Jeppesen Airframe Ch. 9 Sec. A Flashcards

(35 cards)

1
Q
  1. The tailwheel type landing gear arrangement is also known as ______ landing gear
A

Conventional

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2
Q
  1. Retracting the landing gear on an aircraft decreases the ______ drag
A

Parasite

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3
Q
  1. Almost all current production airplanes use the _____ _____ -type landing gear arrangement.
A

Tricycle

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4
Q
  1. Tailwheel aircraft are highly susceptible to an abrupt, uncontrolled change in direction on the ground called a _______ _______ due to the relationship between the main wheels and the __________.
A

Ground Loop
Center Of Gravity

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5
Q
  1. The streamlined fairings used to enclose the wheels are referred to as ______ ______.
A

Wheel pants

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6
Q
  1. A(n) ______ cord is a bundle of small strands of rubber encased in a loosely woven cloth tube.
A

Bungee

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7
Q
  1. The most widely used shock absorber for aircraft is the ______
    _____ shock absorber or more commonly known as an ______ strut.
A

Air-oil
Oleo

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8
Q
  1. An oleo strut absorbs the landing impact shock with the _____ .
A

Oil

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9
Q
  1. An oleo strut absorbs the taxi shocks with the _____ .
A

Air

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10
Q
  1. Oleo strut inflation is checked by measuring the length of the exposed _______.
A

Piston Tube

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11
Q
  1. Modern aircraft wheels are almost always _____ -piece units.
A

Two

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12
Q
  1. Aircraft wheels may be cast or forged of either _____ or _____ alloy.
A

Aluminum
Magnesium

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13
Q
  1. The _______ area is the most critical part of a wheel.
A

Bead Seat

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14
Q
  1. Steel keys or keyways on the inboard wheel half drive the rotating ______
A

Brake Disk

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15
Q
  1. One or more ______ ______ may be installed in the inboard half of the main wheels of jet aircraft to release the air from the tire in case of extreme overheating.
A

Fusible Plugs

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16
Q
  1. Before loosening the bolts joining the halves of a wheel, it is critically important that you _____
A

Make sure it is completely deflated

17
Q
  1. To safely insure complete deflation of a tire, first use a _____ screwed onto the _____ then remove the _____.
A

Deflator cap
Valve
Valve Core

18
Q
  1. Screwdrivers or tire tools _____ to pry a tire bead away from the
19
Q
  1. Aircraft bearings _______ be cleaned with steam.
20
Q
  1. Water stains on a wheel bearing is cause for rejection, because this may be an indication of _____ corrosion.
A

Intergranular

21
Q
  1. Discolored bearings indicate damage due to _____
22
Q
  1. Dye penetrant inspection _____a good method to use to locate cracks in the bead seat area of an aircraft wheel.
23
Q

23.______ inspections should be used to detect cracks on the bead seat area.

24
Q
  1. Wheel bolts should be inspected using the ______ ______ indication inspection method.
A

Magnetic Particle

25
25. If ______ (how many) of the fusible plugs in the wheel show any signs of softening, they must all be replaced.
Any
26
26. A(n) _____ is used to reduce the back and forth oscillations of the nose wheel at certain speeds.
Shimmy Damper
27
27. If the front sides of the wheels of an aircraft are closer together than the rear sides, the landing gear is _____,
Toed-in
28
28. If the tops of the wheels of an aircraft are closer together than the bottoms, the landing gear has a _______ camber.
Negative
29
29. Large aircraft use a system to apply the brakes when the landing gear is selected UP in order to prevent a ______ hazard or possible ______to the aircraft due to spinning wheels.
Fire Damage
30
30. All retractable landing gear systems must have some means of ______ the gear if the primary method fails.
Lowering
31
31. Among the methods emergency gear extension systems may use are:
Mechanical Alternate Hydraulic Compressed Air Free-Fall
32
32. A(n) ______ switch may be installed in a landing gear retraction system to prevent the landing gear from being raised while the aircraft is on the ground.
Squat
33
33. Retractable gear aircraft generally use a _____ light to indicate that the gear is down and _____.
Green Locked
34
34. A gear warning horn will sound if the throttles are _____ and _____ of the landing gear are in the up position
Retarded Any
35
35. Landing gear warning systems are designed to warn the pilot that the gear ____ down and locked when the aircraft is in the ___ configuration.
Is not Landing