Product Details | AIRCRAFT GAS TURBINE ENGI COMBUSTION CHAMBER LINER

2840-01-424-9900 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: 2840-01-424-9900, 01-424-9900, 2840014249900, 014249900

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

Supply Group (FSG) NSN Assign. NIIN
28 01-424-9900

Cross Reference | NSN 2840-01-424-9900

Part Number Cage Code Manufacturer
4083052 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS
4084082 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS

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Technical Data | NSN 2840-01-424-9900

Characteristic Specifications
MATERIAL NICKEL ALLOY OVERALL
ENGINE SECTION LOCATION COMBUSTION CHAMBER
OVERALL LENGTH 4.160 INCHES MINIMUM AND 4.272 INCHES MAXIMUM
SPECIAL FEATURES T.O. 2J-F100-54, FIG 100, IND 34;USE ONLY ON 4083214, 4083215, 4083216,4083095, 4083127 AND 4083129
CRITICALITY CODE JUSTIFICATION AGAV
END ITEM IDENTIFICATION ACFT ENG F100PW229 ACFT ENG

Restrictions/Controls & Freight Information | NSN 2840-01-424-9900

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