| AXIS DISPLACEMENT LIMITATION IN DEG | PORM 82 DEG FOR PITCH AXIS,PORM 180 DEG FOR ROLL AXISPORM 82 DEG FOR PITCH AXIS,PORM 180 DEG FOR ROLL AXISPORM 82 DEG FOR PITCH AXIS,PORM 180 DEG FOR ROLL AXIS |
| CURRENT TYPE | ACACAC |
| DESIGN TYPE | NONCAGEABLENONCAGEABLENONCAGEABLE |
| FREEDOM AXIS QUANTITY | 222 |
| FREQUENCY IN HERTZ | 400.0400.0400.0 |
| FSC APPLICATION DATA | AUTOMATIC FLIGHT CONTROL SYSTEM,AIRCRAFTAUTOMATIC FLIGHT CONTROL SYSTEM,AIRCRAFTAUTOMATIC FLIGHT CONTROL SYSTEM,AIRCRAFT |
| GIMBAL QUANTITY | 222 |
| GIMBAL TORQUE APPLICATION METHOD | AC TORQUE MOTORAC TORQUE MOTORAC TORQUE MOTOR |
| INSTRUMENT TYPE | UNFLOATEDUNFLOATEDUNFLOATED |
| OVERALL HEIGHT | 4.400 INCHES MAXIMUM4.400 INCHES MAXIMUM4.400 INCHES MAXIMUM |
| OVERALL LENGTH | 7.510 INCHES NOMINAL7.510 INCHES NOMINAL7.510 INCHES NOMINAL |
| OVERALL WIDTH | 6.000 INCHES MAXIMUM6.000 INCHES MAXIMUM6.000 INCHES MAXIMUM |
| SENSING OUTPUT/SIGNAL LEVEL METHOD | SYNCHRO OUTPUT 11.5V INTERNAL EXCITATIONSYNCHRO OUTPUT 11.5V INTERNAL EXCITATIONSYNCHRO OUTPUT 11.5V INTERNAL EXCITATION |
| PHASE | SINGLESINGLESINGLE |
| TORQUED GIMBAL QUANTITY | 222 |
| UNIT TYPE | VERTICALVERTICALVERTICAL |
| VOLTAGE IN VOLTS | 115.0115.0115.0 |
| WHEEL POWER METHOD | ELECTRICELECTRICELECTRIC |