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 = '525' 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 = '525' 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 9JLA20110630001Ahrs · defectiveCREW REPORTED THE NR 1 AHRS FAILED DURING THE THIRD LEG OF TRIP AND HAD TO SWITCH TO REVERSIONARY AHRS NR 2. TROUBLESHOOTING FOUND THE AHRS COMPUTER DEFECTIVE P/N 822-1110-001 S/N 49YM.SDR LOMA2011042201000Engine · slowUPON TAKE-OFF, ACFT ACCELERATION DETERMINED SLOW BY PILOT AND COPILOT. AT 80 KNOTS INDICATED, TAKEOFF ABORTED. CREW SLOWED AIRCRAFT TO STOP USING ACFT BRAKES. LT MAIN TIRE DEFLATED AT WALKING SPEED, FROM FUSE PLUG RELEASE, TIRE BEAD SEPARATED FROM WHEEL. ACFTSDR 2011FA0000071Gyro · malfunctionedDRIVES COMPASS CARD +70 DEGREES. FOUND ON INITIAL POWER UP AFTER INSTALLATION/ REPLACEMENT.SDR 2011FA0000070Gyro · malfunctionedDRIVES COMPASS CARD +15 DEGREES. FOUND ON INITIAL POWER UP AFTER INSTALLATION/ REPLACEMENT.SDR 2011FA0000069Gyro · malfunctionedDRIVES COMPASS CARD +10 DEGREES. FOUND ON INITIAL POWER UP AFTER INSTALLATION OF REPLACEMENT.SDR CA091209004Line · cracked(CAN) PILOT REPORTED NO TAIL DE-ICE BOOT INDICATION BETWEEN 72 TO 82 N2. RAN AIC ON GROUND TAIL DEI-CE BOOT WOULD INFLATE, BUT NO INDICATION. INDICATION WOULD WORK UP TO 72 AND PAST 82N2, HOWEVER IN BETWEEN WAS VERY ERRATIC. TUBE FOUND SEPARATED FROM B NUT, FSDR 2009FA0000959Sensor · out of limitsPROBLEM WAS TROUBLESHOT TO A FAULTY BATTERY TEMP SENSOR. THE SPARE SENSOR INSIDE THE BATTERY WAS CONNECTED AND TOOK THE FAULTY SENSOR OFF LINE. BATTERY WAS REINSTALLED AND THE AIRCRAFT WAS OPS CHECKED GOOD AT THAT TIME AND WAS RELEASED.SDR 2009FA0000798Shaft · shearedSHAFT SHEARED ON NR1 (L) HYD PUMP WHILE ACFT WAS IN A CLIMB AFTER TAKE OFF. THIS RESULTED IN THE HYD RESERVOIR TO BE EMPTIED OVERBOARD THRU THE PUMP DRAIN. THE PILOT'S THEN GOT A HYD FLOW LOW ANNUNCIATOR, FIRST ON THE RT SIDE AND THEN A FEW SECONDS LATER ON THSDR EWCR44CK5250401Stud · brokenSTARTING DESCENT, VIBRATION/NOISE WAS AUDIBLE INSIDE ACFT. NO INDICATIONS OF SYSTEM ISSUES OTHER THAN THE VIBRATION BUZZ NOISE. FLT DIVERTED. WHEN LANDING GEAR WAS EXTENDED FOR LANDING VIBRATION/NOISE WENT AWAY. ACFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS TUSDR CA090617002Trim Tab · displaced(CAN) PILOT REPORTED "JERKINESS: OF ELEVATOR CONTROL - GROUNDED ACFT ELEVATOR TRIM/TAB OPERATION INSPECTED - LT TAB INGFS FOUND MIGRATED INBD. CONTRACTING TAILCONE. HINGE PIN RETAINING LOCKWING FOUND MISSING. LOCKWING HOLES (2) FOUND "PULLED THRU" TAB SKIN.SDR 2009FA0000391Bearing · damaged38K FEET, AUTO PILOT