Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE BLADE RETAINER

2840-01-307-6380 An item specifically designed to position and/or restrain the movement of one or more BLADE, or BLADE SET, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may be the full 360 degrees required for one turbine stage or a segment thereof.

Part Alternates: 2840-01-307-6380, 01-307-6380, 2840013076380, 013076380

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

Supply Group (FSG) NSN Assign. NIIN
28 01-307-6380

Cross Reference | NSN 2840-01-307-6380

Part Number Cage Code Manufacturer
1387M99 07482 GENERAL ELECTRIC COMPANY DBA GE
1387M99P01 07482 GENERAL ELECTRIC COMPANY DBA GE
1387M99P03 07482 GENERAL ELECTRIC COMPANY DBA GE
1387M99P04 07482 GENERAL ELECTRIC COMPANY DBA GE

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Technical Data | NSN 2840-01-307-6380

Characteristic Specifications
MATERIAL NICKEL ALLOY
OVERALL LENGTH 1.660 INCHES MINIMUM AND 1.680 INCHES MAXIMUM
OUTSIDE DIAMETER 19.370 INCHES MINIMUM AND 19.380 INCHES MAXIMUM
REFERENCE DATA AND LITERATURE T.O. 2J-F110-14, FIG 90 IND 10
SPECIAL FEATURES USED ON THE LOW PRESSURE TURBINE;MATL NICKEL, COBALT, CHROMIUM ALLOY
III END ITEM IDENTIFICATION ACFT ENG F110G129
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 1387M99P03

Restrictions/Controls & Freight Information | NSN 2840-01-307-6380

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