Rotomotion SR-20

Service difficulty reports · 298

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 = 'SR20'
  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 2013FA0000418Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BOLT CHAFING INTO NR 1 HEADER.Jul 18, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/NozzleSDR 2013FA0000417Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED. BOLT CHAFED AND REPLACED.Jul 18, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/NozzleSDR 2013FA0000400Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLT CHAFED AND REPLACED.Jul 8, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/NozzleSDR 2013FA0000399Exhaust Header · damagedNR 1 AND NR 6 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLTS CHAFED AND REPLACED.Jul 8, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/NozzleSDR 2013FA0000398Exhaust Header · chafedNR 1 HOLE ENLONGATED AND BOLT CHAFED. NR 6 HEADER SUPPORT BRACKET COMPLETELY BROKEN OUT, BOLT CHAFED.Jul 8, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/NozzleSDR 2013FA0000397Support Bracket · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLT CHAFED AND REPLACED.Jul 8, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/NozzleSDR 2013FA0000360Pump · failedENGINE WOULD NOT START. FUEL PUMP PRESSURE ON PFD SHOWS "0" PSI.Jun 20, 2013 · Cirrus SR20 · Fuel Boost PumpSDR 2013FA0000359Pump · failedENGINE WOULD NOT START. FUEL PUMP PRESSURE ON PFD SHOWS "0" PSI.Jun 20, 2013 · Cirrus SR20 · Fuel Boost PumpSDR 2013FA0000291Coil · failedDURING GROUND RUN-UP PRIOR TO TAKEOFF, AS PILOT CYCLED TO RT MAGENTO, ENGINE ATTEMPTED TO CUT-OUT BUT PILOT WAS ABLE TO KEEP RUNNING BY SWITCHING MAGNETO SWITCH BACK TO "BOTH". FLIGHT CREW RETURNED TO RAMP AND SQUAWKED ACFT FOR DEAD MAGNETO ON RT SIDE. MX PEMay 20, 2013 · N851ST · Cirrus SR20 · Magneto/DistributorSDR 2013FA0000245Plate · damagedPROPELLER SPINNER BACKING PLATE DISCOVERED WITH SEVERAL SHEARED RIVETS DURING 100HR INSPECTION. THIS IS THE THIRD UNIT FOUND IN THIS CONDITION DURING ROUTINE INSPECTIONS.Apr 25, 2013 · Cirrus SR20 · Propeller Spinner SectionSDR 2013FA0000244Plate · damagedPROPELLER SPINNER BACKING PLATE DISCOVERED WITH SEVERAL SHEARED RIVETS DURING 100HR INSPECTION. THIS IS THE THIRD UNIT FOUND IN THIS CONDITION DURING ROUTINE INSPECTIONS.Apr 25, 2013 · Cirrus SR20 · Propeller Spinner SectionSDR 2013FA0000230Spinner · crackedINTERNAL MOUNTING AND ALIGNMENT COMPONENTS OF THE PROPELLER SPINNER CRACKED DURING NORMAL OPERATIONS.Apr 15, 2013 · N813JG · Cirrus SR20 · Propeller Spinner SectionSDR 2013FA0000176Fairing · crackedFLAP INBD HINGE FAIRINGS ARE CRACKING.Mar 19, 2013 · Cirrus SR20 · Trailing Edge FlapsSDR 2013FA0000197Wire · brokenDURING TAXI IN, ENGINE WAS VIBRATING AND MIS-FIRING AT OR BELOW 1000 RPM. MX PERSONNEL DUPLICATED PROBLEM BY PLACING MAGNETO SWITCH ON RT MAG ONLY. RT MAGNETO WAS REMOVED TO DISCOVER COIL PRIMARY LEAD TO POINTS HAD BROKEN OFF. COIL LEAD WIRE HAD NOT BEEN CRMar 14, 2013 · N36PL · Cirrus SR20 · Ignition System WiringSDR 2013FA0000145Ignition