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 AU510001764Battery · faulty(AUS) AIRCRAFT BATTERY INTERNAL FAULT. BATTERY HAD HIGH CURRENT DRAW CAUSING LOSS OF ELECTRICAL POWER. (CASA# 510001764)SDR AU510001760Solenoid · failed(AUS) STARTER SOLENOID FAILED. SUSPECT CAUSED BY FAILURE AND CRACKING OF END CAP WHICH ALLOWED COPPER DUST TO LEAK OUT. (CASA# 510001760)SDR AU510001691Line · leakingFUEL SUPPLY PIPE P/N 20139-001 AND FUEL RETURN PIPE P/N 20138-001 LEAKING AT `TEE` FITTING. `TEE` FITTINGS ARE PART OF THE FERRY TANK SYSTEM AND SHOULD BE REMOVED WHEN THE FERRY TANK IS REMOVED. PIPE FLARES WERE POORLY MANUFACTURED. INCORRECT PART.SDR AU510002175Line · damaged(AUS) FUEL PIPES LEAKING. FUEL WAS FOUND TO HAVE BEEN LEAKING FROM THE BLANKED T-FITTINGS THAT WERE INSTALLED IN THE FUEL SELECTOR TO FIREWALL SUPPLY LINE PN 11443-005 AND THE RETURN LINE PN 11444-005. ON REMOVAL THE FUEL LINES WERE FOUND TO HAVE VERY POOR/DASDR ALG2005F00118Indicator · malfunctionedIN FLIGHT TRANSMISSION PRESSURE DROPPED TO ZERO, RETURNED TO NORMAL AND BACK TO ZERO IN A 15 MINUTE FLIGHT. INSPECTION BY MAINT REVEALED THE NR 8 TAIL ROTOR DRIVE SHAFT HAD FAILED. A WO WAS OPENED FOR REPAIR OF THIS AIRCRAFT. REMOVED AND REPLACED TRANSMISSISDR CA051108002Bolt · wornINDUCTION AIR BOX SUPPORT MOUNTING BOLT (AN3-34 BOLT) IS WORN PREMATURELY BY SUPPORT BRACKET 15671-002. THE SAME BOLT ALSO IS WEARING AT CONTACT AREA FROM ALTERNATE AIR DOOR SUPPORT BEARING P/N 50200-101. THIS BOLT SUPPORTS THE INDUCTION AIR BOX ONTO THE CRASDR CA051108003Spring · wornDURING FIRST 100 HOUR INSPECTION, FOUND LEFT EXHAUST TAIL PIPE SUPPORT SPRING END LOOP WORN ABOUT 80 PERCENT AT CONTACT AREA TO MOUNTING BRACKET.SDR AMSA10280502Actuator · brokenPILOT SIDE DOOR PISTON, THAT GOT DISCONNECTED, JAMMED PILOT'S CONTROL STICK. THERE IS NO WAY, THAT AC COULD BE FLOWN IN THIS CONDITION. IN ORDER TO FREE CONTROLS DOOR, UPHOLSTERY HAD TO BE REMOVED PISTON ON DOOR SIDE HAD TO BE DISCONNECTED, DOOR HAD TO BE OPESDR AMSA102805Strut · damagedPILOT SIDE DOOR PISTON, THAT GOT DISCONNECTED AND JAMMED PILOT'S CONTROL STICK. THERE IS NO WAY, THAT AC COULD BE FLOWN IN THIS CONDITION. IN ORDER TO FREE CONTROLS, DOOR UPHOLSTERY HAD TO BE REMOVED AND PISTON ON DOOR SIDE HAD TO BE DISCONNECTED, DOOR HAD TOSDR 2005FA0001508Exhaust Header · crackedNR 5 EXHAUST HEADER CRACKED AT CYLINDER FLANGE JUST BELOW WELD UNDER NORMAL USE. HEADER NEEDS REDESIGN OR SOME SORT OF SUPPORT. IT IS OVER CANTILEVERED FOR STRESSES IMPOSED ON IT. AIRFRAME ADN EXHAUST HOURS: 33.7SDR 2005FA0001507Exhaust Header · crackedNR 5 EXHAUST HEADER CRACKED AT CYLINDER FLANGE JUST BELOW WELD UNDER NORMAL USE. HEADER NEEDS REDESIGN OR SOME SORT OF SUPPORT. IT IS OVER CANTILEVERED FOR STRESSES IMPOSED ON IT. AIRFRAME AND EXHAUST HOURS.SDR 2005FA0001506Exhaust Header · crackedNR 5 EXHAUST HEADER CRACKED AT CYLINDER JUST BELOW FLANGE HALF THE WAY AROUND HEADER UNDER NORMAL USE. HEADER NEEDS REDESIGN OR SOME SORT OF SUPPORT. IT IS OVER CANTILEVERED FOR STRESSES IMPOSED ON IT. NR 6 EXHAUST HEADER CRACKED THRU THE