Product Details | AIRCRAFT GAS TURB TURBINE CASE AND NOZZLE ASSEMBLY

2840-01-118-3601 A NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE with a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE.

Part Alternates: 9184M51G17, 2840-01-118-3601, 01-118-3601, 2840011183601, 011183601

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

Supply Group (FSG) NSN Assign. NIIN
28 01-118-3601

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Technical Data | NSN 2840-01-118-3601

Characteristic Specifications
MATERIAL TITANIUM ALLOY OVERALL
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION TURBINE
OVERALL LENGTH 11.659 INCHES NOMINAL
DIAMETER 95.930 INCHES MINIMUM AND 95.950 INCHES MAXIMUM
SPECIAL FEATURES ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION ACFT ENG TF-39
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 9184M51G17

Restrictions/Controls & Freight Information | NSN 2840-01-118-3601

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