Flashcards in Landing Gear Deck (19)
Positioning the LANDING GEAR Lever _____ removes hydraulic pressure form the Landing Gear System.
The Lever Lock Override Trigger in the LANDING GEAR lever bypasses the _____ under certain conditions.
the lever lock if the lever lock solenoid fails.
A Main Gear Position Light is not illuminated with the LANDING GEAR lever in the DOWN position. The Supplemental Gear Position light is green. The respective gear is _____.
down and locked.
The _____ supplies hydraulic fluid to raise the landing gear when Hydraulic System A engine driven pump volume is lost due to an engine failure.
Landing Gear Transfer Valve
Opening the Manual Extension Access Door _____ Landing Gear _____.
Pulling a Manual Gear Extension Handle _____ allowing the respective gear to free fall.
releases the mechanical uplocks
With the flaps greater than _____ pushing the HORN Cutout switch will not silence the Landing Gear Configuration Aural Warning Horn.
_____ supplies pressure to the Alternate Brake System if normal brake system pressure is low or fails.
Hydraulic System A automatically
Braking _____ if both Hydraulic System A and B are lost.
is available through a Brake Accumulator
_____ System(s) provide(s) skid locked wheel touchdown and hydroplane protection.
the Normal and Alternate Brake
Maximum braking automatically begins during a rejected takeoff _____.
above 90 knots and retarding the forward thrust levers to IDLE
Landing with the Autobrake set to RTO
results in no autobraking
The Autobrake select switch allows selection of _____.
increasing rates of deceleration.
Auto brakes when engaged _____ when thrust reversers and spoilers deploy during landing.
reduce pressure to maintain selected deceleration rate
Disarm the Autobrake System after braking begins by _____.
applying manual brakes, moving the SPEED BRAKE lever to DOWN detent or advancing forward thrust lever(s) more than 3 seconds.
How d you set the PARKING BRAKE?
depress both brake pedals and pull the lever up and aft.
The PSEU detects a fault while in flight
the PSEU does not illuminate
Hydraulic System B was operating normally. If Hydraulic System B is then lost (both pumps inoperative) the Hydraulic Brake Pressure Accumulator indicates
approximately 3000 psi