Part Details | ELECTRICAL PLUG CONNECTOR BODY
5935-00-255-2186 The main or principal part of a CONNECTOR, PLUG, ELECTRICAL which includes insert(s) designed to accommodate but does not include removable contacts. It may have a hood or shell, a jackscrew and jacksocket, or other means for polarizing and aligning. It is not designed to be mounted on a bulkhead, chassis, panel, wall, or the like. Excludes CONNECTOR BODY, MODULAR PLUG, ELECTRICAL. For items without insert(s), see SHELL, ELECTRICAL CONNECTOR.
Alternate Parts: 4141942118, 414-1942-118, KV94C10T5SNM, 38068105SN, 38068-10-5SN, 5935-00-255-2186, 00-255-2186, 5935002552186, 002552186
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 23, 1969 | 00-255-2186 | 61924 ( CONNECTOR BODY, PLUG, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT SHAPE, INTERNAL COUPLING W/BACKSHELL
Cross Reference | NSN 5935-00-255-2186
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 414-1942-118 | 94756 | BOEING COMPANY, THEDBA BOEING |
| KV94C10T5SNM | 71468 | ITT CORPORATIONDBA I T T CANNON |
| 38068-10-5SN | 11139 | TE CONNECTIVITY CORPORATIONDBA DEFENSE AEROSPACE OPERATIONS |
Technical Data | NSN 5935-00-255-2186
| Characteristic | Specifications |
|---|---|
| BODY STYLE | STRAIGHT SHAPE, INTERNAL COUPLING W/BACKSHELL |
| OVERALL LENGTH | 1.330 INCHES NOMINAL |
| OVERALL DIAMETER | 0.906 INCHES MAXIMUM |
| CONNECTOR LOCKING METHOD | INTERNALLY THREADED COUPLING NUT |
| THREAD SERIES DESIGNATOR | UNEF |
| NOMINAL THREAD SIZE | 0.688 INCHES |
| THREAD CLASS | 2B |
| THREAD DIRECTION | RIGHT-HAND |
| SHELL TYPE | SOLID |
| SHELL MATERIAL | ALUMINUM ALLOY 6061 |
| SHELL MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367 FED SPEC SINGLE MATERIAL RESPONSE |
| SHELL SURFACE TREATMENT | CHROMIUM |
| SHELL SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-C-320,CLASS 2 FED SPEC SINGLE TREATMENT RESPONSE |
| POLARIZATION METHOD | KEYWAY OR MULTIPLE KEYWAY |
| INSERT POSITION IN DEG | 0.0 |
| MATING END QUANTITY | 1 |
| SPECIAL FEATURES | DESIGN ANALYSIS |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |