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2840-01-481-6878
Aircraft Gas Turbine Engine Turbine Disk
2840014816878 014816878 3002618-1
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
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3002618-1 /www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-481-6878 Aircraft Gas Turbine Engine Turbine
Restrictions 2840-01-481-6878
2840-01-481-6878 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. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 2840-01-481-6878
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-481-6878
- France (ZF01)
- Effective Date:
- 1 Jan 2001
Approved Sources 2840-01-481-6878
- Part Number
- Manufacturer
- Status
- 3002618-1
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-481-6878
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Engine Section Location [CZBJ]
- Turbine
- Stage Number [CZCJ]
- 6
- End Item Identification [AGAV]
- Atf3-6A-3C Engine
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Freight Information 2840-01-481-6878
2840-01-481-6878 has freight characteristics.. 2840-01-481-6878 has a variance between NMFC and UFC when transported by rail and the description should be consulted.