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2840-01-596-1918
Aircraft Gas Turbine Engine Fan Vane Assembly
2840015961918 015961918 1529517-114
A stationary item designed for the purpose of directing air at the proper angle and velocity from a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE, FAN, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Fan Vane Assembly
January 2023
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Restrictions 2840-01-596-1918
2840-01-596-1918 is a Aircraft Gas Turbine Engine Fan Vane Assembly 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 Non-Critical Munitions List Item or a Non-Sensitive Commerce Control List Item and cannnot be in the possession of any party outside of the USA who is a 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 2840-01-596-1918
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-596-1918
- United Kingdom (ZK01)
- Effective Date:
- 1 May 2011
Approved Sources 2840-01-596-1918
- Part Number
- Manufacturer
- Status
- 1529517-114
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-596-1918
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Special Features [FEAT]
- 1 Unit Per Assy;Det In 57-53-03,Fig.1
- End Item Identification [AGAV]
- Tri-Star L1011-500 Acft
- Part Name Assigned By Controlling Agency [CXCY]
- Vane Assy, No. 3, Outbd, Rh
NATO Stock Numbers Related to 2840-01-596-1918
Freight Information 2840-01-596-1918
2840-01-596-1918 has freight characteristics.. 2840-01-596-1918 has a variance between NMFC and UFC when transported by rail and the description should be consulted.