Cirrus Design SR22

Service difficulty reports · 438

Newest first. General aviation reporting is voluntary.

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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.

SDR 2012FA0000100Distributor Gear · failedCREW REPORTED SEVERE ENGINE VIBRATION DURING TAKEOFF. QUICK INSPECTION ON GROUND REVEALED THAT LT WAS INOPERATIVE. OPERATOR DECIDED TO REPLACE MAGNETO WITH A BRAND NEW ONE. DURING THE DISASSEMBLING OF THE MAGNETO THE DISTRIBUTOR GEAR`S FAILURE WERE FOUND . Jan 24, 2012 · Cirrus SR22 · Magneto/DistributorSDR 2012FA0000101Distributor Gear · failedCREW REPORTED SEVERE ENGINE VIBRATION AND EGT RAISED AT THE SAME TIME IN CYLINDER NR 3. QUICK INSPECTION ON GROUND REVEALED THAT RT MAGNETO IS INOPERATIVE. OPERATOR DECIDED TO REPLACE MAGNETO WITH A BRAND NEW ONE. AFTER REPLACEMENT WAS ACCOMPLISHED, PERFORMJan 23, 2012 · Cirrus SR22 · Magneto/DistributorSDR FCPR20121223003Housing · leakingWHILE PERFORMING A 100 HR INSPECTION, FOUND ENGINE DRIVEN FUEL PUMP LEAKING FUEL AT ANDROID HOUSING FLANGE. REMOVED FUEL PUMP AND SENT TO MFG FOR REPAIRS.Dec 23, 2011 · N351SR · Cirrus SR22 · Fuel Boost PumpSDR 2012FA0000072Tube · failedMAIN TIRE BLOWOUT ON RUNWAY DURING A TURN. MX REPLACED THE TIRE AND TUBE STATED, REPLACED A FEW OF THESE TYPES (BUTYL RUBBER) TUBES IN THE PAST DUE TO HOLES IN VARIOUS PLACES FOR NO APPARENT REASONS.Dec 22, 2011 · N217TJ · Cirrus SR22 · Tire TubeSDR FCPR20121214002Housing · leakingWHILE PERFORMING AN OIL CHANGE, FOUND ENGINE DRIVEN FUEL PUMP LEAKING FUEL AT ANEROID HOUSING FLANGE. REMOVED FUEL PUMP AND SENT TO MFG FOR REPAIRS.Dec 14, 2011 · N542PF · Cirrus SR22 · Fuel Boost PumpSDR LC1R2011120700001Air Filter · splitDURING AN ANNUAL INSPECTION, THE AIR FILTER WAS DISCOVERED TO BE SPLIT OPEN AT THE SEAM. THIS SAME CONDITION HAS BEEN FOUND ON SEVERAL OTHER AIR FILTERS OF THE SAME PN. WHILE NOT AN IMMEDIATE SAFTEY OF FLIGHT ISSUE, THIS CONDITION ALLOWS UNFILTERED AIR TO ENDec 7, 2011 · N212MM · Cirrus SR22 · Engine Air Intake SystemSDR 2011FA0000728Distributor Gear · brokenTHIS MAGNETO HAD UNDERGONE A 500 HOUR INSP PRIOR TO FAILURE OF THE COMPONENT SOME 100 TO 150 OPERATING HOURS LATER (AFTER INSPECTION). THIS MAGNETO WAS INSPECTED IAW THE SYSTEM SUPPORT MANUAL. THE MAGNETO WAS OPENED AND THE DISTRIBUTOR GEAR WAS FOUND WITH SEVNov 3, 2011 · N977CV · Cirrus SR22 · Magneto/DistributorSDR 2011FA0000725Tube · flatAPPROACH SPEED WAS APPROX 78 KTS WITH FULL FLAPS. PRIOR TO TOUCHDOWN, POWER WAS PULLED BACK TO IDLE AND