Product Details | AIRCRAFT GAS TURBINE ENGIN COMBUSTION CHAMBER DUCT

2840-00-072-9691 A cylindrical shaped item or a segment thereof designed to direct air into or around a CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes.

Part Alternates: 506274, 2840-00-072-9691, 00-072-9691, 2840000729691, 000729691

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

Supply Group (FSG) NSN Assign. NIIN
28 00-072-9691

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Technical Data | NSN 2840-00-072-9691

Characteristic Specifications
MATERIAL NICKEL ALLOY OVERALL
ENGINE SECTION LOCATION COMBUSTION CHAMBER
OVERALL LENGTH 2.785 INCHES NOMINAL
DIAMETER 20.281 INCHES MINIMUM AND 20.287 INCHES MAXIMUM
CRITICALITY CODE JUSTIFICATION AGAV
END ITEM IDENTIFICATION J52 ENG

Restrictions/Controls & Freight Information | NSN 2840-00-072-9691

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