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 = 'A119' 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 = 'A119' 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 QMLA2016102916129Strap · crackedWHILE PERFORMING AN AMC AIRWORTHINESS CHECK, A CRACK WAS DISCOVERED ON THE LT SIDE OF THE FUSELAGE AT STA 5741 FROM WL 1303.6 THRU 1153.6. PER APPROVAL OF PSEAW119-2016-55713-183344 AND AN AMC SPECIAL FLIGHT PERMIT, AIRCRAFT WAS REPOSITIONED TO MAINTENANCE FACSDR QMLA2016102616132Skin · crackedWHILE PERFORMING FURTHER INSPECTIONS A CRACK DISCOVERED ON THE LT SIDE OF THE FUSELAGE SKIN, BY THE FOOT STEP AT STA 4710 WL 715 LOCATED APPROX 3.5 IN LONG.SDR QMLA2016102516133Skin · crackedWHILE PERFORMING AN AIRWORTHINESS CHECK, CRACKS WERE DISCOVERED ON THE LT SIDE OF THE FUSELAGE SKIN AT STA 4010 WL 1419 LOCATED 3 CRACKS 1/2 LONG. PER SERVICE ENGINEERING AND AN SPECIAL FLIGHT PERMIT, AIRCRAFT WAS REPOSITIONED TO MAINTENANCE FACILITY FOR SHEESDR QMLA2016092116109Retainer · crackedON THE EVENING OF 9/21/2016, A CRACK WAS DISCOVERED VERTICALLY ADJACENT OF THE LT A/F DOOR PILLAR LATCH DURING A PREFLIGHT BY THE PILOT. A REPAIR SCHEME HAS BEEN REQUESTED FROM MFG FOR A/F PILLAR AND A/F SLIDING DOOR POST OUTER SHEET METAL COVER IS ON ORDER.SDR QMLA2016090716104Retainer · damagedDURING TROUBLESHOOTING FOR THE DOOR WARNING CAUTION LIGHT, IT WAS NOTED THAT THE DOOR LATCH ITSELF SHOWED SIGNS THAT IT WAS NOT STRAINGHT AGAINST THE PILLAR CHANNEL. AFTER REMOVING THE DOOR SEAL IT WAS DETERMINED THAT THE A/F SLIDING DOOR POST WAS BENT TO ONE SDR QMLA2016082116095Inverter · malfunctionedARRIVED AT SCENE WITH NO INCIDENT, SHUTDOWN, LOADED PATIENT AND DEPARTED, EN-ROUTE FOR DESTINATION, EXPERIENCED A FULL SAS FAILURE WITH BOTH SAS WARNING LIGHTS ILLUMINATED AND OSCILLATIONS OCCURRING. ONCE THE AIRCRAFT WAS SLOWED TO THE PROPER AIRSPEED IAW EMESDR QMLA2016061716068Transceiver · failedDURING AN IFT AT APPROXIMATELY 1 MINUTE OUT FROM LANDING A SPARK/FLASH WAS NOTICED FROM THE DASH AND A SMALL AMOUNT OF SMOKE WAS NOTICED COMING OUT OF THE TOP OF THE GLARE SHIELD THROUGH SOME VENTS IMMEDIATELY FOLLOWED BY AN ELECTRICAL BURNING ODOR. A QUICK LSDR QMLA2016051616054Transmission · making metalAIRCRAFT WAS PREPARING TO TAKEOFF AFTER START UP, WHEN THE MAIN TRANSMISSION CHIP LIGHT ILLUMINATED. PILOT SHUTDOWN THE ACFT. REMOVED MAIN TRANSMISSION CHIP DETECTOR & FOUND IT SATURATED WITH METAL PARTICLES. IAW THE MM, DRAINED & FLUSHED THE MAIN TRANSMISSSDR QMLA2016051116048Vertical Gyro · unserviceableDURING CRUISE FLIGHT, APPROX 30 MINS INTO THE RETURN LEG, EXPERIENCED A SINGLE & SEVERE JERK & BUMP THROUGH THE ACFT. THE PILOT CONSIDERED THE BUMP SEVERE