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Aviation History
1953
1953 - 0144.PDF
142 FLIGHT, 30 January 1953 SABRE F-86E Installations Fuselage Structure 1. Primary air duct. 2. Longerons. 3. Armour-glass screen (sight reflects on inner surface). Canopy-operating buttons. 5. Canopy manual operating handle 6. Canopy emergency-release. 7. Canopy centre guide-rail. 8. Kick-step. 9. Retractable hand-grip. 10. Fin spars. 11. Main inverter. 12. Antenna and waveguide. 13. Batteries. 14. Transmitter. 15. Computer. 16. Sight amplifier. 17. Voltage regulator. graticule 18. 19. 20. 21. 22. 23. 24. Taxying light (port); landing light (star board). Oxygen filler (two bottles each side of leg-well). Tailplane trim actuator access. Radio compartment (V.H.F. in belly aft of magazines). External power supply to sockets. Rear fuel cell filler. Engine access panel and fuel filter de-icing tank (0.83 gal alcohol). AN/APG 30 radar ELECTRICALLY OPERATED CANOPY \ RADAR SIGHT HEAD TYPE A-1CM (GUNS/ BOMBS/ROCKETS) LIGHT ALLOY BULLET DEFLECTOR PLATES RADAR SERVICING PANEL DIELECTRIC (GLASSCLOTH) NOSECAP NOSEWHEEL ROTATES 90 dtj DURING RETRACTION TO LIE FLAT IN WELL OXYGEN BOTTLES This is by far the most detailed sectional view of the world's first super- ionic fighter to be published to date. It is illustrative, incidentally, of the complex equipment which characterizes the fighting aircraft of today. °J 25. Control-surface cable adjustment access. 26. Hot outlet from air-conditioning unit. 27. Igniter plug access. 28. Compressor section ventilation air intake. 29. Compressor section ventilation air outlet. 30. Rear fuselage ventilation air intake. 31. Ground fire-fighting access; data case; power control emergency hydraulic pump. 32. Speed-brake actuating jack. 33. Emergency control reservoir. 34. Emergency hydraulic accumulator. 35. Power control compensator. 36. Power control normal accumulator. 37. Power control normal reservoir. 38. Heat exchanger (cockpit air-condition ing system). 39. Control-surface cable-duct. 40. Fuel-tank vent. 41. Tailplane front spar moved by (42). 42. Tailpiane actuator jack. 53. Anti-g val 43. Tailplane rear spar (hinged). 54. Navigatio 44. Rudder control quadrant. 45. Tab-actuating motor. Engine 46. Radio compass (type ARN-6) loop 55. Now con antenna. 56. Starter/*' 47. Radio compass sense antenna. 57. Engine *t 48. Cockpit pressure regulator and outlet. 58. Ignition 1 49. Upward identification light. . _ 50. Control column. w,n* 5trlC 51. Port rudder-pedal. 59. Front S|» 52. Engine-power control. 60. Rear spai
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