FLANGE FOR A DISTASDR 2005FA0001505Exhaust Header · crackedNR 5 EXHAUST HEADER CRACKED AT CYLINDER JUST BELOW FLANGE ONE HALF THE WAY AROUND HEADER UNDER NORMAL USE. HEADER NEEDS REDESIGN OR SOME SORT OF SUPPORT. IT IS OVER CANTILEVERED FOR STRESSES IMPOSED ON IT. NR 6 HEADER CRACKED THRU THE FLANGE FOR A DISTANCE SDR 2005FA0001366Muffler · missingREPLACED MUFFLERS ON AC DUE TO THE DETERIORATED CONDITION OF THE SPARK ARRESTERS INSIDE OF THE MUFFLERS. THE SPARK ARRESTER IN THE LT MUFFLER WAS GONE. IT HAD COME LOOSE AND FALLEN OUT OF THE MUFFLER SOMEWHERE. THE SPARK ARRESTER IN THE RT MUFFLER HAD MELTESDR 0509137AExhaust Riser · failedNR 5 EXHAUST RISER HAD SEPARATED FROM ENGINE JUST BELOW THE FLANGE WELD. THE OWNER STATED THIS WAS THE SECOND TIME THIS HAS HAPPENED IN 40 HOURS. REPLACED ALL 3 RISERS AND COLLECTOR.SDR M1555Bracket · splitDURING SCHEDULED ENGINE OIL CHANGE, FOUND BRACKET INDUCTION AIR FILTER SPLIT AT MANUFACTURED SEAM. SUSPECT ADHESIVE USED AT MANUFACTURE OF THE FOAM TYPE FILTER IS INADEQUATE FOR THE TASK.SDR 2005FA0001232Line · chafedMAIN FUEL SUPPLY LINE FROM FUEL SELECTOR TO FIREWALL HAD HOLE CHAFED IN IT. THE WIRE BUNDLE TO THE CB PANEL WAS CHAFING LINE. (K)SDR 2005FA0001128Door · failedBOTH DOORS WILL (POP) OPEN IN FLIGHT, CAUSING A SAFETY DISTRACTION TO THE PILOT AND WIND NOISE THAT KEEPS THE PILOT FROM HEARING AT INSTRUCTIONS. THIS STILL HAPPENS AFTER SEVER TRIPS TO MFG REPAIR STATION AND BACK TO FACTORY FOR REPAIRS. MFG RESPONSE IS THATSDR CA050803009Exhaust Header · separated(CAN) PILOT HEARD UNUSUAL EXHAUST NOISE FROM ENGINE.ON INSPECTION, FOUND NR 5 CYLINDER EXHAUST HEADER HAD SEPARATED .1875 INCH FROM THE FLANGE JUST BELOW THE WELD.SDR 2005FA0001099Mount · brokenALTERNATOR MOUNT BROKEN AND OIL LEAK. (THE ALTERNATOR CASE MOUNT FLANGE BROKEN) DRIVESHAFT IN ALTERNATOR SHEARED. THE ENGINE DRIVE SHAFT HUB HAS NO DAMAGE. (K)SDR 2005FA0000821O-Ring · flatAC LANDED AND DISCOVERED THEY HAD NO RT BRAKE. AC LOST DIRECTIONAL CONTROL AND IMPACTED A PARKED AIRCRAFT CAUSING SUBSTANTIAL DAMAGE TO THE PARKED AIRCRAFT. INVESTIGATION REVEALED THE RT BRAKE O-RING WAS FLAT AND THE HOUSING AND DATA PLATE SHOWED EXTREME HEASDR 2005FA0001088Battery · corrodedSECOND ELT FOUND WITH BATTERIES IN THIS CORRODED CONDITION. (K)SDR 2005FA0000723Exhaust Header · crackedDURING AN ANNUAL INSPECTION OF THIS AC. THE NR5 EXHAUST HEADER WAS FOUND TO BE CRACKED .7500 WAY AROUND THE CIRCUMFERENCE OF THE PIPE. NR 5 EXHAUST HEADER WAS REPLACED. (K)SDR AHDR051179Display · smokePILOT REPORTED SMOKE COMING FROM INSTRUMENT PANEL ABOVE MFD. DISPLAY WENT BLANK AND SMOKE CONDITION ENDED. AIRCRAFT WAS NEARING DESTINATION SO PILOT CONTINUED TO LANDING. ON SHORT FINAL MFD CAME BACK ON. UNIT REMOVED AND RETURNED TO MFG FOR INSPECTION AND SDR 2005FA0000523Skin · debondedLT DOOR HANDLE IS MOUNTED IN A TURNED ALUMINUM RECESS THAT IS SUPPOSED TO BE BONDED TO THE DOOR. THIS RECESS HAS COME LOOSE FROM THE DOOR AND IS FREE TO ROTATE. WHEN IT ROTATES, IT JAMS THE HANDLE AND MAKES THE DOOR EXTREMELY DIFFICULT TO OPEN. THE PART HAS