Product Details | AIRCRAFT GAS TURBINE ENGI COMBUSTION CHAMBER LINER

2840-01-267-1559 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: 4073523, 2840-01-267-1559, 01-267-1559, 2840012671559, 012671559

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

Supply Group (FSG) NSN Assign. NIIN
28 01-267-1559

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Technical Data | NSN 2840-01-267-1559

Characteristic Specifications
OVERALL LENGTH 12.770 INCHES MINIMUM AND 12.870 INCHES MAXIMUM
CRITICALITY CODE JUSTIFICATION ABHP AND AGAV
END ITEM IDENTIFICATION ACFT ENG F100PW220
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 4073523

Restrictions/Controls & Freight Information | NSN 2840-01-267-1559

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