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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. |