ENOUGH TO WARRANT CHANGING COURSE TOWARDS THE NEAREST SUITABLE LANDING AREA. AFTER 3 MINS OF FLIGHT THESDR QMLA2016042016042Inlet Screen · obstructedAT APPROX 2000 LOCAL TIME, DURING CRUISE FLIGHT, CREW COMPLAINED OF AN ELEC BURNING SMELL. PILOT NOTICED IT SOON AFTERWARD. SHUT OFF A/C, SMELL REMAINED BUT FADED SLIGHTLY. TURNED A/C BACK ON & SMELL GOT MUCH STRONGER. TURNED OFF A/C, OPENED ALL VENTS, MONSDR QMLA2016040716037Converter · failedDURING THE FLIGHT TO THE HOSPITAL, AN ELEC BURNING SMELL WAS NOTICED BY THE MED CREW. THE MEDICAL EQUIPMENT WAS NOT WORKING DO TO SOME TYPE OF ELEC FAILURE. TURNED OFF THE POWER TO THE MEDICAL OUTLET & DIVERTED FROM MY COURSE & LANDED SAFELY. ACFT WAS INSPESDR CA160301009Engine · leaking(CAN) THE CUSTOMER REPORTED THAT ON A STRAIGHT AND LEVEL FLIGHT, THE ROTOR SPEED DECAYED IN ELECTRONIC ENGINE CONTROL MODE WHICH RESULTED IN THE PILOT SELECTING MECHANICAL MODE. PILOT THEN ROLLED INTO MANUAL MODE AND REPORTED NR AT 90 PERCENT. THE ACFT LANDEDSDR QMLA2015070915056Cowling · crackedFOUND CRACKED ENG COWLING ON PREFLIGHT, PORT SIDE OF FWD ENG COWLING AFT EDGE OF ACCESS DOOR OPENING. VERTICAL STIFFENER ALSO FOUND CRACKED WHEN INVESTIGATING FURTHER.SDR CA150408008Engine · power loss(CAN) THE CUSTOMER REPORTED THAT ON MARCH 25, EXPERIENCED A NR DROOP TO 96%. TROUBLESHOOTING FOUND NO CAUSE OR REPEATABILITY. ON MARCH 27 AFTER THREE FLIGHTS IT DROOPED AGAIN. ACFT IS GNDED AT THIS TIME. THE FIELD SERVICE REPRESENTATIVE WAS CALLED TO SUPPOSDR QMLA2014092514119Door Frame · crackedRIGHT SLIDING DOOR FRAME WHERE DOOR LATCHES TO AIRFRAME IS CRACKED & NOT SUPPORTING LATCHING STRUCTURE. THREADED INSERT LOOSE IN SECTION OF CRACKED AREA. UPON FURTHER DISASSEMBLY THE DOOR FRAME WAS FOUND TO HAVE MORE DAMAGE IN THE UNDERLYING LAYERS OF SHEET SDR QMLA2014092514116Door Frame · crackedRIGHT SLIDING DOOR FRAME WHERE DOOR LATCHES TO AIRFRAME IS CRACKED & NOT SUPPORTING LATCHING STRUCTURE. THREADED INSERT LOOSE IN SECTION OF CRACKED AREA.SDR DT1R20140206002Window · crackedDURING POST FLIGHT CHECK, TECHNICIAN DISCOVERED LT UPPER CANOPY WINDOW TO BE CRACKED.SDR DT1R20140206001Window · crackedDURING POST FLIGHT CHECK, TECHNICIAN DISCOVERED RT UPPER CANOPY WINDOW WAS FOUND TO BE CRACKED.SDR CA140203003Fcu · malfunctioned(CAN) THE CUSTOMER ADVISED MFG THAT AFTER THE 0 TIME O/H ENGINE FROM MFG SAINT-HUBERT FACILITY WAS INSTALLED AND AN UNCONTROLLED ACCELERATION EVENT OCCURRED ON THE GROUND. DURING THE TROUBLESHOOTING, THE FCU WAS CHANGED AND THE ISSUE WAS CORRECTED.SDR 2013FA0000211Connector · contaminatedACFT HAD TO MAKE AN UNSCHEDULED LANDING DUE TO A ENGINE RGB CHIP LIGHT THAT ILLUMINATED DURING FLIGHT, THE