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 (10-00791) and panel screws are now included with each unit.
Optional Slip Indicator to satisfy FAA AC91-75 (10-02586).
Additional core charge added to purchase at time of checkout
Exchange core must be a like core* and the core must be returned no later than 20 days from the invoice date to receive core credit.
BK-2: Standard look, 28 VDC, Lighted, Moveable pointer, Stationary Roll Dial. Yellow airplane and pointer. Connector pin out: A: GND Motor, B: GND Lights, C: +28VDC Motor, D: +28VDC Lights.
BK-6: Standard look. 28 VDC, Fixed Pointer, Moveable Roll Dial. Yellow airplane and pointer. Connector pin out: A: Ground Motor, B: Spare, C: +28 VDC Motor, D: Spare.