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2840-01-623-2303
Aircraft Gas Turbine Engine Compressor Rotor
2840016232303 016232303 6071T67P02
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor
January 2023
2

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Related Documents 2840-01-623-2303 1+ Documents (More...)
United States (US) 4. 2840-01-623-2303 Marketplace Restrictions Approved Sources Datasheet Management
Restrictions 2840-01-623-2303 DEMIL: D | DEMILI : 1 | CRITICALITY : X | HMIC : N | PMIC : A | EDC
Restrictions 2840-01-623-2303
2840-01-623-2303 is a Aircraft Gas Turbine Engine Compressor Rotor that does not have a nuclear hardened feature or any other critical feature 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.
Import and Export 2840-01-623-2303
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-623-2303
- Spain (YB01)
- Effective Date:
- 1 Nov 2013
Approved Sources 2840-01-623-2303
- Part Number
- Manufacturer
- Status
- 6071T67P02
- Manufacturer
- 05326 - General Electric Co Aviation (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 2840-01-623-2303
Freight Information 2840-01-623-2303
2840-01-623-2303 has freight characteristics.. 2840-01-623-2303 has a variance between NMFC and UFC when transported by rail and the description should be consulted.