2840-00-675-7263

Aircraft Gas Turbine Engine Compressor Vane Assembly

2840006757263 006757263 369002

A stationary item designed for the purpose of directing air at the proper angle and velocity from a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Compressor Vane Assembly

2840-00-675-7263 VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840006757263 006757263

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
7
NATO Data Quality
2840-00-675-7263 VANE ASSEMBLY,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840006757263 006757263 1/1
NSN 2840-00-675-7263 (Generic Image) 1/1

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2840-00-675-7263 Related Documents Related Documents 2840-00-675-7263 5+ Documents (More...)

to enable JavaScript in your web browser . 4730-17-101-6255Tube Tee4730171016255 171016255 0369002 369002
2840006757263 006757263,369002 browser . 2840-00-675-7263Aircraft Gas Turbine Engine Compressor
Vane Assembly2840006757263 006757263 369002 enable JavaScript in your web browser . 5975-01-702-3751Rigid
Aircraft Gas Turbine Engine Compressor Vane Assembly 274875RNCC: 3 | RNVC: 2 | DAC: 5 1 Jan 1963 2840-00-675-7263
1680-01-341-1993 1680013411993 013411993 is a device designed to actuate the mechanism of a door latch, either by a turning or pulling of the handle, or by operation of a push button or trigger, and it may be with or without an escutcheon plate. exludes items having an integral latch. see also doorknob.
5970-00-764-9622 5970007649622 007649622 is an insulator that is essentially thin and flat, with one through hole centrally located. the general shape may vary by the addition of features such as beveled edges, indented surfaces, through hole keys, and/or peripheral flats. the thickness measured between the two parallel bearing surfaces must not exceed 25 percent of the outside diameter or the shortest distance between peripheral flats. the thickness measured between the two parallel bearing surfaces must not exceed 25 percent of the outside diameter or the shortest distance between peripheral flats. excludes items with more than one hole. see also insulator, disk; insulator, bead; insulator, bushing; and insulator, plate
enable JavaScript in your web browser . 5975-01-702-3751Rigid Metal Conduit5975017023751 017023751 130-369002
Code Subscribe to View HTS Code Approved Sources 5975-01-702-3751 Part NumberManufacturerStatus130-369002

2840-00-675-7263 Demil Restrictions 2840-00-675-7263

DEMIL: B | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-00-675-7263 is a Aircraft Gas Turbine Engine Compressor Vane Assembly that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

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