Landing Gear Flashcards

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1
Q

When should the PWR STEER sw be placed to OFF?

A

In the event of a hydraulic leak of either the brakes, swivel locks, or power steering

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2
Q

What provides a source of pressure for brake operation when the PWR STEER sw is OFF?

A

Brake accumulator

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3
Q

What procedure should you use to Restore power steering control if the PWR STEER caution light comes on while taxiing?

A

Landing gear must be returned to within operation limits and switch must be cycled between STEER and UNLOCK

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4
Q

What provides a source of pressure for swivel lock operation when the PWR STEER switch is OFF?

A

PWR STEER module accumulator

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5
Q

How much pressure should be in the brake accumulator on preflight?

A

600-1400 psi

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6
Q

What should be the position of the swivel switch for all takeoffs and landings?

A

Lock

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7
Q

Which three sub systems are affected by the power steer switch?

A

Brakes, swivel lock, and PWR steering

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8
Q

With the swivel switch on the steer position, what automatic DAFCS function is disabled?

A

Heading hold

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9
Q

The turning limits for the CH47 are ______ degrees left and _____ degrees right

A

58

82

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10
Q

What is the purpose of the aft wheel swivel locks?

A

To lock the wheels in Trail position

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11
Q

What are the three positions of the swivel switch?

A

Steer\unlock\lock

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12
Q

Which landing gear assembly is steered by using the steering control knob in the cockpit?

A

Aft right

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13
Q

The pressure reducer reduces the normal System Pressure from _______ psi to ________ psi for brake operation.

A

3,000 psi

1,390 psi

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14
Q

The air/oil shocks struts utilize ______ to absorb shock and ______ to dampen movement

A

Air

Oil

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15
Q

Pressure to the centering cam piston is applied when the swivel switch is placed to the what position?

A

LOCK

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16
Q
A

Power Steering/Swivel Lock Module