PART I - DESCRIPTIVE
reading of the triple pressure gauge main needle. The
audio warning cut-off switch (60) on the starboard side
of the instrument panel enables the noise to be silenced
once the warning has been given.
(e) Two high pressure air bottles which are charged to
1,800-2,000 lb./sq. in., are provided for the emergency
lowering of the undercarriage and flaps respectively. Air
pressure gauges (6) (7) for the bottles are mounted on
the port shelf.
(f) A hydraulic handpump, for ground test purposes, is
fitted in the engine bay.
POWERED FLYING CONTROLS AND
TRIMMERS
20. Flying controls operation
(a) In power
The ailerons and elevators are power-operated, the power
being supplied by hydraulic oil under pressure from the
aircraft hydraulic system. A hydrobooster consisting of
a valve and jack body and jack piston is fitted close to
each control surface. The control column is connected
direct to the valve control rod so that, depending on the
direction of movement of the control column, the valve
opens to admit pressure oil to one side of the jack
piston and at the same time the other side is opened to
return. The piston rod is anchored to the aircraft
structure by means of spring-loaded hydraulically-
operated pawl. The jack body is directly connected to
one end of the control surface. When the pawl is in
position and hydraulic pressure is fed from the valve to
one side of the jack piston, the jack body moves relative
to the piston and deflects the control surface. When
control column movement ceases, the valve closes
causing a hydraulic lock which prohibits further move-
ment of the jack body and control surface.
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