THE PLANE TOUCH DOWNED PARALLEL WITH THE RUNWAY ON THE CENTERLINE. IMMEDIATELY DIRECTIONAL CONTROL WAS LOST WITH THE PLANE PULLED TO THE LT. RT BRAKE ANDNov 2, 2011 · N230SR · Cirrus SR22 · Tire TubeSDR 2011FA0000701Cylinder Head · crackedNR 6 CYLINDER CRACKED FROM SPARK PLUG HOLE TO FUEL INJECTOR AND LEAKING.Oct 26, 2011 · N528HE · Cirrus SR22 · Reciprocating Engine Cylinder SectionSDR 2011FA0000700Cylinder Head · crackedNR 4 CYLINDER FOUND CRACKED FROM SPARK PLUG HOLE TO FUEL INJECTOR AND LEAKING.Oct 26, 2011 · N528HE · Cirrus SR22 · Reciprocating Engine Cylinder SectionSDR 2011FA0000634Spark Plug · crackedDURING ROUTINE ANNUAL INSP FOUND 1 EACH RHB32S CHAMPION SPARK PLUG TO BE MISSING HALF OF THE CERAMIC INSERT THAT SURROUNDS THE CENTER ELECTRODE. FURTHER CLEANING AND INVESTIGATION REVEALED 3 OTHER SPARK PLUGS WITH CRACKS IN THE CERAMIC. IT ALSO APPEARED THATSep 23, 2011 · N332DA · Cirrus SR22 · Spark Plug/IgniterSDR 2011FA0000590Cylinder Head · crackedDURING INSP OF ENGINE WHILE TROUBLESHOOTING A NR 2 ALTERNATOR PROBLEM, FOUND EACH ENGINE CYL (6 EA) WITH CRACKS FROM FUEL INJECTION NOZZLE BOSS TO SPARK PLUG HOLE BOSS. COMFIRMED CRACKS BY EDDY CURRENT.Sep 14, 2011 · N434TB · Cirrus SR22 · Reciprocating Engine Cylinder SectionSDR 2011FA0000734Piston · mismanufacturedIMPROPER PISTON SKIRT MACHINING CAUSED PISTON CONTACT WITH CONNECTING ROD AND CRANK SHAFT. PISTON, PN 654857C. NEED IMPROVED QA IN MACHINING.Aug 26, 2011 · N135AE · Cirrus SR22 · Reciprocating Engine Power SectionSDR FCPA201108260011Transmitter · leakingDURING ENGINE 100 HR INSP, FOUND FUEL FLOW TRANSMITTER LEAKING FUEL AT TOP CAP.Aug 26, 2011 · N500RC · Cirrus SR22 · Fuel Indicating SystemSDR CA110819002Puck Assy · cracked(CAN) WHILE COMPLETING THE 100HR/ANNUAL INSP REQUIREMENTS IAW THE MM, IT WAS NOTICED THE COTTER PIN THAT LOCKS THE FORK ASSY ON THE NOSE GEAR STRUT WAS SHEARED. UPON FURTHER INVESTIGATION AND NOSE GEAR REMOVAL AND DISASSEMBLY, NUMEROUS CRACKS WERE SUSPECTED.Jul 28, 2011 · Cirrus SR22 · Nose/Tail Landing GearSDR 2011FA0000508Tube · looseON THE ACFT WITH A TURBO NORMALIZED SYS MODIFIED, THE WASTE GATE DUMP TUBE FITS TOO LOOSELY CAUSING WASTE GATE EXHAUST TO BE VENTED INTO THE ENGINE COMPARTMENT. THIS POOR FIT CAUSES THE ENGINE COMPARTMENT TEMPERATURE TO RISE HIGH ENOUGH TO FAIL THE MCU (MASTERJul 19, 2011 · N814LF · Cirrus SR22 · Exhaust TurbochargerSDR 2011FA0000493Points · defectiveTHE RT MAGNETO FAILED ON RUN UP, INSP OF THE MAGNETO REVEALED THAT THE TUNGSTEN CONTACT AREA ON THE FIXED SIDE