Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE SEGMENT

2840-01-151-0372 A portion of a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of two or more NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE cast as one piece.

Part Alternates: 4060952, 4060952CLE, 2840-01-151-0372, 01-151-0372, 2840011510372, 011510372

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

Supply Group (FSG) NSN Assign. NIIN
28 01-151-0372

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Technical Data | NSN 2840-01-151-0372

Characteristic Specifications
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION TURBINE
STAGE NUMBER 2
SPECIAL FEATURES T.O. 2J-F100-14, FIG 153, IND 22; 2.412-2.432 SQ. IN. AREA; 1800 CYCLE; TURBINE DISK AND HUB; REID/REPLACED P/N 4051852CLE AND 4054752CLE
CRITICALITY CODE JUSTIFICATION FEAT
III END ITEM IDENTIFICATION ACFT ENG F100/200
III PART NAME ASSIGNED BY CONTROLLING AGENCY ORIGINAL NAME VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 4060952CLE

Restrictions/Controls & Freight Information | NSN 2840-01-151-0372

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