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 GLBA20061079Wire · detachedSMOKE/FUMES, FLIGHT 5061 AIR RETURN, PILOTS REPORTED THAT WHILE CLIMBING THROUGH 21.5 FOR 240 THEY NOTICED AN ELECTRICAL FUME ODOR. PILOTS PERFORMED WINDSHILED FAULT EMERGENCY CHECKLIST. TURNING OFF WINSHIELD ANTI-ICE GOT RID OF THE FUMES. MAINT SECURED A LOOSSDR GUUA03010803Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINT, DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.SDR GUUA03010802Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINT, DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE BRACKET.SDR GUUA03010801Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINT DISCOVERED LT CTR ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET.SDR GLBA20061075Frame · crackedFUSELAGE FRAME CRACKED .5 NR AT FS 163.9 AND STR 9R MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 163.9 STRINGER 9R IAW SRM REF. 51-70. REPAIR APPROX 5.5 X 2.5 2024-T3 .071. RII INSP COMPLIED IAW TASKCARD 8.2.1.SDR GLBA20061076Frame · crackedFUSELAGE FRAME CRACKED .5 INCH AT FS 183 AT STRINGER 9R. MAINT REPAIRED FRAME CRACK AT STR RELIEF HOLE FS 183, STRINGER 9R IAW SRM REF 51-70. REPAIR APPROXIMATELY 5.5 INCH X 2.5 2024-T3 .071. RII INSPCOMPLIED WITH IAW TASKCARD 8.2.1.SDR GUUA02240801Cable · failedPILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN. REPLACED UPPER AIRSTAIR DOOR CABLES.SDR GLBA20061073Stringer · debondedSTRINGER 9L DISBONDED AT FS 243.25 TO FS 258.25. MAINT REPAIRED DISBONDED STRINGER 9L AT FS 243.25 TO FS 258.25 IAW SRM 53-90. REPAIR APPROX 10.5 INCH. 2024 T3. RII INSP C/W IAW TASKCARD 8.2.1.SDR GLBA20061072Skin · crackedFUSELAGE SKIN CRACK IN/AT PREVIOUS REPAIR CRACK APPROX 1 INCH LENGTH AT FS 248.0 ABOVE STR 9L. MAINT REPAIRED FUSELAGE SKIN AT FS 248.0 IAW SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 14 FT BY 12.5 FT, 2024 T3 .040. RII INSP C/W IAW TASKCARD 8.2.1.SDR GLBA20061070Frame · cracked02/18/08, FRAME CRACKED AT STR 9R CUTOUT. CRACK APPROX .500 IN LENGTH AT FS 177.35. MAINT REPAIRED FRAME CRACK AT STR RELIEF HOLE AT FS 177.35 AND STR 9R IAW SRM 51-70. REPAIR APPROX 5 INCH X 2.5 INCH 2024 T-3 .071. RII INSP C/W IAW TASKCARD 8.2.1.SDR GLBA20061059Angle · crackedLT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 1.750 AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW. SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED IAW TASKCARD 8.2.1.SDR GLBA20061060Angle · crackedRT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 2.125 INCH AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1.SDR CA080214005Drive Shaft · seized(CAN) FLAPS WOULD NOT RETRACT AFTER TAKEOFF AND CIRCUIT BREAKER OPENED. AIRCRAFT RETURNED TO AIRFIELD. FLAP DRIVE SHAFT WAS FOUND SEIZED AND BOUND UP NEAR MOTOR. MOTOR AND DRIVE SHAFT WERE REPLACED. (TC NR20080214005)SDR GLBA20061069Fire Loop · faultyENG SHUTDOWN- FLIGHT NR 5067 ENROUTE, THE PILOTS SHUTDOWN AND SECURED THE NR 2 ENGINE