Part Details | ELECTRICAL PLUG CONNECTOR BODY
5935-00-188-5421 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: 4142497024, 414-2497-024, 4142497015, 414-2497-015, 4142497015, 414-2497-015, KV6M22A55S1L, 5935-00-188-5421, 00-188-5421, 5935001885421, 001885421
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 16, 1973 | 00-188-5421 | 61924 ( CONNECTOR BODY, PLUG, ELECTRICAL ) |
REFERENCE DRAWINGS & PICTURES
STRAIGHT SHAPE, INTERNAL COUPLING
Cross Reference | NSN 5935-00-188-5421
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 414-2497-024 | 94756 | BOEING COMPANY, THEDBA BOEING |
| 414-2497-015 | 94756 | BOEING COMPANY, THEDBA BOEING |
| 414-2497-015 | 71468 | ITT CORPORATIONDBA I T T CANNON |
| KV6M22A55S1L | 71468 | ITT CORPORATIONDBA I T T CANNON |
Technical Data | NSN 5935-00-188-5421
| Characteristic | Specifications |
|---|---|
| BODY STYLE | STRAIGHT SHAPE, INTERNAL COUPLING |
| OVERALL LENGTH | 1.420 INCHES MINIMUM AND 1.460 INCHES MAXIMUM |
| OVERALL DIAMETER | 1.459 INCHES MINIMUM |
| CONNECTOR LOCKING METHOD | INTERNALLY THREADED COUPLING RING |
| THREADED DEVICE TYPE | BACK SHELL AND COUPLING FACILITY |
| THREAD SERIES DESIGNATOR | UNEF AND UNEF |
| NOMINAL THREAD SIZE | 1.500 INCHES AND 1.438 INCHES |
| THREAD CLASS | A2A$$A2B |
| THREAD QUANTITY PER INCH | A18$$A18 |
| NOMINAL THREAD LENGTH | 0.355 INCHES AND 0.260 INCHES |
| SHELL TYPE | SOLID |
| SHELL MATERIAL | ALUMINUM ALLOY 6061 |
| SHELL MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367 FED SPEC SINGLE MATERIAL RESPONSE |
| SHELL SURFACE TREATMENT | NICKEL |
| SHELL SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-26074 MIL SPEC SINGLE TREATMENT RESPONSE |
| POLARIZATION METHOD | KEYWAY OR MULTIPLE KEYWAY |
| INSERT POSITION IN DEG | 10.0 |
| MATING END QUANTITY | 1 |
| SPECIAL FEATURES | DESIGN ANALYSIS |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |