A300 Classic SKV Landing Gear and Brakes Flashcards
Which AUTO BRK system is normally armed for takeoff?
MAX
What temperature on any brake will cause the amber BRK HOT light on the LDG GEAR panel to illuminate?
> 300C
When are auto brakes not available?
When using the Alternate brake system.
When the aircraft is being towed, which Nose Wheel Steering controls are available?
No steering controls are available from the flight deck.
An interlock system prevents unsafe gear retraction until the aircraft is in what configuration?
Weight off wheels, nose wheel centered, and both main bogie beams aligned.
When braking without anti-skid (BRK A/SKID switch selected to ALTN/OFF) the BRAKES indicator should be monitored to limit brake pressure to what psi?
1,000 psi
During normal operation of the braking system, what happens at the first movement of a brake pedal?
The Green hydraulic system brake selector valve electrically opens
When is the anti-skid system deactivated?
ALTN/OFF is selected on the BRK A/SKID panel
Which gear have brakes and A/SKID?
Main gear only
There are two components in which braking is achieved. What are they?
Brake pedals or AUTO BRK system.
When is alternate braking available?
Any time normal brakes are not active.
Which hydraulic system is used for normal braking?
GREEN
What speed must be achieved during takeoff to automatically apply the selected AUTO BRK mode during a rejected takeoff?
85 KTS
What is a way to disarm the auto brakes after landing?
Apply sufficient force to the brake pedals.
Green hydraulic system pressure is not available and ALTN/ON is selected on the BRK A/SKID panel. Prior to landing, which AUTO BRK system should be selected?
NONE
During normal operations, when is hydraulic pressure removed from the nose wheel steering system?
Nose gear shock absorber extended, towing lever selected to ground tow, or both engine fuel levers selected to OFF.
How is the landing gear extended with a Green hydraulic system failure?
Manually, using a gravity extension procedure.
How does the Normal anti-skid system prevent MLG wheel lock/skidding?
It compares each MLG wheel to the nose wheel rotation.
How is aircraft directional control maintained after landing with a Green hydraulic system failure?
Using rudder pedals and differential braking.
When the aircraft in approach or landing configuration, what is indicated when the red arrow on the Landing Gear Control panel is illuminated?
Landing gear are not down and locked.
What gear handle position must be selected to arm the auto brakes?
The DOWN or OFF position.
How may the auto brakes be monitored for proper operation?
The green flow bars on the switch will illuminate when aircraft’s rate of deceleration matches the mode selected
Which hydraulic system is used when normal brakes are not available?
YELLOW
What activates auto brakes?
The ground spoiler extension command.
