Flight Controls Flashcards
The FEEL DIFF PRESS light (amber)”,” when illuminated”,”
indicates ______.
excessive differential pressure in the Elevator Feel
Computer
The Aileron System is jammed. How is roll control provided?
First Officer provides roll control using the Flight Spoilers
Two independent Stall Management Yaw Damper (SMYD)
computers provide _____.
) outputs for all stall warnings in flight
Selecting UP on the ALTERNATE FLAPS position switch_____
electrically retracts the TE flaps
The rudder operates with _____ during Manual Reversion
the Standby Hydraulic System
Approaching the stall angle of attack”,” with Flaps 1 through
25 selected”,” the _____ automatically begin driving to full
extend prior to _____ activation
LE Slats / stick shaker
With a jammed Spoiler System”,” the _____.
Captain provides roll control with the ailerons
The flap load relief system is operational at ______.
Flaps 10, 15, 25, 30 & 40
It is possible to _____ the LEDs using the Standby Hydraulic
System with the loss of Hydraulic System B
fully extend
The Standby Yaw Damper operates with ______
both FLT CONTROL switches positioned to STBY RUD and
the YAW DAMPER switch reset to ON
More than _____ (approximately) control wheel
displacement (in degrees) initiates spoiler deflection
10°
Positioning the Speed Brake Lever to UP”,” _____”,” extends
the _____ Spoilers to their maximum position.
on the ground only / Ground and Flight
Roll control surfaces consist of _____ powered _____
hydraulically / ailerons and flight spoilers
The green band of the STAB TRIM indicator on the Control
Stand indicates the ______.
takeoff trim limits
The LE slats _____ when moving the FLAP lever beyond
_____ degrees
deploy to full extend / 25
The RUDDER trim control electrically repositions the Rudder
Feel and Centering Unit and _____ the rudder pedals
displaces
SPEED TRIM FAIL light (amber)”,” illuminating only during
Master Caution Recall”,” indicates _____ failure.
a single FCC channel
Selecting FLT CONTROL A or B switch to STBY RUD activates
the Standby Hydraulic Pump and arms the _____ light(s)
LOW PRESSURE
Pushing a single Left Wing Down or Right Wing Down
AILERON trim switch ______
) does nothing
Ailerons and elevators operate _____ with loss of both
Hydraulic Systems A and B.
manually
Loss of Hydraulic Systems A and B render _____ spoiler
panels inoperative.
all
2) only the flight
3) only the ground
4) only the outboard
Select the switch(es) used for maintenance purposes only.
SPOILER A and B
Momentarily positioning Alternate Flaps switch DOWN fully
extends the ______ using the _____ Hydraulic System
LEDs / Standby
Aileron trim applied with the autopilot engaged ______
may cause abrupt rolling movement when disconnecting
the autopilot
Actuating either pair of Stabilizer Trim Switches on the
control wheels”,” with the autopilot engaged ______.
disconnects the autopilot
The LE flaps _____ when moving the FLAP lever from UP to 1.
fully extend
STAB TRIM switch on the Aft Electronic Panel”,” positioned
to _____”,” allows operation of the main electric trim
regardless of _______ position.
OVERRIDE / control column
Hydraulic System _____ normally power(s) the primary flight
controls
A and B
The Main Rudder Power Control Unit (PCU) limits full rudder
authority ______.
in flight
The SPEED BRAKE DO NOT ARM light (amber) indicates
_______
an abnormal condition or abnormal test inputs to the
Automatic Speed Brake System
In flight”,” the LE FLAPS TRANSIT light (amber) illuminates
for ______
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
If the Air/Ground System does not sense main landing gear
wheels spin-up after landing”,” with the speed brake
armed”,” the flight spoilers _____.
automatically deploy when Air/Ground System senses ground mode (any strut compresses)
AUTO SLAT FAIL light (amber) Illumination during Master
Caution Recall indicates a failure of _________
a single Stall Management Yaw Damper (SMYD)
Positioning FLT CONTROL A switch to STBY RUD ______.
activates Standby Hydraulic Pump and opens Standby
Rudder Shutoff Valve
