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 = '1900D' 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 = '1900D' 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 CA160203021Connector · broken(CAN) ON DEPARTURE, THE CREW REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER DEPARTURE WHEN THE HANDLE WAS SELECTED TO THE UP POSITION. 3 GREEN LIGHT EXTINGUISHED BUT THE RED LIGHT REMAINED ILLUMINATED IN THE HANDLE. THE GEAR HANDLE WAS SELECTED TO THE DOWN POSDR CA160202001Actuator · cracked(CAN) LEFT MLG END CAP INSPECTION CARRIED OUT INDICATION OF CRACK FOUND BY NDI. LEFT MLG ACTUATOR REPLACED.SDR CA160118009Switch · faulty(CAN) MAINTENANCE WERE UNABLE TO SILENCE LANDING GEAR WARNING HORN ONCE ACTIVATED. TROUBLESHOOTING REVEALED THAT THE RT MLG SWITCH ASSY, A108 WAS AT FAULT. THE SWITCH ASSLY WAS REPLACED. SUCCESSFUL GEAR SWINGS WERE CARRIED OUT AND SYS FUNCTION TESTED SERVICEASDR GLBA2016011900564Cable · brokenPILOT REPORTED THAT THE FWD DOOR SNUBBER WAS INOPERATIVE. MX FOUND THE COUNTER BALANCE CABLE BROKEN, DISCONNECTED & REMOVED BOTH ENDS. INSTALLED NEW CABLE ASSEMBLY. OPS CHECKED GOOD.SDR CA160118013Spar Cap · corroded(CAN) DURING PLATE NUT INSPECTION AT OTBD LT HORIZONTAL STABILIZER, CORROSION WAS FOUND ON LOWER SPAR CAP AT PLATE NUTS AND 2 FASTENERS JUST INBD OF CENTER ELEVATOR HINGE ARM. AFTER INSPECTION CORROSION WAS FOUND ON LOWER OTBD AND UPPER CENTER SPAR CAPS. REPSDR CA160120010Truss · cracked(CAN) DURING A H-CHECK NDT INSPECTION OF AN ENGINE MOUNT IAW MFG RECOMMENDATIONS A SUSPECT CRACK WAS INDICATED IN 1 OF THE WELDED AREAS. THE SUBJECT ENGINE TRUSS WAS REMOVED AND SENT TO AN APPROVED VENDOR FOR REPAIR. DURING THE INSPECTION/REPAIR PHASE THE VSDR CA160118004Actuator · worn(CAN) DURING A DAILY INSPECTION, THE RT FLAP WAS FOUND TO HAVE EXCESSIVE PLAY. UPON INSPECTION FOUND INBD FLAP ACTUATOR HAD EXCESSIVE END PLAY AND WAS REMOVED FOR REPAIR. DURING TEARDOWN IT WAS FOUND THAT THERE WERE INTERNAL INCORRECT PARTS. ACTUATOR REPAIRESDR CA160106007Support Bracket · damaged(CAN) GPU POWER PLUG AND STRUCTURAL SUPPORT BRACKET FOUND DAMAGED DURING LINE INSPECTION. GROUND POWER STRUCTURAL BASE BRACKET REPAIRED. REPAIR PORTION OF BRACKET MADE FROM NEW PART.SDR CA160108008Skin · damaged(CAN) LT AND RT L/E SKINS FOUND DAMAGED AT HSS 5.00. LY L/E SKIN AND DOUBLER AT HSS 5.00 REPAIRED. DAMAGE SKIN AND DOUBLER TRIMMED AWAY. SKIN INSERTION MADE FROM 2024-T3-.032. DOUBLER INSERTION FROM 2024-T3-.040. REPAIR REINFORCEMENT INNER DOUBLERS MADE FSDR CA151229020Spar Cap · cracked(CAN) DURING COMPLETION OF AN I-CHECK AND AD2013-24-03, CRACKING IN