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 = '1900C' 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 = '1900C' 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 CA050517004Hose · chafed(CAN) DURING A TRAINING FLIGHT, THE CREW NOTICED THE LT ENGINE WAS SLOW TO RESPOND TO POWER INPUTS AND THEY WERE SOMEWHAT TORQUE LIMITED. THE AIRCRAFT RESUMED ONTO THE MAINTENANCE BASE AND LANDED IN NORMAL CONFIGURATION. MAINTENANCE WAS INFORMED AND INSPECTEDSDR ACE050805Skin · crackedFOUND CRACKED BELLY SKIN WHILE PERFORMING TURBULENT AIR INSPECTION. CORROSION POSSIBLY ORIGINATING FROM OEM INSTALLATION OF UNPRIMED SHIM STOCK AT STRINGER JOINTS.SDR ACE050705Safety Switch · intermittentPIREP - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED INTERMITTENT RT LANDING GEAR SAFETY SWITCH.SDR FFS2005F00004Bellcrank · mismanufacturedIN ATTEMPTING TO RIG THE ELEVATOR SYSTEM, IT WAS DISCOVERED THE RIGGING HOLE FOR THE FORWARD ELEVATOR BELLCRANK WAS DAMAGED IN THE UPPER ELEVATOR BELLCRANK SUPPORT. IT APPEARED THAT THE HOLE HAD BEEN TORN BY MOVEMENT OF THE BELLCRANK WITH THE RIG PIN INSTALLESDR ACE050405Wire · overheatedPIREP - LEFT LANDING LIGHT CIRCUIT BREAKER POPS OFF APPROXIMATELY 5 MINUTES AFTER LIGHT TURNED ON, ELECTRICAL BURNING SMELL NOTED IN FLIGHT DECK. MAINTENANCE DEFERRED THE DEACTIVATED CIRCUIT. MAINTENANCE WAS UNABLE TO DUPLICATE FAILURE, FOUND EVIDENCE OF HEASDR FFS2005F00003Seat Track · corrodedTHE LT FORWARD SEAT TRACK WAS CORRODED THROUGH THE SIDE OF THE TRACK AND THE TRACK AND THE FLANGE THAT SUPPORTS THE FLOORBOARD. CORROSION WAS PARTICULARLY EVIDENT AT FUSELAGE STA 158.5 - 170.5. THE LOCATION OF THE CORROSION, JUST INSIDE THE AIRSTAIR DOOR, SUSDR ACE041905Downlock Switch · failedPILOT REPORTED NOSE GEAR POSITION INDICATED UNSAFE WITH GEAR SELECTED DOWN. CYCLED GEAR AND PERFORMED GROUND VISUAL CHECK PRIOR TO UNEVENTFUL LANDING. MAINTENANCE CONFIRMED FAILED NOSE GEAR DOWNLOCK SWITCH AND REPLACED SAME.SDR FFS2005F00001Windshield · delaminatedPILOTS WINDSHIELD WAS REPLACED DUE TO ADHESION CHIPS PULLED FROM OB SURFACE OF THE INNER PLY. WINDSHIELD HAD EXPERIENCED SOME PROGRESSIVE DELAMINATION FROM THE RT EDGE. (AL01200503512) (K)SDR CA050407006Windshield · cracked(CAN) RT WINDSHIELD INNER PANE SHATTERED IN CRUISE. CREW CARRIED OUT ABNORMAL PROCEDURES FOR CRACKED WINDSHIELD AND LANDED THE AIRCRAFT.SDR CA050407005Oil Cooler · cracked(CAN) RT ENGINE OIL PRESSURE LOW LIGHT CAME ON IN FLIGHT. ENGINE WAS SECURED AND EMERGENCY LANDING CARRIED OUT. OIL COOLER WAS TESTED UNDER PRESSURE AND WAS FOUND TO BE LEAKING AND WAS REPLACED.SDR FFS2005F00002Door Frame · crackedSEVERAL RIVETS HOLDING THE HINGE TO THE AIRSTAIR DOOR ASSY HAD PULLED THROUGH THE LOWER CLOSURE REINFORCEMENT. THE REINFORCEMENT, A COMPONENT OF AN AIRSTAIR DOOR REINFORCEMENT KIN, 114-4023-3, HAD BEEN INSTALLED 1,374 HOURS EARLIER AS PART OF MFG DESIGNED FIESDR ACE020105Uplock Switch · malfunctionedGEAR WARNING REMAINED ON AFTER GEAR INDICATED THREE GREEN. PILOT DID A GO-AROUND AND ON NEXT GEAR EXTENSION, ALL INDICATIONS NORMAL. UNEVENTFUL LANDING. MAINTENANCE REPLACED NOSE GEAR UPLOCK SWITCH.SDR HSY2005F00002Hose · leaking(MRR NR 02-012405) LOSS OF HYDRAULIC PRESSURE AND QUANTITY LED TO THE INABILITY TO OPERATE THE LANDING GEAR WITH NORMAL PROCEDURES. LANDING GEAR HAD TO BE EXTENDED MANUALLY WITH THE HAND PUMP. NOTE: THIS WAS A PILOT TRAINING FLIGHT ONLY. FAILED LANDING GEARSDR CA050125012Bearing · failed(CAN) AIRCRAFT DEPARTED ENROUTE AT TEMPERATURE AT 5 DEG C. AIRCRAFT ARRIVED WITHOUT ANY INCIDENT, WHEN AIRCRAFT WAS AT THE PAX TERMINAL IT WAS NOTICED THAT THE RT OB MAIN WHEEL ASSEMBLY WAS MISSING. INSPECTION REVEALED THAT THE WHEEL BEARINGS HAD DISINTEGRASDR CA050126011Actuator · leaking(CAN) NOSE LANDING GEAR WOULD NOT EXTEND UPON DESCENT INTO AIRPORT. EMERGENCY GEAR EXTENSION PROCEDURE COMPLETED AND THE AIRCRAFT LANDED SAFELY. NOSE LANDING GEAR ACTUATOR WAS REPLACED, FOLLOWED BY SEVERALGEAR SWINGS IN NORMAL AND EMERGENCY MODES. GEAR GROUSDR ACE011205Annunciator · activatedPILOT REPORTED RIGHT HAND ENGINE FUEL FEED ANNUNCIATOR ON INTERMITTENTLY AFTER TAKEOFF. RETURNED FOR UNEVENTFUL LANDING. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. SYSTEM DEFERRED FOR ADDITIONAL REPORTS.SDR 010605Gauge · leakingDURING CRUISE, FIRST OFFICER NOTICED THAT HIS ALTIMETER, VSI AND AIR SPEED INDICATOR BEGAN TO MOVE. SELECTED THE ALTERNATE STATIC SOURCE AND THE INSTRUMENTS RETURNED TO NORMAL READINGS. DURING DESCENT FIRST OFFICER NOTICED THAT HIS VSI WAS NOT READING THE SASDR TIM2005F00000Blade · brokenAIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)SDR 2005FA0000006Blade · brokenAIRCRAFT DEPARTED, AT CRUISE, THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LEFT ENGINE SEIZED. PRE INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)SDR ACE122404Shaft · shearedPILOT REPORTED THAT INSIDE DOOR HANDLE ON AIRSTAIR DOOR WAS SHEARED. MAINTENANCE REPLACED HANDLE ASSY.SDR ACE120404Seat Track · corrodedDURING CAMP INSPECTION, MAINTENANCE LOCATED CORROSION ON SEAT TRACK FLOOR PANEL FLANGES. SEAT TRACK AND ADJACENT LOCALIZED CORROSION SUSPECTED TO HAVE BEEN CAUSED BY CARGO SPILLAGE. SEAT TRACK REPLACED, OTHER AREAS REPAIRED.SDR 2005FA0000005Cable · brokenON CLIMBOUT THE AIRSTAIR DOOR OPENED. AC RETURNED, WHEN AIRSTAIR DOOR OPENED IN FLIGHT, DOOR DAMPER BROKE AND SUPPORT CHAINS BROKE. CHAIN HIT PROPELLER AND CAUSED NOTICEABLE DAMAGE. DOOR ANNUNCIATOR LIGHT WAS NOT ILLUMINATED SO NO INDICATION OF ANY PROBLEMSDR 32041Switch · will not testLEFT FIRE LOOP WILL NOT TEST.SDR CA041104008Battery Pack · leaking(CAN) UPON ROUTINE 12 MONTH INSPECTION OF TH SUBJECT ELT, IT WAS OBSERVED THAT THE BATTERY HAD LEAKED, SHORTED OUT THE ELT MAIN BOARD AND HAD PRODUCED MAJOR AMOUNTS OF BURNING. ELT BATTERY WAS MANUFACTURED ON JUNE/03. BATTERY EXPIRY DATE IS JULY/05. THIS UNISDR ACE110304Switch · loosePILOT REPORTED USING LANDING GEAR EMERGENCY PROCEDURE DUE CONTINUED GEAR UNSAFE WARNING EVEN WITH ALL GREEN DOWN AND LOCKED LIGHTS ON. UNEVENTFUL LANDING COMPLETED. MAINTENANCE LOCATED AND CORRECTED A LOOSE POWER LEVER POSITION SWITCH.SDR ACE110104Spacer · improper partON OPERATION CHECK FLIGHT AFTER OVERHAULED ENGINE INSTALLATION, PILOT REPORTED THAT THE POWER LEVER GOT HUNG UP ON POWER REDUCTION. AN