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2840-01-435-7430
Aircraft Gas Turbine Engine Turbine Rotor
2840014357430 014357430 726247
A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Rotor
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Restrictions 2840-01-435-7430
2840-01-435-7430 is a Aircraft Gas Turbine Engine Turbine Rotor 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 2840-01-435-7430
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-435-7430
- Portugal (ZP01)
- Effective Date:
- 1 Aug 1996
Approved Sources 2840-01-435-7430
- Part Number
- Manufacturer
- Status
- 726247
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-435-7430
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Used On Tf-30P408 Aircraft Gas Turbine Engine
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Freight Information 2840-01-435-7430
2840-01-435-7430 has freight characteristics.. 2840-01-435-7430 has a variance between NMFC and UFC when transported by rail and the description should be consulted.