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2840-01-337-1663
Aircraft Gas Turbine Engine Combustion Chamber
2840013371663 013371663 3072674-3
The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Aircraft Gas Turbine Engine Combustion Chamber
January 2023
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Related Documents 2840-01-337-1663 1+ Documents (More...)
United States (US) 4. 2840-01-337-1663 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-337-1663 RQST Updated Every Day 2840-01-337-1663 RQST NE Related Documents
Restrictions 2840-01-337-1663
2840-01-337-1663 is a Aircraft Gas Turbine Engine Combustion Chamber 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. The precious metals content of this item is unknown.
Import and Export 2840-01-337-1663
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-337-1663
- Spain (YB01)
- Effective Date:
- 1 Feb 1994
- France (ZF01)
- Effective Date:
- 1 Apr 1991
Approved Sources 2840-01-337-1663
- Part Number
- Manufacturer
- Status
- 3072674-3
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-337-1663
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- Specification/Standard Data [ZZZK]
- 99193-3072574 Manufacturers Standard
NATO Stock Numbers Related to 2840-01-337-1663
Freight Information 2840-01-337-1663
2840-01-337-1663 has freight characteristics managed by France.. 2840-01-337-1663 has a variance between NMFC and UFC when transported by rail and the description should be consulted.