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2840-01-349-5757
Aircraft Gas Turbine Engine Turbine Shaft
2840013495757 013495757 3090763-1
An item designed to transfer rotary motion from a ROTARY, TURBINE, AIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals. View more Aircraft Gas Turbine Engine Turbine Shaft
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Restrictions 2840-01-349-5757
2840-01-349-5757 is a Aircraft Gas Turbine Engine Turbine Shaft 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 2840-01-349-5757
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-349-5757
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 2840-01-349-5757
- Part Number
- Manufacturer
- Status
- 3090763-1
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-349-5757
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Pacer Dawn
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- Low Pressure Turbine
- Material [MATT]
- Steel Shaft
- Overall Length [ABHP]
- 52.752 Inches Minimum And 52.822 Inches Maximum
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Freight Information 2840-01-349-5757
2840-01-349-5757 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-349-5757 has a variance between NMFC and UFC when transported by rail and the description should be consulted.