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 2026FA0000884Brake Disc · fracturedBRAKE ROTOR HUB ASSEMBLY SEPARATED FROM FROM MAIN WHEEL ASSEMBLY AT BRAKE HUB WHEEL ATTACH FLANGE. WHEEL ATTACH BOLTS WERE SECURE AND BRAKE HUB FLANGE REMAINED ATTACHED TO WHEEL ASSEMBLY.SDR 2026FA0000818Drive Gear · spalledFACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING, GALLING, AND CHIPPING OF THE GEAR TEETH.SDR 2026FA0000842Brake Disc · detachedWHILE APPLYING THE BRAKES ON TAXI OUT A LOUD BANG WAS HEARD FOLLOWED BY AN ABRUPT LEFT TURN WITH NO ABILITY TO STEER OR BRAKE RIGHT. AIRCRAFT HAS CASTERING NOSE WHEEL. UPON BRAKE REMOVAL THE MOUNTING FLANGE WAS FOUND COMPLETELY SEPARATED FROM THE REST OF THE BSDR 2026FA0000796Lock Tab · misinstalledREMOVED THE #2 AND #4 CYLINDER INTAKE AND EXHAUST ROCKER COVERS FOR ROUTINE GASKET REPLACEMENT. UPON INSPECTION OF THE VALVE ASSEMBLY, I FOUND THE LOCKING TAB WASHER P/N: 501868, FOR THE CYLINDER ROCKER ARM SHAFT HOLD DOWN BOLTS TO NOT BE BENT INTO THE LOCKINGSDR 2026FA0000820Drive Gear · spalledFACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING, GALLING, AND CHIPPING OF THE GEAR TEETH.SDR 2026FA0000321Brake Disc · failedTHE RH BRAKE FAILED AFTER LANDING. THE PILOT STATED THE BRAKE FELT FIRM. WE FOUND THE DISC ROTOR HAD SEPARATED FROM THE WHEEL ATTACHMENT PORTION OF THE DISC. I HAVE PICTURES.SDR 2026FA0000283Brake Disc · crackedCRACKED - DURING ANNUAL INSPECTION, THE OPPOSITE BRAKE DISC WAS FOUND BADLY CRACKED, SEE SDR 2026FA000282. ADDITIONAL INSPECTION PERFORMED ON LH BRAKE DISC WITH 10X MAGNIFYING GLASS ON INSIDE 90 DEGREE BEND RADIUS WHERE THE BODY MEETS THE FLANGE. POSSIBLE CRACSDR 2026FA0000282Brake Disc · crackedATTACHMENT FLANGE CRACKED THROUGH 270+ DEGREES OF CIRCUMFERENCE - DURING ANNUAL INSPECTION, RT BRAKE DISC/ROTOR DISCOVERED TO HAVE 5 SIZEABLE HOLES AT 90 BEND FROM BODY TO ATTACHMENT FLANGE. SIGNS OF HEAVY CORROSION IN BEND ALSO PRESENT. CRACKS RUNNING BETWEENSDR 2026FA0000281Brake Disc · crackedCRACKED AT ATTACHMENT FLANGE - AFTER DISCOVERY OF SHEARED LH BRAKE ROTOR FLANGE, RH BRAKE ROTOR REMOVED AND INSPECTED. 10X MAGNIFICATION REVEALED SEVERAL SPOTS OF PITTING CORROSION IN THE VALLEYS OF CIRCUMFERENTIAL MACHINING STRIATIONS AND POSSIBLE CRACK INDICSDR 2026FA0000280Brake Disc · failedATTACHEMENT FLANGE SHEARED OFF - ON TAXI, PILOT DISCOVERED AIRPLANE WOULD ONLY TURN RIGHT. AIRCRAFT HAS CASTERING NOSEWHEEL AND USES BRAKES TO STEER. AFTER SHUTDOWN, LH BRAKE DISC/ROTOR FOUND COMPLETELY SHEARED OFF AT 90 DEGREE BEND WHERE THE BODY TRANSITIONS SDR 2026FA0000271Brake Disc · separatedRIGHT MAIN DISC COMPLETELY SEPARATED FROM THE MOUNTING FLANGE OF THE WHEEL ASSY. SIGNIFICANT GRINDING NOISE FELT DURING TAXI AND