2840-14-465-4744
Aircraft Gas Turbine Engine Combustion Chamber
2840144654744 144654744 307-104-409-0
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 30 Sep 1993
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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307-104-409-0 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned.
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Restrictions 2840-14-465-4744
End Users 2840-14-465-4744
- France (ZF)
Approved Sources 2840-14-465-4744
- Part Number
- Manufacturer
- Status
- 307-104-409-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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