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2840-01-499-2512

Aircraft Gas Turbine Engine Front Frame Strut

2840014992512 014992512 305-588-101-0

A rigid piece designed to resist pressure in the direction of its length. It is positioned between the inner and outer rings and is a main component of a FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Front Frame Strut

2840-01-499-2512 STRUT,FRONT FRAME,AIRCRAFT GAS TURBINE ENGINE 2840014992512 014992512

Managed by United States
NSN Created on 17 Jul 2002
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
2840-01-499-2512 STRUT,FRONT FRAME,AIRCRAFT GAS TURBINE ENGINE 2840014992512 014992512 1/1
NSN 2840-01-499-2512 (Generic Image) 1/1

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2840-01-499-2512 Related Documents Related Documents 2840-01-499-2512 5+ Documents (More...)

305-588-101-0 A rigid piece designed to resist pressure in the direction of its length.
RQST NE Updated Every Day 2840-01-499-2512 RQST Updated Every Day 2840-01-499-2512 RQST NE Related Documents
2840014992512 014992512,305-588-101-0 United States (US) 4. 2840-01-499-2512 Marketplace Restrictions
( More... ) https//www.nsnlookup.com /fsg-53/fsc-5365/us 5365-01-524-7765 Updated Every Day 2840-01-499-2512
RQST Updated Every Day 2840-01-499-2512 RQST NE Restrictions https https//www.nsnlookup.com /fsg
2840014992512 014992512,305-588-101-0 United States (US) 4. 2840-01-499-2512 Marketplace Restrictions
2840-01-462-9033 2840-01-567-1790 2840-01-531-0119 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-499-2512
2840014992512 014992512,305-588-101-0 /fsg-28/fsc-2840/us 2840-01-531-0230 2840015310230 015310230
,GE-9540M25G03 2840-01-567-1790 2840-01-531-0119 NATO Stock Numbers Related to 2840-01-499-2512 https
2840-01-656-6663 2840-01-462-0839 2840-01-663-1343 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-499-2512
2840014992512 014992512,305-588-101-0 Restrictions 2840-01-531-0119 DEMIL: B | DEMILI https//www.nsnlookup.com
www.nsnlookup.com /fsg-53/fsc-5365/us 5365-01-524-7765 Nut And Bolt Retainer 5365015247765 015247765 Day 2840-01-499-2512

2840-01-499-2512 Demil Restrictions 2840-01-499-2512

DEMIL: B | DEMILI: 3 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-499-2512 is a Aircraft Gas Turbine Engine Front Frame Strut 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 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.

2840-01-499-2512 HTS and ScheduleB Import and Export 2840-01-499-2512

2840-01-499-2512 End Users End Users 2840-01-499-2512

United Kingdom (ZK01)
Effective Date:
1 Jul 2002

2840-01-499-2512 Manufacturers Approved Sources 2840-01-499-2512

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2840-01-499-2512 has freight characteristics.. 2840-01-499-2512 has a variance between NMFC and UFC when transported by rail and the description should be consulted.