DISTANCE FROM MOUNTING SHOULDER TO FRONT FACE | 0.828 INCHES MAXIMUM |
BODY STYLE | STRAIGHT SHAPE, EXTERNAL COUPLING |
CENTER TO CENTER DISTANCE BETWEEN MOUNTING FACILITIES PARALLEL TO HEIGHT | 1.557 INCHES MINIMUM AND 1.567 INCHES MAXIMUM |
CONNECTOR LOCKING METHOD | EXTERNALLY THREADED SHELL |
CONTACT MAXIMUM AC VOLTAGE RATING IN VOLTS | 500.0 SINGLE MATING END SINGLE CONTACT GROUPING |
CONTACT MAXIMUM CURRENT RATING IN AMPS | 22.0 SINGLE MATING END SINGLE CONTACT GROUPING |
CONTACT MAXIMUM DC VOLTAGE RATING IN VOLTS | 700.0 SINGLE MATING END SINGLE CONTACT GROUPING |
CONTACT POSITION ARRANGEMENT STYLE | 28-12 SINGLE MATING END |
CONTACT REMOVABILITY | NONREMOVABLE SINGLE MATING END SINGLE CONTACT GROUPING |
CRITICALITY CODE JUSTIFICATION | FEAT |
DISTANCE BETWEEN CENTERLINES OF MOUNTING FACILITIES PARALLEL TO BODY WIDTH | 1.557 INCHES MINIMUM AND 1.567 INCHES MAXIMUM |
INCLUDED CONTACT QUANTITY | 26 SINGLE MATING END SINGLE CONTACT GROUPING |
INCLUDED CONTACT TYPE | ROUND PIN SINGLE MATING END SINGLE CONTACT GROUPING |
INSERT MATERIAL | RUBBER SINGLE MATING END |
INSERT POSITION IN DEG | 0.0 |
OVERALL HEIGHT | 2.000 INCHES NOMINAL |
OVERALL LENGTH | 1.566 INCHES MAXIMUM |
OVERALL WIDTH | 2.000 INCHES NOMINAL |
MATING END QUANTITY | 1 |
POLARIZATION METHOD | KEYWAY OR MULTIPLE KEYWAY |
SHELL MATERIAL | ALUMINUM ALLOY |
SHELL SURFACE TREATMENT | ANODIZE |
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 |
THREADED DEVICE TYPE | BACK SHELL AND COUPLING FACILITY |
UNTHREADED MOUNTING HOLE DIAMETER | 0.178 INCHES NOMINAL |