COMMANDING DECENT RATE - LT ENGINE BEGAN UNCOMMANDED SPOOL DOWN. NO PRIOR INDICATIONS ON PANEL. DURING EMERGENCY SHUTDOWN PROCEDURES N1 AND N2 INDICATIONS CONFIRMED, 36K, 30K FEET SLIGHT VIBRATION FELT. AT 30K FEET VIBRATION STOPPED. INSDR 2009FA0000015Tube · brokenDURING AN INSP, DOC 10, LANDING GEAR PNEUMATIC BRAKE SYS FUNCTIONAL CHECK ONE OF THE LINES IN THE RT LANDING GEAR WELL BLEW. FURTHER INVESTIGATION FOUND THAT THE 6327500-12 TUBE ASSY BROKE OFF AT THE FLARE ON THE INBD END OF THE TUBE ASSY. INSP OF THE SAME LSDR CA081020001Mount · misinstalled(CAN) METAL FILINGS WERE FOUND UNDER THE RUDDER SERVO DUE TO THE MOUNTING STRUCTURE HAVING BEEN INSTALLED OFFSET FROM THE FACTORY. THIS CAUSED THE RUDDER CABLE TO EXIT THE DRUM ON AN ANGLE AND RUB THE CAPSTAN. THE SERVO WAS REPLACED AND A PERMANENT FIX IS SCHESDR EWC2008F00000Pressure Sensor · faultyAFTER DEPARTURE, THE CREW NOTICED THE ANNUNCIATOR WARNING LIGHT COME ON FOR THE RT ENGINE FUEL FILTER BYPASS. THE CREW NOTIFIED ATC, DECLARED AN EMERGENCY, AND WERE ROUTED FOR LANDING, AFTER ARRIVING SAFELY AND CONFERRING WITH THE MFG ON FIELD, THE RT FUEL FISDR 2008FA0000705Line · rupturedRUPTURE OF TUBE AT SIDE WHERE BENDING DIES LEFT MARKING, BOTH ABOVE AND BELOW OPENING. AFTER TAKEOFF, LOW FLUID AND PRESSURE WARNING LIGHTS CAME ON AND ACFT RETURNED TO DEPARTURE. ACFT WAS TURNED OVER TO REPAIR STATION. LEAK WAS LOCATED AND LINE REPLACED ALONSDR 2008FA0000686Line · rupturedRUPTURE OF TUBE AT SIDE WHERE BENDING DIES LT MARKING BOTH ABOVE AND BELOW OPENING. AFTER TAKEOFF, LOW FLUID AND PRESSURE WARNING LIGHTS CAME ON AND ACFT RETURNED TO AIRPORT. ACFT WAS TURNED OVER TO SERVICE CENTER. LEAK WAS LOCATED AND THE LINE REPLACED ALONSDR AJC2008F00001Smoke Detector · false activationIN THE DESCENT FROM ALTITUDE FL430, THE BAGGAGE SMOKE LIGHT ILLUMINATED (RED). ACTION TAKEN BY CAPTAIN WAS REQUEST FOR PRIORITY HANDLING TO A SAFE LANDING IN MINUTES WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION OF THE FWD AND AFT BAGGAGE COMPARTMENTS FOUND NOSDR Z5F2008F00005Switch · failedDURING CLIMB THROUGH FL 270, RT HYDRAULIC FLOW LIGHT ILLUMINATED. DIVERTED, DURING DECENT RT HYD FLOW LIGHT WENT OUT. REMOVED DEFECTIVE RT FLOW SWITCH AND INSTALLED NEW SWITCH. HYDR INDICATION CHECKS NORMAL, AND AC RETURNED TO SERVICE. (K)SDR 2008FA0000606Fork · brokenDURING ROUTINE TAXI TO PERFORM MAINT CHECKS AFTER AC HAD BEEN PAINTED, NOSE GEAR AXLE BROKE LOOSE FROM NOSE GEAR STRUT. INVESTIGATION SHOWED BOTH WHEEL BEARING HAD HEAVY RUST AND DID NOT TURN FREELY ON THE AXLE. VERY LITTLE GREASE WAS FOUND IN EIGHER OF THE