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OPERATIONS MANUAL

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Landing Gear<br />

System Overview:<br />

Gear steering<br />

The landing gear consists of 2 body gear, 2 wing gear, and 1 nose gear.<br />

The body gear and the nose gear are steerable. The steering mechanism is<br />

powered by hydraulic system 1. The flight deck provides a steering tiller for<br />

the captain and one for the first officer. When the tiller is fully rotated to<br />

the left or right, the nose gear is turned by 70° into the respective direction.<br />

The body gear turns out of its center position when the nose gear turn<br />

angle exceeds 20°, and when the wheel speed is below approximately 18 kt.<br />

Otherwise, the body gear is centered. It is also centered when the IRS is<br />

aligned and the IRS computed groundspeed is above circa 45 kt, or when<br />

the air-ground logic is in air mode. When the body gear turns, it turns<br />

opposite to the nose gear direction; this is because the body gear is located<br />

aft of the aircraft’s center axis. Body gear steering reduces the turning radius<br />

of the aircraft.—The nose gear can also be turned by the rudder pedals up<br />

to 7° in either direction.<br />

Wheel brakes<br />

The pilots’ brake pedals allow symmetric and asymmetric braking of the<br />

wing and body gear. There are no brakes on the nose gear. The normal<br />

brake system is powered by hydraulic system 4. If this fails, the alternate<br />

brake system activates. The alternate brake system is powered by hydraulic<br />

system 1; or, if that fails, by hydraulic system 2.—Autobrakes may be<br />

armed with a preselected, fixed groundspeed deceleration for the landing<br />

rollout; or may be armed for a rejected takeoff which will aim at maximum<br />

deceleration.—A parking brake lever can be used to lock the brake pedals<br />

in the fully depressed positions. (In the simulator, the brakes can be promptly<br />

cooled by the Cool brakes button on Instructor > Situation > Service.)<br />

Antiskid<br />

The antiskid system operates during autobrake activity as well as during<br />

manual braking. It detects skidding by comparing the wheel speeds with the<br />

IRS computed groundspeed. When skidding is detected, the brake pressure<br />

on the affected wheels is automatically reduced.<br />

Brake torque limiters<br />

Each wheel is fitted with a brake torque sensor. When an excessive torque<br />

is detected, the brake pressure is reduced in order to prevent structural<br />

damage.<br />

(continued next page)<br />

— Page 470 —<br />

For preview only. Not for sale. Many pages are intentionally removed.

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