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2840-01-413-7671
Aircraft Gas Turbine Engine Turbine Rotor Blade
2840014137671 014137671 107R476P14
An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade
January 2023
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Restrictions 2840-01-413-7671
2840-01-413-7671 is a Aircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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 2840-01-413-7671
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-413-7671
- Italy (ZR01)
- Effective Date:
- 1 May 1995
Approved Sources 2840-01-413-7671
- Part Number
- Manufacturer
- Status
- 107R476P14
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-413-7671
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Part Name Assigned By Controlling Agency [CXCY]
- Blade,Turbine Engine
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Freight Information 2840-01-413-7671
2840-01-413-7671 has freight characteristics.. 2840-01-413-7671 has a variance between NMFC and UFC when transported by rail and the description should be consulted.