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Flight Safety Lear 45/40 Required Knowledge Areas > Gear & Brakes > Flashcards

Gear & Brakes Flashcards

1
Q

The maximum speed with the landing gear extended and the inboard gear doors retracted is:

A

260 KI-AS. AFM Pg. 1-7

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2
Q

The maximum speed for lowering or raising the landing gear is ( ) KIAS.

A

200 KIAS. AFM Pg. 1-7

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3
Q

Main landing gear tire limit speed is ( ) Knots.

A

165 Knots. PTM 14-4

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4
Q

The landing gear should not be extended above ( ’) feet.

A

18,000’ feet. AFM Pg. 1-10

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5
Q

The landing gear is lowered and raised using ( ) system hydraulic pressure.

A

Main system hydraulic pressure. PTM Pg. 14-2

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6
Q

The landing gear can be lowered using the ( ) pump and the ( )
valve.

A

Auxiliary hydraulic pump and the hydraulic crossflow. PTM Pg. 14-2

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7
Q

The landing gear can be lowered using the ( ) free fall lever.

A

Landing gear free fall lever. PTM Pg. 14-2

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8
Q

Landing gear position indications after successfully using the free fall system to lower the landing gear will be( ).

A

Three green down lights and two in transit lights above the main gear down lights because the inboard gear doors will remain extended. PTM Pg. 14-6

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9
Q

The NWS “ ” indication is a valid nose gear down and locked signal if no other NWS monitor faults are present.

A

ON. PTM Pg. 14-7

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10
Q

Should a main landing gear GREEN position light fail to illuminate following gear extension, illumination of the taxi light when selected “ ” is a valid confirmation that the corresponding main gear is down and locked.

A

The taxi light when selected “ON”. PTM Pg. 14-7

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11
Q

Landing gear free fall extension does ( ) require hydraulic or electrical power.

A

Not. PTM Pg. 14-14

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12
Q

Landing gear free fall extension should take no more than ( ) minute. PTM Pg. 14-14

A

1 minute. PTM Pg. 14-1

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13
Q

Auxiliary Hydraulic extension of the landing gear may take up to ( ) seconds. PTM 14-17

A

30 seconds. PTM 14-17

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14
Q

There is ( ) anti-skid protection using the Emergency/Parking brake system.

A

NO. PTM Pg. 14-23

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15
Q

Normal brake accumulator pressure is approximately ( ) psi. PTM 14-23

A

3,000 psi. PTM 14-23

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16
Q

If the “ ” aural warning sounds, the only braking available is the Emergency/Parking brake.

A

BRAKES FAIL. PTM Pg. 14-23

17
Q

In the event the red NORMAL BRK FAIL CAS message illuminates, the only braking available is
the ( ) brake. PTM Pg. 14-23

A

Emergency/Parking brake. PTM Pg. 14-23

18
Q

Nose Wheel Steering system in the Lear 40/45 is ( ) powered.

A

Electrically. PTM Pg. 14-2

19
Q

As the aircraft’s ground speed is increased , the nose gear steering authority gradually decreases from ( ) degrees to ( ) degrees at 70 KIAS. PTM Pg. 14-25

A

60 degrees to 7 degrees at 70 KIAS. PTM Pg. 14-25

Flight Safety Lear 45/40 Required Knowledge Areas (22 decks)

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