| BODY STYLE | STRAIGHT SHAPE, INTERNAL COUPLING |
| CONNECTOR LOCKING METHOD | INTERNALLY THREADED COUPLING NUT |
| CONTACT MATERIAL | COPPER SINGLE MATING END 3RD CONTACT GROUPING |
| CONTACT MATERIAL | NICKEL ALLOY SINGLE MATING END 2ND CONTACT GROUPING |
| CONTACT MATERIAL | NICKEL SINGLE MATING END 1ST CONTACT GROUPING |
| CONTACT MAXIMUM AC VOLTAGE RATING IN VOLTS | 500.0 SINGLE MATING END ALL CONTACT GROUPINGS |
| CONTACT MAXIMUM CURRENT RATING IN AMPS | 23.0 SINGLE MATING END ALL CONTACT GROUPINGS |
| CONTACT REMOVABILITY | NONREMOVABLE SINGLE MATING END ALL CONTACT GROUPINGS |
| CONTACT MAXIMUM DC VOLTAGE RATING IN VOLTS | 700.0 SINGLE MATING END ALL CONTACT GROUPINGS |
| CONTACT POSITION ARRANGEMENT STYLE | 14S-7 SINGLE MATING END |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENVIRONMENTAL PROTECTION | MOISTURE RESISTANT AND VIBRATION RESISTANT |
| INCLUDED CONTACT QUANTITY | 1 SINGLE MATING END 1ST CONTACT GROUPING |
| INCLUDED CONTACT QUANTITY | 1 SINGLE MATING END 2ND CONTACT GROUPING |
| INCLUDED CONTACT QUANTITY | 1 SINGLE MATING END 3RD CONTACT GROUPING |
| INCLUDED CONTACT TYPE | ROUND SOCKET SINGLE MATING END ALL CONTACT GROUPINGS |
| INSERT MATERIAL | RUBBER SINGLE MATING END |
| INSERT POSITION IN DEG | 315.0 |
| OVERALL DIAMETER | 1.000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.094 INCHES NOMINAL |
| MATING END QUANTITY | 1 |
| NOMINAL THREAD SIZE | 0.750 INCHES AND 0.875 INCHES |
| POLARIZATION METHOD | KEYWAY OR MULTIPLE KEYWAY |
| SHELL MATERIAL | ALUMINUM ALLOY |
| SHELL SURFACE TREATMENT | CADMIUM AND CHROMATE |
| SHELL TYPE | SOLID |
| SPECIAL FEATURES | CRITICAL SPARE PARTS FOR T56 AIRCRAFT ENGINE LISTED ON T56 ENGINE CRITICAL PARTS LIST |
| TERMINAL LOCATION | BACK SINGLE MATING END SINGLE CONTACT GROUPING |
| TERMINAL TYPE | SOLDER WELL SINGLE MATING END SINGLE CONTACT GROUPING |
| THREAD CLASS | 2A AND 2B |
| THREAD DIRECTION | RIGHT-HAND |
| THREAD SERIES DESIGNATOR | UNEF |
| THREADED DEVICE TYPE | BACK SHELL AND COUPLING FACILITY |