2840-14-537-5495

Aircraft Gas Turbine Engine Combustion Chamber

2840145375495 145375495 329-01-009-01 329-01-009 329-01-009-001

The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Aircraft Gas Turbine Engine Combustion Chamber

2840-14-537-5495 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840145375495 145375495

Managed by France
NSN Created on 3 Nov 2003
Data Last Changed
January 2023
NATO Update Count
1
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2840-14-537-5495 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840145375495 145375495 1/1
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2840-14-537-5495 Related Documents Related Documents 2840-14-537-5495 5+ Documents (More...)

| RNVC: 2 | DAC: 5 1 Jan 1960 6625-00-912-0427 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-537-5495
2840145375495 145375495,329-01-009-01 web browser . 2840-14-537-5495Aircraft Gas Turbine Engine
Combustion Chamber2840145375495 145375495 329-01 -009-01 329-01-009 329-01-009-001 The portion of an
Aircraft from France (FR) Sep 1979 2995-14-451-6417 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-537-5495
2840145375495 145375495,329-01-009-01 and outer case. https//www.nsnlookup.com /cage Safran Power
2840-14-231-8093 2840142318093 142318093 is the portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Nov 1989 2995-14-451-6417 De Demarreur Corps 047-02-011RNCC: 3 | RNVC: 2 | DAC: 2 28 Nov 1991 2840-14-537-5495
Aircraft Gas Turbine Engine Combustion Chamber 329-01-009-01RNCC: 3 | RNVC: 2 | DAC: 2329-01-009RNCC
Turbine Engine Combustion Chamber NO PRIMARY REF14-361-4535RNCC: 3 | RNVC: 2 | DAC: 6 24 Jan 1980 2840-14-537-5495

2840-14-537-5495 Demil Restrictions 2840-14-537-5495

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-14-537-5495 is a Aircraft Gas Turbine Engine Combustion Chamber

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