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2840-01-074-9662
Aircraft Gas Turbine Engine Combustion Chamber
2840010749662 010749662 3001745-13
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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United States (US) 4. 2840-01-074-9662 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-074-9662 RQST Updated Every Day 2840-01-074-9662 RQST NE Related Documents
Restrictions 2840-01-074-9662
2840-01-074-9662 is a Aircraft Gas Turbine Engine Combustion Chamber 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 2840-01-074-9662
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-074-9662
- US Coast Guard (C057)
- Effective Date:
- 1 Apr 1991
Approved Sources 2840-01-074-9662
- Part Number
- Manufacturer
- Status
- 3001745-13
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 2840-01-074-9662
Freight Information 2840-01-074-9662
2840-01-074-9662 has freight characteristics.. 2840-01-074-9662 has a variance between NMFC and UFC when transported by rail and the description should be consulted.