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.
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
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 2013FA0000418Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BOLT CHAFING INTO NR 1 HEADER.SDR 2013FA0000417Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED. BOLT CHAFED AND REPLACED.SDR 2013FA0000400Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLT CHAFED AND REPLACED.SDR 2013FA0000399Exhaust Header · damagedNR 1 AND NR 6 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLTS CHAFED AND REPLACED.SDR 2013FA0000398Exhaust Header · chafedNR 1 HOLE ENLONGATED AND BOLT CHAFED. NR 6 HEADER SUPPORT BRACKET COMPLETELY BROKEN OUT, BOLT CHAFED.SDR 2013FA0000397Support Bracket · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLT CHAFED AND REPLACED.SDR 2013FA0000360Pump · failedENGINE WOULD NOT START. FUEL PUMP PRESSURE ON PFD SHOWS "0" PSI.SDR 2013FA0000359Pump · failedENGINE WOULD NOT START. FUEL PUMP PRESSURE ON PFD SHOWS "0" PSI.SDR 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 PESDR 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.SDR 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.SDR 2013FA0000230Spinner · crackedINTERNAL MOUNTING AND ALIGNMENT COMPONENTS OF THE PROPELLER SPINNER CRACKED DURING NORMAL OPERATIONS.SDR 2013FA0000176Fairing · crackedFLAP INBD HINGE FAIRINGS ARE CRACKING.SDR 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 CRSDR 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 10111SDR 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 SHESDR 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.SDR 2012FA0000740Bolt · crackedNR 1 ALTERNATOR SUPPORT BOLT FOUND CRACKED DURING INSPECTION, THIRD OCCURENCE.SDR 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.SDR 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.SDR 2012FA0000709Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WOULD NOT DELIVER ADEQUATE FUEL FLOW AFTER ADJUSTMENT.SDR 2012FA0000649Bracket · crackedCRACK DISCOVERED IN ALTERNATOR MOUNTING BRACKET, PN 657046. THIRD OCCURANCE OF THIS PROBLEM.SDR 2012FA0000720Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.SDR 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 COWLINGSDR 2012FA0000725Magneto · malfunctionedENGINE MISFIRES WHEN CHECKING LEFT MAGNETO.SDR 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.SDR 2012FA0000721Magneto · malfunctionedRIGHT MAGNETO WOULD NOT FIRE DURING MAGNETO CHECK. ENGINE QUIT RUNNING WHEN RIGHT MAGNETO SELECTED.SDR 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).SDR 2012FA0000724Magneto · malfunctionedLEFT MAGNETO MISFIRES DURING MAGNETO CHECK.SDR 2012FA0000527Transducer · looseOIL PRESSYRE INDICATION IN YELLOW RANGE CAUSED BY LOOSE OR DIRTY CONTACT PIN AT OIL PRESSURE TRANSDUCER AND AIRFRAME WIRE HARNESS.SDR 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.SDR 2012FA0000723Magneto · malfunctionedRIGHT MAGNETO DOES NOT FIRE. ENGINE QUITS WHEN RT MAGNETO SELECTED DURING MAGNETO CHECK.SDR 2012FA0000719Magneto · malfunctionedENGINE MISFIRES DURING MAGNETO TEST.SDR 2012FA0000718Magneto · malfunctionedRIGHT MAGNETO WOULD NOT FIRE.SDR 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 SDR 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.SDR 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.SDR 2012FA0000343Case · crackedDURRING PRE FLIGHT FOUND OIL ON COWLING. INVESTIGATION FOUND A CRACK IN THE RT FWD TOP OF THE ENGINE CASE.SDR 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 BRSDR 2012FA0000179Relay · faultyFLAPS STUCK IN DOWN POSITION. CONDITION TRACED TO A FAULTY RELAY. THIS IS A CHRONIC PROBLEM ENCOUNTERED ON 6 ACFT.SDR 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 SDR 2012FA0000722Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.SDR 2012FA0000582Spark Plug · crackedENGINE RAN ROUGH. PRECAUTIONARY LANDING. FOUR SPARK PLUGS, FOUND CRACKED AND SOME MISSING INSULATORS.SDR 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 DISSDR 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 ESDR 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 WERESDR 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 CSDR 2011FA0000702Crankcase · crackedCRANKCASE CRACKED JUST AFT AND ABOVE NR1 ALTERNATOR MOUNT AREA AND LEAKING.SDR 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 WERESDR 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 EXHAU
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