OF THE POINTS HAD SEPARATED FROM THE BASE. THIS LOOKS TO BE SPOT WELDED TO THE NON TUNGSTEN PORTION OF THE CONTACT. WHEN THIS SEPARATED, IT WOULD NJul 11, 2011 · N241CM · Cirrus SR22 · Magneto/DistributorSDR 2011FA0000420Wire · arcedALT1 FIELD WIRE T120 NOT SECURED PROPERLY RESULTING IN CHAFING THEN ARCING TO CYLINDER NR 5 INTAKE STUD CAUSING ALT1 AND ALT1 FIELD CONTROL MODULE FAILURE AND ALT1 FAILURE INDICATION. THE AIRCRAFT HAS APPROX 40 HRS SINCE ANNUAL INSP. THE FAILURE RESULTED IN ANJun 26, 2011 · N907SE · Cirrus SR22 · DC Generating SystemSDR 2011FA0000343Air Filter · splitAIR FILTER FOUND SPLIT OPEN AT GLUED SEAM DURING ANNUAL INSP. SPLIT AREA COMPRISES 4-6 SQ INCHES OF UNFILTERED OPEN AIR PATH TO ENGINE INDUCTION SYS. THIS IS THE 2ND TIME THIS INSP HAS FOUND THIS DEFECT ON THIS TYPE OF FILTER ELEMENT.May 17, 2011 · N965GH · Cirrus SR22 · Air Distribution SystemSDR 2011FA0000262Display · failedPRIMARY FLIGHT DISPLAY RED X'D EVERYTHING INCLUDING THE AHRS AND FLIGHT DATA COMPUTER. WITH BOTH CIRCUIT BREAKERS IN THERE WAS A PARTIAL POWER LOSS TO THE PFD. A FEW MINUTES LATER IT RECOVERED ITSELF. HAPPENED TWICE IN FLIGHT ON THE SAME DAY. VFR CONDITIONApr 27, 2011 · N710SR · Cirrus SR22 · Central DisplaySDR 2011FA0000215Tube · cutLT MLG TIRE TUBE CUT ON LANDING, CAUSING ACFT TO NEED RESCUE/RECOVERY FROM ACTIVE RUNWAY. TUBE WAS TR20, AND HAD A .2500" X .2500" CUT IN THE SIDE OF THE TUBE. TIRE ITSELF SHOWED NO SIGNS OF FOD DAMAGE.Mar 31, 2011 · N170EJ · Cirrus SR22 · Tire TubeSDR 2011FA0000312Antenna · noisyDIGITAL DATA NOISE IN HEADSETS. ACFT MODE S TRANSPONDER SYS. CURRENT ANTENNA LOCATION IS TOO CLOSE TO CABIN ENVIRONMENT.Mar 24, 2011 · N289CM · Cirrus SR22 · Dependent Position Determining SystemSDR 2011FA0000113Air Filter · separatedTHE AIR FILTERS, PN BA-24, USED ON THESE ACFT ARE 12 MONTH/200 HR REPLACE ITEMS. THESE FILTERS ARE FOAM CYLINDRICAL SHAPED MADE FROM A SHEET OF FOAM ROLLED AND GLUED TO FORM THEIR SHAPE. ALMOST EVERY ACFT THAT HAS BEEN SEEN WITH THIS FILTER INSTALLED, THE FILTFeb 17, 2011 · N543SK · Cirrus SR22 · Hydraulic Filter, MainSDR FCPR20110003Pressure Sensor · failedLOW OIL PRESSURE WARNING IN FLIGHT. READ ZERO. OIL PRESSURE SENSOR FOUND INOPERATIVE.Feb 3, 2011 · N271CP · Cirrus SR22 · Engine Oil Indicating SystemSDR 2011FA0000137Camshaft · brokenDURING CRUISE PHASE OF FLIGHT AT NIGHT, PILOT REPORTED THAT THE AIRCRAFT ENGINE SURGED AND LOST POWER. ATTEMPTED TO RESTART WITH NO SUCCESS. PILOT DEPLOYED THE AIRCRAFT PARACHUTE AND LANDED IN A FIELD. ON ENGINE TEARDOWN, IT WAS NOTED THAT THE CAMSHAFT HAD BROJan 27, 2011 · N8135B · Cirrus SR22 · Reciprocating Engine Power SectionSDR 2011FA0000099Gear · fracturedWHILE THE ACFT WAS IN FOR MX, WHILE ATTEMPTING TO START THE ENGINE, A METAL GRINDING NOISE WAS HEARD BY THE MECHANIC. SUBSEQUENT REMOVAL OF THE STARTER ADAPTER REVEALED AT LEAST 2 TEETH MISSING ON THE CRANKSHAFT GEAR AND MARRED TEETH ON THE ADAPTER. THIS CONJan 19, 2011 · N99KE · Cirrus SR22 · Reciprocating Engine Power SectionSDR 2011FA0000098Sensor · inaccurateTHE MANIFOLD PRESSURE SENSOR WOULD GIVE ERRONEOUS READINGS IN FLIGHT, BUT ON THE GROUND WOULD BE ACCURATE. THE REMEDY IS TO REPLACE THE SENSOR.Jan 19, 2011 · N99KE · Cirrus SR22 · Engine Pressure Ratio (EPR)SDR 2011FA0000097Seal · failedTHE ENGINE SEAL THAT SEALS ENGINE OIL OUT OF ALTERNATOR NR2 FAILED. THE RESULT WAS ENGINE OIL PASSING INTO THE ALTERNATOR AND DOWN THE BELLY OF THE ACFT. THE REMEDY IS TO REPLACE THE SEAL AND REBUILD THE ALTERNATOR.Jan 19, 2011 · N99KE · Cirrus SR22 · Reciprocating Engine Oil SystemSDR 2011FA0000096Controller · failedUNABLE TO SET ENGINE IDLE AND MIXTURE SETUP. REMEDY WAS TO REPLACE THROTTLE CONTROLLER.Jan 19, 2011 · N99KE · Cirrus SR22 · Power LeverSDR 2011FA0000095Check Valve · failedOIL FOUND IN INTAKE MANIFOLD. REMEDY WAS TO REPLACE TURBO INLET CHECK VALVE.Jan 19, 2011 · N99KE · Cirrus SR22 · Reciprocating Engine Oil SystemSDR 2011FA0000094Adapter · failedSTARTER ADAPTER WAS SLIPPING. AS A RESULT THE ENGINE WOULD BARELY TURN OVER WHEN STARTING. THE REMEDY WAS TO REPLACE THE STARTER AND STARTER ADAPTER. THESE STARTERS HAVE A LONG HISTORY OF TEARING UP STARTER ADAPTERS. THESE STARTERS WILL NOT RELEASE THE ADAJan 19, 2011 · N99KE · Cirrus SR22 · Engine StarterSDR 2011FA0000093Module · failedTHE OXYGEN SYS WOULD NOT TURN ON IN FLIGHT BUT WORKED ON THE GROUND. REMEDY WAS TO REPLACE THE SWITCH, WIRE HARNESS, AND LOGIC MODULE.Jan 19, 2011 · N99KE · Cirrus SR22 · Crew Oxygen SystemSDR 2011FA0000092Support Bracket · chafedTHE VERTICAL SUPPORT ROD SUPPORTING THE TURBOS WAS BEING CHAFED BY THE SUPPORT BRACKET. THE SUPPORT BRACKET CHANGED PN OLD: ETI-62-103-1, NEW: 22-625-0006 AND 22-625-0005. THE VERTICAL SUPPORT ROD DID NOT CHANGE PN, HOWEVER BOTH LT AND RT RODS WERE REPLACED Jan 19, 2011 · N99KE · Cirrus SR22 · Engine (Reciprocating)SDR 2011FA0000091Exhaust Duct · crackedTHE RT EXHAUST SYS DEVELOPED GUSSET CRACKS AROUND 250 HRS TT. THE MFG SAID THE CRACKS WERE "NON SAFETY CONCERNS" AND DID NOT ADDRESS THEM AT THE TIME. AT 432 HRS TT