

b)

B. independent on each side but with the same power source.

c)

C. independent on each side with different power sources.

72.
Prior to securing a leading edge de-icing boot you must.
a)

A. remove all paint.

b)

B. paint the surface.

c)

C. shave rivet to prevent further abrasion.

73.
On a 'hot rod' type of ice detector, it is switched on.
a)

A. all the time.

b)

B. when selected by the crew.

c)

C. when in the air.

74.
Ice formation on wings is due to.
a)

A. suspended ice crystals melting on contact with the wing and instantly re-freezing.

b)

B. ice crystals forming layers on contact with the wing.

c)

C. supercooled water changing state on contact with the wing.

75.
When a vibrating rod ice detector has de-iced, the warning lamp on the flight deck
a)

A. goes out immediately.

b)

B. goes out after one more cycle.

c)

C. goes out after a set period of time.

76.
De-misting of passenger windows is provided by.
a)

A. sealed window.

b)

B. an electrical heating element.

c)

C. air from the cabin.

77.
A deicer boot is completely bonded to the leading edge to.
a)

A. provide smoother airflow over leading edge.

b)

B. prevent electrical static build up.

c)

C. provide more efficient deicer cycles.