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 2016FA0000513Bolt · shearedDURING START FOR MAINTENANCE THE PROPELLER JERKED TO A STOP. SUBSEQUENT START ATTEMPTS SHOWED NO MOVEMENT OF PROPELLER WHILE STARTER WAS RUNNING. REMOVAL OF THE STARTER AND STARTER ADAPTER REVEALED ALL SIX BOLTS THAT ATTACH THE LARGE GEAR TO THE CRANKSHAFT HADSDR IVLA2016F00193Nut · loosePILOT EXPERIENCED A LACK OF THROTTLE RESPONSE UPON SHORT FINAL. FOUND NUT SECURING THROTTLE LEVER LOOSE.SDR 2016FA0000185Case · crackedENGINE WITH STC SE10589SC, FOUND CASE CRACKED BETWEEN CYLINDER 2 AND CLYINDER 4.SDR YD5R201604068442Manifold · distortedDISTORTION AND BULGE IN LT EXHAUST MANIFOLD. THIS ACFT HAS AN ENGINE THAT WAS MODIFIED BY STC SE10589SC AND INSTALLED ON THE ACFT UNDER SA10588SC. THIS REPORT IS TO GIVE MY OPINION THAT THERE IS A POTENTIAL FOR FAILURE OF THIS EXHAUST ASSY AND THAT SI11-01 SDR YD5R201604068441Manifold · crackedCRACK IN A WELD ATTACHING AN EXHAUST DUCT TO THE RT WASTE GATE. THIS ACFT HAS AN ENGINE THAT WAS MODIFIED BY STC SE10589SC AND INSTALLED ON THE ACFT UNDER SA10588SC. PAST EXPERIENCE ON MULTIPLE ACFT HAS SHOWN THAT THIS VERSION OF THE EXHAUST ASSEMBLY IS PRONSDR YD5R2016033017830Manifold · failedSIGNIFICANT DISTORTION AND HEAT STRESS IN THE LT EXHAUST MANIFOLD BETWEEN CYLINDERS 2 AND 4. DAMAGE OF THIS TYPE IS FREQUENTLY FOUND IN THIS GENERAL AREA ON ENGINES MODIFIED WITH STC SE10589SC. WE HAVE ANOTHER SIMILARLY MODIFIED ACFT WITH SIMILAR DAMAGE IN TSDR PAIR2015010801496Crankcase · crackedPILOT NOTED OIL LEAK FROM ENGINE AFTER LANDING. MAINTENANCE FOUND A CRACK, APPROXIMATELY 1" LONG, IN THE LT SIDE CRANKCASE APPROXIMATELY 1" AFT OF THE 7TH STUD FOR THE NR 2 CYLINDER WHICH IS LOCATED BEHIND THE OIL COOLER. UNABLE TO SEE THIS CRACK WITH THE OISDR CA160115002Distributor Gear · broken(CAN) ENGINE WOULD NOT RUN ON RT MAGNETO. INSPECTION OF MAGNETO REVEALED NYLON DISTRIBUTOR GEAR NOT TURNING WHEN MAGNETO ROTOR TURNED. FOUND 8 TEETH BROKEN OFF OF THIS GEAR. TEETH FOUND INSIDE MAGNETO, NEAR GEAR. NO REASON FOR FAILURE WAS FOUND. THE CONDITSDR CA160106008Distributor Gear · failed(CAN) DISTRIBUTION GEAR ON RT MAGNETO FAILED IN FLIGHT.SDR YD5R2015102000497Dipstick · mismarkedTHIS ACFT RETURNED TO SERVICE CENTER FOR A REPORTED EXCESSIVE OIL CONSUMPTION ISSUE. THROUGH INVESTIGATION AND VISUAL COMPARISON, IT WAS FOUND THAT THE OIL LEVEL DIPSTICK WAS INCORRECTLY MARKED. COMPARING TO ANOTHER DIPSTICK FROM THE SAME MODEL ENGINE, THE 2SDR 2015FA0000473Adapter · failedFAILED SLIPPING STARTER ADAPTER.SDR 2015FA0000408Tire · out of roundCUSTOMER COMPLAINED OF INTERMITTENT LT MAIN WHEEL VIBRATION DURING TAKEOFF. REMOVED TIRE FROM WHEEL ASSY AND FOUND A 1.4 OZ WEIGHT HAD COME DETACHED FROM THE INNER WALL OF TIRE. SUSPECT WEIGHT WAS POORLY ATTACHED DUE TO LACK OF ADHESIVE MATERIAL. AS BEST DESDR 2015FA0000407Tire · out of balanceCUSTOMER COMPLAINED OF SEVERE