IN FLIGHT, DUE TO A NR 2 FIREWALL FUEL VALVE HANDLE THAT ILLUMINATED DURING FLIGHT. MAINT REMOVED AND REPLACED THE NR 2 ENG FW FIRELOOP IAW MM 26-10-01. OPS CHECK OF THE SYS SDR CA080220008Engine · seized(CAN) SHORTLY AFTER TAKEOFF, WHEN SELECTING BLEED AIR ON, THE CREW HEARD TWO (2) LOUD BANGS FOLLOWED BY SEEING SPARKS FROM THE EXHAUST. PILOT SECURED THE ENGINE AND RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSP REVEALED A SEIZED PROP AND IMPACT DAMAGE INSSDR GLBA20061068Skin · corrodedBELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND STRINGERS 13L TO 15R. MAINT REPAIRED BELLY SKIN 15R TO 13L AT/FROM FS 213.25 TO FS 228.25 IAW SRM 51-70. REPAIR DIMENSION 26.250 INCHES X 33.5SDR GLBA20061067Frame · crackedFRAME AT FS 177.35 AND STR 9R CRACKED APPROX .500 INCHES IN LENGTH. **SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR**SDR GLBA20061066Frame · crackedFRAME AT FS 163.97 AND STR 9L CRACKED APPROX .40 INCH IN LENGTH. RII REQUIRED TC 8.2.1. MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE F.S. 163.97 AND STRINGER 9L IAW SRM 51-70. REPAIR APPROX 5 INCHES X 2.7 INCHES. 2024-T3 .071. RII C/W IAW TC 8.2.1SDR GLBA20061065Skin · corrodedBELLY CORROSION FS 213.25 AND FS 228.25 AT STRINGERS 15R, 16R, 14L/13L AT FS 213.25 AND 15L/14L AT FS 228.25. MAINT REPAIRED DEBONDED STR 15R,15L,14L, FOR FS 213.25 TO FS 228.25 IAW SRM 53-90. STR REPAIR DIMENSIONS APPROX 10.5 INCHES. 2024 T-3. RII C/W IAW TASDR 20061068Skin · corrodedBELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND STRINGERS 13L TO 15R. OPENSDR 20061067Frame · crackedFRAME AT FS 177.35 AND STRINGER 9R CRACKED APPROX .500 INCH IN LENGTH. OPENSDR 20061066Frame · crackedFRAME AT FS 163.97 AND STR 9R CRACKED APPROX .40 INCH IN LENGTH - RII REQUIRED TC 8.2.1. OPENSDR GUUA02100801Bleed Air Sys · contaminatedFLIGHT: 5401, DURING FLIGHT, FUNKY SMOKE ODOR IN THE COCKPIT WITH BLEED OPEN. CLEANED RESIDUAL OIL, FROM OIL SERVICING.SDR GUUA02090801Latch · brokenDURING SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT DOOR TOP CAM BROKEN. REPLACED EMERGENCY EXIT ARM LATCH ASSY.SDR GUUA02070802Arm · brokenDURING SCHEDULED ROUTINE MAINT, DISCOVERED THE LT EMERGENCY EXIT ARM ASSY BROKEN. REPLACED LT EMERGENCY EXIT ARM ASSY.SDR GUUA02070801Door · delaminatedFLIGHT: 5402, PILOT REPORTED LT EMERGENCY EXIT IS DELAMINATED. REPLACED LT EMERGENCY EXIT.SDR AMWA89978Control Head · smokeDURING SHORT FINAL APPROACH, SMOKE WAS DETECTED COMING OUT OF THE NR1 NAV CONTROL HEAD. THE NR1 NAV CB'S WERE PULLED, THE SMOKE STOPPED AND AC LANDED WITHOUT FURTHER INCIDENT. MAINT REMOVED AND REPLACED CONTROL HEAD AND CLEARED DISCREPANCY. SUBSEQUENT TEARDOWNSDR GUUA02060801Actuator · bypassingFLIGHT: 9149, DURING FLIGHT DC LOAD METERS BOTH SPIKE 20 PERCENT EVERY 20 SECONDS. REPLACED THE RT MLG ACTUATOR.SDR GUUA02020801Door · unsecureFLIGHT: 9179, PILOT REPORTED: DISCOVERED LT EMERGENCY EXIT DOOR APPEARS UNSECURE. RIGGED LT EMERGENCY EXIT DOOR.
