| ELASTIC RESTRAINT APPLICATION METHOD | ELECTRIC |
| AXIS DISPLACEMENT LIMITATION IN DEG | PORM 360 DEG PER MIN MAX |
| CURRENT TYPE | DC |
| DIRECT CURRENT RATING IN AMPS | 0.250 |
| FREEDOM AXIS QUANTITY | 1 |
| FUNCTIONAL DESCRIPTION | PROVIDES ELECTRICAL SIGNALS DIRECTLY PROPORTIONAL TO THE RATE OF YAW OF AIRCRAFT |
| GIMBAL QUANTITY | 1 |
| INSTRUMENT TYPE | UNFLOATED |
| OVERALL HEIGHT | 2.8125 INCHES NOMINAL |
| OVERALL LENGTH | 4.750 INCHES NOMINAL |
| OVERALL WIDTH | 2.875 INCHES NOMINAL |
| NONDEFINITIVE SPEC/STD DATA | TRU-2A/A TYPE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TRANSMITTER RATE GYROSCOPE |
| SENSING OUTPUT/SIGNAL LEVEL METHOD | VARIABLE INDUCTIVE PICKOFF AND 4 MA MAX |
| SPECIAL FEATURES | FOUR PIN ELECTRICAL RECEPTACLE BENDIX SCINTILLA PT SERIES, OR EQUAL; CONNECTOR MATES WITH SCINTILLA TYPE PT06P-8-4S, OR EQUAL |
| WHEEL POWER METHOD | ELECTRIC |
| VOLTAGE IN VOLTS | 28.0 |