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2840-01-413-7662
Aircraft Gas Turbine Engine Turbine Disk
2840014137662 014137662 108R747P4
An item having provisions on the outer periphery for attaching a designated number of BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Disk
January 2023
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2840-01-413-7662 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-413-7662
Day 2840-01-413-7662 RQST NE Restrictions 2840-01-413-7662 DEMIL: A | DEMILI : | CRITICALITY : X | HMIC
Restrictions 2840-01-413-7662
2840-01-413-7662 is a Aircraft Gas Turbine Engine Turbine Disk 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 2840-01-413-7662
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-413-7662
- Italy (ZR01)
- Effective Date:
- 1 May 1995
Approved Sources 2840-01-413-7662
- Part Number
- Manufacturer
- Status
- 108R747P4
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-413-7662
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Part Name Assigned By Controlling Agency [CXCY]
- Disk,Gas Turbine Engine
NATO Stock Numbers Related to 2840-01-413-7662
Freight Information 2840-01-413-7662
2840-01-413-7662 has freight characteristics.. 2840-01-413-7662 has a variance between NMFC and UFC when transported by rail and the description should be consulted.