| ACTUATOR FREE POSITION HEIGHT | 0.640 INCHES NOMINAL |
| ACTUATOR LENGTH | 0.539 INCHES MINIMUM AND 0.549 INCHES MAXIMUM |
| ACTUATOR MOVEMENT | 0.040 PRETRAVEL INCHES MAXIMUM AND 0.075 OVERTRAVEL INCHES MAXIMUM AND 0.020 DIFFERENTIAL INCHES MAXIMUM |
| ACTUATOR ROLLER DIAMETER | 0.209 INCHES MINIMUM AND 0.213 INCHES MAXIMUM |
| ACTUATOR ROLLER WIDTH | 0.154 INCHES MINIMUM AND 0.158 INCHES MAXIMUM |
| ACTUATOR STYLE | ROLLER ARM |
| BODY STYLE | HOLE MOUNTED |
| BODY WIDTH | 0.390 INCHES MAXIMUM |
| CENTER TO CENTER DISTANCE BETWEEN MOUNTING FACILITIES PARALLEL TO LENGTH | 0.997 INCHES MINIMUM AND 1.003 INCHES MAXIMUM |
| CONTACT LOAD CURRENT RATING AT MAXIMUM RATED VOLTAGE | 7.000 AMPERES RESISTIVE DC AND 1.000 AMPERES INDUCTIVE DC AND 2.000 AMPERES LAMP DC |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FEATURES PROVIDED | ACTUATOR SEAL |
| HAZARDOUS LOCATIONS/ENVIRONMENTAL PROTECTION | WEATHERPROOF |
| INCLOSURE TYPE | FULLY INCLOSED |
| MAXIMUM VOLTAGE RATING IN VOLTS | 28.0 DC |
| MOUNTING METHOD | THREADED BUSHING |
| NONPILE-UP CONTACT ARRANGEMENT | 1 POLE, DOUBLE THROW, ONE POSITION MOMENTARY SINGLE SWITCH UNIT |
| SPECIAL FEATURES | MUST BE PROCURED IAW GRUMMAN AEROSPACE CORP. DWG GS838S AND IS UTILIZED IN A CRITICAL APPLICATION ON A F-14A AIRCRAFT |
| SWITCH RELEASE FORCE | 4.0 INCH-OUNCES MINIMUM |
| SWITCH ACTUATING FORCE | 1.5 INCH-OUNCES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 3 WIRE LEAD |
| UNTHREADED MOUNTING HOLE DIAMETER | 0.140 INCHES MINIMUM AND 0.144 INCHES MAXIMUM |