Product Details | AIRCRAFT GAS TURBINE ENGI COMBUSTION CHAMBER LINER

2840-01-362-5078 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: 2840-01-362-5078, 01-362-5078, 2840013625078, 013625078

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

Supply Group (FSG) NSN Assign. NIIN
28 01-362-5078

Cross Reference | NSN 2840-01-362-5078

Part Number Cage Code Manufacturer
4080358 52661 UNITED TECHNOLOGIES CORPORATION DBA PRATT & WHITNEY
4080358 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS
4083063 52661 UNITED TECHNOLOGIES CORPORATION DBA PRATT & WHITNEY
4083063 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS

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Technical Data | NSN 2840-01-362-5078

Characteristic Specifications
ENGINE SECTION LOCATION COMBUSTION CHAMBER
OVERALL LENGTH 6.281 INCHES MINIMUM AND 6.393 INCHES MAXIMUM
DIAMETER 3.000 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION AGAV
END ITEM IDENTIFICATION F100-PW-229 TURBO-FAN ENGINE

Restrictions/Controls & Freight Information | NSN 2840-01-362-5078

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
Category Code Description
No Freight Information