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2840-01-495-3506
Aircraft Gas Turbine Engine Combustion Chamber Liner
2840014953506 014953506 5921T95G02
A cylindrical shaped item positioned inside the CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. It is designed to direct the flow of hot gasses to the TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Combustion Chamber Liner
January 2023
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Restrictions 2840-01-495-3506
2840-01-495-3506 is a Aircraft Gas Turbine Engine Combustion Chamber Liner 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 2840-01-495-3506
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-495-3506
- Spain (YB01)
- Effective Date:
- 1 Mar 2002
Approved Sources 2840-01-495-3506
- Part Number
- Manufacturer
- Status
- 5921T95G02
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-495-3506
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- Special Features [FEAT]
- Next Higher Assembly Hot Section Module, Part Number 5074T00g01
- End Item Identification [AGAV]
- Engine Model Ct7-5 And Ct7-7 Turboprop, Part Number 6053T87g01
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Freight Information 2840-01-495-3506
2840-01-495-3506 has freight characteristics.. 2840-01-495-3506 has a variance between NMFC and UFC when transported by rail and the description should be consulted.