Cirrus Design SR22
Service difficulty reports · 438
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'SR22' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'SR22' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR YD5R2010F00102Brush Holder · damaged23-80.001 COMMUNICATIONS DISC EXCESS STATIC IN HEADSET INTERMITTNETLY ((YD5R)) INTERFERES WITH RECEPTION ON BOTH COMS. ISOLATED NOISE TO BE FROM ALTERNATOR (1) (NOISE GOES AWAY WHEN UNIT IS TURNED OFF). PERFORMED INSP IAW (KAES SIL-A-135). FOUND INBD BRUSH SDR 2010FA0000416Control Module · failedPILOT WAS FLYING ALONG AND NOTICED THE ALTERNATOR 1 CIRCUIT BREAKER TRIPPED. UPON LANDING THE LOCAL SHOP FOUND THE FIELD CONTROL MODULE TO BE FAULTY. REPLACED MODULE AND EVERYTHING WAS OK.SDR 2010FA0000408Torque Tube · looseTHE (2) BLIND RIVETS ATTACHING THE FLANGE TO THE TORQUE TUBE WERE FOUND LOOSE AND "WORKING" ON THE ELEVATOR. NOT THAT AD 01-25-03 WAS PREVIOUSLY COMPLIED WITH, AND THE DIMPLED (AD) RIVET WAS INSTALLED. THIS COMPONENT MAY REQUIRE CONTINUED INSP AT SOME HOURLYSDR CA100507003Seal · leakingSEAL ON RT TURBO LEAKING OIL INTO HEAT MUFF, CAUSING SMOKE IN COCKPIT.SDR 2010FA0000407Wire · broken(YD5R) WHILE COMPLING WITH A 500 HR INSPECTION, THE BRUSH HOLDER ASSY WAS REMOVED FOR INSP OF BRUSHES. IT WAS FOUND THAT (1) BRUSH HAD A BROKEN WIRE. THE WIRE HAD PULLED AWAY FROM THE CONTACT BUTTON. TT ON COMPONENT ONLY 30.0 HOURS. IT WAS LIKELY CAUSED BSDR 2010FA0000413Spark Plug · cracked(5CSR) DURING ROUTINE MX OF SPARK PLUGS IT IS FOUND THA THE CTR ELECTRODE INSULATING CERAMIC IS CRACKED AND/OR MISSING CHUNKS. ON AVERAGE, ARE FINDING ABOUT (1) OUT OF 20 SPARK PLUGS OF THIS MODEL HAVE THIS CONDITION AND THIS HAS BEEN THE CASE FOR ABOUT THE SDR 2010FA0000175Distributor Gear · brokenMAGNETO WAS REMOVED FROM ACFT FOR ROUTINE 500 HR MAGNETO INSP. DURING INSP, DISTRIBUTOR GEAR WAS FOUND TO BE MISSNG A FEW TEETH. THE ELECTRODE WAS LOOSE IN THE DISTRIBUTOR GEAR AND HAD WORN THE DISTRIBUTOR BLOCK ELECTRODE POSTS. BOTH PARTS WERE REPLACED. TSDR 2010FA0000176Distributor Gear · damagedDURING PRE-TAKEOFF ENG RUN-UP, IT WAS NOTED THAT THERE WAS SOME ENGINE ROUGHNESS. THE MAG CHECK INDICATED THE THE LT MAGNETO WAS NOT FIRING PROPERLY (THE ENG WAS QUITTING). THE MAGNETO WAS REMOVED AND OPENED FOR INSP. THE DISTRIBUTOR GEAR WAS FOUND TO BE MISDR 2009FA0000804Cylinder · crackedDURING VISUAL INSP CONCURRENT WITH OIL AND FILTER CHANGE, THE NR 4 CYLINDER WAS FOUND CRACKED, UPPER, OUTBOARD FIN, RADIUSING DOWN TO CYLINDER HEAD BASE LT OF SPARK PLUG AND IN BETWEEN LOWER FIN AND HEAD.SDR J4PA4995Pump · inoperativeON 9-28-09 DURING FINAL APPROACH FOR LANDING INTO KROA FROM KMCN N383CD (SYK 02)THE THROTTLE