ALL BRAKING AUTHORITY WAS LOST ON THE RIGHT MAIN, CAUSING AIRPLANE TO UNCONTROLLABLY PIVOT AROUND LEFT MAIN WHEN THE BRAKES WERE APSDR 2026FA0000210Alternator · failedFACTORY NEW ALTERNATOR SUDDENLY FAILED AFTER ONE MONTH AND 52 FLIGHT HOURS SINCE INSTALLATION. FAILURE OCCURRED IN CRUISE FLIGHT RESULTING IN A TOTAL ELECTRICAL POWER LOSS TO THE MAIN AIRCRAFT BATTERY. THIS NECESSITATED A PROMPT DIVERSION AND UNSCHEDULED LANDISDR 2026FA0000068Brake Disc · separatedAPPROX. 12 MONTH OLD RIGHT MAIN GEAR BRAKE DISC, RAPCO PART #RA164-02504, SEPARATED DURING APPLICATION OF BRAKES DURING LANDING SEQUENCE. RESULTING DAMAGE REQUIRED REPLACEMENT OF INNER HUB AND PADS.SDR M8VR2026020300001Brake Disc · crackedDURING ANNUAL INSPECTION, THE BRAKE DISC FAILED MINIMUM THICKNESS CHECK ON THE FRICTION SURFACE. DURING ROTOR REPLACEMENT THREE SEPARATE, SIGNIFICANT CRACKS WERE NOTED IN THE WEB/RADIUS ADJACENT TO EACHOF THE THREE BOLT HOLES.SDR 2026FA0000051Brake Disc · separatedWHILE TAXIIING AFTER LANDING THE PILOT APPLIED BRAKES AND THE AIRCRAFT VEERED LEFT OFF THE TAXI WAY AND INTO THE GRASS. MAINTENANCE REMOVED THE RIGHT WHEEL AND FOUND THE RIGHT BRAKE DISK HAD FULLY SEPARATED FROM THE MOUNTING FLANGE THAT BOLTS TO THE INNER WHEESDR 2026FA0000016Puck · failedNOSE LANDING GEAR COLLAPSED WHILE TAXING LEADING TO A PROP STRIKE. THIS IS A KNOWN ISSUE. THE CIRRUS NOSE GEAR IS SUPPORTED BY SIX RUBBER "PUCKS" HELD IN PLACE BY METAL PANS AT THE TOP AND BOTTOM WITH A METAL ROD RUNNING THROUGH THE CENTER OF THE PUCKS. THE ROSDR 2025FA0000742Rotor · crackedOWNER NOTICED A NOISE FROM THE MAIN GEAR AND SOME VIBRATION. UPON INSPECTION THE RIGHT BRAKE ROTOR WAS CRACKED AT THE MOUNTING FLANGE 90% AROUND. LEFT ROTOR WAS BEGINNING TO CRACK AT THE SAME LOCATION. BOTH BRAKE ROTORS WERE REPLACED AT THE JUNE 2025 ANNUAL INSDR 2025FA0000538Relay · failedFLAP UP RELAY FAILED ON DEPARTURE CAUSING FLAPS TO NOT RETRACT FROM TAKE OFF POSITION. AIRCRAFT DIVERTED TO KMGY AND WAS REPAIRED. EXAMINATION OF INTERIOR OF RELAY ASSEMBLY SHOWED BURNED CONTACTS.SDR 2025FA0000408Oil Cooler · crackedWHILE PERFORMING AN OIL CHANGE, IT WAS DISCOVERED THE DIAGONAL STIFFENERS ON BOTH SIDES OF THE OIL COOLER WERE BROKEN AND HALF GONE. THE OIL COOLER WAS NOT LEAKING. THE OIL COOLER WAS REPLACED WITH NEW. INSTALLED PART NUMBER: 658767, SERIAL NUMBER: H22-12342-2SDR 2025FA0000446Brake Disc · corrodedRIGHT MAIN WHEEL BRAKE DISC IS CRACKED 60% AROUND THE CINRCUMFRENECE, SIGNIFICANT AMOUNT OF MATERIAL MISSING. BRAKE DISC IS CORRODED, RUSTED & HOLES IN IT.SDR 2025FA0000445Rheostat · unknownAIRCRAFT IS A CIRRUS SR22 WITH THE GARMIN PERSPECTIVE AVIONICS SUITE CONSISTING OF 2 GARMIN 1000 DISPLAYS SERVING AS A PFD & MFD. PILOT REPORTS THAT WHILE FLYING ON AN IFR FLIGHT PLAN BOTH THE PFD & MFD WENT COMPLETELY BLACK & UNREADABLE. AUTOPILOT REMAINED ENSDR 2025FA0000282Cylinder Head · crackedCRACKS / SEPARATION OF CYLINDER EVEN AFTER COMPLYING WITH AD 2020-16-11 OVER 5 YEARS AGO.SDR 2025FA0000110Piston · failedENGINE SEIZED UP ON RUN UP. PISTON IN # 3 CYLINDER BROKE INTO TWO PARTS AT THE PISTON PIN BORE. CYLINDER ASSEMBLY P/N 658815A1 PISTON P/N 654726.SDR 2025FA0000113Connecting Rod · bindingDURING FLIGHT THE AIRCRAFT OWNER/OPERATOR NOTICED A DRONING VIBRATION AT CRUISE. UPON LANDING, ALL CYLINDERS WERE INSPECTED AND BORE-SCOPED. MOVED PROPELLER BACK AND FORTH AND HEARD A CLUNKING NOISE, NARROWED DOWN TO CYLINDER #2 PISTON SHOWING SIGNS OF EXCESSISDR 2025FA0000010Cylinder Head · burnedENGINE COMPRESSION CHECK CYLINDER #5 WAS 10/80 PSI. REMOVED CYLINDER, PISTON WAS BURNED BADLY AROUND THE OUTSIDE EDGES. TOP SPARK PLUG PORCELAIN WAS BROKEN AND DAMAGED.SDR 2024FA0000963Brake Disc · brokenRAPCO BRAKE ROTOR TOTAL SEPARATION. IN WORKING WITH THE COPA GROUP AND THIS SITE'S SEARCH THERE SEEMS TO BE A CRITICAL QUALITY ISSUE WITH THE RAPCO BRAKE ROTOR. I HAD A SEPARATION THAT COULD HAVE BEEN CATASTROPHIC, BUT LUCKILY, IT WAS MANAGED WITH NO DAMAGE ORSDR 2024FA0000961Cylinder · crackedI PREVIOUSLY REPORTED THIS CYLINDER FOR A LOOSE VALVE GUIDE (CONTROL # 2024FA0000818). UPON FURTHER INSPECTION, THIS CYLINDER IS ALSO CRACKED IN THE TARGET AREA OF AD20-16-11. CRACK CONFIRMED BY 10X MAGNIFIER AND FLORESCENT PENETRANT INSPECTION. THIS CYLINDERSDR 2024FA0000938Hinge · looseDURING ANNUAL INSPECTION, FOUND THE RIGHT ELEVATOR, OUTBOARD HINGE BRACKET, 3 OF 5 POP RIVETS FASTENING THE HINGE BRACKET TO THE MAIN SPAR AND RIB OF THE ELEVATOR HAVE SEVERELY LOOSENED UP, CAUSING THE HINGE BRACKET TO FLOAT AROUND, UNSECURED. I BELIEVE, IF TSDR 2024FA0000855Governor · abnormalPILOT REPORTED A VIBRATION OR SURGE FROM PROPELLER WHEN DESCENDING OR LANDING. GOVERNOR SHOP REPORTED THE SPOOL VALVE IS THE PROBLEM AND EVEN THOUGH HE PURCHASES NEW SPOOL VALVE FROM HARTZELL. IT DOESN'T ALWAYS FIX IT, NEW SPOOL VALVES ARE DEFECTIVE. HAVE TO SDR 2024FA0000818Valve Guide · loosePILOT REPORTED AN UNUSUAL VIBRATION DEVELOPING IN FLIGHT BETWEEN 2200-2400 RPM. I FOUND THE #5 CYLINDER EXHAUST VALVE GUIDE, PN: 636242P005, WAS LOOSE, FLOATING IN THE CYLINDER. LOGBOOKS INDICATE THE #5 CYLINDER WAS AN OVERHAULED CYLINDER. THE CYLINDER WAS OSDR 2024FA0000777Drive Shaft · damagedAC DRIVE ASSEMBLY, CIRRUS PN: 21119-102, ALSO PN: 1133180-4. THE 4 BOLTS, THAT WERE ALSO SAFETY WIRED, ALL SHEERED OFF IN FLIGHT, CAUSING THE AC DRIVE SHAFT TO BACK OUT, RESULTING IN HEAVY DAMAGE TO THE AC DRIVE ASSEMBLY. NO ENGINE ROUGHNESS FROM THE PILOT WASDR 2024FA0000775Cylinder Head · crackedPILOT REPORTED THAT THEY TOOK OFF AT KESN AND SHORTLY HAD A SIGNIFICATE LOSE OF POWER AND FELT ROUGH. TURNED AROUND AND LANDED BACK AT KESN. AFTER REMOVING COWLING FOUND THAT #3 CYLINDER LOWER EXHAUST SIDE OF CYLINDER HEAD WAS CRACKED HAD BROKEN FREE. THE ONLSDR 2024FA0000677Engine · blownON AUGUST 21,2024 I HAD A MAJOR ENGINE FAILURE ON TAKEOFF AT 2800 FT AGL. FORTUNATELY I WAS ABLE TO RETURN TO THE AIRPORT AND LAND. I HAD FLOWN THE PLANE FOR 6 HOURS IN THE 2 PREVIOUS DAYS WITH NO ISSUES. EVERYTHING SEEMED FINE DURING THE PRE-FLIGHT AND RUN UPSDR 2025FA0000380Screw · shearedPILOT WAS FLYING WHEN THE ENGINE STARTED SHAKING AND CYLINDER 1 CHT AND EGT WENT COLD. PILOT DECLARED AN EMERGENCY AND LANDED AT KRDG. UPON REMOVAL OF THE COWLING THE INSPECTOR NOTED THERE WAS A HOLE PUNCTURED IN THE CYLINDER #1 ROCKER COVER. IT APPEARS ONE SDR 2024FA0000367Cylinder Head · crackedCYLINDERS 1, 3 AND 5 EXHIBIT CRACKS IDENTICAL TO SDR MSB09-1B, ALTHOUGH THEY ARE NOT INCLUDED IN THE SERVICE BULLETIN. CYLINDER PNS ARE UNREADABLE BUT SNS ARE AS FOLLOWS: • CYLINDER 1 - ACO6CA702, CYLINDER 2 - AC04HC272, CYLINDER 3 - AC05BB268, CYLINDER 4 - ACSDR 2024FA0000370Pulley · damagedAIR CONDITIONING COMPRESSOR DRIVE PULLEY SHEARED OFF BOLT, IMPACTED ALTERNATOR #2, DAMAGED ALTERNATOR #2 TO THE POINT THAT IT WAS INOP. COULD NOT LOCATE BOLT OR SAFETY WIRE.SDR 2024FA0000343Control Unit · burnedCOMPLETE ELECTRICAL FAILURE EN-ROUTE FROM KGTF TO 6S8. STARTED WITH ATC REPORTING MODE C FAILURE; RECYCLED TRANSPONDER. ATC UNABLE TO RECEIVE MODE C; AVIONICS POWER RECYCLE. PANEL LIGHTS FLASHED, GPS/MFD/PFD FLICKERED. BATTERY AND ALTERNATOR GAUGES OK FOR APPRSDR 2024FA0000306Mcu · failedAIRCRAFT WAS TAKEN ON MAINTENANCE TEST FLIGHT AFTER ENGINE INSTALLATION. UPON THE SECOND TOUCH-AND-GO, AIRCRAFT LOST ELECTRICAL POWER ON CLIMB OUT AFTER A TOUCH-AND-GO FROM MSO AIRPORT. BOTH ALTERATORS INDICATED AS NO LONGER FUNCTIONING, AND MAIN BATTERY VOLTASDR 2024FA0000297Mcu · failedAIRCRAFT WAS TAKEN ON MAINTENANCE TEST FLIGHT AFTER ENGINE INSTALLATION. UPON THE SECOND TOUCH-AND-GO, AIRCRAFT LOST ELECTRICAL POWER ON CLIMB OUT AFTER A TOUCH-AND-GO FROM MSO AIRPORT. BOTH ALTERNATORS INDICATED AS NO LONGER FUNCTIONING, AND MAIN BATTERY VOLTSDR 2023FA0000818Motor · looseFOUND EXCESSIVE PLAY IN ELEVATOR DURING 100 HOUR INSPECTION. UPON FURTHER INSPECTION, FOUND PITCH TRIM MOTOR LOOSE IN MOUNTING PLATE. PITCH TRIM MOTOR WILL ROTATE SLIGHTLY WHEN ELEVATOR MOVED IN EITHER DIRECTION. REMOVED PITCH TRIM MOTOR AND DISASSEMBLED PITCHSDR 2023FA0000738Igniter · faultedWHILE PERFORMING A CAPS SYSTEM EXCHANGE ON N842WT, THE TOOL SPECIFIED TO INSTALL AND TORQUE THE IGNITER ASSEMBLY INTO THE ROCKET ASSEMBLY WAS DIFFICULT TO INSTALL. WHILE