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2840-01-302-6541
Aircraft Gas Turbine Engine Turbine Shaft
2840013026541 013026541 23030957
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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/fsc-2840/us 2840-01-302-6541 Aircraft Gas Turbine Engine Turbine Shaft 23030957 An item designed to
DEMIL: D | DEMILI : | CRITICALITY : X | HMIC : N | PMIC : A | Restrictions 2840-01-302-6541 DEMIL
Restrictions 2840-01-302-6541
2840-01-302-6541 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. This item does not contain a precious metal.
Import and Export 2840-01-302-6541
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-302-6541
- Austria (WB01)
- Effective Date:
- 1 Feb 2005
Approved Sources 2840-01-302-6541
- Part Number
- Manufacturer
- Status
- 23030957
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-302-6541
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- T63-A-700 Engine
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Freight Information 2840-01-302-6541
2840-01-302-6541 has freight characteristics.. 2840-01-302-6541 has a variance between NMFC and UFC when transported by rail and the description should be consulted.