THE EXHAUST CRACKED IN 2 DIFFERENT WELD JOINTS ON THE COLLECTORS LEADING FROM 2 CYLINDERS. RJan 19, 2011 · N99KE · Cirrus SR22 · Engine Collector/Tailpipe/NozzleSDR 2010FA0001227Alternator · failedNR 2 ALTERNATOR FAILED.Nov 30, 2010 · N69YY · Cirrus SR22 · AC Generator-AlternatorSDR 2010FA0001110Tube · splitUPON LANDING, NOSE TIRE WAS FLAT. SUBSEQUENT INSPECTION REVEALED A .2500" SPLIT IN TUBE AT A LOCATION CORRESPONDING TO SIDEWALL OF TIRE. NO PUNCTURE OF THE TIRE HAD OCCURED.Aug 31, 2010 · N93VG · Cirrus SR22 · Tire TubeSDR CA100820008Computer · failed(CAN) PILOT REPORTED AP COMPUTER U/S. REMOVED S-TEC 55X AP COMPUTER FROM AIRCRAFT, FOUND PIN 34 BURNED OFF COMPUTER AND AIRCRAFT CONNECTOR P551 HAD MINOR DAMAGE. REPLACE AIRCRAFT 50 PIN CONNECTOR, PINS 34 AND 35. S-TEC 55X COMPUTER WAS REPAIRED BY S-TEC: MIDAug 20, 2010 · Cirrus SR22 · Autopilot SystemSDR 2010FA0000900Brush Block · damagedPILOT REPORTED ALTERNATOR STOPPED CHARGING. UPON INSP OF ALTERNATOR, IT WAS NOTED THAT BOTH BRUSHES WERE RIPPED OUT OF THE BRUSH BLOCK AND WERE FOUND IN THE ALTERNATOR.Aug 17, 2010 · N315CM · Cirrus SR22 · DC Generator-AlternatorSDR WVBA OM1Fuel Line · chafedACFT OWNER REQUESTED CLEANING OF HIS FUEL INJECTORS, WHICH WE DID. ALMOST COMPLETED WITH THE TASK, TIGHTENING THE NUT FOR THE NR1 CYL FUEL INJECTION LINE, NOTICED THAT THE LINE WAS VERY LOOSE, AND UPON FURTHER INSP FOUND THAT THE RETAINING CLIP THAT WAS SUPPOAug 5, 2010 · N517SW · Cirrus SR22 · Engine Fuel DistributionSDR 2010F00187Exhaust Stack · crackedDURING 50 HR INSP, MECHANIC DISCOVERED 360 DEGREE CRACK AROUND NR 1 EXHAUST STACK FLANGE.Aug 5, 2010 · N88WZ · Cirrus SR22 · Engine Collector/Tailpipe/NozzleSDR CA100730003Mount · malfunctionedLOSS OF GLIDESLOPE FUNCTION ON S-TEC 55X. ACFT HAS BEEN TO 2 DIFFERENT AMO`S THAT CONCLUDED THAT THE AUTOPILOT COMPUTER WAS AT FAULT. THE UNIT WAS SENT AWAY TWICE AND TESTED BY THE MFG WITH NOT FAULTS FOUND. IT WAS FOUND THAT TRACKING OF THE AUTOPILOT COMPUJul 29, 2010 · Cirrus SR22 · Autopilot ComputerSDR 2010FA0000716Suppressor · burnedITEM APPARENTLY OVERHEATED CAUSING EXCESSIVE SMOKE IN COCKPIT. THE CASE OF THE TVS IS BURNED AND THE SURROUNDING AREA ON BACK OF THE CIRCUIT BREAKER PANEL IS DISCOLORED FROM THE SMOKE.Jun 28, 2010 · N224BR · Cirrus SR22 · Electrical Power System WiringSDR 2010FA0000599Attach Fitting · fracturedENGINE HAD CEASED TO OPERATE AT 10,000 FT, BOOST PUMP TURNED ON, ENG RE-STARTED, PILOT UNABLE TO ADVANCE THROTTLE BEYOND "1ST DETENT" WITHOUT ENG VIBRATION. ACFT RETURNED TO BASE. MX GROUND RUN, MAG DROPS & FUEL SYS PARAMETERS WITHIN LIMITS UNTIL FULL POWER AJun 21, 2010 · N7855Z · Cirrus SR22 · Pneumatic Distribution SystemSDR 2010FA0000634Rotor · splitDURING MAG CHECK ON RUN-UP, RT MAGNETO WAS INOPERATIVE. REMOVED MAG AND FOUND ROTOR SPLIT AT KEY WAY LOCATION. 