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2840-01-510-4605
Aircraft Gas Turbine Engine Compressor Rotor
2840015104605 015104605 4014T18G04
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
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Restrictions 2840-01-510-4605
2840-01-510-4605 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 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.
Import and Export 2840-01-510-4605
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-510-4605
- Italy (ZR01)
- Effective Date:
- 1 Jul 2003
Approved Sources 2840-01-510-4605
- Part Number
- Manufacturer
- Status
- 4014T18G04
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-510-4605
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- 58-5E Disc 1I Compressor
- Part Name Assigned By Controlling Agency [CXCY]
- Compressor Spool
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Freight Information 2840-01-510-4605
2840-01-510-4605 has freight characteristics.. 2840-01-510-4605 has a variance between NMFC and UFC when transported by rail and the description should be consulted.