2840-99-687-1641

Aircraft Gas Turbine Engine Combustion Chamber

2840996871641 996871641 NN 16361 G01

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

2840-99-687-1641 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840996871641 996871641

Managed by United Kingdom
NSN Created on 16 Sep 1999
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
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NN 16361 G01 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned.
RQST NE Updated Every Day 2840-99-687-1641 RQST Updated Every Day 2840-99-687-1641 RQST NE Related Documents
,NN 16361 G01 NN 16361 G01 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned.

2840-99-687-1641 Demil Restrictions 2840-99-687-1641

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2840-99-687-1641 is a Aircraft Gas Turbine Engine Combustion Chamber

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