Product Details | AIRCRAFT GAS TURBINE ENGINE HEAT SHIELD

2840-01-322-6282 A rigid item, fabricated from a heat resistant allow, with or without insulation material added. Designed to protect parts, areas or systems of an ENGINE, GAS TURBINE, AIRCRAFT from excessive heat damage. See also INSULATION BLANKET, THERMAL, AIRCRAFT GAS TURBINE ENGINE.

Part Alternates: 2840-01-322-6282, 01-322-6282, 2840013226282, 013226282

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

Supply Group (FSG) NSN Assign. NIIN
28 01-322-6282

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Technical Data | NSN 2840-01-322-6282

Characteristic Specifications
MATERIAL NICKEL ALLOY SHIELD
MATERIAL DOCUMENT AND CLASSIFICATION AMS5540 ASSN STD SINGLE MATERIAL RESPONSE SHIELD
ENGINE SECTION LOCATION TURBINE
OVERALL LENGTH 4.230 INCHES NOMINAL
DIAMETER 13.670 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION AGAV
END ITEM IDENTIFICATION F110GE129 AIRCRAFT ENGINE
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 1364M98G03

Restrictions/Controls & Freight Information | NSN 2840-01-322-6282

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