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2840-01-623-2301
Aircraft Gas Turbine Engine Turbine Rotor Blade
2840016232301 016232301 5051T48P02
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
2
Marketplace 2840-01-623-2301
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United States (US) 4. 2840-01-623-2301 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 2840-01-623-2301
2840-01-623-2301 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. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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 2840-01-623-2301
- Schedule B
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- HTS Code
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End Users 2840-01-623-2301
- Spain (YB01)
- Effective Date:
- 1 Nov 2013
Approved Sources 2840-01-623-2301
- Part Number
- Manufacturer
- Status
- 5051T48P02
- Manufacturer
- 05326 - General Electric Co Aviation (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 2840-01-623-2301
Freight Information 2840-01-623-2301
2840-01-623-2301 has freight characteristics.. 2840-01-623-2301 has a variance between NMFC and UFC when transported by rail and the description should be consulted.