UNEVENTFUL LANDING WAS COMPLETED AND MAINTENANCE LOCATED AND CORRECTED INCORRECT (FOR THIS MODEL ENGINE) PROPELLER REVERSINGSDR ACE103004Actuator · erraticPILOT REPORTED, AFTER 3 GEAR EXTENSION CYCLES AND THE QRH MANUAL EXTENSION PROCEDURE, NOSE GEAR GREEN LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE COULD NOT DUPLICATE (SUSPECT INTERMITTENT SWITCHES) AND REPLACED NOSE GEAR ACTUATOR.SDR T2BA4Wire · loosePA SYSTEM INOPERATIVE, DEFFERRED IAW MEL 23-1 AND 23-2, PERFORMED PUBLIC ANNOUNCEMENT USING THE BULL HORN, PROCEEDED WITH FLIGHT, RETURNED TO HOME BASE AND PERFORMED TROUBLESHOOTING OF PA SYSTEM, FOUND A LOOSE WIRE, REPAIRED, SIGNED OFF WRITE UP AND RELEASED SDR T2BA2Circuit Breaker · trippedON FINAL APPROACH TO ZQA, BAHAMAS, SELECTED GEAR DOWN, LANDING GEAR RELAY CIRCUIT BREAKER (2AMP) POPPED, SELECTED GEAR UP AND EXECUTED A MISS APPROACH AND WAITED 5 MINUTES TO RE-SET CIRCUIT BREAKER, UPON RE-SETTING C/B, NOTICE THE HYDRAULIC LOW ANNUNCIATOR ILLSDR T2BA3Sensor · malfunctionedLT FUEL QUANTITY ANNUNCIATOR ILLUMINATED THROUGHOUT ENTIRE FLIGHT 20 MINUTE FLIGHT, PERFORMED TROUBLESHOOTING OF FUEL INDICATING SYSTEM, FOUND THE LOW FUEL QTY. SENSOR TO BE MALFUNCTIONING, REPLACED PART IAW MANUFACTURERS RECOMENDATIONS, PERFORMED AN OPERATIONSDR T2BA1Pitot System · contaminatedWHILE EN ROUTE FROM AUA TO DED, PILOT REPORTED DURING CLIMB AND DESCENT, ALTIMETER AND VSI WAS ACTING ERRATIC. UPON ARRIVAL TO DED, THE PITOT STATIC SYSTEM WAS TESTED IAW MANUFACTURES RECOMMENDATIONS AND COULD NOT REPRODUCE PROBLEM ON THE GROUND. AIRCRAFT WASDR FFS2005F00000Windshield · brokenPILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED DURING CRUISE AT FL250, OUTSIDE AIR TEMPERATURE OF -35 DEGREES C WITH THE WINDSHIELD HEAT ON. THE CRACKS APPEARED SUDDENLY ALL OVER WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE UNKNOWN. (AL0120040542SDR FFS2004F00002Windshield · failedPILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED DURING CRUISE AT FL250, OUTSIDE AIR TEMPERATURE OF -35 DEGREES C. WITH THE WINDSHIELD HEAT ON. THE CRACKS APPEARED SUDDENLY AL OVER WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE UNKNOWN. (AL012004054SDR CA041004003Disc · fractured(CAN) ON PUSH BACK INTO THE HANGAR AN UNUSUAL NOISE WAS HEARD FROM NR 2 MAINWHEEL. ON REMOVING THE MAIN WHEEL, A SECTION OF THE STATIONARY DISC FELL OUT OF THE BRAKE ASSEMBLY. WHEN THE BRAKE ASSY WAS REMOVED THE REST OF THE STATIONARY DISC WAS REMOVED WITHOUTSDR ACE09242004Duct · contaminatedUNUSUAL ODOR EMANATING FROM AIR DUCTS WHEN BLEED AIR SYSTEM TURNED ON. RETURNED TO AIRPORT FOR INVESTIGATION, MAINTENANCE RECONNECTED MAIN HEATER DUCT IN BELLY (BELLY HAD CARGO SPILL RESIDUE IN AREA).SDR FFS2004F00003Windshield · failedCOPILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED AFTER THE AIRCRAFT LEVELED OFF AT FL240, OUTSIDE AIR TEMPERATURE OF -37 DEGREES C WITH THE WINDSHIELD HEAT OFF. THE CRACKS APPEARED SUDDENLY ALL OVER, WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE, USDR ACE0910204Pump · rupturedPILOT REPORTED FUEL LEAKING FROM LT ENGINE OB LOWER DRAIN. REPLACED LOW PSI FUEL PUMP DUE FAILED PRESSURE