PERFORMING THE TORQUE, THE TOOLING SNAPPED. THIS LEFT A DOWEL IN THE SQUIB THAT CANNOT BE SDR 2023F00233Unknown · unknownON 7/20/2023, VAN NUYS AIRLINES-VNY- DBA, AD AIRLINES' CAPTAIN REPORTED: "WE HAD SMOKE IN THE CABIN AROUND 17 MILES AWAY FROM KHFD. WE HAD THE AIR CONDITIONING ON FROM BEING ON THE GROUND AT KGON. WE SMELT SMOKE THEN A COUPLE OF SECONDS LATER WE SAW SMOKE COMISDR E5ZR202308070001Crankshaft · rustedCONTINENTAL SUPPLIED, UNDER WARRANTY, A NEW REPLACEMENT CRANKSHAFT ASSEMBLY P/N: 649900 S/N: N23BA108 (8130-3 DATED 02/JUN/2023) TO REPLACE A PREVIOUSLY SUPPLIED NEW CRANKSHAFT ASSEMBLY. THE S/N: N23BA108 CRANKSHAFT (#2) WAS SUPPLIED BY CMI BECAUSE IT WAS FOSDR 2023FA0000374Crankshaft · corrodedCONTINENTAL SUPPLIED, UNDER WARRANTY, A NEW REPLACEMENT CRANKSHAFT ASSEMBLY P/N: 649900 S/N: N23BA108 (8130-3 DATED 02/JUN/2023) TO REPLACE A PREVIOUSLY SUPPLIED NEW CRANKSHAFT ASSEMBLY. THE S/N: N23BA108 CRANKSHAFT (#2) WAS SUPPLIED BY CMI BECAUSE IT WAS FSDR 2023FA0000336Unknown · unknownCHAPTER 4 REQUIRED REPLACEMENT IN THE CAW ANNUAL REQUIRES EVERY 6 YEARS REPLACEMENT OF THE PARACHUTE LINE CUTTERS. EACH AIRCRAFT HAS 2 LINE CUTTERS THAT ARE REPLACED EVERY 6 YEARS. INSTALLATION REQUIRES THE OLD REMOVED UNITS ARE LITE OFF. ON THIS REPLACEMENT CSDR 2023FA0000276Mount · destroyedDEPARTED TETERBORO LATE AT NIGHT. WHILE ENROUTE NOTICED A REDUCTION IN MANIFOLD PRESSURE CONSISTENT WITH A SUPERCHARGER BELT FAILURE. RECONFIGURED FOR NORMALLY ASPIRATED OPERATION AND LANDED AT BRIDGEPORT. REMOVED THE ENGINE COWLING TO INSPECT THE SUPERCHARGERSDR 2023FA0000148Magneto · shearedAIRCRAFT WAS IN CRUISE FLIGHT FROM LAS VEGAS, NV TO NORTH DAKOTA AND PILOT NOTICED ENGINE POWER LOSS AND ENGINE RUNNING ROUGH. AIRCRAFT LANDED AT KBIL WITHOUT INCIDENT. MAINTENANCE FOUND ROTOR GEAR MISSING TEETH IN LEFT MAGNETO.SDR 2022FA0000678Nut · looseSEE ATTACHED IPC 32-20-02 COTTER PIN ITEM 123. PAGE 2 19 SEP 2017 . CD MM INSTALLATION NOTES REDUCE THE POSSIBLE SHEAR FACTOR ON A "EDGE" OF THE PIN, SEE MM32-20 PAGE 28 (5) (G) AND FIGURE 32-206 (ATTACHED). AIRCRAFT RECEIVED FOR ANNUAL INSPECTION, DURINGSDR 2022FA0000466Isolation Mount · distressedPICKED UP CIRRUS SR22 FROM OWNER FOR PRE-BUY AT WELLS AIRCRAFT IN HUTCHINSON. ON DEPARTURE HAD SUCH VIBRATION THE ONLY WAY TO CONTROL WAS PULLING POWER/RPM'S TO 50%. UPON ARRIVING AT CIRRUS SERVICE CENTER UN COWLED AND FOUND MOTOR MOUNT IDOLATOR RUBBERS GONE SDR 2022FA0000217Mount · crackedENGINE MOUNT TRUSS ASSEMBLY HAS CRACKS APPROXIMATELY HALF WAY THROUGH THE BOTTOM TRUSS TUBE AT THE JUNCTION FOR THE MID-SPAN DOWN TUBE WELDS. THE CRACKS ARE PRESENT ON BOTH SIDES OF THE LOWER TRUSS (INBD AND OUTBD).
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