J79-8/10 Aircraft Parts

End item NSN parts page 1 of 6
Part Number
NSN
NIIN
02-15080 Wearing Ring
000817106
02-15326-02 Retainer Stop
008715839
02-15326-03 Retainer Stop
008715850
02-15326-04 Retainer Stop
008715853
02-15326-06 Retainer Stop
008715865
02-15326-10 Retainer Stop
008715836
02-15326-15 Retainer Stop
008715834
02-15326-16 Retainer Stop
008715837
02-15326-18 Retainer Stop
000825395
0607-0350-0101 Air Duct Hose
008038359
0607-0350-0102 Air Duct Hose
008038359
10159820 O-ring
005858398
10163871 O-ring
002881953
105B2246P1 Angle Bracket
007988136
105B2281G1 Restrictor Assembly
009118670
105B3357G1 Ab Oil Cool Bracket
008634245
105B3359G1 Ab Oil Cool Bracket
008634246
105B3980P1 Engine Angle Bracket
000192571
105B4607P2 Val Filter Retainer
000195754
105B5186P1 Exhaust Duct Hanger
000206356
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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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