WAS RETARDED AND THE ENGINE QUIT OPERATING. TRIED TO RESTART BUT NO GO. PILOT DEAD STICKED THE AIRCRAFT ONTO THE RUNWAY WITHOUT INCIDENT. NO PASSENGERS WERE ON BOARD TSDR 2009FA0000899Ring · failedJACKED ACFT IAW MM. TAIL TIEDOWN RING FAILED WITH ACFT ON JACKS. TIEDOWN RING MADE OF RUBBER ONLY. SITUATION CAUSES THREAT TO PERSONNEL UNDER AND AROUND ACFT. ACFT WILL FALL-NOSE DOWN WHEN FAILURE OCCURS. (K)SDR 2009FA0000851Pan · damagedPILOT REPORTED THE PROPELLER APPEARED TO BE MUCH CLOSER TO THE GOUND THAN NORMAL & OIL WAS LEAKING FROM COWL. OWNER REMOVED COWL ENOUGH TO OBSERVE UPPER BUNGEE ASSY CUP ROTATED UP INTO THE OIL PAN. SHAFT WELD FAILED, ALLOWING CUP ASSY TO ROTATE. AT SOME POSDR 2009FA0000820Screw · brokenPILOTS REPORTED THAT THE DOOR POPPED OPEN ON TAKEOFF, 800 FEET. THE PILOT GRABED THE DOOR BY THE HANDLE TO PULL IT CLOSED AND THE HANDLE CAME OFF IN HIS HAND. PLASTIC SCREWS BROKE OOF A THE HEAD. RECOMMEND REPLACING HARDWARE WITH STEEL. (K)SDR 2009FA0000490Starter · defectiveSTARTER ADAPTER FAILED DUE TO STARTER STAYING ENGAGED AFTER ENGINE STARTED.SDR 2009FA0000656Cartridge · corrodedON SHORT FINAL APPROACH, PILOT REDUCED THE THROTTLE TO IDLE PR FOR LANDING. ABOUT 25 FT ABOVE GROUND LEVEL, THE NOSE PITCHED DOWN. PILOT TRIED TO PULL BACK ON THE YOKE TO FLARE, BUT ELEVATOR CONTROL WAS STUCK IN THE MID-RANGE POSITION. ACFT TOUCHED DOWN ON SDR 2009FA0000698Screw · looseIN CRUISE FLIGHT THE CFI EXPERIENCED ELEVATOR FLUTTER WHICH DECREASED AIR SPEEDS BELOW 140KTS. REPORTS THE COCKPIT WAS VIBRATING NOTICEABLY AND WHEN HE LOOKED BACK HE SAW THE ELEVATOR VIBRATING. INSP OF THE ELEVATOR SYS SHOWED NO DEFECTS EXCEPT FOR THE FACT SDR CA090507011Injector · failed(CAN) WHILE REMOVING NR2 CYLINDER INJECTOR NOZZLE FOR 300 HR CLEANING, THE PART IN QUESTION WAS FOUND TO SHEAR AT THE CYLINDER UPON REMOVAL ATTEMPT. THIS IS THE SECOND SUCH FAILURE OF THIS TYPE ON THIS ENGINE IN RECENT MONTHS. DUE TO SUSPICION OF OTHER NOZZLESSDR 2009FA0000340Cylinder · crackedDURING ANNUAL INSP, FOUND NR 4 CYLINDER CRACKED BETWEEN TOP SPARK PLUG HOLE AND FUEL INJECTOR PORT. (K)SDR 2009FA0000295Flange · crackedCUSTOMER REPORTED LARGE OIL LEAK. INSPECTED AND FOUND NR 2 STANDBY ALTERNATOR MOUNTING FLANGE CRACKED. .7500 OF THE FLANGE HAD COMPLETELY SEPARATED FROM THE ALTERNATOR. ONLY ONE MOUNTING STUD HELD THE ALTERNATOR ON THE ENGINE. CORRECTIVE ACTION WAS TO INSTSDR 2009FA0000103Throttle Body · seizedCUSTOMER COMPLAINED THAT HE WAS UNABLE TO GET ENGINE TO RECOMMENDED IDLE SPEED AND THAT THE THROTTLE WAS VERY HARD TO MOVE. INSPECTED ACFT AND ENGINE, FOUND THOTTLE BODY SEIZED. REMOVED AND REPLACED WITH NEW PART SUPPLIED BY MFG. (K)SDR 2009FA0000442Starter · damagedSTARTER ADAPTER FAILURE 3 TIMES SINCE BUYING THE ACFT NEW IN NOV 02. THE MFG SUPPLIED STARTER DOES NOT RELEASE THE STARTER ADAPTER AFTER START UP CAUSING DAMAGE TO THE ADAPTER. FAILURE IS NOTED AS THE STARTER FAILS TO TURN THE PROP BUT THE SOUND OF THE STARTERSDR J4PA4438Trim Motor · shortedAT 1656 LOCAL DEPARTED FROM KCUB TO KIGX WITH 2 PAXS, CRUISE TO 5,000 FT. AUTOPILOT WAS PULLING TO RIGHT. AFTER RESETTING OF THE AP SMOKE WAS SEEN FROM THE RIGHT SIDE OF THE CENTER AVIONICS RACK. THE AUTOPILOT WAS DISCONNECTED AND THE SMOKE STOPPED. AFTER LSDR 2009FA0000046B-Nut · looseWHILE PERFORMING A 100 HR INSP ON AN ENGINE, THE OIL LINES FOR THE TURBO NORMALIZED SYS WERE BEING CHECKED FOR SECURITY. MX TO OIL LINE THAT CONNECT BETWEEN THE MANIFOLD PRESSURE CONTROLLER AND THE MASTER WASTE GATE IN HIS HAND, APPLIED VERY LITTLE PRESSURE TSDR 2009FA0000027Wire Harness · chafedFOUND THE BLACK PLASTIC WIRE LOOM THAT HOUSES THE MAP WIRING HARNESS FWD OF THE BAFFLE TO HAVE CHAFED THROUGH THE WIRE INSULATION OF THE WIRES IN SEVERAL LOCATIONS. THIS IS CAUSED BY THE WIRE HARNESS BEING ABLE TO MOVE INSIDE THE LOOM AND THE LOOM BEING MADE SDR S8Y2008F00001Muffler · warpedORIGINAL EQUIPMENT INSTALLED NEW AT FACTORY. FUND BY VISUAL INSPECTION AT THIRD 100 HR INSPECTION CYCLE. MUFFLER CONE/BAFFLE SAGGING AND WARPED. DOWN LOAD OF RECENT ENGINE DATA, EGT/CHT, SHOWS NO ANOMALIES THAT WOULD HAVE CAUSED DEFECT. (K)SDR S8Y2008F00000Antenna · looseTHE GPS ANTENNAS, NR 1 AND NR 2 ON THIS ACFT ARE HELD IN POSITION WITH DOUBLE SIDED TAPE. IN 272 HRS THEY HAVE COME LOOSE 3 TIMES. THE ANTENNAS SHOULD HAVE MOD TO PERMANENTLY MOUNT THEN ON THE AIRFRAME.SDR 2008FA0000639Hinge · corrodedFLAP HINGES IN ALL POSITIONS BOTH LT AND RT HAVE INTERGRANDULAR CORROSION NEAR THE POINT OF FAILURE. PN 13431-003, PN 13431-004, 13432-002, QTY 2, 13433-006, 13433-005. CONDITION WAS FOUND AT ANNUAL INSPECTION. (K)SDR 2008FA0000589Drive Shaft · shearedTHIS AC HAS HAD 5 FAILURES OF THE AIR CONDITIONING COMPRESSOR DRIVE SHEAR SHAFT. THE AVERAGE TIME BETWEEN FAILURES IS 35.8 HOURS. THE SAME SHAFT BUILT BY ANOTHER MFG, HAS HAD ZERO FAILURES. WE HAVE HAD SEVERAL FAILURES IN DIFFERENT AC WITH THIS PART. THE DESIGSDR 2008FA0000532Buss Bar · loosePILOT REPORTED THE NR 2 ALTERNATOR WAS INTERMITTENT. WHILE TROUBLESHOOTING THE NR 2 ALTERNATOR, FOUND 13 SCREWS LOOSE AND 1 SCREW MISSING ON THE COPPER CIRCUIT BREAKER BUSS BAR. THE 1 SCREW MISSING WAS ON THE NR 2 ALTERNATOR CIRCUIT BREAKER BUSS FEED. PROBASDR J4P2008F00000Autopilot Sys · failedFLIGHT ORIGINATED AT PBI TO CCO AT 1319L WITH 2 PAX, WHILE EN ROUTE AUTO PILOT FAILED AND DIVERTED TO SGT AND WITHOUT INCIDENT. (A)SDR 2008FA0000439Bearing