SDR GUUA01310801Cam · out of adjustAT SCHEDULED INSPECTION, DISCOVERED AIRSTAIR DOOR WILL NOT LATCH WHEN CLOSED. ADJUSTED CAM ON DOOR.SDR GLBA20061054Engine · deterioratedENGINE SHUTDOWN, FLT 5041 ENROUTE 10 MILES OUT ON FINAL THE NR1 ENGINE FEATHERED INFLIGHT AND THE PILOTS PERFORMED THE ENG SECURE PROCEDURES AND SHUTDOWN THE ENG MAINT REMOVED AND REPLACED THE NR1 ENG ASSY IAW TASKCARD NR 1900-7100.00. RII INSP COMPLIED WITH.SDR GUUA01290801Skin · corrodedAT SCHEDULED INSP, DISCOVERED EXFOLIATED SECTION OF SKIN AT FS 318.250 STR 15L. REMOVED EXFOLIATED SECTION OF SKIN FABRICATED AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 51-70-06.SDR NSVA2008003Light · intermittentRIGHT "T" HANDLE FLICKERS MULTIPLE TIMES IN FLIGHT. INSPECTED RT ENG FIRE LOOP, NO DEFECTS NOTED AT THIS TIME. PERFORMED FIRE HANDLE TEST IAW BEECHCRAFT AMM 26-10-01-101.SDR AMWA89766BCBattery · dischargedAFTER TAKEOFF, BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.SDR SJ3R080124001Cam Follower · brokenREMOVED DUE TO SUSPECTED INTERNAL HUB COMPONENT FAILURE. BLADE S/N 4152 WAS FOUND TO ROTATE FREELY +/- 12.5 DEGREE POST FIRST GROUND RUN AFTER INSTALLATION. INSPECTION AFTER DISASSEMBLY REVEALED ONE BROKEN B-6545 PITCH CHANGE KNOB CAM FOLLOWER. THIS PART WASSDR GUUA01230801Circuit Breaker · poppedFLIGHT: 9167, DURING APPROACH WHEN SELECTING THE LANDING GEAR DOWN THE LANDING GEAR CB FOR THE MOTOR POPPED. INSPECTED THE LANDING GEAR SYS, PERFORMED LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK NORMAL.SDR 938012108ASkin · crackedAT SCHEDULED INSPECTION, DISCOVERED ONE INCH LATERAL CRACK IN FUSELAGE BELLY SKIN IN SPAR AREA AT BL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REF SRM 53-90-18, (FUSELAGE SKIN CRACK REPAIR IN SPAR AREA).SDR GUUA01210801Skin · crackedAT SCHEDULED INSPECTION, DISCOVERED A 1.0 INCH CRACK BETWEEN FS 230.75 AND 310.75 AT BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 53-90-18.SDR GUUA01200801Door · lack of lubeFLIGHT: 9257, PILOT REPORTED THE CABIN DOOR WILL NOT SHUT. LUBED CABIN DOOR.SDR 933011308ASkin · crackedAT SCHEDULED INSPECTION, DISCOVERED (2) CRACKS IN FUSELAGE BELLY SKIN AT FS 281, ONE WAS A (2) INCH LATERAL CRACK, AND THE OTHER A ONE INCH LONGITUDINAL CRACK, STOP DRILLED CRACKS AND INSTALLED ONE EXTERNAL DOUBLER OVER BOTH CRACKED AREA. REFERENCE SRM 53-90-SDR GUUA01130801Uplock Switch · out of adjustAFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT ON WHEN GEAR HANDLE PLACED IN THE UP POSITION. DIVERTED AND LANDED WITHOUT INCIDENT.
ADJUSTED NOSE LANDING GEAR UPLOCK SWITCH.SDR AMWA89563BCPcb · malfunctionedBATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINT REPLACED PCB A130 AND CLEARED DISCREPANCY.SDR AMWA89557BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.SDR AMWA89551BCGcu · malfunctionedDURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT PARALLELED BOTH GCU'S AND CLEARED DISCREPANCY.SDR CA080116009Bellcrank · cracked(CAN) THE RT POWER LEVER BELLCRANK LOCATED IN THE BOTTOM OF THE PEDESTAL WAS REPLACED DUE TO WEAR. AFTER REMOVAL THE PART WAS FOUND TO BE CRACKED. (TC NR 20080116009)SDR AMWA89439BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE FOUND EACH CELL TO BE LOW VOLTAGE, CLEANED POSITIVE BATTERY TERMINAL CORROSION, RETORQUED CELL LINKS, AND CHARGED BATTERY THEN CLEARED DISCREPANCY.SDR GUUA01050802Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET.SDR GUUA01050801Hinge Bracket · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOILATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.SDR AMWA89426BCBattery · dischargedBATTERY CHARGE ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY.SDR AMWA89415BCGcu · inoperativeBATTERY CHARGE ANNUNCIATOR ILLUMINATED 8 TIMES IN FLIGHT, AMMETER SHOWED DISCHARGE DURING ILLUMINATION (NEEDLE DOWN ON AMMETER). MAINTENANCE PARALLELED GENERATOR CONTROL UNITS AND CLEARED DISCREPANCY.
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