TSDR 2005FA0000584Connector · dirtyAT HIGH POWER SETTINGS THE RPM AND TEMPERATURE INDICATIONS WOULD BECOME INTERMITTENT. INVESTIGATION REVEALED THE EGT/CHT HARNESS ON THE RT BANK OF CYLINDERS WAS ROUTED TOO CLOSE TO THE EXHAUST SYSTEM AND WAS BURNING THROUGH THE INSULATION OF THE WIRES. CONNECTSDR AU510001759Solenoid · failed(AUS) STARTER SOLENOID FAILED. SUSPECT CAUSED BY FAILURE AND CRACKING OF END CAP WHICH ALLOWED COPPER DUST TO LEAK OUT. (CASA NR 510001759)SDR CA050202006Control Unit · restricted(CAN) PILOT NOTICED ELEVATOR CONTROL WAS STIFFER THAN USUAL ON APPROACH. UPON LANDING, FOUND THE LT ELEVATOR BALANCE WEIGHT HORN IS RUBBING AGAINST THE HORZIONTAL STABILIZER. FOUND THE ELEVATOR WILL NOT RUB ONCE THE AIRCRAFT IS WARMED UP. THE ELEVATOR TIP FSDR 270112Bolt · chafedTHE BOLT (P/N 3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFFED BY THE INDUCTION DUCT SUPPORT BRACKET P/N 15671-002. IN ADDITION TO THE CHAFFED BOLT THE PLASTIC DUCT IS SUSCEPTABLE TO CRACKINGSDR 27641204Bracket · chafedTHE PILOT REPORTED A LOSS OF VOLTAGE INDICATION ON THE MFD WITH ALL OTHER SYSTEMS OPERATING NORMALLY. THROUGH TROUBLESHOOTING IT WAS DISCOVER THAT WIRE #ANEN983-22 WAS CHAFFED THROUGH THE INSULATION (THE AREA IN QUESTION IS LOCATED ABOVE THE CO-PILOTS KICK PASDR 27011204Bolt · chafedTHE BOLT (P/N 3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFED BY THE INDUCTION DUCT SUPPORT BRACKET P/N 15671-002. IN ADDITION TO THE CHAFED BOLT THE PLASTIC DUCT IS SUSCEPTABLE TO CRACKING ASDR 2005FA0000332Exhaust Pipe · crackedAIRCRAFT OWNER SQUAWKED MANIFOLD PRESSURE AT 11 PERCENT. FOUND EXHAUST CRACKED AT NR 5 CYLINDER EXHAUST PORT. CRACK EMINATES FROM REAR OF MOUNTING FLANGE AND SPIRALS DOWN COUNTER CLOCKWISE SEVERAL INCHES FROM THERE.SDR 26251204Bolt · chafedTHE BOLT (P/N 3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFED BY THE INDUCTION DUCT SUPPORT BRACKET (P/N 15671-002). IN ADDITION TO THE CHAFFED BOLT THE PLASTIC DUCT IS SUSCEPTIBLE TO CRACKISDR 25921104Bolt · chafedTHE BOLT (P/N AN3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFED BY THE INDUCTION SUPPORT BRACKET (P/N 15671-002). IN ADDITION TO THE CHAFED BOLT THE PLASTIC DUCT IS SUSCEPTIBLE TO CRACKING ARSDR LC12005F00000Oil Cooler · crackedOIL COOLER IS CRACKED AT THE LOWER LT FLANGE AREA.SDR 2005FA0000018Oil Cooler · crackedTHIS AIRCRAFT HAS HAD AN OIL COOLER REPLACED FOR THE SAME DEFECT AT <300 HOURS. THE NEW OIL COOLER IS CRACKED AGAIN AT THE LOWER LT FLANGE AREA. NOTE: MFG HAS A SIX POINT ENGINE MOUNT OPTION AVAILABLE TO REDUCE VIBRATION IN THE AIRCRAFT. THIS AIRCRAFT HAD SDR 2005FA0000164Lifter · corrodedDURING A RECENT MFG SYMPOSIUM, THE PROBLEM OF UNAIRWORTHY LIFTERS IN MFG ENGINES DISCUSSED. MFG ENGINE HAVE BEEN NOT HOLDING UP WELL IN THESE AREAS AND MANY SC`S ARE RECOMMENDING AN INSPECTION OF THE LIFERS DURING SCHEDULED MAINTENANCE. THIS AC WAS UNDERGOINSDR 110404N103CS1Bulb · burned outUNSAFE GEAR INDICATION ON APPROACH TO KSFB. CREW FOLLOWED CHECKLIST AND DECIDED TO DIVERT TO KMCO AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. FAULT