391-400

Question 1

_______ allows the aircraft to push back or be towed without depressurizing system A.
a)
A bypass switch on the forward panel
b)
A lockout pin
c)
Pulling nose wheel circuit breaker

Answer 1

A lockout pin

Question 2

If hydraulic system B is low or fails, _______ automatically supplies pressure to the alternate brake system.
a)
hydraulic system A
b)
electric friction
c)
standby system pressure

Answer 2

hydraulic system A

Question 3

The parking brake can be set with:
a)
hydraulic system A
b)
hydraulic system B
c)
A or B hydraulic system, or the accumulator if A and B are not pressurized

Answer 3

A or B hydraulic system, or the accumulator if A and B are not pressurized

Question 4

An amber illuminated AUTO BRAKE DISARM light indicates:
a)
the auto brakes are set to MAX
b)
the AUTO BRAKE select switch is set to OFF
c)
a malfunction exists in automatic braking system

Answer 4

a malfunction exists in automatic braking system

Question 5

Placing the AUTO BRAKE Select Switch to 1, 2, 3, or MAX, selects desired ________ for landing.
a)
brake pressure
b)
deceleration rate
c)
air run

Answer 5

deceleration rate

Question 6

An amber illuminated ANTISKID INOP light indicates:
a)
the anti-skid system need to be reset
b)
the auto brakes need to be armed
c)
a system fault is detected

Answer 6

a system fault is detected

Question 7

On dry runways, the maximum autobrake deceleration rate in the landing mode is _______ that produced by full pedal braking.
a)
more than
b)
equal to
c)
less than

Answer 7

less than

Question 8

Pushing the Landing Gear Warning Cutout Switch silences landing gear configuration warning aural indications at:
a)
flaps up through 10 and below 800 feet RA
b)
flaps 15 through 25 and below 800 feet RA
c)
flaps 30 through flaps 40 and below 800 feet RA

Answer 8

flaps up through 10 and below 800 feet RA

Question 9

How do you recall all existing fault annunciations?
a)
Press either master caution light
b)
Examine your flight papers
c)
Press either system annunciator light panel

Answer 9

Press either system annunciator light panel

Question 10

In flight, the Proximity Switch Electronic Unit (PSEU):
a)
will illuminate during a landing gear configuration warning
b)
is inhibited from thrust lever advance for takeoff until 30 seconds after landing
c)
will illuminate for an air / ground sensing disagree

Answer 10

is inhibited from thrust lever advance for takeoff until 30 seconds after landing