Cap · crackedPILOT REPORTE TO HAVE AN ALTERNATOR NR 1 FAILURE DURING GROUND PRE-FLIGHT RUN-UP. AC WAS BROUGHT IN FOR MAINTENANCE TO TROUBLESHOOT ALTERNATOR ISSUE. ALTERNATOR BEARING END CAP WHICH IS PART OF THE ALTERNATOR CASE COMPLETED CRACKED OFF AND WAS LYING ON THE ENSDR 2008FA0000492Fan · crackedALTERNATOR NR 2 (BELT DRIVEN ALTERNATOR) COOLING FAN DEVELOPED CRACK AT FAN BLADE RADIUS. CRACK ELONGATED UNTIL FAN SEPARATED FROM ALTERNATOR. (K)SDR 2008FA0000493Wire · fatiguedWIRES THAT CONNECT TO THE ALTERNATE AIR DOOR (WHICH ARE SOLDERED TO THE SWITCH) FOR THE TORNADO ALLEY TURBO SYSTEM ARE BECOMING FATIGUED AND SOLDER IS BREAKING AT SWITCH. IF THE ALTERNATE AIR WAS TO OPEN AND THESE WIRES WERE BROKEN, IT WOULD NOT GIVE THE PILOSDR 2008FA0000469Mount · crackedSTANDBY ALTERNATOR MOUNTING FLANGE CRACKED IN (2) PLACES. OIL GALLING AT MOUNT FLANGE WHERE CRACKS WERE NOTED. (K)SDR 2008FA0000451Elbow · misinstalledWHILE ACCOMPLISHING SERVICE ADVISORY 08-03 IT WAS DISCOVERED THAT RT SIDE EXHAUST ELBOW WHICH IS INSERTED BETWEEN WASTEGATE OUTLET FITTING AND TAILPIPE WAS ORIGINALLY INSTALLED BACKWARDS A THE FACTORY. THIS INCORRECT INSTALLATION RESULTED IN ELBOW HAVING ONLY SDR 3657Alternator · failedAIRCRAFT DEPARTED KCLT AT 0825 FOR DESTINATION KJAX. DURING CRUISE, ALTERNATOR 1 ANNUNCIATOR LIGHT ILLUMINATED INDICATING A FAILURE. THE PILOT DIVERTED TO KGMU WITH AN UNEVENTFUL LANDING. THE ALT 1 FIELD WIRE WAS FOUND TO BE BROKEN. FIELD WIRE WAS REPAIREDSDR 3611Probe · inoperativeAIRCRAFT DEPARTED KPGV TO KGMU WITH 2 PASSENGERS. DURING CRUISE, THE NR 6 CHT INDICATOR FAILED AND THE PILOT MADE AN UNSCHEDULED LANDING AT KJQF. THE LANDING WAS WITH OUT INCIDENT. SATSAIR MAINTENANCE WAS FLOWN TO KJQF AND THE NR 6 CHT WAS REMOVED AND REPLACSDR 2008FA0000378Transmitter · malfunctionedFOLLOWING ACTIONS WERE TAKEN AS A RESULT OF A PRECAUTIONARY LANDING, WHERE PILOT REPORTED A LOSS OF OIL PRESSURE. AT CRUISE, AT 8000 FT, OIL PRESSURE ANNUNCIATOR LIGHT ILLUMINATED, OIL PRESSURE GAUGE INDICATED NO OIL PRESSURE. AFTER LANDING, OIL PRESSURE RESDR 18937Vhf Comm · inoperativeFLYING FROM GMU TO PHF IN SERVER RAIN, THE PILOT DIVERTED TO GSO. THE PILOT REPORTED HEAVY STATIC ON THE RADIOS AND COULD TRANSMIT BUT COULD NOT RECEIVE. LANDING WAS UNEVENTFUL. ONE PASSENGER ONBOARD.SDR 3324Display · malfunctionedFLYING FROM CEU TO JZI, AT 7000 FT IN IMC AND MODERATE RAIN 40 MILES EAST OF JZI, FOUR RED X'S APPEARED ON THE PFD. BURNING ELECTRICAL WIRE FUMES WERE ALSO DETECTED BUT REMAINED FAINT. PFD FAILURE AND SMOKE AND FUME CHECKLISTS WERE REVIEWED. AN EMERGENCY WASDR 3257Sensor · erraticIN TAKEOFF CLIMB AND THE OIL PRESSURE WAS FLUCTUATING BETWEEN 25 PSI AND 60 PSI. AIRCRAFT