2840-00-875-9980

Aircraft Gas Turbine Engine Combustion Chamber

2840008759980 008759980 623020

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

2840-00-875-9980 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840008759980 008759980

Managed by United States
NSN Created on 6 Nov 1967
Data Last Changed
November 2023
NATO Update Count
25
NATO Data Quality
2840-00-875-9980 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840008759980 008759980 1/1
NSN 2840-00-875-9980 (Generic Image) 1/1

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623020 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned.
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2840-00-875-9980 Demil Restrictions 2840-00-875-9980

DEMIL: B | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: U | EDC: | ADPEC:

2840-00-875-9980 is a Aircraft Gas Turbine Engine Combustion Chamber that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. The precious metals content of this item is unknown.

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