MECHANIC CLEANED OIL OUT OF THE RGB CHIP DETECTOR CONNECTOR PLUG THE OPS CHECK WAS GOOD AND THERE HAS BEEN NO FURTHER CHIP LIGHTS SINCE THE CONNECTOR PLUSDR DT1R20130212001Baffle · unlacedDURING PRE-FLIGHT CHECK, FUEL CELL INTERNAL BAFFLE STRING WAS FOUND UNLACED AND SHREDDED. NEW LACE CORD WAS INSTALLED FOLLOWING THE MALFUNCTION.SDR CA121105014Fcu · malfunctioned(CAN) AFTER LANDING, UPON ROTATING THROTTLE FROM FLY TO IDLE, THE ENGINE SHUT DOWN UNEXPECTEDLY. THE ENGINE WAS RE-STARTED AND EXHIBITED SIGNS OF COMPRESSOR STALL AND SO IT WAS SHUTDOWN IMMEDIATELY. THE OPERATOR HAS ALREADY REPLACED THE FUEL CONTROL UNIT WHICSDR DT1R2012041204Gear · crackedDURING 4800 HR O/H INSPECTION, SUBJECT GLEASON CROWN GEAR WAS FOUND TO HAVE A CRACK.SDR DT1R2012020800003Seal · misinstalledPILOT AND CO-PILOT DOOR WINDOW SEALS FOUND NOT TO HAVE ADHEASIVE/SEALANT APPLIED. APPLIED SEALANT RTV 732 TO COCKPIT DOOR WINDOWS IAW TEMPORARY MAINTENANCE INSTRUCTION NR 109-244.SDR DT1R2012020500002Seal · discoveredPILOT AND CO-PILOT DOOR WINDOW SEALS FOUND NOT TO HAVE ADHEASIVE/SEALANT APPLIED. APPLIED SEALANT RTV 732 TO COCKPIT DOOR WINDOWS IAW TEMPORARY MAINTENANCE INSTRUCTION NR 109-244.SDR IFJA2011FA0000361Latch · brokenDURING A 135 FLIGHT WITH A PATIENT ON BOARD A CREW MEMBER TRIED TO CLOSE THE RT REAR SLIDING DOOR THE DOOR WOULD CLOSE BUT WOULD NOT LATCH SHUT, THE AIRCRAFT LANDED AT IFP WHERE THE DOOR WAS REPLACED, THE MECHANICS VERIFIED THAT THE DOOR CLOSED AND LATCHED. AFSDR 2011FA0000160O-Ring · brokenFAILURE OF O-RING AT SLIP JOINT OIL PRESSURE STAINLESS STEEL LINE ON LT SIDE OF ENGINE FEEDING THE ENGINE REDUCTION GEAR BOX. LARGE AMOUNT OF ENGINE OIL FOUND ON THE GROUND AFTER SHUTDOWN FROM FLIGHT. ALSO, LARGE AMOUNT OF ENGINE OIL SATURATING THE TAIL BOOMSDR 2010FA0001204Circuit Breaker · shortedTHE PILOT REPORTED THAT THE SAS NR1 , NR1 INVERTER AND THE NR2 ECU FAILED DURING FLIGHT. THE PILOT MADE A PRECAUTIONARY LANDING AT AIRPORT WITH OUT INCIDENT. AFTER TROUBLESHOOTING THE DISCREPANCY THE MECHANIC FOUND THAT THE EMERGENCY BUS CIRCUIT BREAKER SHORTESDR 2010F00219Connector · contaminatedON THE FIRST FLIGHT AFTER A TORRENTIAL DOWNPOUR, DURING TAKEOFF FROM A SCENCE CALL THE PILOT NOTICED A LOSS IN OIL PRESSURE INDICATION, THE PILOT IMMEDIATLY PERFORMED A NORMAL LANDING AT THE ORIGIN OF THE FLIGHT WITH OUT INCIDENT. THE MX WAS DISPATCHED AND AFTSDR CA100810006Bypass Valve · failed(CAN) -DEFECT- ENGINE OIL TEMPERATURE HOT IN FLIGHT. EXCEEDANCE ABOVE 115 C AS INDICATED ON EDU (78 SEC.) -DEFECT RECTIFICATION- REMOVED ENGINE OIL THERMOMETRIC BYPASS VALVE P/N 727029, S/N 303 AND INSTALLED NEW PART P/N SAME, S/N 280 AND O-RING P/N 730058-SDR CA100730009Drain