Part Details | ELECTRICAL PLUG CONNECTOR BODY
5935-00-405-1127 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: 4142113001, 414-2113-001, 3806883SN, 38068-8-3SN, 5935-00-405-1127, 00-405-1127, 5935004051127, 004051127
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 07, 1971 | 00-405-1127 | 61924 ( CONNECTOR BODY, PLUG, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT SHAPE, INTERNAL COUPLING W/BACKSHELL
Cross Reference | NSN 5935-00-405-1127
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 414-2113-001 | 94756 | BOEING COMPANY, THEDBA BOEING |
| 38068-8-3SN | 11139 | TE CONNECTIVITY CORPORATIONDBA DEFENSE AEROSPACE OPERATIONS |
Technical Data | NSN 5935-00-405-1127
| Characteristic | Specifications |
|---|---|
| BODY STYLE | STRAIGHT SHAPE, INTERNAL COUPLING W/BACKSHELL |
| CONNECTOR LOCKING METHOD | INTERNALLY THREADED COUPLING RING |
| THREADED DEVICE TYPE | BACK SHELL AND COUPLING FACILITY |
| THREAD SERIES DESIGNATOR | UNF AND UNEF |
| NOMINAL THREAD SIZE | 0.500 INCHES AND 0.562 INCHES |
| THREAD CLASS | A2A$$A2B |
| THREAD QUANTITY PER INCH | A20$$A24 |
| THREAD DIRECTION | RIGHT-HAND AND RIGHT-HAND |
| SHELL MATERIAL | ALUMINUM ALLOY 6061 |
| SHELL MATERIAL DOCUMENT AND CLASSIFICATION | AQQ-A-367$AQQ-A-225 TO 8 1ST MATERIAL RESPONSE |
| SHELL SURFACE TREATMENT | CHROMIUM |
| SHELL SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-C-320,CLASS 2A FED SPEC SINGLE TREATMENT RESPONSE |
| POLARIZATION METHOD | KEYWAY OR MULTIPLE KEYWAY |
| INSERT POSITION IN DEG | B0.0$$B105.0$$B140.0$$B215.0$$B265.0 |
| MATING END QUANTITY | 1 |
| SPECIAL FEATURES | DESIGN ANALYSIS |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |