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) |
---|---|---|---|
39 | MAR 05, 1994 | 01-387-5018 | 30555 ( ADAPTER, HOISTING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3940-01-387-5018
Part Number | Cage Code | Manufacturer |
---|---|---|
PWA81360 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 3940-01-387-5018
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY |
OVERALL LENGTH | 34.600 INCHES NOMINAL |
OVERALL WIDTH | 33.400 INCHES NOMINAL |
OVERALL HEIGHT | 2.000 INCHES NOMINAL |
USAGE DESIGN | AIRCRAFT ENGINE |
ATTACHMENT METHOD | BOLTED RING |
SPECIAL FEATURES | C/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 CLASSIFICATION | HH-1.1 |
FUNCTIONAL DESCRIPTION | ALLOWS THE SECOND STAGE TURBINE ROTOR ASSEMBLY TO BE MOVED WITHOUT DAMAGE TO THE TURBINE BLADES |
END ITEM IDENTIFICATION | F117-PW-100 ENGINE |