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2840-01-074-7246
Aircraft Gas Turbine Engine Turbine Shaft
2840010747246 010747246 3001758-2
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 2840-01-074-7246
2840-01-074-7246 is a Aircraft Gas Turbine Engine Turbine Shaft that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-074-7246
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-074-7246
- US Coast Guard (C057)
- Effective Date:
- 1 Apr 1991
Approved Sources 2840-01-074-7246
- Part Number
- Manufacturer
- Status
- 3001758-2
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-074-7246
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Diameter [ABMZ]
- 1.775 Inches Nominal
- Engine Section Location [CZBJ]
- High Pressure Turbine
- Material Thickness [ABPX]
- 0.167 Inches Nominal
- Material [MATT]
- Steel Corrosion Resisting Overall
- Overall Length [ABHP]
- 3.815 Inches Nominal
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Freight Information 2840-01-074-7246
2840-01-074-7246 has freight characteristics.. 2840-01-074-7246 has a variance between NMFC and UFC when transported by rail and the description should be consulted.