J79-8/10 Aircraft Parts

(Page 5) End item NSN parts page 5 of 6
Part Number
NSN
NIIN
5018M12P01 Nozzle Segment
008347628
5019M36P01 Fuel Tube Bracket
009455089
5022M71G01 Fuel Tube Assembly
000865899
5022M74P01 Engine Angle Bracket
002000189
51154 Air Duct Hose
008038359
51154-60FT Air Duct Hose
008038359
517D227G1 Am Bracket Assembly
000192570
517D548G1 Lube No 3 Tube Assembly
009455095
517D628P03 Nonmetallic Hose Assembly
009173843
517D628P04 Nonmetallic Hose Assembly
009173843
517D733G01 Lube No 3 Tube Assembly
009455095
5208-034 Fuel Fitting Assembly
004209574
54400-428-637 Compressor Roto Self Locking Nut
007032184
54400-428S37 Compressor Roto Self Locking Nut
007032184
54406-524-537 Co Self Locking Nut
007032200
54406-524-S37 Co Self Locking Nut
007032200
5505E310F Push On Nut
006852551
5505F310F Push On Nut
006852551
560917-2 Valve
007162665
560921 Adjusting Screw
007162609
Page: 5

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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