Flight Controls Flashcards

1
Q

Ailerons and elevator operation method

A

Control rods

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2
Q

Rudder operation method

A

Control cables

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3
Q

Flaps operation method

A

Electric actuator operated control rods

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4
Q

Fixed aileron trim tab location

A

Left aileron

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5
Q

How long must only 1 trim switch be operated before system detects a fault, and how does it respond

A

3 seconds, electric pitch trim system is disabled

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6
Q

Criteria for stick limiter activation

A

Flaps LDG and both engines ~20%< power

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7
Q

Elevator normal range and limited range

A

Normal: 15.5 deg

Stick limited: 13 deg

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8
Q

Flaps deg when UP

A

0 deg

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9
Q

Flaps deg when APP

A

20 deg

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10
Q

Flaps deg when LDG

A

42 deg

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11
Q

How are the flaps stopped from exceeding UP or LDG

A

Limit switches prevent by tripping flap circuit breaker

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12
Q

Stall warning system detector type and location

A

Flapper switch on left wing

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13
Q

How is stall warning system detector de-iced

A

Heated via pitot heat switch

n.b. Cannot be operated on the ground

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14
Q

How are the trim tabs operated

A

Bowden cables

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