Lead · chafedIGNITION HARNESS DISCOVERED CHAFING IN SEVERAL LOCATIONS DUE TO FACTORY ROUTING OF WIRES. THIS CONDITION WAS FOUND ON 5 T-53 ACFT. ADDITIONAL AIRCRAFT TAIL NUMBERS INCLUDE 10104, 10102, 10107 AND 10111Mar 4, 2013 · N10110 · Cirrus SR20 · Ignition System WiringSDR LC1R20130206001Bulkhead · crackedDURING ANNUAL INSPECTION SOME CRACKS WERE DISCOVERED IN THE SPINNER BACK BULKHEAD NECESITATING A REPLACEMENT OF THE BULKHEAD. WHEN THE PROP WAS REMOVED AND THE BOLTS HOLDING THE BULKHEAD TO THE PROP WERE LOOSENED, IT WAS DISCOVERED THAT ALL 16 RIVETS WERE SHEFeb 6, 2013 · N615D · Cirrus SR20 · Propeller Spinner SectionSDR 2012FA0000770Wire Harness · wornMORE THAN 10 AREAS OF THE IGNITION WIRE HARNESS HAD WORN THROUGH THE SHIELDING. TWO WIRES WOULD NOT PASS HIGH TENSION TEST. THIS IS THE THIRD ACFT WITH THIS CONDITION BUT IT IS THE WORST.Nov 7, 2012 · N156KT · Cirrus SR20 · Ignition System WiringSDR 2012FA0000740Bolt · crackedNR 1 ALTERNATOR SUPPORT BOLT FOUND CRACKED DURING INSPECTION, THIRD OCCURENCE.Nov 1, 2012 · Cirrus SR20 · DC Generating SystemSDR CA130402004Hinge · corroded(CAN) INSPECTION OF FLAP HINGES FOUND CORROSION, EXFOILATION AND INTERGRANULAR CORROSION ON UPPER PORTION OF HINGES. REPLACE ALL FLAP HINGES, PIN 14572-008, INBD RT PIN 14571-007, MIDDLE LT AND RT PIN 14572-004 OTBD LT AND RT PIN 14573-004.Oct 30, 2012 · Cirrus SR20 · Trailing Edge FlapsSDR 2012FA0000727Power Supply · failedLEFT STROBE INOPERATIVE. TESTED FLASH TUBE WITH ANOTHER POWER SUPPLY - FUNCTION CHECK OK. PULLED THE POWER SUPPLY AND OPENED - EVIDENCE OF CAPACITOR EXPLOSION AND ELECTROLYTE SPILLAGE.Oct 25, 2012 · N2075T · Cirrus SR20 · Exterior LightingSDR 2012FA0000709Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WOULD NOT DELIVER ADEQUATE FUEL FLOW AFTER ADJUSTMENT.Sep 29, 2012 · N610DA · Cirrus SR20 · Engine Fuel PumpSDR 2012FA0000649Bracket · crackedCRACK DISCOVERED IN ALTERNATOR MOUNTING BRACKET, PN 657046. THIRD OCCURANCE OF THIS PROBLEM.Sep 26, 2012 · Cirrus SR20 · Electrical Power SystemSDR 2012FA0000720Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.Sep 1, 2012 · N476DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000603Starter · burnedAFTER ENGINE START THE MAP, ENGINE PERCENT POWER AND FUEL FLOW INDICATIONS BECAME INOPERATIVE. ACFT WAS NOT FLOWN. FLIGHT CREW SQUAWKED PROBLEM AND BROUGHT ACFT AND TIN TO MX. GROUND RUN-UP PERFORMED AND AMT WAS ABLE TO DUPLICATE PROBLEM. ACFT ENGINE COWLINGAug 24, 2012 · N156CS · Cirrus SR20 · Engine StarterSDR 2012FA0000725Magneto · malfunctionedENGINE MISFIRES WHEN CHECKING LEFT MAGNETO.Aug 18, 2012 · N610DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000707Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL NOT OUTPUT HIGHER THAN 13 GPH AFTER ADJUSTMENT. OUTPUT SHOULD BE IN THE 17 - 18 GPH RANGE.Aug 16, 2012 · N478DA · Cirrus SR20 · Engine Fuel PumpSDR 2012FA0000721Magneto · malfunctionedRIGHT MAGNETO WOULD NOT FIRE DURING MAGNETO CHECK. ENGINE QUIT RUNNING WHEN RIGHT MAGNETO SELECTED.Aug 12, 2012 · N476DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000704Pump · out of adjustWHILE WORKING TO COMPLETE A FUEL SYSTEM ADJUSTMENT, FOUND THAT THE METERED FUEL PRESSURE WOULD NOT OUTPUT ABOVE 10 PSI AT WIDE OPEN THROTTLE, AFTER ADJUSTMENT (SERVICE INFORMATION DIRECTIVE 97-3 CALLS FOR 13.8 -15.5 PSI).Aug 7, 2012 · N471DA · Cirrus SR20 · Fuel Boost PumpSDR 2012FA0000724Magneto · malfunctionedLEFT MAGNETO MISFIRES DURING MAGNETO CHECK.Aug 6, 2012 · N483DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000527Transducer · looseOIL PRESSYRE INDICATION IN YELLOW RANGE CAUSED BY LOOSE OR DIRTY CONTACT PIN AT OIL PRESSURE TRANSDUCER AND AIRFRAME WIRE HARNESS.Aug 2, 2012 · N496DA · Cirrus SR20 · Engine Oil Indicating SystemSDR 2012FA0000706Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL NOT OUTPUT HIGHER THAN 14.3 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. SHOULD BE IN THE 17 - 18 GPH RANGE.Jul 31, 2012 · N476DA · Cirrus SR20 · Engine Fuel PumpSDR 2012FA0000723Magneto · malfunctionedRIGHT MAGNETO DOES NOT FIRE. ENGINE QUITS WHEN RT MAGNETO SELECTED DURING MAGNETO CHECK.Jul 21, 2012 · N483DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000719Magneto · malfunctionedENGINE MISFIRES DURING MAGNETO TEST.Jul 13, 2012 · N473DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000718Magneto · malfunctionedRIGHT MAGNETO WOULD NOT FIRE.Jul 12, 2012 · N472DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000570Commutator · shortedAFTER START UP, CREW NOTED THAT THE RT IFD WENT BLANK. MAINTENANCE CREW SUSPECTED A BAD BATTERY/LOW VOLTAGE AND INSTALLED A NEW BATTERY. WHEN THE NEGATIVE WIRE WAS INSTALLED, THERE WAS A LARGE SPARK. THE BATTERY 1 RELAY WAS FOUND TO BE STUCK. AFTER REPLACING Jul 7, 2012 · N94RS · Cirrus SR20 · Engine StarterSDR 2012FA0000708Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL ONLY OUTPUT 10.5 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. OUTPUT SHOULD BE IN THE 17-18 GPH RANGE.Jun 27, 2012 · N488DA · Cirrus SR20 · Engine Fuel PumpSDR 2012FA0000705Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL ONLY DELIVER 13 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. CORRECT OUTPUT SHOULD BE IN THE RANGE OF 17 - 18 GPH.Jun 24, 2012 · N473DA · Cirrus SR20 · Engine Fuel PumpSDR 2012FA0000343Case · crackedDURRING PRE FLIGHT FOUND OIL ON COWLING. INVESTIGATION FOUND A CRACK IN THE RT FWD TOP OF THE ENGINE CASE.May 29, 2012 · N579RC · Cirrus SR20 · Reciprocating Engine Power SectionSDR 2012FA0000326Tube · chafedTHE ACFT DEPARTED GTU AND SHORTLY AFTER, THE PILOT EXPERIENCED A ROUGH RUNNING ENGINE. THE PILOT ELECTED TO RETURN TO THE AIRPORT IMMEDIATELY. REMOVED TOP COWLING, NOTICED THAT NR 1 AND 5 INTAKE TUBES, WHERE THEY ATTACH TO THE CYLINDER HEAD WAS CHAFED AND BRApr 24, 2012 · N5959A · Cirrus SR20 · Reciprocating Engine Cylinder SectionSDR 2012FA0000179Relay · faultyFLAPS STUCK IN DOWN POSITION. CONDITION TRACED TO A FAULTY RELAY. THIS IS A CHRONIC PROBLEM ENCOUNTERED ON 6 ACFT.Apr 4, 2012 · Cirrus SR20 · Trailing Edge Flap Control SystemSDR 2012FA0000177Fuel Line · splitON TAKEOFF ROLL, NOTICED AN EXCESSIVE