120 HRS SINCE NEW.Jun 11, 2010 · N422GH · Cirrus SR22 · Magneto/DistributorSDR 2010FA0000642Pump · erraticTURBO NORMALIZER EQUIPMENT INSTALLED IAW STC SA10588SC (AIRFRAME), AND STC SE 10589SC. ENGINE DRIVE FUEL PUMP ETI-SR22-2-12 IS REQUIRED UNDER STC FOR TURBO NORMALIZER EQUIPMENT. THIS FUEL-PUMP FEATURES AN ANEROID COMPENSATOR TO REGULATE MIXTURE FOR TURBONORJun 9, 2010 · N642TL · Cirrus SR22 · Engine Fuel PumpSDR 2010FA0000592Lifter · worn((5CSR)) DURING A CYLINDER CHANGE JOB PROMPTED BY LOW CYLINDER COMPRESSION AND HIGH IRON CONTENT IN OIL IT WAS NOTED AN ABNORMAL AND UNSAFE AMOUNT OF WEAR AND SPALLING ON THE LIFTER FACE. THIS DIRECTLY CAUSED EXCESSIVE AND UNSAFE WEAR ON THE CAM SHAFT LOBES.Jun 1, 2010 · N764SR · Cirrus SR22 · Reciprocating Engine Power SectionSDR 2010FA0000591Camshaft · worn((5CSR)) DURING A CYLINDER CHANGE JOB PROMOTED BY LOW CYLINDER COMPRESSION AND HIGH IRON CONTENT IN OIL, IT WAS NOTED AN ABNORMAL AND UNSAFE AMOUNT OF WEAR ON THE CAM SHAFT LOBES. IT WAS DIRECTLY CAUSED BY LIFTERS THAT HAD EXCESSIVE AMOUNTS OF SPALLING. IT IJun 1, 2010 · N764SR · Cirrus SR22 · Reciprocating Engine Power SectionSDR SIMA201013301Light · inoperativeDURING PREFLIGHT INSPECTION FOR FLIGHT 4091 THE EMERGENCY FLOOR STRIP LIGHTING WAS DISCOVERED TO BE INOPERABLE BETWEEN 8A AND 11A. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK PER EMB 145 AMM 33-50-00. NO DEFECTS NOTED THIS TIME. NMay 12, 2010 · N608AE · Cirrus SR22 · Emergency LightingSDR 2010FA0000455Spark Plug · crackedCHAMPION SPARK PLUG, PART NUMBER RHB32S, BATCH 2D05 FIVE (5) SPARK PLUGS WITH CRACKS. 400 HOURS OF OPERATING TIME ON THE SPARK PLUGS. THE CENTER ELECTRODE ON 2 SPARK PLUGS DEVELOPED CRACKS ON THE TIPS. THE WIRE ELECTRODE ON 2 OTHER SPARK PLUGS DEVELOPED A May 10, 2010 · N700HG · Cirrus SR22 · Spark Plug/IgniterSDR YD5R2010F00101Brushes · wornALTERNATOR WAS WORKING AT TIME OF REMOVAL FOR OTHER DISCREPANCY ((YD5R)) (LEAKING SEAL). BRUSH HSG WAS REMOVED TO CHECK CONDITION DUE TO TIME ON COMPONENT. UPON REMOVAL (SEVERAL PIECES OF THE BRUSH ASSEMBLIES FELL OUT OF HOLDER. BOTH CARBON BLOCKS WERE WORNMay 6, 2010 · N462SR · Cirrus SR22 · DC Generator-Alternator
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