RC Allen 26Ak-4 Factory Overhauled Attitude Indicator

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) not included. Order separately.

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.