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2835-01-273-0948

Nonaircraft Gas Turbine Engine

2835012730948 012730948 3800050-5-1

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

2835-01-273-0948 ENGINE,GAS TURBINE,NONAIRCRAFT 2835012730948 012730948

Managed by United States
NSN Created on 19 Feb 1988
Data Last Changed
January 2023
NATO Update Count
7
NATO Data Quality
2835-01-273-0948 ENGINE,GAS TURBINE,NONAIRCRAFT 2835012730948 012730948 1/1
NSN 2835-01-273-0948 (Generic Image) 1/1

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2835-01-273-0948 Related Documents Related Documents 2835-01-273-0948 5+ Documents (More...)

| RNVC: 2 | DAC: 6 2 Apr 2002 8430-38-000-5051 https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-273-0948
Nonaircraft Gas Turbine Engine 2835012730948 2835-01-273-0948 2835012730948 012730948 is a continuous
Documents 2835-01-389-1928 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-273-0948
Nonaircraft Gas Turbine Engine 2835012730948 https//www.nsnlookup.com /nato/nato-stock-numbers/
In; Width 4.350 InEnd Item Identification [AGAV]Used On Gas Turbine Engine P/N 3800050-5 Nsn 2835-01-273-0948
2835-00-809-8316 2835008098316 008098316 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.
2835-01-389-1928 Nonaircraft Gas Turbine Engine 3800556-1RNCC: 3 | RNVC: 2 | DAC: 5 19 Apr 1994 2835-01-273-0948

2835-01-273-0948 Demil Restrictions 2835-01-273-0948

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

2835-01-273-0948 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.

2835-01-273-0948 HTS and ScheduleB Import and Export 2835-01-273-0948

2835-01-273-0948 End Users End Users 2835-01-273-0948

Canada (ZC01)
Effective Date:
1 Apr 1991
Denmark (ZS01)
Effective Date:
1 Jul 1999

2835-01-273-0948 Manufacturers Approved Sources 2835-01-273-0948

2835-01-273-0948 Technical Data Datasheet 2835-01-273-0948

Characteristic
Specifications
FIIG
A526A0
Part Name Assigned By Controlling Agency [CXCY]
Engine,Gas Turbine

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2835-01-273-0948 Freight Data Freight Information 2835-01-273-0948

2835-01-273-0948 has freight characteristics managed by Canada.. 2835-01-273-0948 has a variance between NMFC and UFC when transported by rail and the description should be consulted.