Cirrus SR22 SDRs

The following is derived from maintenance facility submissions to the FAA’s Service Difficulty Reports database.

Gemini Sparkle

Key Takeaways:

  • Mechanical failures included a stuck throttle due to a broken alternate air valve and excessive elevator play caused by a loose pitch trim motor assembly with backed-out screws.
  • Two separate incidents involved failures of the Master Control Unit, leading to partial or complete loss of aircraft electrical power and critical flight systems.
  • Other electrical problems reported were tripped circuit breakers for essential systems, found to be caused by corroded and damaged data logger wiring connectors.
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Stuck Throttle

Broken Alternate Air Valve

Pilot reported throttle stuck half way open during flight. Disassembled wye pipe housing the alternate air flapper valve and filter. Discovered most of the flapper valve broken off and lodged in the throttle body, preventing the throttle from closing. Installed new alternate air flapper valve assembly (p/n 15710-002). The failure seems to originate where the radius of the hinge meets the flat surface of the valve on either side of the sandwiched flapper.

Part total time: Unknown


Inflight electrical failure

Master Control Unit Lost Power

During a post-maintenance test flight after engine installation, the aircraft lost electrical power on climb out after a touch-and-go. Both alternators went off-line and main battery voltage began to drop. Remedial efforts failed to restore power. Emergency was declared; a successful landing ensued. Investigation revealed the master control unit had lost power during climb out.

Part total time: 165.0 hours


Excessive elevator play

Loose Pitch Trim Motor Assembly

Found excessive play in elevator during 100-hour inspection. Investigation revealed the pitch trim motor was loose in its mounting plate. Removed pitch trim motor and disassembled. Found two out of four mounting screws completely backed out, and the other two with 1-2 threads of engagement. This issue has been found on two other aircraft.

Part total time: 2774.0 hours


Tripped Circuit breakers

Damaged Data Logger Wiring

Pilot found stall warning and fuel-quantity circuit breakers tripped. Troubleshooting found connectors for the recoverable data logger were corroded, burned and melted. Installed a new P1048 connector and installed repaired data logger.

Part total time: Unknown


Complete Electrical Failure

Failed Master Control Unit

Aircraft’s electrical system completely failed while en route. Troubleshooting had MFD/PFD and nav/comms online briefly. Circuit breakers popped, electrical systems all were offline with loss of flaps, trim control, nav and comm. Turned off all electrical components and navigated with an EFB. Flew with battery-powered backup of airspeed/attitude/altitude. Made traffic calls with handheld radio at non-towered airport. Landed without flaps or trim control. Investigation revealed a burned-out/charred master control unit.

Part total time: 2827.0 hours

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