2840-14-480-8100
Aircraft Gas Turbine Engine Combustion Chamber
2840144808100 144808100 300-555-125-0
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 4 Apr 1996
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
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drives, thumb drives and subsystem device drivers. https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-480-8100
2840144808100 144808100,300-555-125-0 2840-14-480-8100 2840144808100 144808100 is the portion of
2840144808100 144808100,300-555-125-0 2840-14-480-8100 2840144808100 144808100 is the portion of
Restrictions 2840-14-480-8100
End Users 2840-14-480-8100
- France (ZF)
Approved Sources 2840-14-480-8100
- Part Number
- Manufacturer
- Status
- 300-555-125-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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