Landing Gear

Landing Gear

1. Key Componets

   • Steering
     • Tiller up to 70 degree
     • Rudder pedal to 7 degree
     • Main gear Aft axle steering began when angle greater than 13 degree
   • Breaking
     • Normal Brakes
       • 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
     • Alternated Brakes
       • If HYD R pressure low, C/Reserve system automatically supplies pressure
         • 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
       • IF loss right and C system BRAKE SOURCE light illuminating
         • The following may not be available
           • Alternate brake from the reserve Hydraulic source
           • Normal nose gear extenson
           • Nose wheel Steering
         • Brake Accumulator can Provide several applications or Parking brake applicatoin
     • Anti-skid
       • Normal Wheels independently controlled
       • Alternate brakes controlled as follows
   • Moinoring On GEAR synotpic

2. Air/Grond sensing System

   • Sensors located on each main landing ear beam

3. Operation

   • Gear lever

Images and files in the map