Landing Gear Flashcards

1
Q

757: When the RESERVE BRAKES switch is activated, fluid trapped below a standpipe in the right hydraulic system reservoir is made available to the

A

Right system electric hydraulic pump

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2
Q

764: The alternate landing gear extension system uses
to release all door and gear
uplocks, and allow the landing gear to free-fall to the down and locked position.

A

An electric hydraulic pump

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3
Q

757/767: According to the graphic, the AUTO BRAKES light is illuminated because:

A

The autobrake system is disarmed or inoperative

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4
Q

767: When the RESERVE BRAKES & STRG switch is activated, fluid from the ___ is made available for reserve brakes operation.

A

The center hydraulic system reservoir

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5
Q

757/763: The PARK BRAKE light illumination on the pedestal indicates that:

A

The parking brake handle is not stowed

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6
Q

763: The alternate landing gear extension system uses ___ to trip the locking mechanism for each gear.

A

An electric motor

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7
Q

757/767: The tiller can turn the nose wheel up to ___ in either direction

A

65°

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8
Q

757/763: The landing gear lever is placed in the OFF position to:

A

Depressurize the landing gear system

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9
Q

757/767: The autobrake system disarms immediately without pilot input when:

A

An autobrake or normal antiskid system fault occurs

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10
Q

757/767: When using the alternate brake system, what antiskid protection is provided?

A

Alternate (paired wheel) antiskid

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11
Q

757: When the RESERVE BRAKES switch is activated, fluid from ___ is made available for reserve brakes operation.

A

Below a standpipe in the right hydraulic system

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12
Q

757: A white BRAKE TEMP light indicates a relative brake temperature ____ or greater exists on of one or more brakes.

A

5

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13
Q

757/767: The normal brake system is powered by the ___ hydraulic system

A

Right

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14
Q

757/767 the ____ if the RESERVE BRAKES (757), or RESERVE BKS & STRG (767) is selected and pressure is available

A

BRAKE SOURCE light and EICAS message extinguish

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15
Q

757/767: The BRAKE SOURCE light illuminates and the corresponding EICAS message displays if:

A

Both the normal and alternate brake system pressures are low

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16
Q

753/767: The TAILSKID light illuminatos and the EICAS advisory message TAILSKID displays when

A

The tailskid position disagrees with the landing gear lever position

17
Q

767: The alternate brake system is powered by the ___ hydraulic system

A

Center

18
Q

757/767: The alternate brake system has all the capabilities of the normal brake system except for ___, which requires that the normal antiskid system is operating.

A

Automatic braking

19
Q

757: In the event of a total electrical failure, the landing gear can be extended:

A

By using normal gear extension

20
Q

757/767: Limited steering control is available through the rudder pedals, allowing turns up to ___ in either direction.

A

21
Q

764: If any brake temperature is __ or more, a BRAKE TEMP EICAS message displays.

A

22
Q

757/767: Inflight and ground operation of various aircraft systems are controlled by the air/ground sensing system and the nose air/ground sensing systems. They receive logic signals from:

A

Tilt sensors located on each main landing gear and nose gear strut compression sensors

23
Q

757/767: With the rejected takeoff (RTO) mode armed, the autobrake system applies maximum braking when:

A

Both thrust levers are retarded to idle above 85 knots