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2840-01-443-0611
Aircraft Gas Turbine Engine Diffuser
2840014430611 014430611 3077058-8
A frame with stationary struts, designed to diffuse and direct air from the COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have mounting facilities for external components. It may provide support and house a compressor rear bearing. May include a CASE (3), DIFFUSER, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Diffuser
January 2023
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Related Documents 2840-01-443-0611 2+ Documents (More...)
2840-01-443-0611 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-443-0611
Day 2840-01-443-0611 RQST NE Restrictions 2840-01-443-0611 DEMIL: B | DEMILI : | CRITICALITY : X | HMIC
Restrictions 2840-01-443-0611
2840-01-443-0611 is a Aircraft Gas Turbine Engine Diffuser 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 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 2840-01-443-0611
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-443-0611
- Spain (YB01)
- Effective Date:
- 1 Mar 1997
Approved Sources 2840-01-443-0611
- Part Number
- Manufacturer
- Status
- 3077058-8
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-443-0611
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Motor Garrett Tfe731-2-2J,C-101
NATO Stock Numbers Related to 2840-01-443-0611
Freight Information 2840-01-443-0611
2840-01-443-0611 has freight characteristics.. 2840-01-443-0611 has a variance between NMFC and UFC when transported by rail and the description should be consulted.