Black Box ME262C Instruções de Operação descarregar pdf (Página 4)

c. Wing flaps.

(1) The Handley-Page type flaps are operated by two push

buttons. (See fig. 3-2). Flap position is indicated by grad-

uations of 0°, 10% 20°, 30°, 40% and 50° marked on the upper

surface of the flap; the 20° position used for take-off is

marked in red.

(2) Emergency lowering of the wing flaps is accomplished by

the use of an emergency compressed air system. Operation is

accomplished by opening the operating handle (See fig. 2-2),

two complete turns. Warning: Be sure the valve is opened

two complete turns.

THROTTLE CONTROLS

a. The throttle controls are located at the pilot's left, (See

fig. 2-9) and are the only power controls on the airplane.

The black buttons, one on each throttle, are used to close

the circuits for starting ignition on the engines. The

throttles are equipped with stops to prevent accidental full

closing and stalling of the engines.

LANDING GEAR CONTROLS

a. Under normal conditions the landing gear is raised or lowered

by use of the two push buttons. (See fig. 3-3). It is

hydraulically operated, but because of the low capacity of

the hydraulic pump, it is slow in operation.

b. Compressed air is used for emergency operation of the under

carriage, but lowers the nose wheel and main undercarriage fair

ing only. The undercarriage itself falls under the influence

of gravity, and locking may require the assistance of slide

slipping.

Operation of the compressed air emergency system is

accomplished by opening the operating handle (See fig. 2-1)

at least two complete turns. Warning: Be sure to open two

complete turns.

c. Landing gear position indicators are provided for each unit

of the undercarriage indicator, (See fig. 3-5) left main gear

indicator, (See fig. 3-6) nose wheel, and indicator, (See

fig. 3-7) right main gear.

BRAKE CONTROLS

a. The brakes embody a conventional hydraulic system, independent

of the landing gear and flap hydraulic system. Operation is

accomplished by applying pressure with the toes on the rudder

pedals.

b. A brake is also incorporated in the nose wheel. Operation is

accomplished by use of the nose wheel brake control lever, (See

fig. 1-17).

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