Issued with A.L.No.19/F A.P.1565B, Vol.I Sect.I
37. Camera
(a) A G.4B cine-camera is fitted in the leading edge of the
port plane, near the root end and is operated by the
cannon-firing button on the control column spade grip,
a succession of exposures being made during the whole
time the button is depressed, providing the selector
switch (5) on the left-hand side of the cockpit is ON.
(b) A footage indicator and an aperture switch are mounted
on the wedge plate above the throttle lever. The switch
enables either of the two camera apertures to be selected,
the smaller aperture being used for sunny weather.
A stowage clip is provided to receive the electrical
cable (13) when the indicator and switch are not fitted.
NAVIGATIONAL, SIGNALLING AND LIGHTING EQUIPMENT
38. Wireless
(a) The aeroplane is equipped with a combined transmitter,
receiver, either type T.R.9D or T.R.1133, and an R.3002
set.
(b) With the T.R.9D installation a type C mechanical
controller (19) is fitted on the port side of the
cockpit above the throttle lever and a remote contactor
(66) and contactor master switch are fitted on the right
hand side of the cockpit. The master contactor is
mounted behind the pilot's headrest and a switch
controlling the heating element is fitted on the forward
bracket of the mounting. The heating element should
always be switched OFF when the pilot leaves the
aeroplane. The microphone/telephone socket is fitted
on the right hand side of the pilot's seat.
(c) With the T.R.1133 installation the contactor gear and
microphone/telephone socket are as for the T.R.9D
installation, but the type C mechanical controller is
replaced by a push-button electrical control unit.
39. Navigation and identification lamps
(a) The switch (24) controlling the navigation lamps is on
the instrument panel.
F.S/6
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