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2840-01-575-4549
Aircraft Gas Turbine Engine Compressor Duct
2840015754549 015754549 4318542
A cylindrical shaped item or a segment thereof designed to direct air into or around a COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. The air is further compressed or used for cooling purposes. View more Aircraft Gas Turbine Engine Compressor Duct
January 2023
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Restrictions 2840-01-575-4549
IUID Required
2840-01-575-4549 is a Aircraft Gas Turbine Engine Compressor Duct 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 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 US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-575-4549
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-575-4549
- Federal Bureau of Investigation (FDD4)
- Effective Date:
- 1 Jul 2009
Approved Sources 2840-01-575-4549
- Part Number
- Manufacturer
- Status
- 4318542
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-575-4549
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- Criticality Code Justification [CRTL]
- Agav
- End Item Identification [AGAV]
- F119-Pw-100 Engine On F22 Aircraft Apu
Management Data 2840-01-575-4549
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2010
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 2840-01-575-4549
2840-01-575-4549 has freight characteristics.. 2840-01-575-4549 has a variance between NMFC and UFC when transported by rail and the description should be consulted.