NOSDR 7302008N401CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)SDR 7302008N409CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)SDR 7282008N430CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361210-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)SDR 7282008N406CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)SDR 2008FA0000491Blade · departedDURING ROUTINE INSP, FOUND DAMAGE TO THE 1ST STAGE STATOR ASSY, UPON FURTHER INSPECTION, FOUND 1 BLADE HAD FAILED AND DEPART THE LP ROTOR ASSY CAUSING DAMAGE TO THE REST OF THE ENGINE DOWN STREAM. (K)SDR 070808N408CSISmoke Detector · defectiveON APPROACH INTO BOS, CREW OBSERVED BAGGAGE SMOKE ANNUNCIATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT, FIRE DEPARTMENT PERSONNEL FOUND NO INDICATION OF SMOKE OR FIRE. MAINTENANCE PERSONNEL TROUBLESHOT SYSTEM AND REPLACED SUSPECTED DEFECTIVE SMOSDR Z5F2008F00000Smoke Detector · defectiveON APPROACH, CREW OBSERVED BAGGAGE SMOKE ANNUNCIATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT, FIRE DEPARTMENT PERSONNEL FOUND NO INDICATION OF SMOKE OR FIRE. MAINT PERSONNEL TROUBLESHOT SYSTEM AND REPLACED SUSPECTED DEFECTIVE SMOKE DETECTOR ANDSDR Z5F2008F00002Engine · leakingLIGHT SMOKE IN CABIN, THEN LT ENG MADE A LOUD POPPING SOUND, LOW OIL PRESSURE ILLUMINATED AND ENGINE ROLLED BACK, SHUTDOWN IN FLIGHT. AFTER LANDING, FOUND THAT ENGINE HAD LOST OIL. (COMING OUT OF TAIL PIPE, DRAIN MAST AND SG EXHAUST). AC CURRENTLY IN MAINTESDR CA080625001Line · ruptured(CAN) ACFT DEPARTED AND EXPERIENCED COMPLETE HYDR FLUID LOSS. ACFT GEAR ALTERNATE EXTENDED AND RETURNED TO AIRPORT. TROUBLESHOOTING REVEALED RUPTURED HYDR PRESSURE LINE INBD OF SERVICE QUICK CONNECT. LINE REPLACED WITH NEW, AND SYS BLED. ACFT RUN FOR 10 MIN ANSDR 26N2008F00000Valve · unserviceableWHILE ON A TRAINING FLIGHT THE FLIGHT CREW SELECTED "FLAPS" ON APPROACH. AS THEY LINED UP ON THE ILS THEY SELECTED "SPEED BRAKES" AND REALIZED THAT THY HAD NO HYDRAULICS ON THE AIRCRAFT. WHEN "GEAR DOWN" WAS SELECTED, THE CREW DID NOT SEE A DOWN AND LOCKED CSDR 042908N412CSDetection Sys · false activationDURING APPROACH, BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED AND AC DIVERTED AND LANDED WITHOUT INCIDENT. NO SMOKE EVIDENT DURING AFTER LANDING CHECK. BOTH FWD AND AFT BAGGAGE SMOKE DETECTORS WERE REPLACED, OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT RETURNED TO SDR AMCR200800001Heating Element · failedPILOT REPORTED T2 HEATER FAIL ON RT ENGINE. FOUND T2 PROBE BAD.SDR 3302008N406CSPcb · burned outDURING APPROACH, WHEN LANDING GEAR WAS SELECTED DOWN, THE