Valve · leakingDEFECT- OIL NOTICED ON TAILBOOM AND VERT FIN AFTER SHUTDOWN. NO SECONDARY INDICATIONS NOTED (IE CAUTION, TEMP, OR PRESSURE). MGB SERVICED WITH 3 LITRES OF BP 2380 OIL AND OIL SYS DRAIN LINES DISCONNECTED FOR TROUBLESHOOTING AS NO OIL WAS FOUND ON DECK PANS.SDR 2010F00123Fire Loop · brokenAFTER DROPPING A PATIENT OFF AT AIRPORT, ACFT DEPARTED THE AIRPORT AND WAS ON INITIAL CLIMB OUT WHEN THE PILOT REPORTED A " FIRE DETECT" LIGHT ILLUMINATED ON THE CAP PANEL, AT THIS POINT THE THE PILOT RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT. WHEN TSDR 2010FA0000453Control Box · looseDURING MANUAL THROTTLE TRAINING, ON GROUND, IT WAS NOTICED THAT THROTTLES WERE NOT MOVING SYNCHRONOUSLY AND PLA INDICATION DID NOT MOVE WITH PILOT'S THROTTLE. AIRCRAFT WAS SHUTDOWN. AFTER TROUBLESHOOTING IT WAS FOUND THAT THE THROTTLE CONTROL BOX ASSEMBLY DISDR CA100831001Engine · failedACCIDENT DURING TAKEOFF, CREW NOTICED A LOW OIL PRESSURE INDICATION. A LANDING ATTEMPT RESULTED IN A HARD LANDING AND DAMAGE TO THE ROTORCRAFT. 2 CREW AND 4 PASSENGERS WERE REPORTED TO BE ONBOARD. INJURIES ARE BEING REPORTED. NO FURTHER DETAILS ARE AVAILABLSDR 2010FA0000182Regulator Valve · wornENGINE OIL TEMPERATURE ROSE HIGHER THAN USUAL. FOUND TEMPERATURE REGULATOR VALVE (THERMAL VALVE)TO BE THE PROBLEM.SDR 2009FA0000945Crossmember · crackedFORWARD RIGHT HAND LANDING SKID CROSS MEMBER FAILED NEAR ATTACHMENT POINT BRACKET. CIRCUMFERENTIAL CRACK APPEARS TO HAVE STARTED AT CROSS MEMBER RIVET ATTACHMENT POINT, ORIGINATING FROM RIVET HOLES. HEAVY CORROSION NOTED FROM LACK OF CORROSION PREVENTIVE COATISDR IFJA119AHFuel Control · malfunctionedAFTER PICKING UP A PATIENT FROM AN AIRPORT JUST OUTSIDE OF BLYTHE, CA. ABOUT 8 MINUTES INTO THE FLIGHT THE PILOT FELT A SLIGHT VIBRATION IN THE HELICOPTER FOLLOWED BY A LOW LIGHT AND A LOW NR HORN. THE PILOT LOWERED THE COLLECTIVE AND WENT TO MEC MODE WITH NOSDR 2009FA0000912Rotor Head · crackedDURING INSP OF THE TAIL ROTOR ASSY, A CRACK WAS FOUND BETWEEN THE BLADE RETENTION BOLT AND THE FACTORY BALANCE WEIGHT PLATES.SDR IFJA103Fuel Control · malfunctionedDURING CRUISE, PILOT FELT A VERY MILD VIBRATION AND NOTICED THE NR WAS 1 PERCENT LOW, PILOT THEN LOWERED THE COLLECTIVE TO MAKE A LT TURN FOR LANDING. THE NR DECREASED AS PILOT LOWERED THE COLLECTIVE TO THE POINT WHERE THE NR HORN SOUNDED AND THE VIBRATION GOSDR IFJA207Fuel Control · malfunctionedTHIS DISCREPANCY WAS TROUBLESHOT FOR SEVERAL DAYS, THE INITIAL DISCREPANCY WAS NR DROP TO 96 PERCENT WITH A COLLECTIVE CHANGE THAN IT WENT TO 94 PERCENT WITH AN COLLECTIVE CHANGE AND FINALLY TO 94 PERCENT WITH NOT COLLECTIVE INPUT AT ALL. BOTH THE MECHANIC