Revised December 1941. AIR PUBLICATION 1565B
Issued with A.L.No.19/F Volume I and
Pilot's Notes.
SECTION I
PILOT'S CONTROLS AND EQUIPMENT
INTRODUCTION
1. The Spitfire IIA and IIB are single seat, low wing
monoplane fighters each fitted with a Merlin XII
engine and a de Havilland 20° (P.C.P.) or Rotol 35°
constant speed airscrew.
MAIN SERVICES
2. Fuel System -
Fuel is carried in two tanks mounted one above the
other (the lower one is self-sealing) forward of the
cockpit and is delivered by an engine driven pump.
The tank capacities are as follows:
Top tank: 48 gallons
Bottom tank: 37 gallons
The top tank feeds into the lower tank, and the
fuel cock controls (38 and 39), one for each tank,
are fitted below the instrument panel.
3. Oil System -
Oil is supplied by a tank of 5.8 gallons capacity
fitted below the engine mounting, and two oil coolers
in tandem are fitted in the underside of the port
plane.
4. Hydraulic System -
An engine-driven hydraulic pump supplied the power
for operating the undercarriage.
5. Pneumatic System -
An engine-driven air compressor feeds two storage
cylinders for operation of the flaps, brakes, guns
and landing lamps. The cylinders are connected in
series, each holding air at 200 lb/sq.in pressure.
6. Electrical System -
A 12 Volt generator, controlled by a switch (56)
above the instrument panel, supplies an accumulator
which in turn supplies the whole of the electrical
installation. There is a voltmeter (55) on the left
of the switch.
|