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2840-01-502-5397
Aircraft Gas Turbine Engine Combustion Chamber
2840015025397 015025397 6064T54G10
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. 2840-01-502-5397 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 2840-01-502-5397
2840-01-502-5397 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. 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 2840-01-502-5397
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-502-5397
- Spain (YB)
- Spain (YB01)
- Effective Date:
- 1 Nov 2002
Approved Sources 2840-01-502-5397
- Part Number
- Manufacturer
- Status
- 6064T54G10
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-502-5397
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- Ct7-5-7 Turboprop Engine
- Part Name Assigned By Controlling Agency [CXCY]
- Liner-Combustion
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Freight Information 2840-01-502-5397
2840-01-502-5397 has freight characteristics.. 2840-01-502-5397 has a variance between NMFC and UFC when transported by rail and the description should be consulted.