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2840-01-419-5857
Aircraft Gas Turbine Engine Turbine Disk
2840014195857 014195857 868630-7
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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2840-01-419-5857 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-419-5857
Day 2840-01-419-5857 RQST NE Restrictions 2840-01-419-5857 DEMIL: A | DEMILI : | CRITICALITY : X | HMIC
Restrictions 2840-01-419-5857
2840-01-419-5857 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 2840-01-419-5857
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-419-5857
- Spain (YB01)
- Effective Date:
- 1 Sep 1995
Approved Sources 2840-01-419-5857
- Part Number
- Manufacturer
- Status
- 868630-7
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-419-5857
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Ppe 31 Turbo Propeller 331
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Freight Information 2840-01-419-5857
2840-01-419-5857 has freight characteristics.. 2840-01-419-5857 has a variance between NMFC and UFC when transported by rail and the description should be consulted.