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Aviation History
1953
1953 - 0145.PDF
GLASSCLOTH FIN-TIP HOUSING V.H.F./I.F.F ANTENNA 143 TRIM TAB (RUDDER NOT POWER OPERATED) LI GENERAL ELECTRIC J-47 TURBOJET IE EIGHT SINGLE- COMBUSTION STAGE CHAMBERS TURBINE ^ ' ' ,,.*'" ivttUS* .* HlW" ,wvV « te¥* • FLYING TAIL " LINKAGE WITHIN "(SEE SEPARATE •54 DIAGRAM) -JET PIPE ,40 STAINLESS STEEL REAR FUSELAGE •SV 31 MAIN ENGINE- MOUNTING TRUNNION FUSELAGE BREAK-LINE (QUICK DISCONNECTIONS FOR ALL SERVICES) WING FUEL CELL 56 imp gal EACH SIDE SPEED BRAKES These diagrams show the "flying tail" oftheF-86E. The tailplane is seen at its maximum positive and maximum negative settings, and the corresponding movement of the elevators is indicated in each case. ACTUATING JACK AND VALVE FROM CONTROL COLUMN OUTER LIMIT OF DOUBLE SKIN ries within). Utioii FULL-SPAN AUTOMATIC SLATS (FOUR SECTIONS EACH SIDE) 61. Corrugations between double skin. 62. Constructional posts bolted through 63. Gl'assclo'th liner (anti-chafe and bullet deflector). 64- Fuel fillers. 65. Moulded wing-tip. 66. Irving balanced ailerons. 67. Aileron control cables. 68. Aileron actuator access. 69. Slat roller and guide-rail assemblies. 70. Gyrosyn compass flux unit. 71. Flap actuating motor and flexible co ordinating shaft. 72. Flap roller-and-guide-rail assemblies. Undercarriage Unit* 73. Mainwheel operating jack. Uplock cylinder. Downlock cylinder. Wheel-well with raised portion brake drum. 77. Nosewheel operating jack (under air- duct). 74 75 76 for TAILPLANE FULCRUM 78. Steer/damp unit (nosewheel steers 23 deg each side). 79. Nosewheel door and jack. Armament 80. Gun access panel. 81. Magazine door/entry step. 82. Flexible belt-guides. 83. Feed boosters. 84. Gun-heating cables. 85. Spent case and link compartments. 86. Camera gun.
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