VERTICAL STABILIZER. MAINTENANCE DISCOVERED THAT BOTH LT AND RT VERTICAL STABILIZER. SPAR CAPS WERE FOUND CRACKED AT UPPER HOLES. ALSO, BOTH HAT SECTIONS WERE ALSO CRACKED WHICH WILL BE MISDR CA151223007Proximity Switch · out of adjust(CAN) ON APPROACH CREW REPORTED RT MAIN GEAR WAS NOT INDICATING DOWN AND LOCKED WHEN IN THE AIR AND GEAR HANDLE IS IN THE DOWN POSITION. CHECKLIST PROCEDURES CARRIED OUT AND ACFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO INVESTIGATE THE ISSUE. TSDR GLBA2015122100561Bolt · unsecurePILOT REPORTED THAT A BOLT FELL OUT OF THE AIR STAIR DOOR COUNTER BALANCE. REPLACED THE BOLT & WASHER.SDR CA151221008Uplock Switch · corroded(CAN) CREW REPORTED LANDING GEAR INDICATION CIRCUIT BREAKER POPPED. LOST THREE (3) GREEN INDICATION. CREW FOLLOWED CHECKLIST, RESET CB, 3 GREEN INDICATION WAS EVIDENT AND ACFT LANDED WITHOUT INCIDENT. ACFT WAS INSPECTED BY MAINTENANCE AND IT WAS DISCOVERED TSDR GLBA2016010600563Doubler · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, MX FOUND THE RT SIDE WALL AT FS 163.97 & STRINGER 9 AR, REPAIR DOUBLER CRACKED. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-019. MATERIALS UTILIZED ARE INCLUDED IN THE EO.SDR GLBA2015122100562Annunciator · inoperativePILOT REPORTED THAT ON GEAR EXTENSION, RT MAIN H FAILED TO ILLUMINATE, RT ANNUNC ILLUMINATED AS NORMAL. PRECAUTIONARY RAN CHECKLIST & ALL ILLUMINATED. OPERATIONS CHECKED NORMAL. TROUBLE SHOT SYS, R & R MLG 3 GREEN ANNUNC ASSEMBLY IAW BMM 31-10-00. PN 90-412SDR CA151221001Keelbeam · cracked(CAN) INBD KEEL WEB FLANGE, PN: 114-980024 OF RT NACELLE FOUND CRACKED APPROXIMATELY 1.0 IN LENGTH. REPAIR CARRIED OUT. DAMAGED PORTION OF KEEL WEB FLANGE REMOVED 1.25. INSERTION PACKER AND REPAIR ANGLE MADE FROM 2024-T3, 0.063" ALUMINUM. ALL REPAIR MADE SDR CA151218003Display · malfunctioned(CAN) ELECTRICAL BURNING ODOR WAS DETECTED DURING FLIGHT, ISAT SYS CONTROL PANEL WAS SUSPECTED THE SOURCE. ISAT CIRCUIT BREAKER PULLED. ISAT CONTROL HEAD INSPECTED AND FOUND BURNED INTERNALLY. CONTROL HEAD REPLACED, TEST FOUND SERVICEABLE.SDR CA151207007Packing · leaking(CAN) DURING REPLACEMENT OF AN ENGINE OIL FILTER MAINTENANCE FOUND A BATCH OF AS3209-224 RINGS, ENGINE OIL FILTER, THE ONE THAT GOES AROUND THE OUTSIDE OF THE FILTER, THAT ARE THE INCORRECT SIZE. THE CORRECT SIZE FOR AN AS3209-224 IS 1.75 ID AND 2 OD. LOT 150SDR CA151201011Switch · out of adjust(CAN) WHILE ENROUTE THE CREW NOTICED THE, CARGO DOOR, ANNUNCIATOR HAD ILLUMINATED. THE CREW ELECTED TO DIVERT TO AIRPORT AS MAINTENANCE PERSONNEL WERE AVAILABLE TO ASSESS THE SITUATION. THE ACFT LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND THE ASDR CA151130011Switch · out of adjust(CAN) ON A FLIGHT THE CREW NOTICED THE, CABIN DOOR, WARNING LIGHT WAS ILLUMINATED. THE CREW ELECTED TO RETURN TO THE AIRPORT AS MAINTENANCE WAS AVAILABLE AT THIS STATION. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND SWITCH, PN: MSDR CA151202004Engine · overtemp(CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING AN IN FLIGHT-SHUTDOWN IFSD, THE ENGINE TEMPERATURE CLIMBED BEYOND NORMAL OPERATING LEVELS. NO OVERTEMP EVENT WAS RECORDED. THE OPERATOR ALSO REPORTED FOD AND A GRINDING NOISE WHEN ROTATING THE COMPSDR CA151210006Stringer · corroded(CAN) DURING A SCHEDULED FUEL TANK INSPECTION UTILIZING X-RAY THE FOLLOWING DEFECTS WERE NOTED. LEFT LOWER STR CORRODED BETWEEN LT WING STA 114-124 AT 39.5 PERCENT CHORD. RT AFT FLANGE OF FWD WING SPAR CORRODED BETWEEN RT WING STA 114-124 -LT FUEL STRAINER BSDR CA151125009Duct · cracked(CAN) BRAKE DEICE WARNING ILLUMINATED IN FLIGHT. FOUND CRACK ON BLEED AIR DUCT 129-550067-1 CAUSING EVA TUBE TO MELT AND TRIGGER LIGHT.SDR CA160106002Switch · out of adjust(CAN) CREW REPORTED A DOOR UNSAFE LIGHT ON DEPARTURE. THE CREW CANCELLED IFR AND RETURNED TO THE AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO INSPECT THE ACFT. AFTER INSPECTING THE ACFT THE CARGO DOOR SILL SWITCH WAS FOUND OUT OSDR GLBA2015111700560Warning System · false activationPILOT REPORTED THAT WHILE IN CRUISE, THE DISCHARGE LIGHT ON THE NR 1 FIRE EXTINGUISHER ILLUMINATED. REPLACED SOFT SPLICE, PN M81714/11-20D, ON WIRE W23B22 IAW EO 13-1900-26-001. OPERATIONAL CHECK OF DISCHARGE INDICATION GOOD.SDR GLBA2015111600558Bolt · unsecurePILOT REPORTED THAT THE DOOR SNUBBER BOLT CAME OFF. APPLIED LOCTITE 242 TO THE BOLT THREADS & REINSTALLED THE BOLT IAW TC 1900-5210 01 STEP 13. OPERATIONAL CHECKED GOOD.SDR CA151201010Oil System · pressure loss(CAN) THE AIRCRAFT WAS ON A FLIGHT AND WAS DIVERTED DUE TO LOSS OF OIL PRESSURE. THE PILOT NOTICED THE OIL PRESSURE DROPPING OFF LINE AND THE TQ WAS FLUCTUATING. THE ENGINE AUTO FEATHERED ON ITS OWN AND THE PILOT SHUTDOWN THE ENGINE. THE ACFT DID AN UNEVENTFULSDR CA151116009Frame · cracked(CAN) DURING STRUCTURAL INSPECTION A-CHECK ITEM 37, WHICH STATES AT FS 288 CHECK FOR STRESSED AND MISSING FASTENERS ON THE LOWER FUSELAGE BULKHEAD, PN 114-430094-13 OR -15. PERFORM AN NDI EDDY CURRENT CHECK ON SPECIFIC FASTENERS ON THE LT AND RT SIDE OF THE BSDR GLBA2015110900557Spar Cap · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR LOWER WING SPAR CAP FROM WING STATION 215.08 - 310. CORROSION ON THE AFT FLANGE GOING UP ON THE