DETERMINED TO BE A FAILED LIGHT BULB.SDR 24331Bolt · chafedTHE BOLT (P/N AN3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSEMBLY (P/N 15708-001) IS BEING CHAFFED BY THE INDUCTION DUCT SUPPORT BRACKET (P/N 15671-002). IN ADDITION TO THE CHAFFED BOLT THE INDUCTION DUCT ASSY IS SUSCEPTSDR 2004FA0000898Fairing · departedNOSE WHEEL FAIRING DEPARTED AIRPLANE ON CROSSWIND LANDING. HAD SIGNIFICANT SHIMMY IN THE FRONT WHEEL UPON TOUCHDOWN. DISCOVERED UPON REACHING RAMP AREA OF REAR PART OF FRONT WHEEL FAIRING.SDR 24041004Bracket · chafedTHE INDUCTION DUCT SUPPORT BRACKET P/N 15671-002 HAS BEEN FOUND TO BE CHAFING INTO THE ALTERNATE AIR DOOR PIVOT BOLT P/N AN3-34. REPORTED THIS CONDITION BEFORE. A CHECK OF MULTIPLE AIRCRAFT HAVE SHOWED SIGNS OF CHAFFING AT THIS LOCATION. SUGGEST CLOSE LOOK SDR 2004FA0000844Elt · incorrectDURING A RECENT INSPECTION OF A NEW AC IT WAS NOTED THAT THE ELT SWITCH WAS IN THE OFF POSITION FROM THE MANUFACTURE, UPON FURTHER INVESTIGATION THE PILOT RECEIVED THE AIRCRAFT FROM THE FACTORY AND WAS NOT INFORMED THAT THE SWITCH WAS OFF DURING HIS FLY-OFF FRSDR 2201092004Bolt · chafedDURING REMOVAL AND REPLACEMENT OF THE P/N 15708-001 INDUCTION DUCT ASSY IT WAS NOTED THAT DUCT WAS CRACKED IN THE AREA OF THE AN3-34 BOLT THAT SERVES AS THE HINGE POINT FOR THE ALTERNATE AIR DOOR. AFTER REMOVING THE BOLT IT WAS FOUND TO BE CHAFFED ALL THE WAYSDR 22010904Bolt · chafedDURING REMOVAL AND REPLACEMENT OF THE P/N 15708-001 INDUCTION DUCT ASSY. IT WAS NOTED THAT THE INDUCTION DUCT WAS CRACKED IN AREA OF AN3-34 BOLT WHICH SERVES AS HINGE POINT FOR ALTERNATE AIR DOOR. AFTER REMOVING BOLT IT WAS FOUND TO HAVE A GROOVE WORN INTO BSDR 220192004Bolt · chafedDURING REMOVAL AND REPLACEMENT OF PN 15708-001 INDUCTION DUCT ASSY IT WAS NOTED THAT INDUCTION DUCT WAS CRACKED IN AREA OF AN3-34 BOLT WHICH SERVES AS HINGE POINT FOR ALTERNATE AIR DOOR. AFTER REMOVING BOLT IT WAS FOUND TO HAVE A GROOVE WORN INTO BOLT SHANK ASDR NF22004FCCCWire · chafedALTERNATOR OUTPUT WIRE CHAFED ON THE RT FWD VALVE COVER AND BURNED A .2500 INCH HOLE IN THE VALVE COVER. WIRE AND BAFFLE ABOVE VALVE COVER NEED TO BE SECURED BETTER. SHORTING OF THE WIRE ALSO CAUSED DAMAGE TO COMPONENTS IN THE MCU AND SUBSEQUENT NR 1 ALTERNASDR 16970704Exhaust Header · crackedTHIS AIRCRAFT HAD THE NR 1,NR 3,NR 5 HEADERS REPLACED WITH NEW PARTS AT 154.0 HRS. THE AIRCRAFT THEN EXPERIENCED A CRACK IN THE NR 5 HEADER AT 180.0 HRS. THERE DOES NOT SEEM TO BE ANY ABNORMAL STRESS ON THE PART/INSTALLATION. AIRCRAFT EXHAUST SYSTEM WILL BE MSDR CA040615015Hinge · corroded(CAN) WING FLAP HINGE HAS INTERGRANULAR CORROSION ON THE LEADING EDGE OF HINGE JUST BELOW THE WING SKIN AND FLAP HINGE FAIRING.SDR CA040615014Hinge · corroded(CAN) FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGEJUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.SDR CA040615013Hinge · corroded(CAN) FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGEJUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.
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