2835-01-214-1069

Nonaircraft Gas Turbine Engine Combustion Chamber

2835012141069 012141069 623514 POSITION 5

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

2835-01-214-1069 CHAMBER,COMBUSTION,NONAIRCRAFT GAS TURBINE ENGINE 2835012141069 012141069

Managed by United States
NSN Created on 6 Aug 1985
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
2835-01-214-1069 CHAMBER,COMBUSTION,NONAIRCRAFT GAS TURBINE ENGINE 2835012141069 012141069 1/1
NSN 2835-01-214-1069 (Generic Image) 1/1

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623514 POSITION 5 The portion of a ENGINE, GAS TURBINE, NONAIRCRAFT in which fuel is burned.
United States (US) 4. 2835-01-214-1069 Marketplace Restrictions Approved Sources Datasheet Management
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Combustion Chamber2835012141069 012141069 623514 //www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-214
Y | DAC: 5 20 Oct 1974 2835-01-714-5035 GEK 134492 FIG 30 INDEX 7RNCC: 5 | RNVC: 2 | DAC: D 2835-01-214-1069

2835-01-214-1069 Demil Restrictions 2835-01-214-1069

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

2835-01-214-1069 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. This item does not contain a precious metal.

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