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2840-01-506-0261
Aircraft Gas Turbine Engine Turbine Shaft
2840015060261 015060261 6068T41G01
An item designed to transfer rotary motion from a ROTARY, TURBINE, AIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals. View more Aircraft Gas Turbine Engine Turbine Shaft
January 2023
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Restrictions 2840-01-506-0261
2840-01-506-0261 is a Aircraft Gas Turbine Engine Turbine Shaft 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 2840-01-506-0261
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-506-0261
- Spain (YB01)
- Effective Date:
- 1 Mar 2003
- Republic of Korea (ZH01)
- Effective Date:
- 1 Sep 2014
- NATO Maintenance and Supply Agency (ZX01)
- Effective Date:
- 1 Jan 2014
Approved Sources 2840-01-506-0261
- Part Number
- Manufacturer
- Status
- 6068T41G01
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-506-0261
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Ct7-9 Turboprop Engine
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Freight Information 2840-01-506-0261
2840-01-506-0261 has freight characteristics.. 2840-01-506-0261 has a variance between NMFC and UFC when transported by rail and the description should be consulted.