NSN 3940-01-387-5018

Part Details | HOISTING ADAPTER

3940-01-387-5018 An item usually rigid in construction designed to be attached to another item to adapt it to an eye, ring, loop, or the like, for hoisting. For items designed to be used for hoisting and also provide accommodations for adapting a jack to an aircraft jacking point, see ADAPTER, AIRCRAFT JACKING POINT. Excludes BOLT, EYE; and SLING (as modified).

Alternate Parts: PWA81360, 3940-01-387-5018, 01-387-5018, 3940013875018, 013875018

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
39MAR 05, 199401-387-501830555 ( ADAPTER, HOISTING )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3940-01-387-5018
Part Number Cage Code Manufacturer
PWA8136077445UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS
Technical Data | NSN 3940-01-387-5018
Characteristic Specifications
MATERIAL ALUMINUM ALLOY
OVERALL LENGTH34.600 INCHES NOMINAL
OVERALL WIDTH33.400 INCHES NOMINAL
OVERALL HEIGHT2.000 INCHES NOMINAL
USAGE DESIGN AIRCRAFT ENGINE
ATTACHMENT METHOD BOLTED RING
SPECIAL FEATURESC/O A SPLIT, CIRCULAR RING WHOSE INSIDE DIAMETER IS MACHINED INTO A "U"CHANNEL, LINED WITH NEOPRENE. THE CHANNEL FITS OVER AND PROTECTS THE TURBINEBLADES FROM DAMAGE. A FIXED HINGE JOINS THE TWO HALVES AT ONE END. A HAND KNOB ASSY CLOSES THE RING AT THE OTHER END. TWO TRUNNION SPOOLS ARE LOCATED ONEACH HALF-RING.
WARNING STREAMER NOT INCLUDED
FUNCTIONAL CLASSIFICATIONHH-1.1
FUNCTIONAL DESCRIPTIONALLOWS THE SECOND STAGE TURBINE ROTOR ASSEMBLY TO BE MOVED WITHOUT DAMAGE TO THE TURBINE BLADES
END ITEM IDENTIFICATIONF117-PW-100 ENGINE