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2840-01-621-3882
Aircraft Gas Turbine Engine Turbine Rotor Blade
2840016213882 016213882 5101T38G05
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
3

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Related Documents 2840-01-621-3882 1+ Documents (More...)
United States (US) 4. 2840-01-621-3882 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 2840-01-621-3882
2840-01-621-3882 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. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 2840-01-621-3882
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-621-3882
- Australia (ZA01)
- Effective Date:
- 1 Sep 2013
Approved Sources 2840-01-621-3882
- Part Number
- Manufacturer
- Status
- 5101T38G05
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-621-3882
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Engine Section Location [CZBJ]
- Low Pressure Turbine
- Part Name Assigned By Controlling Agency [CXCY]
- Blade, Rotor-Low Pressure Turbine
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Freight Information 2840-01-621-3882
2840-01-621-3882 has freight characteristics managed by Australia.. 2840-01-621-3882 has a variance between NMFC and UFC when transported by rail and the description should be consulted.