NSN 5340-00-655-8000 · NIIN 006558000 · FSC 5340
NO DASHES 5340006558000
In Stock
CLAMP,LOOP
Hardware, Commercial
Application: W/S: ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); JOINT STARS TARGET RADAR SYSTEM; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, AWACS, E-3A; HELICOPTER, RH-53; KC-46 AIRCRAFT
Technical characteristics
15 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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); JOINT STARS TARGET RADAR SYSTEM; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, AWACS, E-3A; HELICOPTER, RH-53; KC-46 AIRCRAFT |
| BZTN | LOOP INSIDE DIAMETER | INCHES NOMINAL 0.688 |
| STYL | STYLE DESIGNATOR | |
| AAAL | TONGUE HOLE TYPE | UNTHREADED ROUND |
| AAAP | CUSHIONING ENVIRONMENTAL PROTECTION | HEAT |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | BAND FED SPEC SINGLE TREATMENT RESPONSE QQ--416,TY 1,CL 2 |
| AZDC | DISTANCE FROM LOOP CENTER TO TONGUE END | INCHES NOMINAL 0.967 |
| ABPX | MATERIAL THICKNESS | INCHES NOMINAL 0.032 |
| AZCY | CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE | INCHES NOMINAL 0.749 |
| ABMZ | DIAMETER | INCHES MINIMUM 0.194 AND INCHES MAXIMUM 0.209 |
| ZZZK | SPECIFICATION/STANDARD DATA | MANUFACTURERS SPECIFICATION 81205-BACC10GE |
| FEAT | SPECIAL FEATURES | APPROVED FOR FAA USE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | CUSHION MFR REF SINGLE MATERIAL RESPONSE D6-54312-1 FSC-81205 |
| SFTT | SURFACE TREATMENT | BAND CADMIUM |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 0.500 |
Supersedes
This item replaces cancelled NIIN 006856102. An older drawing citing one of those numbers resolves here.