2840-14-485-6918
Turbo-Jet Engine
2840144856918 144856918 304-840-002-0
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 6 Feb 1997
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-14-485-6918 5+ Documents (More...)
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Turbo-Jet Engine 2840144856918 144856918 Turbines and Jet Engines, Aircraft, Prime Moving; and
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Documents 2840-39-000-0730 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-485-6918
Turbo-Jet Engine 2840144856918 144856918 .. ) https//www.nsnlookup.com /nato/nato-stock-numbers
Turbo-Jet Engine 2840144856918 144856918 .. ) https//www.nsnlookup.com /nato/nato-stock-numbers
2004 2840-39-000-0730 Turbo-Jet Engine NOMIM 4080400199RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-14-485-6918
26 Apr 1994 2840-14-544-0351 Turbo-Jet Engine CFM56-2CRNCC: 3 | RNVC: 2 | DAC: 4 23 Dec 2004 2840-14-485-6918
Restrictions 2840-14-485-6918
End Users 2840-14-485-6918
- France (ZF)
Approved Sources 2840-14-485-6918
- Part Number
- Manufacturer
- Status
- 304-840-002-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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