J79-8/10 Aircraft Parts

(Page 3) End item NSN parts page 3 of 6
Part Number
NSN
NIIN
180207 Annular Ball Bearing
005554042
19415-2 Fuel Control Parts Kit
000889934
2-233 N506-65 O-ring
008210664
2-233-N506-65 O-ring
008210664
2-239 L677-70 O-ring
002881953
2-239L1120-70 O-ring
002881953
2-239L677-7 O-ring
002881953
213-10D Hose Coupling Nut
005852955
2400 Thermal Flasher
000847985
25100A15A1B1 Pressure Indicator
005145334
25200A15A1-1A1 Pressure Indicator
005145334
25200A15B1-1A1 Pressure Indicator
005145334
25201-A15B-4-1C2 Pressure Indicator
005145334
25201A15B2-1A1 Pressure Indicator
005145334
25201A15B4-1A1 Pressure Indicator
005145334
25201A15C7-2B2 Pressure Indicator
005145334
260323 Valve
007988316
260333 Seat
007988317
2779K19P001 Balance Weight
008973183
2834 Pin
011292136
Page: 3

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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