NOSE WHEEL VIBRATION. FOUND TIRE OUT OF BALANCE DURING A SPIN CHECK INDICATING A BROKEN OR DAMAGED BELT. SUSPECT MATERIAL FAILURE. AS BEST DETERMINED, THIS DEFECTIVE TIRE WAS PLACED ON AIRCRAFT DURING PRODUCTION, 1/2015.SDR 2015FA0000235Pump · inoperativeBOOST PUMP INOPERATIVE.SDR IVLA2015FA0000191Display · intermittentPILOT DEPARTED. AFTER DEPARTING, THE PERSPECTIVE PFD SHUTDOWN AND THE MFD WENT INTO REVERSIONARY MODE. THE PILOT RETURNED TO DEPARTURE.SDR CA150325027Attach Bracket · cracked(CAN) UPON OF REMOVAL OF NOSE WHEEL PANT ASSY DURING ANNUAL INSPECTION, IT WAS NOTED THAT BOTH LT AND RT NOSE WHEEL PANT ATTACH BRACKETS WERE CRACKED. UNITS WERE REPLACED WITH NEW UNITS SUPPLIED BY MFG.SDR 2015FA0000208Exhaust Stack · damagedINSTALLED MANIFOLD WAS USED AT THIS ANNUAL INSPECTION TO FIND NR 4 CYLINDER EXHAUST STACK AFT END AT SLIP JOINT BULGED AND CRACKED. STAINS IN THAT AREA WERE NOTED, HEATSHIELD DEFLECTED LEAT FROM ANY FURTHER DAMAGE. PART NOT SOLD SEPARATELY, NEW REDESIGN LEFTSDR 2015FA0000094Diode · blownELECTRICAL FAILURE IN FLIGHT. ALT 2 INDICATION CAME ON, THEN LOW VOLTAGE. LOST AUTOPILOT FIRST, THEN GPS1, THEN MFD, THEN AHARS INFO ON THE PFD. HAD JUST HAD ALT2 OVERHAULED 1 MONTH PRIOR. MADE PARTIAL PANEL IAP AND LANDED SAFELY. AFTER MUCH DIAGNOSIS, THSDR 2015FA0000088Scavenge Pump · looseACFT WAS COMING OUT OF ANNUAL INSPECTION. LOW ALTITUDE FUNCTIONAL FLIGHT CHECK INDICATED NO ABNORMALITIES. HIGH ALTITUDE FUNCTIONAL FLIGHT CHECK INDICATED SMOKING EXHAUST PIPE AND LOSS OF TURBO SYSTEM. DECOWLING SHOWED OIL SPRAY. TRACED BACK TO FITTING ON SCASDR 2015FA0000081Injector · brokenDURING FLIGHT THE FUEL INJECTOR BROKE IN HALF. ONE PORTION WAS IN THE NR 1 CYLINDER AND THE OTHER WAS ATTACHED TO THE FUEL LINE FROM THE SPIDER. LUCKILY THERE WAS NOT A FIRE.SDR 2015FA0000070Distributor Gear · brokenENGINE SUDDENLY BEGAN RUNNING ROUGH AND LOSING POWER AT CRUISE POWER SETTING. PILOT EXECUTED PARTIAL POWER LOSS EMERGENCY PROCEDURE AND RETURNED TO DEPARTURE FOR UNEVENTFUL LANDING. ENGINE LOG DATA SUGGESTED IGNITION PROBLEM, TRACEABLE TO RT MAGNETO, CAUSINGSDR SIMA20141125011Door Frame · corrodedSERVICE DOOR CUT OUT CORROSION REPAIR. INSTALLED NEW FRAME 20 SECTION & L SHAPE REPAIR ANGLES IAW ERS-EM-53MR-900.SDR SIMA20141125012Door Frame · corrodedSCREW HOLE BELOW LOWER SERVICE DOOR STOP IS CORRODED ON FWD SIDE OF FRAME 22. INSTALLED NEW FRAME SECTION & L SHAPE DOUBLERS IAW ERS-EM-53MR-899.SDR SIMA20141125013Skin · crackedFRAME 75 SKIN CRACKED AT FASTENER HOLE, BELOW STRINGER 2R - 2L. FABRICATED & DRILLED DOUBLER, FILLER & REPAIR ANGLE FOR FRAME 75 SKIN DAMAGE AT STRINGER 2R - 2L IAW ERS-EM-53MR-901.SDR I2JR20141119001Magneto · inoperativeOPERATOR REPORTED ROUGH ENGINE DURING CLIMBOUT NEAR 300 FT. LANDED WITHOUT INCIDENT. OPERATOR REPORTED PREFLIGHT ENGINE RUN UP AND MAGNETO CHECKS WERE NORMAL. UPON INSPECTION MECHANIC NOTED LT MAGNETO MODEL: S6RSC-25, PN: 10-500556-1 WAS INOPERATIVE. VISUALSDR 5CSR2015FA0000046Cylinder · leakingAIRCRAFT WAS REPORTED TO BE CONSUMING AN EXCESSIVE AMOUNT OF OIL AFTER FLIGHT, ESTIMATED AT 1 QT PER HOUR. AIRCRAFT BELLY WAS HEAVILY COVERED IN OIL AND APPEARED TO BE COMING FROM THE EXHAUST SYSTEM. PERFORMED BORE SCOPE INSPECTION AND FOUND CYCLINDERS 1, 3,SDR IVLA2014103000001Wire · brokenALTERNATOR 1 FIELD TERMINAL FAILED IN FLIGHT CAUSING THE ALTERNATOR 1 TO GO OFF LINE AND STOP CHARGING BATTERY 1.SDR 2014FA0000552Pump · leakingFUEL PUMP LEAKING FROM THE MIXTURE CONTROL SHAFT. THE AMOUNT OF FUEL LEAKING WAS ENOUGH THAT THERE WAS SOME BLUE STAINING OF THE ENGINE CASE UNDER THE PUMP. THIS AIRCRAFT HAS THE TORNADO ALLEY TURBO NORMALIZING SYSTEM INSTALLED UNDER STC SA10588SC AND SE1058SDR 2014FA0000550Pump · leakingFUEL PUMP LEAKING FROM THE MIXTURE CONTROL SHAFT. THE AMOUNT OF FUEL LEAKING WAS ENOUGH THAT THERE WAS SOME BLUE STAINING OF THE ENGINE CASE UNDER THE PUMP. ACFT HAS THE TURBO NORMALIZING SYSTEM INSTALLED UNDER STC SA10588SC AND SE10589SC. SB12-02, THAT ADDSDR U43R2014FA0000509Bracket · crackedPROPELLER CONTROL CABLE BRACKET BROKEN WHICH CHAFES THE CONTROL CABLE.SDR 2014FA0000574Adapter · damagedSTARTER ADAPTER HAS THREE MISSING TEETH AND A CRACK WAS FOUND ON THE CRANK SHAFT GEAR.SDR U43R2014FA0000508Bracket · crackedPROPELLER GOVERNOR CONTROL CABLE BRACKET BROKEN AND CHAFED .SDR 2014FA0000485Anti-Ice System · restrictedIT WAS REPORTED THAT THE ANTI-ICE PANELS ON THE ELEVATOR TIPS WERE NOT FLOWING ON THIS ACFT. THE SYSTEM WAS DISABLED AND THE ACFT CAME TO OUR SERVICE CENTER FOR AN ANNUAL INSPECTION. THE ELEVATOR TIP FLUID FEED LINES WERE FOUND TO HAVE A CREAMY WHITE SUBSTANSDR CA140711007Dipstick · broken(CAN) THE ENGINE OIL DIP STICK CAME APART DURING A ROUTINE OIL CHANGE. THE DIP STICK IS MADE UP OF A CAP, A FLEXIBLE PORTION THAT RESEMBLES A CABLE AND A SOLID END PORTION THAT HAS THE OIL LEVEL MARKINGS ETCHED INTO IT. THE END PORTION IS BONDED TO THE CABLE. SDR 2014FA0000380Distributor Gear · looseDISTRIBUTOR GEAR ROTOR CAME LOOSE FROM GEAR AND INTERFERED WITH ALL SIX BLOCK TERMINALS CAUSING BRASS DUST TO BE GROUND FROM TOWERS AND CONTAMINATED MAGNETO INTERNALLY. BRASS DUST WAS VISIBLE THROUGH TIMING PLUG ACCESS HOLE DURING ROUTINE MAGNETO TO ENGINE TISDR 2014FA0000260Bracket · crackedNR 1 ALTERNATOR BRACKET FOUND CRACKED DURING ROUTINE 50 HOUR INSPECTION. THIS IS THE 6TH WITHIN A YEAR.SDR 2014FA0000248Adapter · slippedA REBUILT STARTER ADAPTER, WAS INSTALLED AT 336.8 HRS. AT 818 HRS, STARTER ADAPTER BEGAN SLIPPING DURING START, REPAIRED.SDR S8YA2014031300086Bolt · shearedAIRCRAFT ENGINE WOULD NOT START. STARTER NOISE COULD BE HEARD BUT THE PROPELLER DID NOT TURN. FLIGHT THE PRIOR DAY HAD BEEN NORMAL WITH NO ANOMALIES. DURING INVESTIGATION, FOUND THE BOLTS WHICH HOLD THE ACCESSORY GEAR DRIVE TO THE BACK OF THE ENGINE CRANK SSDR