DOWN AND LOCKED GREEN LIGHTS DID NOT ILLUMINATE ALTHOUGH THE GEAR FELT LIKE IT EXTENDED. THE GEAR WAS BLOWN DOWN BUT THE INDICATION DID NOT APPEAR. THE COCKPIT FLOOD LIGHTS WERE SELECTED AND THE DOWN ANSDR AIH2008F00000Pump · seizedLT HYD PUMP LOW FLOW ANNUNCIATOR ILLUMINATED. MAINT FOUND THE LT HYD PUMP WAS SEIZED. PUMP WAS REPLACED WITH NEW AND PROBLEM WAS SOLVED. (K)SDR AMCR200700004Jam-Nut · wrong partDURING COMPLIANCE WITH SL525B-27-01 WHICH IS CHECKING FLAP PUSH ROD FOR IMPROPER SAFETY WIRING, FOUND THAT THE AFT JAM NUT (NAS509L6) WAS UP AGAINST THE CENTER STUD (6365028-10) RATHER THAN TIGHT AGAINST THE ROD END TUBE (6365028-9). EVERYTHING WAS SAFETIED INSDR 113007N423CSSmoke Detector · false indicationDURING CLIMB AT 15,000 FT, THE BAGGAGE SMOKE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO HPN AND MADE AN UNEVENTFUL LANDING. THE SYSTEM WAS TROUBLESHOT AND THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 110407N420CS1Bulb · burned outDURING APPROACH CREW NOTICED NO RT GEAR DOWN INDICATION. CREW FOLLOWED EMERGENCY PROCEDURES, BLEW GEAR DOWN AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE PERSONNEL FOUND CAUSE TO BE BURNED OUT BULB. BULB REPLACED, SYSTEM OPS CHECKESDR CA071114008Wire Harness · shorted(CAN) THE EMERGENCY BRAKE HAD TO BE USED UPON LANDING AS IT WAS DISCOVERED THAT THE ANTI-SKID WIRING HARNESS HAD A SMALL AMOUNT OF SLACK BETWEEN THE TRAILING LINK AND THE TRUNNION. THIS ALLOWED IT TO RUB AGAINST THE TIRE, WEARING OFF THE COATING AND UPON LANDISDR 101107N423CSTire · rupturedDURING LANDING ROLL OUT, BEFORE BRAKES WERE APPLIED A SEVERE VIBRATION WAS FELT AND THE AIRCRAFT SUDDENLY PULLED TO THE RIGHT. AIRCRAFT WAS STOPPED ON A TAXIWAY AND CREW DISCOVERED RIGHT MAIN TIRE MISSING AND WHEEL DAMAGED.SDR 100607N409CSCowling · departedDURING FLIGHT, THE RT ENGINE LOWER COWL SEPARATED FROM THE ENGINE. DAMAGE TO THE RT HORIZONTAL STABILIZER OCCURRED CAUSED BY IMPACT DAMAGE. CREW REPORTED FEELING A SLIGHT "BUMP" DURING THE FLIGHT, HOWEVER THERE WAS NO INDICATION OR ABNORMAL FLIGHT CHARACTERISTSDR CA080207003Converter · inoperative(CAN) MFD FAIL TO COME ON WHEN ACFT MASTER SWITCH TURNED ON. DC-DC CONVERTER REPLACED - SAME PROBLEM OCCURED AT 102.6 AIRFRAME HRS. - 66 AIRFRAME CYLES, AND DC-DC CONVERTER REPLACED AGAIN (33 HRS + 19 CYCLES) MFG IS AWARE OF THE POOR QUALITY OF THE RR18 DC-DC SDR 082907N413CS1Trim System · out of adjustENROUTE, AT CRUISE ALTITUDE OF 5000 FT AIRCRAFT STARTED TO TURN RT, DISENGAGED AUTO-PILOT, TURN STILL EXISTED. DIVERTED TO TOL AND LANDED WITHOUT INCIDENT. AIRCRAFT CURRENTLY IN