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).
Please note, Aircraft Spruce's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
These are 3-1/8" gyros.
No, 8130-3 forms have to be requested when ordering any certified instruments and has an additional charge.
See our part # 10-00466.
PER INSTALL MANUAL: Use 6-32 UNC-2b screws or equivalent. Screw length should not exceed .38 inches plus bezel and panel thickness.
MS35214 instrument screws recommended. Choose correct length for your panel.