ANSDR CA090512004Crosstube · sheared(CAN) WHILE CLIMBING OUT FROM A LANDING AREA AT APPROX 70 KNOTS THE PILOT HEARD A LOUD BANG COMING FROM UNDERNEATH THE PILOT SEAT AREA. ALL ENGINE PARAMETERS AND FLIGHT CONTROLS WERE NORMAL AND THE PILOT LANDED AS SOON AS PRACTICAL. ONCE ON THE GROUND UPON FURSDR CA090512005Crosstube · sheared(CAN) AFTER LANDING THE ACFT IN THE SNOW AND LOWERING THE COLLECTIVE LEVER A LOUD BANG WAS HEARD BY THE PILOT UNDER THE ACFT. UPON SHUTDOWN AND FURTHER INVESTIGATION THE FWD LANDING GEAR CROSSTUBE WAS FOUND SHEARED AT THE RT ATTACHMENT SADDLE. NO OTHER DAMAGE SDR RMXA119112008Bulkhead · crackedA CRACK LOCATED AT STA 3627, WL 1235, BL 510 (LT SIDE) FWD BULKHEAD RADIATING INBD AND OTBD FROM A RIVET. THE CRACK MEASURES APPROX 3.5 INCHES TOTAL. THE RIVET IS USED TO ATTACH A CAST FITTING TO THE BULKHEAD AND IS THE LOWER LT RIVET. THE CAST FITTING IS PARTSDR RMXA11911708Skin · crackedA CRACK DEVELOPED IN THE TAILBOOM SKIN AT APPROXIMATELY STA 9725, WL 1895, LT SIDE EMANATING FROM A RIVET FORE AND AFT WITH A TOTAL LENGTH OF APPROX 79 MM.SDR 2008FA0000774Trim Tab · delaminatedUPON POST FLIGHT IT WAS NOTICED THE MAIN ROTOR BLADE TRIM TAB WAS SERIOUSLY DELAMINATED AND SEPARATED IN FLIGHT. THIS PROBLEM HAS OCCURRED NUMEROUS TIMES IN THE PAST. SOME OCCASIONS REQUIRED THE BLADE TO BE REMOVED AND SENT BACK TO THE MFG FOR REPAIR. AS IN SDR RMXA011408001Door Frame · crackedMAJOR REPAIRS: LT CORNER DOOR POST FRAME STA. 2044 WL 1400 CRACKED. LT INNER DOOR FRAME CRACKED. LT/RT INNER UPPER DOOR FRAME CRACKED. LT INNER DOOR FRAME, PATCH. MINOR REPAIRS: LT/RT UPPER FRAME AT THE GREENHOUSE WINDOW SUPPORT FRAME. INSTALLED NEW UPPSDR 14011NOV2907Stiffener · crackedENGINE COWLING STIFFENER CRACKED AT APPROX. STA. 4960, WL 1979, BL 510. THE CRACK RUNS COMPLETELY THROUGH THE STIFFENER IN THE AREA OF THE CUTOUT FOR THE OIL BREATHER TUBE INSTALLED ONTO THE ENGINE.SDR 14011OCT3107Scissor Link · brokenUPON THE PILOTS DAILY INSPECTION HE FOUND THE SUSPECT PART APPERARED TO BE CRACKED. THE MECHANIC REMOVED THE PART FROM AIRCRAFT AND PART CAME APART AT ONE OF THE MOUNTING EARS.SDR N820NA103107Scissor Link · brokenUPON THE PILOTS DAILY INSPECTION, HE FOUND THE SUSPECT PART APPEARED TO BE CRACKED. THE MECHANIC REMOVED THE PART FROM AIRCRAFT AND PART CAME APART AT ONE OF THE MOUNTING EARS.SDR 2007F00049Bypass Valve · malfunctionedON A FLIGHT, AC EXPERIENCED AN ENGINE OIL HOT LIGHT, THE EMERGENCY PROCEDURE IN THE AFM IS TO LAND AS SOON AS POSSIBLE. THE AIRCRAFT WAS LANDED IN A FIELD WITHOUT INCIDENT. FAA POI, WAS NOTIFIED. UPON INVESTIGATION IT WAS DETERMINED THAT THE OIL COOLER BYP
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