MAINTENANCE. CAUSE UNKNOWN AT THIS TIME. 09-03-07 ALL CONTROL RUDDER, AILERON ANSDR 2007FA0000566Fuel · contaminatedPERFORMED AN EMERGENCY LANDING, DUE TO A FUEL BYPASS LIGHT COMING ON IN FLIGHT. THE AIRCRAFT LANDED AND TAXIED TO THE SERVICE CENTER WITHOUT INCIDENT. THE CAUSE OF THE LIGHT HAS BEEN DETERMINED TO BE THE FUEL ITSELF. THE FUEL IS CONTAMINATED WITH VISIBLE DESDR 052407N412CSLanding Gear · malfunctionedON APPROACH, AFTER GEAR WAS EXTENDED, NO GEAR DOWN INDICATION WAS NOTED ON ANY OF THE (3) ANNUNCIATORS. ABORTED APPROACH INITIATED A GO-AROUND AND RAN THE GEAR CHECKLIST. TOWER ADVISED ALL GEAR APPEARED TO BE DOWN. BLEW GEAR DOWN AND REQUESTED EMERGENCY EQUIPMSDR 052107N151CSStructure · damagedON APPROACH, CREW ENCOUNTERED FLOCK OF GEESE RESULTING IN NUMEROUS STRIKES. ABORTED APPROACH, INITIATED AFM ABNORMAL CHECKLIST WITH NO ABNORMALITIES NOTED. DIVERTED, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING AND EXITING AIRCRAFT, CREW NOSDR 050807N406CS1Unknown · unknownON DESCENT INTO CYYZ THE BAGGAGE SMOKE LIGHT ILLUMINATED. NO VISUAL OR ODOR OF SMOKE WAS DETECTED BY THE FLIGHT CREW. THE CREW DECLARED AN ENERGENCY AND DIVERTED TO BUF. LANDING WAS UNEVENTFUL. NO SIGNS OF SMOKE OR FIRE INSIDE THE BAGGAGE COMPARTMENT WAS DETECSDR CA070427004Starter Gen · failed(CAN) GENERATOR OUTPUT FAILURE, NO OUTPUT. (TC NR 20070427004)SDR 33107N128CS1Attenuator · malfunctionedAFTER ROTATION MASTER CAUTION, HYD PRESS ON AND ATTENUATOR UNLOCKED RT ILLUMINATED. THE CREW SELECTED STOW WITH NO EFFECT AND THE ATTENUATOR COULD BE HEARD OPENING AND CLOSING IN FLIGHT. CREW NOTIFIED TOWER THEY HAD AN EMERGENCY AND REQUESTED RETURN TO ROCHESDR 031307N425CS1Smoke Detector · dirtyON DESCENT FL110 THE BAGGAGE SMOKE LIGHT ILLUMINATED ON THE ANNUNCIATOR PANEL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. NO SMOKE OR SMELL WAS NOTICED IN THE CABIN BY THE FLIGHT CREW. MAINTENANCE TROUBLESHOT THE SYSTEM FOUND DUST ON THE CEILISDR CA070213002Valve · failed(CAN) POST INSPECTION RUN REVEALED HYDRAULIC PRESSURE ON ANNUNCIATOR LIGHT DID NOT EXTINGUISH WHEN SYSTEM SHOULD HAVE BEEN AT REST. HYDAULIC LOADING VALVE FOUND FAILED. BLEED ORIFICE RECOVERED FROM HYDRAULIC MANIFOLD UNDER RELIEF VALVE (3RD FROM LOADING VALVESDR 011607N152CS1Actuator · faultyAFTER TAKE-OFF FROM SAT, CREW NOTICED POWER BRAKE FAIL AND POWER BRAKE PRESS LOW ANNUNCIATORS. CREW PERFORMED AFM PROCEDURE CHECKS FOR THIS INDICATION WITH NO EFFECT. CREW DECLARED AN EMERGENCY AND RETURNED TO SAT FOR INSPECTION AND REPAIR OF FAULT.MAINTENANCE
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