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2840-01-512-7715
Aircraft Gas Turbine Engine Compressor Disk
2840015127715 015127715 23071396
An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Disk
January 2023
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Restrictions 2840-01-512-7715
2840-01-512-7715 is a Aircraft Gas Turbine Engine Compressor 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 2840-01-512-7715
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-512-7715
- Australia (ZA01)
- Effective Date:
- 1 Nov 2004
- Belgium (ZB01)
- Effective Date:
- 1 Nov 2004
- Canada (ZC01)
- Effective Date:
- 1 Dec 2011
- United Kingdom (ZK01)
- Effective Date:
- 1 Sep 2003
Approved Sources 2840-01-512-7715
- Part Number
- Manufacturer
- Status
- 23071396
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-512-7715
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Engine Section Location [CZBJ]
- Compressor
- End Item Identification [AGAV]
- Ae2100a, Ae2100c, Ae3007, Ae2100d2, Ae2100d3, J Engines, Aircraft Engines
NATO Stock Numbers Related to 2840-01-512-7715
Freight Information 2840-01-512-7715
2840-01-512-7715 has freight characteristics.. 2840-01-512-7715 has a variance between NMFC and UFC when transported by rail and the description should be consulted.