|The RCA26 series electric attitude gyro employs an electrically driven rotor to sense movement in the roll and pitch axis and transmits the information to the pilot through a pictorial presentation. They have a built in inverter which converts aircraft DC power to the required AC voltage and frequency. All units have a pull cage knob and a power failure flag. Slip indicator can be added upon request.
Mating connector MS3116E8-4S and panel screws are now included with each unit.
Optional Slip Indicator to satisfy FAA AC91-75.