IVLA20140206004Starter · malfunctionedPILOT STATED THAT ENG WOULD NOT START & STARTER WOULD NOT ENGAGE. ALSO STATED THAT THERE WAS ONLY A CLICKING SOUND WHEN START WAS SELECTED.SDR IVLA20140124003Magneto · damagedAFTER TAKEOFF AT PDK THE PILOT REPORTED A SUDDEN POWER LOSS & ROUGHNESS SHORTLY AFTER SWITCHING TO DEPARTURE CONTROL. PILOT ALSO STATED THAT ENG WOULD RUN SMOOTHLY ON THE LT MAGNETO, BUT WOULD QUIT ON THE RT MAGNETO. UPON REMOVING THE RT MAGNETO, TURNING THESDR 2014FA0000041Engine · power lossENGINE LOSS OF POWER ON CLIMB.SDR EWGR2013111900100Display · shutdownDURING CRUISE, HAD MALFUNCTION OF EQUIPMENT THAT RESULTED IN THE LOSS OF THE LOWER HALF OF BOTH IFD DISPLAYS AND THE LOSS OF ALL INPUT FROM THE KEYBOARD. DECLARED AN EMERGENCY AND LANDED SAFELY. THE LOGS DOWNLOADED FROM THE IFDS ALERTED AVIDYNE TO A SEQUENCSDR CA131018013Cylinder · cracked(CAN) ENGINE RECEIVED FOR PROP STRIKE INSPECTION. DURING ROUTINE INSPECTION IT WAS FOUND THAT ALL 6 OF THE CYLINDERS AND PISTONS EXHIBITED STRESS CRACKING. THE CRACKING IS NOT CONDUCIVE WITH PROP STRIKE DAMAGE, BUT RATHER WITH OVER-BOOST OR OVER-STRESS OF THSDR 2013FA0000635Attach Fitting · wornEXCESSIVE WEAR NOTED AT SLAVE, RT, WASTEGATE BUTTERFLY SHAFT CONTROL ATTACHMENT TAB. WEAR ON ATTACH POINT OF ACTIVATOR LINKAGE ALSO. ENGINE HAS BEEN ALTERED STC SE10589SC TORNADO ALLEY TURBO INSTALL. NEED TO REQUIRE RECURRING DETAILED INSPECTIONS OF THIS ASDR 2013FA0000578Starter · failedTHIRD FLIGHT OF THE DAY WITH A FULLY CHARGED BATTERY, CREW BEGAN TO START ENGINE BUT STARTER WAS SLOW TO TURN THEN CAME TO A COMPLETE STOP AFTER SEVEN SECONDS.SDR 2013FA0000498Starter · failedSTARTER FAILED ON FIRST ATTEMPT. WHEN CREW RELEASED STARTER SWITCH ABORTING THE START THEY NOTICED A SMALL "PUFF OF SMOKE" COMING FROM UNDER THE COWLING. MX NOTED A BURN MARK ON STARTER CASE AT THE BASE OR ATTACHING POINT ON THE OUSIDE. STARTER CIRCUIT ALSOSDR MAOA2013FA0000432Support · brokenAIR FILTER SUPPORT, MADE OF A CYLINDRICALLY SHAPED WIRE SCREEN WAS FOUND TO HAVE THE SCREEN MATERIAL BREAKING AT THE JUNCTION OF THE RADIAL TO VERTICAL WIRES. CAUSING, IN SEVERAL INSTANCES, TO SHED SECTIONS OF THE WIRE, UP TO AN INCH LONG. WHEN THESE WIRES SSDR SIMA20130702008Flashlight Assy · inoperativeCREW REPORTED FLASHLIGHT IN CABIN WAS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. RETURNED TO SERVICE.SDR 2013FA0000449Structure · corrodedDURING A PRELIMINARY MX INSPECTION, FOUND ACFT TO HAVE EXCESSIVE CORROSION ON AIRFRAME. MOVED THE RUDDER FULL DEFLECTION AND CONTROL ROD END ON PUSH PULL TUBE SNAPPED AT EXPOSED THREADED PORTION. FOUND SEVERAL STEEL PARTS THAT HAVE CORROSION, ALONG WITH THESDR 2013FA0000257Pump · failedWHILE IN FLT, WHEN ELEC FUEL PUMP IS TURNED ON ENGINE RPM DECREASES BECAUSE OF RICH MIXTURE. GROUND CHECKS SHOWED FUEL PUMP PRESSURE TO HIGH. R2 ELEC FUEL PUMP.
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