2835-01-166-1272

Nonaircraft Gas Turbine Engine Combustion Chamber

2835011661272 011661272 2182038

The portion of a ENGINE, GAS TURBINE, NONAIRCRAFT 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 Nonaircraft Gas Turbine Engine Combustion Chamber

2835-01-166-1272 CHAMBER,COMBUSTION,NONAIRCRAFT GAS TURBINE ENGINE 2835011661272 011661272

Managed by United States
NSN Created on 8 Nov 1983
Data Last Changed
November 2023
NATO Update Count
8
NATO Data Quality
2835-01-166-1272 CHAMBER,COMBUSTION,NONAIRCRAFT GAS TURBINE ENGINE 2835011661272 011661272 1/1
NSN 2835-01-166-1272 (Generic Image) 1/1

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2182038 The portion of a ENGINE, GAS TURBINE, NONAIRCRAFT in which fuel is burned.
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2835-01-166-1272 Demil Restrictions 2835-01-166-1272

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: U | EDC: A | ADPEC: 0

2835-01-166-1272 is a Nonaircraft Gas Turbine Engine Combustion Chamber that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.

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