RETURNED TO HOME STATION WITHOUT INCIDENT. ONE PASSENGER ONBOARD, NO INJURIES OR DAMAGE TO AIRCRAFT. TROUBLESHOT SYSTEM, FOUND THE OIL PRESSURE SENSOR WAS READING ERRASDR 2009FA0000491Adapter · defectiveSTARTER ADAPTER FAILED DUE TO STARTER STAYING ENGAGED AFTER ENGINE HAD STARTED.SDR 2007FA0001106Wire Harness · damagedALTERNATOR FAILED ON FIRST FLIGHT AFTER INSTALLATION FROM OVERHAUL. FOUND FIELD WIRE RIPPED OUT OF FIELD BRUSH AND BARE WIRE DEBRIS INSIDE ALTERNATOR CASE. SUSPECT WIRE EPOXY HOLD DOWN VIBRATED LOOSE ALLOWING ROTOR ASSEMBLY TO SNAG WIRE.SDR FAA010208001Unknown · malfunctionedPFD AND GPS/NAV1 BOTH REBOOTED AT THE SAME TIME. RESTARTED WITHOUT GOING THROUGH EITHER ITS STANDARD INITIALIZATION OR ITS FAST START ROUTINE. THE AUTOPILOT SEEMED TO BE STILL ENGAGED BUT THE VS SELECTION, QNH, ALTITUDE PRE-SELECT AND HEADING WERE RESET AND SDR 11470Circuit Breaker · trippedDURING A FLIGHT FROM KAAF TO KLUL, THE NR 1 GARMIN BECAME INOPERATIVE. RETURN TO ORIGIN NO INCIDENT. FERRIED TO KSGJ FOR REPAIR. FOUND CB FOR PARTIAL POWER OF MAIN BUSS OPEN. RESET CB. GROUND CHECKED GOOD. LEFT KSGJ FOR KMLB AND THE CB TRIPPED AGAIN. FESDR 2007FA0000957Magneto · misoverhauledAIRCRAFT ENGINE RUNNING ROUGH AND BACKFIRING ON FLIGHT TEST. PILOT RETURNED AND GROUNDED AIRCRAFT FOR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED INTERNAL INSPECTION OF CONVERTED MAGNETOS TO PRESSURIZATION. MAGNETO CONVERTED TO PRESSURIZED, INSPECTION REVESDR 2007FA0000849Fairing · separatedLOWER SECTION OF RT WING ROOT FAIRING SEPARATED FROM AIRCRAFT IN FLIGHT. FAIRING IS RETAINED WITH JUST A FEW SCREWS AND AN AREA OF THE LOWER PORTION OF FAIRING IS RETAINED WITH DOUBLE SIDED TAPE AND AN AREA OF DOUBLE SIDED TAPE CAME DEBONDED AND AIR GOT UNDERSDR 02783Spark Plug · brokenDURING CRUISE FLIGHT FROM KPDK TO KGEV, THE ENGINE DEVELOPED A VIBRATION AND AIRCRAFT WAS LANDED AT KMRN. TWO PASSENGERS ONBOARD AND LANDED WITHOUT INCIDENT. IT WAS FOUND TO BE A NR 1 CYLINDER SPARK PLUG WITH A BROKEN INSULATOR CAUSING THE ROUGH RUNNING AND SDR 2009FA0000443Wire · looseROLL TRIM ACTUATOR HAS MALFUNCTIONED ON 3 OCCASSIONS SINCE BUYING ACFT NEW IN 02. IN EACH CASE THE WIRES LEADING TO THE ELECTRIC MOTOR HAD COME LOOSE CAUSING THE TRIM ACTUATOR TO HOLD FULL LT AILERON. WITHOUT OVERPOWERING THE UNIT A FATAL CRASH WOULD HAVE RESUSDR 2007FA0000861Exhaust Header · crackedNR 5 EXHAUST HEADER HAS CRACKED OFF AT FLANGE, JUNE 6/06 AT 440.6, NOV 18/06 AT 636.1 HOBBS, MAY 18/07 AT 746.7 HOBBS AND AGAIN AUG 20/07 HOBBS NOT AVAILABLE. AFTER INSPECTING HEADER IT WOULD SEEM THAT A HEAVER GAUGE PIPE WOULD RESOLVE THE PROBLEM. THE LAST
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