Skid, locked wheel, touchdown, and hydroplane protection is available:
a)
only with the normal braking system
b)
with the normal and alternate braking system
c)
only with the alternate braking system
with the normal and alternate braking system
The brake wear indicators should extend beyond the brake flange with the parking brake:
a)
set
b)
released
set
Arming the RTO feature is _________ for all takeoffs, if operable.
a)
required
b)
not required
required
Moving the LANDING GEAR lever to the OFF position:
a)
is not recommended below 235 knots
b)
removes hydraulic pressure from the landing gear system
c)
engages the over center locks
removes hydraulic pressure from the landing gear system
An extinguished green landing gear indicator light indicates:
a)
landing gear is down and locked
b)
landing gear is not down and locked
c)
the landing gear manual extension must be used
landing gear is not down and locked
When the LANDING GEAR lever is moved to UP:
a)
the landing gear retracts
b)
the landing gear extends
c)
hydraulic pressure is removed from the landing gear
the landing gear retracts
The landing gear transfer unit allows hydraulic system B to supply the volume of hydraulic fluid required to raise the landing gear at the normal rate when airborne, LANDING GEAR lever is positioned UP, either main landing gear is not up and locked and:
a)
No. 1 engine RPM drops below a limit value
b)
No. 2 engine RPM drops below a limit value
c)
the A electric hydraulic pump is inoperative
No. 1 engine RPM drops below a limit value
Manual gear releases on the flight deck are used to_________ that allow the gear to_________ to the down and locked position.
a)
engage uplocks; hydraulically extend
b)
release uplocks; free-fall
c)
release uplocks; hydraulically extend
release uplocks; free-fall
The nose wheel steering wheel _____ rudder pedal steering.
a)
works in the opposite direction of the
b)
is secondary to the
c)
overrides
overrides
Nose wheel steering is available:
a)
when the nose gear is in the down position and compressed by the weight of the airplane
b)
when the nose gear is in the down position
c)
at all times
when the nose gear is in the down position and compressed by the weight of the airplane