CLAMP,LOOP
Hardware, Commercial
Application: ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); RADAR SET, FIREFINDER (AN/TPQ-36); AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, J69-T-25 (T-37B); SUPPORT EQUIPMENT, B-1 AIRCRAFT; ENGINE, AIRCRAFT F33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT, J85-GE-5/13 (F-5A/B, T-38A); ENGINE, AIRCRAFT, TF33-P-3/5/9 (C/EC-135, B-52H)
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 |
|---|---|---|
| ABMK | OVERALL WIDTH | INCHES NOMINAL 0.375 |
| AZDC | DISTANCE FROM LOOP CENTER TO TONGUE END | INCHES NOMINAL 0.717 |
| MATT | MATERIAL | BAND STEEL COMP 1017 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | BAND FED SPEC SINGLE MATERIAL RESPONSE QQ-S-636,COND 4 |
| AAAL | TONGUE HOLE TYPE | UNTHREADED ROUND |
| ABPX | MATERIAL THICKNESS | INCHES NOMINAL 0.032 |
| AGAV | END ITEM IDENTIFICATION | ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); RADAR SET, FIREFINDER (AN/TPQ-36); AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, J69-T-25 (T-37B); SUPPORT EQUIPMENT, B-1 AIRCRAFT; ENGINE, AIRCRAFT F33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT, J85-GE-5/13 (F-5A/B, T-38A); ENGINE, AIRCRAFT, TF33-P-3/5/9 (C/EC-135, B-52H) |
| SFTT | SURFACE TREATMENT | BAND CADMIUM |
| STYL | STYLE DESIGNATOR | |
| BZTN | LOOP INSIDE DIAMETER | INCHES NOMINAL 0.375 |
| AZCY | CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE | INCHES NOMINAL 0.529 |
| ABMZ | DIAMETER | INCHES NOMINAL 0.204 |
Cross-references
8 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| HBCC161-6 | 71785 |
| MIL-C-8603 | 81349 |
| MIL-DTL-8603 | 81349 |
| AN742-6 | 81352 |
| AN742-6 | 88044 |
| 01208532 | F0215 |
| 5340002002741 | A00AM |
| 5340002002741 | SCY13 |
Supersedes
This item replaces cancelled NIINs 001969942 · 002002742 · 004809929 · 013022962. An older drawing citing one of those numbers resolves here.