Landing Gear/Brakes Flashcards
Which hydraulic system powers the landing gear extension/retraction?
Hydraulic system 2
Which hydraulic system powers the inboard/outboard brakes?
Outboard: System 1
Inboard: System 2
What must the captain verify with the pushback crew prior to pushback?
- Steering OFF
- Brakes RELEASED
- Green Light VERIFIED
When is the STEER OFF message populated?
- Hydraulic System 2 becomes depressurized
- Steering disconnect switch is pressed
- External steering disengage switch is set to disengage
When must you verify the STEER OFF message?
Prior to pushback and during flight control check
How do you recharge the emergency/parking brake accumulator?
If yellow, recharge by turning ON ACMPs for hydraulic system 1 and 2.
When do the autobrakes activate for RTO?
Recognizes RTO when:
- Wheel speed above 60 kts AND
- Thrust levers IDLE or REV
Releases brakes when:
- Brake pedal pressure is applied (20%) or
- System faults (below 60 kts) or
- Thrust levers greater than IDLE
What is the rate of deceleration with LO autobrake?
2 knots per second
What is the rate of deceleration with MED autobrake?
4 knots per second
What is the rate of deceleration with HI autobrake?
8 knots per second
When does the EMERG/PRKG BRAKE light illuminate?
When the parking brake is actuated and there is hydraulic pressure.
What is the DN LOCK REL button?
When weight on wheels is true, the gear lever is mechanically locked in the down position. Pressing the DN LOCK REL button overrides this function.
What are the other two ways to extend the landing gear if normal operation is not working?
Using the electrical override switch or the gear extension lever.
What happens when pulling the gear extension lever?
Releases all hydraulic pressure in the landing gear lines and mechanically releases all landing gear uplocks. Allows gravity to drop the gear.
What happens when selecting the electrical override switch to gear down?
Electronically bypasses the sensors and evaluation computers, and extends the landing gear.