Premium Information is available for this item - Upgrade for $1 a day
2840-01-519-6006
Aircraft Gas Turbine Engine Heatshield Stiffener
2840015196006 015196006 3609467-1
A rigid item designed to maintain the shape of a SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE. It may be made of one piece or an assembly of several pieces. View more Aircraft Gas Turbine Engine Heatshield Stiffener
January 2023
3
Marketplace 2840-01-519-6006
Request a Quotation from participating marketplace vendors
Related Documents 2840-01-519-6006 1+ Documents (More...)
United States (US) 4. 2840-01-519-6006 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-519-6006 RQST Updated Every Day 2840-01-519-6006 RQST NE Related
Restrictions 2840-01-519-6006
2840-01-519-6006 is a Aircraft Gas Turbine Engine Heatshield Stiffener that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-519-6006
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-519-6006
- Australia (ZA01)
- Effective Date:
- 26 Apr 2004
- Republic of Korea (ZH01)
- Effective Date:
- 1 Sep 2012
Approved Sources 2840-01-519-6006
- Part Number
- Manufacturer
- Status
- 3609467-1
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Similar Supply Items to 2840-01-519-6006
Freight Information 2840-01-519-6006
2840-01-519-6006 has freight characteristics managed by Australia.. 2840-01-519-6006 has a variance between NMFC and UFC when transported by rail and the description should be consulted.