Landing Gear Flashcards
The autobrake system is disarmed by _____.
Gouge answer [incorrect]: loss of center system hydraulic loss.
Correct answer: manual braking
The center hydraulic system powers ______.
alternate/reserve brake system
Hydraulic pressure for landing gear retraction, extension, and steering is supplied by the ______ hydraulic system(s)
center
Autobrakes are applied if takeoff is aborted above ______ knots.
85
Autobrakes provide braking to _______.
a complete stop or until disarmed
During extension how are the landing gear lowered?
They free-fall to the down and locked position.
Do not use speed brakes in flight below ______ feet.
1000
Which input has steering override authority, nose wheel steering tiller or rudder pedal?
Nose wheel tiller steering overrides rudder pedal steering.
If the right hydraulic system pressure is low, the ______ hydraulic system automatically supplies pressure to the alternate/reserve brake system.
center
Following an alternate extension, positioning the landing gear lever to ______ then _____ retracts the gear using the normal system, if the normal system is available.
DN, UP
When the landing gear lever is moved to DN, the landing gear doors open and the gear are unlocked. During extension ______.
main gear trucks tilt to flight position
When selected prior to takeoff, RTO will operate _____ groundspeed above 85 knots.
with both throttles retarded to idle and
If any gear is not completely locked down after normal transit time ______.
the EICAS gear position indicator changes to the expanded format
The word BRAKE in this graphic indicates the brake ______ on the respective wheel.
is deactivated
On dry runways, the maximum autobrake deceleration rate in the landing mode is _____.
less than that produced by maximum effort manual braking
When the parking brakes are set, _____.
PARKING BRAKE SET displays on EICAS