RELIEF DIAPHRAGM.SDR FFS2004F00004Latch · brokenTHE AFT UPPER CAMLOCK LATCH WAS BROKEN. THE SHAFT ROTATED PROPERLY AS THE DOOR HANDLE WAS ROTATED TO THE LOCK POSITION, BUT APPROXIMATELY HALF OF THE LIP OF THE CAMLOCK WAS MISSING MAKING IT UNABLE TO CAPTURE THE LATCH POST. TOTAL TIME ON PART UNKNOWN.SDR ACE09042004Spar · corrodedWHILE REPAIRING A FUEL LEAK IN THE RIGHT WING MAIN FUEL TANK, FOUND CORROSION ON THE MAIN SPAR LOWER CAP FORWARD FLANGE REQUIRING MAJOR REPAIR. THIS AREA WAS IDENTIFIED AS A SUSPECT CORROSION LOCATION IN RAYTHEON COMMUNIQUÉ NR 71.SDR ACE08282004Stringer Clip · missingDURING SCHEDULED STRUCTURAL INSPECTION OF THE AREA, FOUND STRINGER CLIP PN. 114-430066-5 NEVER INSTALLED AND THE BULKHEAD AT FS 363.25 HAD CRACKS IN THE FLANGE ABOVE AND BELOW THE MISSING CLIP LOCATION.SDR ACE082304Limit Switch · out of adjustPILOT REPORTED LANDING GEAR HANDLE WARNING LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. CREW RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR UP LIMIT SWITCH FOR PROPER OPERATION.SDR CA040810004Line · worn(CAN) WHEN INSTALLING INSPECTION PANEL ON LT OB NACELLE FOUND FUEL LINE FROM FUEL BOWL FORWARD TO ENGINE WAS CHAFING ON BULKHEAD IN SIDE OF NACELLE. THE LINE WAS WORN ABOUT A QUARTER OF ITS WALL THICKNESS.SDR ACE071504Roll Pin · shearedPIREP - COCKPIT DOOR HANDLE DOES NOT WORK FROM OUTSIDE. REPLACED SHEARED DOOR HANDLE ROLL PIN.SDR ACE071204Skin · corrodedMAINTENANCE OBSERVED DEFORMATION OF FUSELAGE SKIN AT LAP JOINTS AT STATIONS 348.25 & 430.75 UNDER STRINGER 16. REPAIRS MADE INCLUDED REMOVAL OF EXFOLIATED SHIMS AND FAILED BONDING AGENT. PREVIOUS REPAIRS OF THIS TYPE AND ON THIS MODEL HAVE DISCLOSED PRIOR USSDR CA040707002Filter · separatedDURING SCHEDULED INSPECTION OF THE INLINE HYD FILTERS (INSTALLED USING RAYTHEON KIT NR 114-8022-1S) IT WAS DISCOVERED THAT TWO OF THE FILTERS HAD SEPARATED FROM THERE CONICAL END AND HAD MIGRATED DOWN THE HYD RETURN LINE ABOUT 2 INCHES FROM THERE NORMAL POSITISDR ACE062804Windshield · crackedPILOT REPORTED LEFT WINDSHIELD CRACKED ONE HALF HOUR INTO FLIGHT. RETURNED TO ORIGINAL AIRPORT.SDR 2004F00350Windshield · crackedPILOT'S OUTER WINDSHIELD PANE CRACKED. CRACKING OCCURRED DURING THE CRUISE PHASE OF THE FLIGHT AT FL 240 WITH WINDSHIELD HEAT ON. CRACKS DEVELOPED FROM LOWER INBOARD CORNER OF WINDSHIELD AND SPREAD UPWARD AND ACROSS THE AREA INCORPORATING THE HEATING ELEMENTSDR 173041Clamp · looseRIGHT FIRE HANDLE FLICKERING INTERMITTENTLY IN FLIGHT. REMOVED TOP AND SIDE COWLS, INSPECTED FIRE LOOP ASSY AND CLAMPS REPOSITIONED AND SECURED LOOP ASSY PER MM 26-10-01, PERFORMED LAMP TEST, OP CHECKED GOOD.SDR ACE060204Relay · contaminatedPILOT REPORTED LANDING GEAR DID NOT EXTEND WHEN HANDLE WAS SELECTED DOWN. ALTERNATE HAND PUMP EXTENSION PERFORMED, FERRY WITH GEAR DOWN FOR REPLACEMENT OF MS24171D1 POWER PACK RELAY (CONTAMINATED WITH WATER).SDR ACE052804Relay · contaminatedPILOT REPORTED LANDING GEAR DID NOT EXTEND WHEN HANDLE WAS SELECTED DOWN. ALTERNATE (HAND PUMP) EXTENSION PERFORMED. REPLACED HYDRAULIC MOTOR RELAY (CONTAMINATED WITH WATER).
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