PWA81360: ADAPTER,HOISTING.
The ADAPTER,HOISTING is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, usage_design: AIRCRAFT ENGINE, overall_width: 33.400 INCHES NOMINAL IN, overall_height: 2.000 INCHES NOMINAL IN, overall_length: 34.600 INCHES NOMINAL IN, attachment_method: BOLTED RING. This part is cataloged in the U.S.
Government catalog under NSN 3940-01-387-5018, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY |
| usage_design | AIRCRAFT ENGINE |
| overall_width | 33.400 INCHES NOMINAL IN |
| overall_height | 2.000 INCHES NOMINAL IN |
| overall_length | 34.600 INCHES NOMINAL IN |
| attachment_method | BOLTED RING |
| 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 |
| functional_classification | HH-1.1 |
| NSN | 3940-01-387-5018 |
| OVERALL HEIGHT | 2.000 INCHES NOMINAL IN |
| USAGE DESIGN | AIRCRAFT ENGINE |
| OVERALL LENGTH | 34.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 33.400 INCHES NOMINAL IN |
| FUNCTIONAL CLASSIFICATION | HH-1.1 |
| 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. |
| 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 |
| MATERIAL | ALUMINUM ALLOY |
| ATTACHMENT METHOD | BOLTED RING |
No substitute or cross-reference records for this part.