2840-14-469-4468
Turbo-Jet Engine
2840144694468 144694468 CF6-80C2-A2
A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust. View more Turbo-Jet Engine
Managed by France
NSN Created on 26 Apr 1994
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality

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RQST NE Updated Every Day 2840-14-469-4468 RQST Updated Every Day 2840-14-469-4468 RQST NE Related
Components from France (FR) 26 Apr 1994 2840-14-544-0351 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-469-4468
Turbo-Jet Engine 2840144694468 144694468 Turbines and Jet Engines, Aircraft, Prime Moving https
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Turbo-Jet Engine 2840144694468 144694468 Turbines and Jet Engines, Aircraft, Prime Moving https
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Turbo-Jet Engine 2840144694468 144694468 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving
Turbo-Jet Engine 2840144694468 144694468 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving
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Turbo-Jet Engine 2840144694468 144694468 enable JavaScript in your web browser . 2840-14-469-4468Turbo-Jet
Engine2840144694468 144694468 CF6-80C2 www.nsnlookup.com /fsg-28/fsc-2840 Gas Turbines and https//www.nsnlookup.com
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1975 2840-14-386-8385 Fluid Filter Cover 613-558-031-0RNCC: 3 | RNVC: 2 | DAC: 4 24 Aug 1983 2840-14-469-4468
Restrictions 2840-14-469-4468
End Users 2840-14-469-4468
- France (ZF)
Approved Sources 2840-14-469-4468
- Part Number
- Manufacturer
- Status
- CF6-80C2-A2
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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