J79-8/10 Aircraft Parts

(Page 2) End item NSN parts page 2 of 6
Part Number
NSN
NIIN
105B5366G1 Oil Tank Plate Assembly
000192573
108R241P82 Turbine Frame Pad
008046817
109R178P44 Turbine Frame Pad
008046817
110R102P4 Exhaust Duct Hanger
000206356
110R246G01 Exhaust Nozzle Flap
001780905
110R246G02 Exhaust Nozzle Flap
001780905
110R246G03 Exhaust Nozzle Flap
001780905
12005-74 Airframe Ball Bearing
010045070
12859-2 Wheel
000225136
128999B Instrument Shunt
004968776
133A1083 Duct Anti Parts Kit
007988246
1391-041046 Pressure Indicator
005145334
142794-239ES O-ring
002881953
147-29140 Hose Coupling Nut
005852955
1560-911-1 Dial Pointer
005193354
1570-041040 Pressure Indicator
005145334
1570B041040 Pressure Indicator
005145334
18-1101 Pressure Indicator
005145334
18-2021 Pressure Indicator
005145334
180192 Needle Roller Bearing
005800464
Page: 2

J79-8/10 Aircraft

Picture of J79-8/10 Aircraft

The General Electric J79 is an axial-flow turbojet engine built for use in a variety of fighter and bomber aircraft and a supersonic cruise missile. The J79 was produced by General Electric Aircraft Engines in the United States, and under license by several other companies worldwide.

A commercial version, designated the CJ805, powered the Convair 880, while an aft-turbofan derivative, the CJ805-23, powered the Convair 990 airliners and a single Sud Aviation Caravelle intended to demonstrate to the U.S. market the benefits of a bypass engine over the existing Avon turbojet.

In 1959 the gas generator of the J79 was developed as a stationary 10MW-class (13,000 bhp) free-turbine turboshaft engine for naval power, power generation, and industrial use, called the LM1500. Its first application was in the research hydrofoil USS Plainview.

The J79 was developed in the 1950s for reliable Mach 2 performance. The U.S.A.F. had a requirement to power their next generation bomber which became the Convair B-58 and this application launched the J79.

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