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2840-01-337-1659
Aircraft Gas Turbine Engine Turbine Shaft
2840013371659 013371659 3072715-3
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
January 2023
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Related Documents 2840-01-337-1659 1+ Documents (More...)
/fsc-2840/us 2840-01-337-1659 Aircraft Gas Turbine Engine Turbine Shaft United States (US) 4. 2840-01
RQST NE Restrictions 2840-01-337-1659 DEMIL: D | DEMILI : | CRITICALITY : X | HMIC : N | PMIC :
Restrictions 2840-01-337-1659
2840-01-337-1659 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 is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. The precious metals content of this item is unknown.
Import and Export 2840-01-337-1659
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-337-1659
- France (ZF01)
- Effective Date:
- 1 Apr 1991
Approved Sources 2840-01-337-1659
- Part Number
- Manufacturer
- Status
- 3072715-3
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-337-1659
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Specification/Standard Data [ZZZK]
- 99193-3072715 Manufacturers Standard
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Freight Information 2840-01-337-1659
2840-01-337-1659 has freight characteristics managed by France.. 2840-01-337-1659 has a variance between NMFC and UFC when transported by rail and the description should be consulted.