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Aviation History
1944
1944 - 0123.PDF
JANUARY 2OTH, 1944 FLIGHT 63 Typhoon rawing by M. A. Millar WARM AIR CONDUIT TO CANNON / UNDERCARRIAGE WHEEL BAY WINC MAIN SPARS SELF-SEALING PETROL TANK AMMUNITION MAGAZINES Most of the main structural features are shown in this drawing. The fuselage is a girder in front while the rear portion is of stressed-skin construction. A more detailed view of this is on page 64. The pilot's cockpit is roomy, in spite of the quantity of equip ment installed there. The new Perspex bubble hood is^i great improvement on the original one and gives a remad^»ly un restricted view. The seat is mounted on a parallelogrSR frame which allows of raising and lowering it. Gun firing control is electro-pneumatic, the press-button on the spade-grip being a switch which closes the circuit and opens the pneumatic valves. AILERON LANDING LIGHT NAVIGATION UCHT
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