2835-01-381-6186

Nonaircraft Gas Turbine Engine

2835013816186 013816186 GTC85-SUPER71

A continuous combustion type engine. Consists primarily of a COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE; CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It may have a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft and/or pneumatic power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE. View more Nonaircraft Gas Turbine Engine

2835-01-381-6186 ENGINE,GAS TURBINE,NONAIRCRAFT 2835013816186 013816186

Managed by United States
NSN Created on 20 Oct 1993
Data Last Changed
November 2023
NATO Update Count
4
NATO Data Quality
2835-01-381-6186 ENGINE,GAS TURBINE,NONAIRCRAFT 2835013816186 013816186 1/1
NSN 2835-01-381-6186 (Generic Image) 1/1

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2835-01-381-6186 Related Documents Related Documents 2835-01-381-6186 4+ Documents (More...)

Documents 2835-01-400-2135 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-381-6186
Nonaircraft Gas Turbine Engine 2835013816186 nato-stock-numbers/inc Nonaircraft Gas Turbine Engine
3 | RNVC: 2 | DAC: 4 30 Sep 1999 2835-01-400-2135 Nonaircraft Gas Turbine Engine 10 Dec 1994 2835-01-381-6186
2835-01-341-5955 2835013415955 013415955 is a continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft and/or pneumatic power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.

2835-01-381-6186 Demil Restrictions 2835-01-381-6186

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

2835-01-381-6186 is a Nonaircraft Gas Turbine Engine 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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