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.
WARNING: Cancer and Reproductive Harm - www.P65Warnings.ca.gov.
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.
As long as the core is a RCA 26 series instrument it can be used for the core exchange.
Per the manufacturer:
Length: 8.14 in. max.
Width: 3.38 in. max
Height: 3.38 in. max
Weight: 2.3 lbs.
The domestic FAA 8130-3 form is included in the box along with the work order. If an export 8130-3 form is required, it must be requested at checkout. Additional fees apply for export form.