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King Air 200 Memory Items > Landing Gear & Brakes > Flashcards

Flashcards in Landing Gear & Brakes Deck (8)
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1
Q

When the wing flaps are beyond the 40% (APPROACH) position, the warning horn sounds if:

A. Both power levers are retarded below a specified setting
B. Either power lever is retarded below a specified setting
C. Any one gear is not down and locked and power levers are below 80% N1 position.
D. Any one gear is not down and locked, regardless of power lever setting

A

D. Any one gear is not down and locked, regardless of power lever setting

2
Q
  1. If the wing flaps are up or at 40% (APPROACH) position, the warning horn sounds if:

A. Either or both power levers are retarded below a specified power setting
B. Both power levers are retarded below a specified setting and any one gear is not down and locked
C. Either or both power levers are retarded below a specified setting and any one gear is not down and locked
D. There is no other requirement

A

C. Either or both power levers are retarded below a specified setting and any one gear is not down and locked

3
Q
  1. If the rudder pedals are deflected with the aircraft stationary:

A. The nosewheel steers, the rudder does not move
B. The spring-loaded link in the system compresses, the nosewheel does not steer
C. The nosewheel does not steer and the rudder does not move
D. The nosewheel steers and the rudder moves

A

B. The spring-loaded link in the system compresses, the nosewheel does not steer

4
Q
  1. When the PARKING BRAKE handle is pulled:

A. Two master cylinders are mechanically actuated, applying the brakes
B. The parking brake valve is actuated to trap pressure from that point to brake assemblies
C. Two master cylinders, already actuated, are mechanically held in that position
D. The parking brake valve is mechanically actuated to build pressure for brake application

A

WAG

C. Two master cylinders, already actuated, are mechanically held in that position

5
Q
  1. The landing gear is held retracted by:

A. Mechanical uplock mechanisms
B. Continuously applied hydraulic pressure
C. Internal uplock mechanisms in all three gear actuators
D. Spring tension

A

B. Continuously applied hydraulic pressure

6
Q
  1. The landing gear is locked down by:

A. Continuously applied hydraulic pressure
B. Internal downlock mechanisms in all three gear actuators
C. An internal lock in the nose gear actuator and overcenter drag brace (nose gear) or by mechanical downlock mechanisms on the drag braces (main gear)
D. Bungees

A

C. An internal lock in the nose gear actuator and overcenter drag brace (nose gear) or by mechanical downlock mechanisms on the drag braces (main gear)

7
Q
  1. With the aircraft airborne, positioning the LDG GEAR CONTROL switch handle UP:

A. Completes a circuit to the UP solenoid of the gear selector valve
B. Completes a circuit to the pump motor relay, pulling in 28 VDC to start the pump motor
C. A and B
D. None of the above

A

WAG

C. A and B

8
Q
  1. When the landing gear is fully retracted, the electrically driven hydraulic pump:

A. Stops, and does not start again
B. Stops, but cycles as required
C. Operates continuously
D. Continues to operate for five minutes, then stops

A

B. Stops, but cycles as required