TEE. REPAIRED IAW EO 15-1900-57-003.SDR GLBA2015110900556Spar · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR WING SPAR OTBD WEB CORRODED. REPAIRED IAW EO 15-1900-57-003.SDR 7C7A20151104094Stringer · debondedDIS-BOND STRINGER IN THE CENTER FUSELAGE, STRINGER 15R. REPAIRED IAW FR-CO-106062 REV 1.SDR CA151121002Wire Harness · burned(CAN) PILOT REPORTED LT PROPELLER HEAT AMPERAGE INDICATING "LOW". UPON FURTHER EXAMINATION/TROUBLESHOOTING, MAINTENANCE DISCOVERED THE PROP HEAT WIRING HARNESS HAD NO PROTECTIVE SHEATHING INSTALLED. WITH NO PROTECTIVE SHEATHING , THE WIRE RUBBED AGAINST THE SSDR CA151106006Actuator · binding(CAN) AFTER LANDING THE FLIGHT CREW PERFORMED THE AFTER LANDING CHECKLIST AND SELECTED THE FLAPS TO FULL UP POSITION THEY NOTICED THAT THE INDICATOR STOP AT THE 15 DEGREE SETTING. AFTER PARKING THE ACFT THE FLIGHT CREW CHECKED THE FLAPS AND FOUND THEM AT OR LSDR GLBA2015100500555Connector · dirtyPILOT REPORTED THAT THE NR 1 ENG EXTINGUISHER ANNC DISCHARGE NR 1 LIGHT ILLUMINATED, ON CLIMB OUT. FOUND NO CONTINUITY BETWEEN PIN M OF CONNECTOR P281 & THE FIRE BOTTLE SQUIB, CLEANED CONNECTOR P281, OPERATIONS CHECKED GOOD.SDR CA151103008Angle · out of position(CAN) THE PILOT REPORTED THAT THE LT ENGINE WOULD ONLY STAY IN FEATHER IF THE PROP CONTROL LEVER IS HELD DOWN. IT WAS NOTED THAT THE AUTO FEATHER SYS TESTED SERVICEABLE. THE CLIP ITEM, NR 18 AS DEPICTED WAS INCORRECTLY POSITIONED ON THE FWD SIDE OF THE BRACKSDR CA151102008Shaft · sheared(CAN) ELEVATOR TRIM ISSUE IN FLIGHT. TRIM ACTUATOR SHAFT FOUND SHEARED.SDR CA151031004Gearbox · damaged(CAN) ON THE CLIMBOUT THE CREW OBSERVED ABNORMAL TORQUE AND ITT INDICATIONS. AS A PRECAUTION, THE CREW ELECTED TO SHUTDOWN THE LT ENGINE. THE ACFT RETURNED WHERE AN UNEVENTFUL LANDING WAS CARRIED OUT. FLIGHT CREW REPORTED NOISE CAN BE HEARD COMING FROM THE ASDR CA151027001Engine · power loss(CAN) FLIGHT CREW NOTICED LT BLEED FAIL DURING TAKEOFF, JUST AFTER, THE LT TORQUE DECREASED ALONG WITH THE LT PROP RPM. THE ITT STARTED TO INCREASE BEFORE THE CREW SHUTDOWN THE ENGINE. ACFT RETURNED BACK TO THE AIRPORT WITHOUT ANY FURTHER INCIDENT, THE ENGINSDR CA151022010Sensor · dirty(CAN) AFTER TAKEOFF WHILE ENROUTE AND CLIMBING THROUGH 3500 ASL, THE CARGO DOOR LIGHT AND MASTER WARNING ILLUMINATED. A DECISION WAS MADE TO RETURN PROMPTLY SUSPECTING POSSIBILITY OF BEING MORE THAN JUST A FAULTY SENSOR. AFTER CONFERRING WITH ATC THE CREW REQSDR CA151019007Line · cracked(CAN) LINE CRACKED AT FLARED AREA.SDR CA151016009Line · cracked(CAN) BLEED AIR LINE CRACKED AND SEPARATED AROUND FLANGE AREA THAT MOUNTS TO LT ENGINE FIRE