Landing Gear - created from Mind Map

Seite 1

Key Componets

Air/Grond sensing System

Operation

Steering

Breaking

Moinoring On GEAR synotpic

Tiller up to 70 degree

Rudder pedal to 7 degree

Main gear Aft axle steering began when angle greater than 13 degree

Normal Brakes

Alternated Brakes

Anti-skid

Right Hydralic system

Auto BRAKE system

Both throtthles are retracted to idle and the wheels have spun up

Air Plane on the GND and spd less 85 and Both throttle are retard to idle

If HYD R pressure low, C/Reserve system automatically supplies pressure

IF loss right and C system BRAKE SOURCE light illuminating

If C system quantity is low C1 primary pump is isolated from center hydraulic pressure through HDY system to provides and alternate braking pressure source

The following may not be available

Brake Accumulator can Provide several applications or Parking brake applicatoin

Alternate brake from the reserve Hydraulic source

Normal nose gear extenson

Nose wheel Steering

Normal Wheels independently controlled

Alternate brakes controlled as follows

Sensors located on each main landing ear beam

Gear lever