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2840-01-692-5739

Aircraft Gas Turbine Engine Turbine Component Support

2840016925739 016925739 4326504

A support designed for a TURBINE ASSEMBLY,AIRCRAFT GAS TURBINE ENGINE or one of its components. Excludes SUPPORT,SEAL,AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Component Support

2840-01-692-5739 SUPPORT,TURBINE COMPONENT,AIRCRAFT GAS TURBINE ENGINE 2840016925739 016925739

Managed by United States
NSN Created on 22 Dec 2020
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-01-692-5739 SUPPORT,TURBINE COMPONENT,AIRCRAFT GAS TURBINE ENGINE 2840016925739 016925739 1/1
NSN 2840-01-692-5739 (Generic Image) 1/1

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2840-01-692-5739 Related Documents Related Documents 2840-01-692-5739 5+ Documents (More...)

Documents 7025-00-432-6504 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-692-5739
2840016925739 016925739,4326504 | RNVC: 2 | DAC: 5 8 Jun 2017 2840-01-692-5739 https//www.nsnlookup.com
Gas Turbine Engine Turbine Component Support 3091719-5RNCC: 3 | RNVC: 2 | DAC: 5 8 Jun 2017 2840-01-692-5739
3120-99-432-6504 3120994326504 994326504 is a tubular shaped item with or without flange(s) designed to reduce friction and carry a kinetic load on the surface(s) parallel to the axis of the bore. it must have a visible or detectable means of lubrication or be self-lubricated. the over all length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body, except for straight tubular (without flange or shoulder) items having a bearing surface(s) parallel to the axis of the bore only. includes items which are divided into two or more segments which include 180 degrees (3.141 radians) or less of the bearing periphery. see also bushing, sleeve; spacer, sleeve; and washer (as modified). excludes pin, hollow.
1560-01-432-6504 1560014326504 014326504 is a tank installed as a component of an airframe.
1670-14-432-6504 1670144326504 144326504 is a line, cable, or webbing with an attaching device at either end, intended to extend the length of the parachute static line.

2840-01-692-5739 Demil Restrictions 2840-01-692-5739

DEMIL: D | DEMILI: 1 | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-692-5739 is a Aircraft Gas Turbine Engine Turbine Component Support that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-692-5739 HTS and ScheduleB Import and Export 2840-01-692-5739

2840-01-692-5739 Manufacturers Approved Sources 2840-01-692-5739

2840-01-692-5739 Management Data Management Data 2840-01-692-5739

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Dec 2020
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
RF
F-119-PW-100 FOR ATF-ENGINE
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
T
Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).

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