Landing Gear & Brakes Flashcards
What does pulling the LANDING GEAR FREE FALL
LEVER do?
Relieves the hydraulic pressure in the landing
gear lines and mechanically releases the uplock
hooks for all the landing gear (AOM 9-13-30)
What does it mean when the LANDING GEAR
POSITION INDICATIONS turn to red icons?
That more than 20 seconds has passed since
a discrepancy has been detected between the
landing gear lever position and the actual landing
gear position (AOM 9-13-30)
If the parking brake is not fully released on the
ground, what CAS message will be displayed?
Either a white PARKING BRAKE ON CAS or a
cyan CHECK PARKING BRAKE CAS message
(AOM 9-13-30)
If the parking brake is not fully released in flight,
what CAS message will be displayed?
An amber PARK BRAKE NOT REL CAS message
AOM 9-13-30
Where can the emergency/park brake accumulator
pressure and the brake temperature indications
be seen?
On the STATUS synoptic pages (AOM 9-13-30)
How long can the light on the STEERING button
and the STEERING DISC CAS message take to go
off after the first engagement of the nose wheel
steering?
Up to 2 seconds (AOM 9-13-30)
Which steering switch has priority for safe operation
on the ground?
The external STEERING DISENGAGE switch
AOM 9-13-30
When will the green TOWING ALLOWED light in
the external steering panel illuminate?
When the external STEERING DISENGAGE
switch is in the DISENGAGE position and the
parking brake is not applied (AOM 9-13-30)
How far should the airplane be towed slowly in a
straight line before turning?
3 m (10 ft) (AOM 3-01-75)
When should the DN LCK REL (downlock release)
button be used?
Only in the event of a landing gear control lever
failure or when it is necessary to clear obstacles
(AOM 9-13-50)
What type of brake system is on the aircraft?
Brake-by-wire (AOM 9-13-60)
During normal operations, what does the Brake Control Unit (BCU) provide?
Locked wheel protection, anti-skid protection,
gear retract braking, touchdown protection, a
gear extension test, brake temperature monitoring,
and autobrake (optional) (AOM 9-13-60)
Where can the Brake Temperature Monitoring
System (BTMS) information be found and what
does it provide?”
On the STATUS synoptic page; brake temperature
status on the synoptic page and brake
overheat warning on the EICAS (AOM 9-13-60)
Where must the brake temperature indication be
prior to takeoff?
In the green range (AOM 3-15)
What are the two different modes of AUTOBRAKE
control?
Landing mode (LO, MED, HI) and rejected takeoff mode (RTO) (AOM 9-13-60)