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2840-00-571-8854
Aircraft Gas Turbine Engine Turbine Nozzle Assembly
2840005718854 005718854 6846282
A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly
January 2023
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Restrictions 2840-00-571-8854
2840-00-571-8854 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly 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 a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. The precious metals content of this item is unknown.
Import and Export 2840-00-571-8854
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-00-571-8854
- Brazil (YA01)
- Effective Date:
- 1 Jan 2011
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 2840-00-571-8854
- Part Number
- Manufacturer
- Status
- 6846282
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
- 6846282
- 24617 - General Motors Corp (Active)
- Secondary Buy
- Secondary Buy
- 6846282
- 73342 - Allison Transmission Inc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 2840-00-571-8854
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Engine Section Location [CZBJ]
- Turbine
- Criticality Code Justification [CRTL]
- Agav
- End Item Identification [AGAV]
- T-56 Aircraft Engine
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Freight Information 2840-00-571-8854
2840-00-571-8854 has freight characteristics.. 2840-00-571-8854 has a variance between NMFC and UFC when transported by rail and the description should be consulted.