WALL CAUSING BLEED AIR FAIL INDICATION.SDR V0DR20151013004Slip Ring · bulgedRECEIVED PROPELLER ASSEMBLY HC-E4A-3J TO REPAIR A LEAK. THE TECHNICIAN REPORTED THAT DURING DISASSEMBLY THE DIELECTRIC FILLER AROUND THE OUTER COPPER RING HAS DETERIORATED, CRACKED OUT, & THAT THE OUTER COPPER RING WAS LIFTED OR BULGED CAUSING THE SLIP RING RSDR CA151014001Relay · failed(CAN) ON APPROACH THE CREW INDICATED THEY HAD A LANDING GEAR ISSUE, GEAR WOULD NOT EXTEND. THE CREW ABORTED THE APPROACH AND MANUALLY EXTENDED THE GEAR AND LANDED WITHOUT INCIDENT. INSPECTION BY MAINTENANCE REVEALED THAT THE LANDING GEAR MOTOR RELAY WAS AT FSDR CA151013006Panel · burned(CAN) AFTER STARTUP, THE CREW NOTICED WHAT SEEMED TO BE ELECTRICAL BURNING ODOR COMING FROM OVERHEAD AIR GASPER. THE CREW AGREED ON CALLING FOR TAXI TO SEE IF THE ODOR WOULD DISAPPEAR. PRIOR TO LEAVING THE GATE, AS AN EXTENDED PRECAUTION THE CREW REVIEWED THSDR CA151001004Rod · broken(CAN) AFTER TAKEOFF, LANDING GEAR WAS SELECTED UP. THERE WAS LOUD BANGING NOISE COMING FROM THE NOSE GEAR AREA. THE GEAR INDICATED UP, HOWEVER SHORTLY AFTER THE LANDING GEAR UNSAFE LIGHT ILLUMINATE. DURING CLIMB WE SELECTED GEAR DOWN. THE GEAR INDICATION WSDR CA151215016Engine · damaged(CAN) DURING THE INITIAL APPLICATION OF POWER FOR TAKEOFF, A POPPING NOISE, ALONG WITH A SLIGHT SHUDDER, WAS FELT. TAKEOFF WAS ABORTED IMMEDIATELY AND THE ACFT RETURNED TO THE APRON FOR THE PASSENGERS TO DEPLANE. POST EVENT INSPECTION FOUND A SEIZED PROPELLESDR CA150928006Engine · failed(CAN) THE ACFT WAS TAXIED TO RUNWAY AND DURING THE INITIAL APPLICATION OF POWER FOR TAKEOFF, A POPPING NOISE, ALONG WITH A SLIGHT SHUDDER WAS FELT. TAKEOFF WAS REJECTED IMMEDIATELY AND ACFT RETURNED. MAINTENANCE CONSULTED AND BACK UP ACFT DISPATCHED. MAINTESDR GLBA2015092900550Clevis · bentDURING A MX INSPECTION, FOUND THAT THE AIRSTAIR DOOR LOWER FWD HANDRAIL CABLE CLEVIS WAS BENT. R & R THE CABLE ASSEMBLY IAW BMM 52-10-02. PN ON & OFF 1440-43GLA.SDR CA150925016Acm · leaking(CAN) WHILE IN CRUISE FLIGHT, AT FLIGHT LEVEL 210 THE CREW NOTICED A RAPID ONSET OF SMOKE ODOR AND HAZE IN THE COCKPIT. ATC WAS NOTIFIED AND THEN THE PASSENGERS. THE CREW THEN DIVERTED TO THE NEAREST AIRPORT AS A PRECAUTION. THE CREW DID NOT DECLARE AN EMERGSDR GLBA2015092200548Bulkhead · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND 2 CRACKS AT CANT BULKHEAD, AT FS 588.10 AT JUNCTION WITH STRINGER 8R, CANT BULKHEAD AT FIRST FASTENER TOP SIDE AT STRINGER 8R & AT FIRST FASTENER BELOW STRINGER 8R, BOTTOM CRACK RADIATES UPWARD & DOWNWARD FROM
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