Product Details | AIRCRAFT GAS TURBINE ENGI COMBUSTION CHAMBER LINER

2840-01-015-1751 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.

Part Alternates: 643E406G9, 2840-01-015-1751, 01-015-1751, 2840010151751, 010151751

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

Supply Group (FSG) NSN Assign. NIIN
28 15 JAN 1976 01-015-1751

Cross Reference | NSN 2840-01-015-1751

Part Number Cage Code Manufacturer
643E406G9 07482 GENERAL ELECTRIC COMPANY DBA GE

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Technical Data | NSN 2840-01-015-1751

Characteristic Specifications
ENGINE SECTION LOCATION COMBUSTION CHAMBER
OVERALL LENGTH 12.030 INCHES MINIMUM AND 12.080 INCHES MAXIMUM
SPECIAL FEATURES USED ON -7B, -11A, -11B AND -19 SERIES ENGINES
CRITICALITY CODE JUSTIFICATION AGAV
END ITEM IDENTIFICATION J-79 AIRCRAFT TURBINE ENGINES

Restrictions/Controls & Freight Information | NSN 2840-01-015-1751

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:ANon-Munitions List Item/ Non-Strategic List Item - Demilitarization not required.
Precious Metals Indicator Code:AItem does not contain precious metal
Criticality Code:YThe item does not have a nuclear hardened feature but does have other critical feature(s) such as tolerance, fit restriction or application.
Category Code Description
No Freight Information