| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 220.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 2.5 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| BODY SIZE | 10 |
| BODY MATERIAL | ALUMINUM |
| ZRO RESISTANCE IN OHMS | 36.20 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 109.50 NOMINAL |
| ZSO RESISTANCE IN OHMS | 9.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 24.20 NOMINAL |
| ZRS RESISTANCE IN OHMS | 62.30 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 25.20 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 8.70 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 7.85 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 25.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.50 NOMINAL |
| MAXIMUM TEMP RISE | 40.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -15.0 TO 15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2300.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND |
| 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND |
| 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND |
| 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8340 INCHES MINIMUM AND |
| 0.8370 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
| SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
| SHAFT DIAMETER | 0.0895 INCHES MINIMUM AND |
| 0.0900 INCHES MAXIMUM SINGLE SHAFT |
| SHAFT LENGTH | 0.4130 INCHES NOMINAL SINGLE SHAFT |
| SHAFT SLOT DEPTH | 0.0300 INCHES NOMINAL SINGLE SHAFT |
| SHAFT SLOT WIDTH | 0.0250 INCHES NOMINAL SINGLE SHAFT |
| TERMINAL LOCATION | REAR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| THE MANUFACTURERS DATA | |
| MANUFACTURERS CODE | 96774 |
| DESIGN CONTROL REFERENCE | AY503-4A1 |