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
Managed by France
NSN Created on 3 Nov 2003
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
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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
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
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
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
Restrictions 2840-14-537-5495
End Users 2840-14-537-5495
- Finland (WF)
- Australia (ZA)
- New Zealand (ZE)
- France (ZF)
- Germany (ZG)
- Netherlands (ZN)
- Portugal (ZP)
- Italy (ZR)
Approved Sources 2840-14-537-5495
- Part Number
- Manufacturer
- Status
- 329-01-009-01
- Manufacturer
- F1989 - Safran Power Units (Active)
- Primary Buy
- Primary Buy
- 329-01-009
- F1989 - Safran Power Units (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 329-01-009-001
- F1989 - Safran Power Units (Active)
- Canceled/Obsolete
- Canceled/Obsolete
NATO Stock Numbers Related to 2840-14-537-5495
2840-14-546-8351 2840-21-856-9786 2840-14-361-4538 2840-14-319-3838 2840-21-805-4442 2840-14-527-7194 2840-00-873-3285 2840-14-361-4534 2840-14-436-4514 2840-14-411-8922 2840-00-999-6615 2840-01-364-4456 2840-01-618-2301 2840-01-576-8120 2840-01-434-5745 2840-00-731-0622 2840-14-299-2817 2840-01-353-8344