FUEL FLOW INDICATION AND ABORTED TAKEOFF. ON INSPECTION OF THE DISCREPANCY THE MECHANIC WAS ABLE TO DUPLICATE THE HIGH FUEL FLOW READING. AFTER SHUTTING DOWN THE ENGINE AND REMOVING THE ENGINE COWL, A SPLIT IN THE NR 1 Apr 4, 2012 · N613DA · Cirrus SR20 · Engine Fuel DistributionSDR 2012FA0000722Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.Mar 19, 2012 · N477DA · Cirrus SR20 · Magneto/DistributorSDR 2012FA0000582Spark Plug · crackedENGINE RAN ROUGH. PRECAUTIONARY LANDING. FOUR SPARK PLUGS, FOUND CRACKED AND SOME MISSING INSULATORS.Jan 20, 2012 · N192BW · Cirrus SR20 · Spark Plug/IgniterSDR ODAR201112220011Cable · bindingSHORTLY AFTER THE ANNUAL INSP, THE OWNER REPORTED THAT OCCASIONALLY AFTER APPLYING RUDDER DURING TAXI, THE RT WHEEL BRAKE WOULD BE APPLIED, CAUSING THE ACFT TO STEER IN THAT DIRECTION BECAUSE OF THE CASTER TYPE NOSE WHEEL. UPON INVESTIGATION BY MX, IT WAS DISDec 12, 2011 · N938R · Cirrus SR20 · Landing Gear Brake SystemSDR 2012FA0000039Exhaust Valve · bindingAFTER NOTICING THAT THE ENGINE RAN ROUGH DURING TAXI PRIOR TO TAKEOFF, THE PILOT RETURNED TO THE RAMP AND REPORTED THE PROBLEM TO A MX TECH. THE MX TECH VERIFIED THAT THE ENGINE WAS RUNNING ROUGH AND WAS UNABLE TO MAKE TAKEOFF POWER. THE TECH ALSO NOTED LOW ENov 30, 2011 · N592PU · Cirrus SR20 · Reciprocating Engine Cylinder SectionSDR 2012FA0000033Exhaust Valve · bindingDURING A ROUTINE PRE-INSPECTION ENGINE RUN-UP, THE MX TECH DISCOVERED THAT THE ENGINE WAS RUNNING ROUGH AND WAS UNABLE TO REACH STATIC RPM. THE TECH ALSO NOTED LOW EGT ON CYLINDER NR 2. THE CYLINDER NR 2 EXHAUST VALVE ROCKER COVER AND EXHAUST VALVE SPRING WERENov 8, 2011 · N581PU · Cirrus SR20 · Reciprocating Engine Cylinder SectionSDR 2012FA0000038Exhaust Valve · bindingDURING A ROUTINE PRE-INSPECTION ENGINE RUN-UP, THE MX TECH DISCOVERED THAT THE ENGINE WAS RUNNING ROUGH AND WAS UNABLE TO REACH STATIC RPM. THE TECH ALSO NOTED LOW EGT ON CYLINDERS NR 3, NR 4, AND NR 5. THE CYLINDER NR 3, NR 4, AND NR 5 EXHAUST VALVE ROCKER COct 31, 2011 · N590PU · Cirrus SR20 · Reciprocating Engine Cylinder SectionSDR 2011FA0000702Crankcase · crackedCRANKCASE CRACKED JUST AFT AND ABOVE NR1 ALTERNATOR MOUNT AREA AND LEAKING.Oct 26, 2011 · N688PC · Cirrus SR20 · Reciprocating Engine Power SectionSDR 2012FA0000037Exhaust Valve · bindingDURING A ROUTINE PRE-INSPECTION ENGINE RUN-UP, THE MX TECH DISCOVERED THAT THE ENGINE WAS RUNNING ROUGH AND WAS UNABLE TO REACH STATIC RPM. THE TECH ALSO NOTED LOW EGT ON CYLINDER NR 5. THE CYLINDER NR 5 EXHAUST VALVE ROCKER COVER AND EXHAUST VALVE SPRING WEREOct 18, 2011 · N589PU · Cirrus SR20 · Reciprocating Engine Cylinder SectionSDR 2012FA0000036Exhaust Valve · bindingDURING A ROUTINE PRE-INSPECTION ENGINE RUN-UP, THE MX TECH DISCOVERED THAT THE ENGINE WAS RUNNING ROUGH AND WAS UNABLE TO REACH STATIC RPM. THE TECH ALSO NOTED LOW EGT ON CYLINDERS NR 1 AND NR 5. THE CYLINDER NR 1 AND NR 5 EXHAUST VALVE ROCKER COVERS AND EXHAUSep 29, 2011 · N587PU · Cirrus SR20 · Reciprocating Engine Cylinder Section
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