2840-14-363-2160
Aircraft Gas Turbine Engine Combustion Chamber
2840143632160 143632160 RK32129AM0D1147 85-800-5933
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 Apr 1980
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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RK32129AM0D1147 85-800-5933 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned.
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Restrictions 2840-14-363-2160
End Users 2840-14-363-2160
- France (ZF)
Approved Sources 2840-14-363-2160
- Part Number
- Manufacturer
- Status
- RK32129AM0D1147
- Manufacturer
- F0302 - Safran Transmission Systems (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 85-800-5933
- F5385 - Section De Codification 85 (Cancelled)
- NATO Reference
- NATO Reference
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