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2840-01-413-6724
Aircraft Gas Turbine Engine Compressor Rotor
2840014136724 014136724 108R781G28
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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RQST NE Updated Every Day 2840-01-413-6724 RQST Updated Every Day 2840-01-413-6724 RQST NE Related Documents
pressure, direction RQST NE Updated Every Day 2840-01-413-6724 RQST Updated Every Day 2840-01-413-6724
Restrictions 2840-01-413-6724
2840-01-413-6724 is a Aircraft Gas Turbine Engine Compressor Rotor 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 2840-01-413-6724
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-413-6724
- Italy (ZR01)
- Effective Date:
- 1 May 1995
Approved Sources 2840-01-413-6724
- Part Number
- Manufacturer
- Status
- 108R781G28
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 2840-01-413-6724
Freight Information 2840-01-413-6724
2840-01-413-6724 has freight characteristics.. 2840-01-413-6724 has a variance between NMFC and UFC when transported by rail and the description should be consulted.