211-220

Question 1

The APU ground control panel is located in the __________ and contains an APU fire warning light, an APU BOTTLE DISCHARGE switch, an APU fire control handle, and an APU HORN CUTOUT switch.
a)
main wheel well
b)
nose wheel well
c)
water servicing panel

Answer 1

main wheel well

Question 2

What is the flight deck indication when smoke is detected in the lavatory?
a)
Both red FIRE WARN lights illuminate
b)
Both red FIRE WARN lights illuminate and the FIRE BELL sounds
c)
There is no flight deck indication

Answer 2

There is no flight deck indication

Question 3

The stabilizer trim main electric cutout switch and the stabilizer trim autopilot cutout switch are provided to allow the autopilot or main electrical trim inputs to be:
a)
disconnected from the single stabilizer trim motor
b)
disconnected from their respective stabilizer trim motor
c)
to override to opposing stabilizer trim motor

Answer 3

disconnected from the single stabilizer trim motor

Question 4

At Flaps 1, the Auto Slat system _______ as the aircraft approaches the stall condition.
a)
automatically drives the slats to EXTEND
b)
automatically drives the slats to FULL EXTEND
c)
automatically retracts the slats from EXTEND to UP

Answer 4

automatically drives the slats to FULL EXTEND

Question 5

Illumination of the FEEL DIFF PRESS light indicates:
a)
an emergency situation exists due to a complete electrical failure
b)
the elevator trim system is inoperative
c)
excessive differential hydraulic pressure is sensed in the elevator feel computer

Answer 5

excessive differential hydraulic pressure is sensed in the elevator feel computer

Question 6

An illuminated amber Automatic Slat Failure (AUTO SLAT FAIL) Light during MASTER CAUTION recall indicates:
a)
a failure of both Stall Management / Yaw Damper computers
b)
a failure of a single Stall Management / Yaw Damper computer
c)
a failure of the autopilot

Answer 6

a failure of a single Stall Management / Yaw Damper computer

Question 7

Operation of the Rudder Trim Control switch electrically repositions the _____, which results in a shift in the rudder neutral position.
a)
rudder pedals
b)
rudder trim tabs
c)
rudder feel and centering unit

Answer 7

rudder feel and centering unit

Question 8

On the 737-800, the yaw damper uses:
a)
hydraulic system A or B
b)
hydraulic system B or standby hydraulic system pressure during manual reversion (both FLT CONTROL switches placed to STBY RUD)
c)
hydraulic system A or standby hydraulic system pressure (system B FLT CONTROL switch in OFF)

Answer 8

hydraulic system B or standby hydraulic system pressure during manual reversion (both FLT CONTROL switches placed to STBY RUD)

Question 9

The flight spoilers rise on the wing with the up aileron and remain faired on the wing with the down aileron. When the control wheel is displaced more than approximately ________, spoiler deflection is initiated.
a)
5 degrees
b)
10 degrees
c)
15 degrees

Answer 9

10 degrees

Question 10

Above approximately 135 knots, both hydraulic system A and B pressure are each reduced. This function limits full rudder authority:
a)
only before landing
b)
in flight after takeoff and before landing
c)
on the ground

Answer 10

in flight after takeoff and before landing