Building the Supermarine Spitfire

Pilot Controls and Equipment

INTRODUCTION

1. The Spitfire Mk 26 is a two seater low wing monoplane fighter reproduction fitted with a V6 Supersharged 6 Cylinder 310 hp engine with electric variable pitch.

2 .FUEL SYSTEM:

Fuel is carried in a main tank forward of the cockpit and holds 115 litres in total, 110 useable

3. WING TANKS

Port Wing Tank 85 litres

Stbd Wing Tank 85 litres

4. OIL SYSTEM:

The engine is a wet sump of 5 litres

5. ELECTRICAL SYSTEM:

A 12 volt alternator supplies power to two batteries which in turn supplies the whole of the electrical system including the ECU's (engine control units).

6. PRIMARY FLYING CONTROLS:

The control column is of the spade type grip pattern, incorporating the radio PTT button. The rudder pedals are adjustable fore and aft and are fitted with toe brakes.

7.ELEVATOR TRIMMING:

The elevator trim is controlled by a lever on the throttle quadrant.

8. UNDERCARRAIGE CONTROL and INDICATORS:

a)The undercarraige operates with electrical motors on a worm drive and has two main power switches, Up or Down. The motors are activated by two levers in a quadrant on the right hand side of the cockpit marked Chassis.

b) TO RAISE the UNDERCARRAIGE.

First the two switched marked "Undercarriage" must be in the UP position. Next the two levers in the right hand quadrant marked "Undercarriage Chassis" must be gripped firmly and pulled backwards and HELD for 3-4 seconds to allow the undercarriage leg to clear the gate, the two levers engage the electric motors NOT the 2 switches. When the undercarriage is raised the two levers will go in and lock the undercarriage UP

c) To LOWER the UNDERCARRAIGE

The two switches marked Undercarriage must be switched to the DOWN position (the undercarriage will not move until the levers are pulled back.) Grip both levers and pull back marked "Undercarriage Chassis" on the right hand side and hold for 3-4 seconds to clear the lock pin gate when undercarriage is down the handles will go forward again they may need a slight push.

d) UNDERCARRAIGE JAM:

Should the undercarriage levers slip and jam the leg, the undercarriage circuit breaker will pop out. Move the undercarriage switch to the middle position OFF. Push the circuit breaker in and momentarily reverse the electrical switch as the lock pin lever is pulled back, then cycle to undercarriage as required.

9. UNDERCARRIAGE EMERGENCY OPERATION:

In the event of a power or electric motor failure, reach down and pull the handle located on the spar face to release the motor drive, this in turn will allow the undercarriage to fall down. Pull the undercarriage lock pin handle back to unlock the undercarriage. The aircraft may be needed to be banked in some cases to reinsert the main locking pin.

10. ENGINE CONTROLS:

The Thrust lever control is fitted to the left side of the cockpit. Mixture is controlled automatically by the MoTeC ECU.

11. AIRSCREW CONTROLS:

The control for the IVO prop are located forward of the throttle on the dash panel.

12. RADIATOR FLAP CONTROL:

The flap at the outlet end of the radiator duct is operated by a vernier lever forward of the Thrust lever and should be OPEN on take off at all times and only moved when in cruise.

13. FUEL PRIMING:

The V6 Isuzu engine does not need priming or choke for cold start.

14. IGNITION SWITCHES:

The ignition switches are located on the bottom of instrument panel in the middle.

15. COCKPIT ACCOMMODATION AND EQUIPMENT:

Pilots seat has 3 positions of adjustment.

16. RUDDER PEDALS:

Rudder pedals are adjustable forward and aft movement

17. COCKPIT DOOR:

To facilitate entry to the cockpit a portion of the coaming rail on the port side is hinged. The door catches are released by means of a handle at the forward end.

18. HOOD LOCKING CONTROL:

The sliding hood is provided with spring catches for holding it shut. The catches are released by two finger levers at the forward end of the hood from the outside; with the hood closed the catches can be released by lifting a small knob at the top of the hood.

19. COCKPIT VENTILATION:

Two small air vents are on each side of the instrument panel on top. Rotate for air.

20. MIRRORS:

A mirror providing a rearward view is fitted to the top of the windscreen.

21. MAP CASES:

A map case is provided on the left hand side of the cockpit and behind pilots seat.