2840-14-208-8813
Aircraft Gas Turbine Engine Combustion Chamber
2840142088813 142088813 057-39-500 057-39-740 0057395000
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 1 Jan 1964
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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057-39-500 057-39-740 0057395000 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned
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Restrictions 2840-14-208-8813
End Users 2840-14-208-8813
- France (ZF)
Approved Sources 2840-14-208-8813
- Part Number
- Manufacturer
- Status
- 057-39-500
- Manufacturer
- F0228 - Safran Helicopter Engines (Active)
- Primary Buy
- Primary Buy
- 057-39-740
- F0228 - Safran Helicopter Engines (Active)
- Primary Buy
- Primary Buy
- 0057395000
- F0228 - Safran Helicopter Engines (Active)
- Secondary Buy
- Secondary Buy
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