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2840-01-382-0688
Aircraft Gas Turbine Engine Compressor Rotor
2840013820688 013820688 3097270-3 3097270
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor
January 2023
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Restrictions 2840-01-382-0688
2840-01-382-0688 is a Aircraft Gas Turbine Engine Compressor Rotor that does not have a nuclear hardened feature, but does have another critical feature or features 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 2840-01-382-0688
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-382-0688
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 2840-01-382-0688
- Part Number
- Manufacturer
- Status
- 3097270-3
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
- 3097270
- 99193 - Honeywell International Inc. (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 2840-01-382-0688
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Pacer Dawn
- Criticality Code Justification [CRTL]
- Czbj
- Engine Section Location [CZBJ]
- Fan
NATO Stock Numbers Related to 2840-01-382-0688
Freight Information 2840-01-382-0688
2840-01-382-0688 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-382-0688 has a variance between NMFC and UFC when transported by rail and the description should be consulted.