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2835-01-257-1100

Nonaircraft Gas Turbine Engine

2835012571100 012571100 3800280-6-1 DAA3243P003-261 3800280-1 3800280-2-1

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

2835-01-257-1100 ENGINE,GAS TURBINE,NONAIRCRAFT 2835012571100 012571100

Managed by United States
NSN Created on 12 Jun 1987
Data Last Changed
November 2023
NATO Update Count
8
NATO Data Quality
2835-01-257-1100 ENGINE,GAS TURBINE,NONAIRCRAFT 2835012571100 012571100 1/1
NSN 2835-01-257-1100 (Generic Image) 1/1

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2835-01-257-1100 Related Documents Related Documents 2835-01-257-1100 5+ Documents (More...)

Documents 7110-00-872-0125 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-257-1100
Nonaircraft Gas Turbine Engine 2835012571100 on a base, see power unit, gas turbine engine. https
Documents 2835-01-267-4944 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-257-1100
Nonaircraft Gas Turbine Engine 2835012571100 https//www.nsnlookup.com /nato/nato-stock-numbers/
5975-00-458-2680 5975004582680 004582680 is a panel designed to fill a space not occupied by actual operating components, and may have instructions, component designations, or component identifications etched or printed thereon.
2835-01-267-4944 Nonaircraft Gas Turbine Engine 80636-3RNCC: 3 | RNVC: 2 | DAC: 5 12 Nov 1987 2835-01-257-1100
2835-01-242-6668 2835012426668 012426668 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.

2835-01-257-1100 Demil Restrictions 2835-01-257-1100

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

2835-01-257-1100 is a Nonaircraft Gas Turbine Engine that is specifically designed to be or selected as being nuclear hard. In addition it has other critical features such as tolerance, fit restrictions 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.

2835-01-257-1100 Management Data Management Data 2835-01-257-1100

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Mar 2003
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
L
N
Disposal

Air Force Air Force

Fund:
SF
Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
Budget:
8
97X4830.FCL4 - Materiel Support DIV (MSD) - Materiel Support Division (MSD), which includes those Air Force Centrally Managed Investment Items (ERRC XD1=C and XD2=T) except for those still managed in budget programs (BP) 15, 25, 82, 83, and 84 as stock fund exempt. MSD also includes items centrally procured and managed as Expense Items (ERRC XB3=N and XF3=P). Reference AFMAN 23–110, Volume 1, Part 3, Chapter 7, Paragraph 7.3.1
Aggregation Code:
RJ
JET AIRCRAFT ENGINES (FSC RESIDUAL MMAC)
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of “L” or “F”, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
T
Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).

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