Product Details | TURBINE ENGINE COMBUSTION CHAMBER

2840-01-368-6122 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.

Part Alternates: 6080T13G02, 2840-01-368-6122, 01-368-6122, 2840013686122, 013686122

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 04 DEC 1992 01-368-6122

Demand History | NSN 2840-01-368-6122

Part Number Request Date QTY Origin
6080T13G02 2012-10-276 1 Malaysia

Cross Reference | NSN 2840-01-368-6122

Part Number Cage Code Manufacturer
6080T13G02 99207 GENERAL ELECTRIC COMPANY DBA GE

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Restrictions/Controls & Freight Information | NSN 2840-01-368-6122

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Demilitarization Code:BMunitions List Item - Mutilation (MUT) to the point of scrap required. (Formerly: Demilitarization not required. Trade Security Controls (TSCs) required at disposition.)
Precious Metals Indicator Code:UPrecious metal type is unknown
Category Code Description
No Freight Information