CLAMP,LOOP
Hardware, Commercial
Application: ENGINE, AIRCRAFT, J-57 ALL MODELS (C-135, EC-135, B-52);AIRCRAFT, PHANTOM F-4;AIRCRAFT, STRATOLIFTER C-135;HELICOPTER, CH-53A/D/E;AIRCRAFT, STRATOFORTRESS B-52;HELICOPTER, IROQUOIS HH/UH-1;AIRCRAFT, EAGLE F-15;HELICOPTER, RH-53;ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E)
Technical characteristics
12 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| STYL | STYLE DESIGNATOR | |
| AGAV | END ITEM IDENTIFICATION | ENGINE, AIRCRAFT, J-57 ALL MODELS (C-135, EC-135, B-52);AIRCRAFT, PHANTOM F-4;AIRCRAFT, STRATOLIFTER C-135;HELICOPTER, CH-53A/D/E;AIRCRAFT, STRATOFORTRESS B-52;HELICOPTER, IROQUOIS HH/UH-1;AIRCRAFT, EAGLE F-15;HELICOPTER, RH-53;ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E) |
| AAAL | TONGUE HOLE TYPE | UNTHREADED ROUND |
| ABPX | MATERIAL THICKNESS | INCHES NOMINAL 0.051 |
| ABMK | OVERALL WIDTH | INCHES MINIMUM 0.484 AND INCHES MAXIMUM 0.516 |
| ABMZ | DIAMETER | INCHES MINIMUM 0.199 AND INCHES MAXIMUM 0.209 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| BZTN | LOOP INSIDE DIAMETER | INCHES NOMINAL 0.562 |
| MATT | MATERIAL | CUSHION GLASS FIBER AND PLASTIC POLYAMIDE NYLON AND PLASTIC POLYTETRAFLUOROETHYLENE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | BAND ASSN STD SINGLE MATERIAL RESPONSE A-S 5510 |
| AZDC | DISTANCE FROM LOOP CENTER TO TONGUE END | INCHES MINIMUM 0.965 AND INCHES MAXIMUM 0.975 |
| AZCY | CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE | INCHES NOMINAL 0.752 |
Cross-references
7 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| JM44LC17-H09PB | 22175 |
| 23039030-08 | 63005 |
| 11168-08 | 79326 |
| 11168-08 | 83930 |
| MS9825-08 | 96906 |
| S500-9 | 18076 |
| S500-09 | 18076 |
Supersedes
This item replaces cancelled NIIN 005984146. An older drawing citing one of those numbers resolves here.