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1 GALLONS FLUID- SPEC . S.! S . GALLONS WATER INJECTIQN FUJIO TANK ~0~g~~E~6 ~NS_~I'äLONS MAlH WHEEL T1RE FUEL SYSTEM STRAINER ; ! MAIN wHEEL SHQCK STRUT (JL-IR) FL\)ID-SPEC. 000 Las, 111,000 LBS , /: /' f · AIR PRESSURE 111 P,S ,1. >1. >1. , «U >I U ' SERVICING DIAGRAM 33 34 F8F-1/-1 B FORWARD COCKPIT AND INSTRUMENT PANEL 1. Ignition Switch 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. o Supereharger Control Armament Master and Gun Switches Gun Sight Bomb, Tank and R. P. Switches Oxgyen Flow Indicator Carburetor Air Control Landing Gear Emergency Control Clock Airspeed Indicator Attitude Gyro Indicator Panel Lights Compass Indicator Manifold Pressure Gage Cowl Flap Switch 15.

2. Check-Off List- -"Take Off". 3. Cockpit Sliding Canopy Control. 4. Oxygen Pressure Gage. 5. Oxygen Regulator. 6. Oxygen Flow Indicator. 7. Chartboard RaH. 8. Voltmeter. 9. Electrical Distribution Panel. 10. Fresh Air Control. 11. Radio Control Panel. 12. IFF Destruction Switch. 13. Radio Altitude Limit Switch. 14. Circuit Breaker Panel. 15. Hydraulic Hand Pump. 16. Hand Pump Selector. 17. Oxygen Ta nk Valve Early Models Only. 18. H. Wlng Rack. 19. Canopy Open Lock Release. 20. Auto Pilot Controller.

Bottom, F8F-2N left-hand console with radar control at left bottom. 47 I 48 Very large APS-19 radar pod with its bulky connector viewed from behind while mounted on the right wing of an F8F-2N. Below, right-hand view of the APS-19 pod. Note length of t he 20mm cannon barrels and the flared muzzle flash suppressors. (National Archives) F8F-2P INSTRUMENT PANEL The F8F-2P's electrical control panel was located on the left-hand side of the cockpit adjacent to the intervalometer. It contained the master camera switch, manual and automatie switches, and the camera system warning lights.

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Aviation - The First 100 Years by Bill Gunston

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