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ASA 737 Initial 2018 > Flight Controls > Flashcards

Flight Controls Flashcards

1
Q

Hydraulic System _____ normally power(s) the primary flight controls.

A

A and B

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2
Q

Loss of Hydraulic Systems A and B render _____ spoiler panels inoperative.

A

1) all
2) only the flight
3) only the ground
4) only the outboard

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3
Q

Ailerons and elevators operate _____ with loss of both Hydraulic Systems A and B.

A

manually

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4
Q

Roll control surfaces consist of _____ powered _____.

A

hydraulically / ailerons and flight spoilers

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5
Q

Positioning FLT CONTROL A switch to STBY RUD ______.

A

activates Standby Hydraulic Pump and opens Standby Rudder Shutoff Valve

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6
Q

The rudder operates with _____ during Manual Reversion.

A

the Standby Hydraulic System

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7
Q

Pushing a single Left Wing Down or Right Wing Down AILERON trim switch ______.

A

does nothing

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8
Q

Aileron trim applied with the autopilot engaged ______.

A

may cause abrupt rolling movement when disconnecting the autopilot

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9
Q

More than _____ (approximately) control wheel displacement (in degrees) initiates spoiler deflection.

A

10°

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10
Q

Select the switch(es) used for maintenance purposes only.

A

SPOILER A and B

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11
Q

With a jammed Spoiler System”,” the _____.

A

Captain provides roll control with the ailerons

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12
Q

The Aileron System is jammed. How is roll control provided?

A

First Officer provides roll control using the Flight Spoilers.

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13
Q

The FEEL DIFF PRESS light (amber)”,” when illuminated”,” indicates ______.

A

excessive differential pressure in the Elevator Feel Computer

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14
Q

Actuating either pair of Stabilizer Trim Switches on the control wheels”,” with the autopilot engaged ______.

A

disconnects the autopilot

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15
Q

STAB TRIM switch on the Aft Electronic Panel”,” positioned to _____”,” allows operation of the main electric trim regardless of _______ position.

A

OVERRIDE / control column

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16
Q

The green band of the STAB TRIM indicator on the Control Stand indicates the ______.

A

takeoff trim limits

17
Q

SPEED TRIM FAIL light (amber)”,” illuminating only during Master Caution Recall”,” indicates _____ failure.

A

a single FCC channel

18
Q

Two independent Stall Management Yaw Damper (SMYD) computers provide _____.

A

outputs for all stall warnings in flight

19
Q

Selecting FLT CONTROL A or B switch to STBY RUD activates the Standby Hydraulic Pump and arms the _____ light(s).

A

LOW PRESSURE

20
Q

The Main Rudder Power Control Unit (PCU) limits full rudder authority ______.

A

at speeds above approximately 135kts

21
Q

The RUDDER trim control electrically repositions the Rudder Feel and Centering Unit and _____ the rudder pedals.

A

displaces

22
Q

The Standby Yaw Damper operates with ______.

A

both FLT CONTROL switches positioned to STBY RUD and the YAW DAMPER switch reset to ON

23
Q

Positioning the Speed Brake Lever to UP”,” _____”,” extends the _____ Spoilers to their maximum position.

A

on the ground only / Ground and Flight

24
Q

The SPEED BRAKE DO NOT ARM light (amber) indicates _______.

A

an abnormal condition or abnormal test inputs to the Automatic Speed Brake System

25
Q

If the Air/Ground System does not sense main landing gear wheels spin-up after landing”,” with the speed brake armed”,” the flight spoilers _____.

A

automatically deploy when Air/Ground System senses ground mode (any strut compresses)

26
Q

In flight”,” the LE FLAPS TRANSIT light (amber) illuminates for ______.

A

1) any LE device in transit
2) any LE device not in programmed position with respect to TE flaps
3) two (2) or more LE flaps or slats moved from their commanded position
4) all of the above

27
Q

The LE flaps _____ when moving the FLAP lever from UP to 1.

A

fully extend

28
Q

The LE slats _____ when moving the FLAP lever beyond _____ degrees.

A

deploy to full extend / 25

29
Q

The flap load relief system is operational at ______.

A

Flaps 10, 15, 25, 30 & 40

30
Q

Approaching the stall angle of attack”,” with Flaps 1 through 25 selected”,” the _____ automatically begin driving to full extend prior to _____ activation.

A

LE Slats / stick shaker

31
Q

AUTO SLAT FAIL light (amber) Illumination during Master Caution Recall indicates a failure of _________.

A

a single Stall Management Yaw Damper (SMYD)

32
Q

Momentarily positioning Alternate Flaps switch DOWN fully extends the ______ using the _____ Hydraulic System.

A

LEDs / Standby

33
Q

It is possible to _____ the LEDs using the Standby Hydraulic System with the loss of Hydraulic System B.

A

fully extend

34
Q

Selecting UP on the ALTERNATE FLAPS position switch_____.

A

electrically retracts the TE flaps

ASA 737 Initial 2018 (17 decks)

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