NSN 5340-01-162-3151 · NIIN 011623151 · FSC 5340
NO DASHES 5340011623151
In Stock
CLAMP,LOOP
Hardware, Commercial
Application: W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, AWACS, E-3A; AIRCRAFT, STRATOLIFTER C-135
Technical characteristics
9 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 |
|---|---|---|
| ABPX | MATERIAL THICKNESS | INCHES MINIMUM 0.046 AND INCHES MAXIMUM 0.056 |
| AGAV | END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, AWACS, E-3A; AIRCRAFT, STRATOLIFTER C-135 |
| AZCY | CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE | INCHES MINIMUM 0.867 AND INCHES MAXIMUM 0.887 |
| AZDC | DISTANCE FROM LOOP CENTER TO TONGUE END | INCHES MINIMUM 1.080 AND INCHES MAXIMUM 1.110 |
| BZTN | LOOP INSIDE DIAMETER | INCHES NOMINAL 0.938 |
| MATT | MATERIAL | OVERALL STEEL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL ASSN STD SINGLE MATERIAL RESPONSE A-S 5510 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| STYL | STYLE DESIGNATOR |