Landing gear Flashcards

1
Q

Landing gear hydraulic pressure

A

Max 1850
Pump cycles at 1600

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2
Q

How to recover from a compressor stall?

A

Advance power, lower angle of attack

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3
Q

Main tire pressure

A

70psi

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4
Q

Nose wheel psi

A

55 psi

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5
Q

Shock strut limit height

A

3 inches

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6
Q

How is the landing gear operated?

A

The gear is electrically controlled and hydraulically actuated.

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7
Q

How is the gear held in the down position?

A

Internal/mechanical down locks
Spring loaded down locks
Folding braces or “Drag Legs”

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8
Q

How is the gear held up?

A

The gear is held in the up position by hydraulic pressure.

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9
Q

How is hydraulic pressure supplied?

A

Through a hydraulic power pack

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10
Q

Where is the hydraulic reservoir located?

A

Left center wing section

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11
Q

What does the power pack consist of?

A

Hydraulic pump
28-VDC motor
Reservoir
Four way gear selector valve
Solenoid
Fluid level sensor
Unlock pressure switch

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12
Q

Hydraulic pressure range

A

1850
If pressure drops below 1600, pump recharges pressure back to 1850

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13
Q

What conditions will light the in-transit gear light?

A

Gear handle in the up position while on the ground.

Flaps up or Appr and one or both power levers below 79% N1.

Any gear is not in the fully retracted position.

Flaps beyond Appr with gear up.

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14
Q

What configuration will not allow you to silence the gear horn?

A

Gear up, flaps greater than appr.

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15
Q

How is the manual gear extension engaged?

A

Gear handle down
Landing gear circuit breaker pulled
Hand pump lever un-stowed

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16
Q

What can happen if the parking break is left on for an extended period of time?

A

Ground personnel could try to move aircraft.

Ambient temp changes can expand or contract the brake fluid, causing excessive brake pressure or brake release.