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 20030787Switch · inoperativeUPON APPROACH, LANDING GEAR WAS SELECTED DOWN AND CREW NOTED THAT NOSE GEAR SHOWED NO INTRANSIT OR GREEN DOWN AND LOCKED INDICATION. CREW PERFORMED CHECKLIST AND HAD GEAR VERIFIED BY TOWER GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED SDR CA050202003Relay · burned(CAN) DURING APPROACH, FLIGHT CREW SELECTED GEAR DOWN BUT THE CONTROL CB OPENED AND WOULD NOT RESET. THE LANDING GEAR WAS MANUALLY EXDENDED WITH 3 GREENS. MAINTENANCE FOUND THE LANDING GEAR RELAY WAS BURNED AT THE CONTACTS AREA AND THE RELAY WAS REPLACED. THISDR 68837Brake · failedAFTER TAXI IN LEFT BRAKE WEAK. REMOVED AND REPLACED LT BRAKE.SDR CA050213002Engine · failed(CAN) DURING CRUISE THE ENGINE LOW OIL PRESSURE INDICATOR ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION EVIDENSED NOISE FROM THE REDUCTION G EAG THE PROP. MFG WILL INVESTIGATE THE EVENT AND WILL SUPPLIMENT THIS REPORT TO PROVIDE ROOSDR S2YA05008Processor · failedBEFORE FLIGHT, THE CREW REPORTED BOTH CAPTAIN`S DISPLAY TUBES FAILED, THEY RETURNED TO THE GATE FOR MECHANIC. MECHANIC SWAPPED THE DPU-84 DISPLAY PROCESSORS AND ALL DISPLAYS WERE OPERATIONAL, WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE.SDR CA050201004Engine · failed(CAN) AC HAD DEPARTED, LT LOW OIL PRESSURE LIGHT ILLUMINATED, GAUGE ALSO CONFIRMED PRESSURE AT 50-55. ENG WAS SHUTDOWN AND SECURED. EMERGENCY WAS DECLARED, AC DIVERTED TO NEAREST AIRPORT, LANDED UNEVENTFULLY. MAINT FOUND ENGINE LOW BY 3 LITERS. OIL WAS NOTSDR 2005F00050Seal · tornFLT 9197 - TPA/FLL - DURING FLIGHT, CABIN EXPERIENCED RAPID DECOMPRESSION. PAX OXYGEN MASKS DEPLOYED. DIVERTED TO RSW. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. FOUND AIRSTAIR DOOR SEAL OUT OF TRACK AND TORN AT 12 O'CLOCK POSITION. REMOVED AND REPLSDR 68755Brake Assy · weakON CREWS FIRST FLIGHT CHECKS LEFT BRAKE WAS WEAK. A/C RETURNED TO THE HANGAR. MTC BLED BRAKES AND A/C RETURNED TO SERVICE. BLED BRAKES.SDR 20030785Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.SDR GUUA93353012505ASeat Track · brokenDURING SCHEDULED ROUTINE MX DISCOVERED RT SEAT TRACK FLOOR BOARD ATTACH TAB BROKEN AT FS 238. REPAIRED BROKEN RT SEAT TRACK FLOOR SUPPORT TAB AT FS 238.SDR 2006FA0000152Skin · delaminatedBOTH LT AND RT VENTRAL FINS SHOWED AREAS OF DELAMINATION ON FWD TOP CORNERS. DELAMINATION WAS BEYOND REPAIR LIMITS IAW SRM AND REQUIRED DER APPROVAL. FOUND INNER CORE MATERIAL WET DAMAGE WAS APPARENTLY CAUSED BY FREEZE CYCLES. WATER WAS FOUND ALONG TOP OF FSDR 68657Annunciator · illuminatedAFTER T/O FROM PIT TO DUJ, CARGO DOOR ANNUNCIATOR ILLUMINATED. A/C RETURNED TO FIELD WITH NO FURTHER INCIDENT. NO DAMAGE FOUND ON AIRCRAFT. LOCKED CARGO DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS NOTED.SDR CA050126008Connector · corroded(CAN) DURING APPROACH CREW SELECTED GEAR DOWN HOWEVER, THE GEAR CONTROL C/B OPENED AND WOULD NOT RESET. MANUAL EXTENSION COMPLETED. MAINTENANCE FOUND THE CONNECTOR BEWTEEN THE NOSE GEAR ACTUATOR AND THE FRAME INTERNALLY CORRODED. THE CONNECTOR WAS REPLACED, SDR 200105Annunciator · activatedANNUNCIATOR SERVICE LIGHT ILLUMINATED IN FLIGHT.SDR CA050127003Elbow · fractured(CAN) IMMEDIATELY AFTER STARING DESCENT, CREW NOTED OIL PRESSURE DROPPING FOLLOWED BY WARNING ANNUCIATORS ON LT POSITION. ENGINE CONTINUED TO LOSE OIL PRESSURE AND ENGINE WAS SHUTDOWN AND FEATHERED. MAINT FOUND OIL BOSS (ELBOW) FOR REDUCTION GEAR CASE RETURNSDR 160105Annunciator · activatedCABIN DOOR ANNUCIATOR IN FLIGHT.SDR S2YA05005Solenoid · inoperativeBEFORE FLIGHT, THE CREW REPORTED RT PROP WOULD NOT SPOOL UP, THEY RETURNED TO THE GATE FOR MECHANIC. MECHANIC REPLACED THE RT PROP GOVERNOR FOR TROUBLESHOOTING BUT THE PROBLEM REMAINED. MECHANIC REPLACED THE RT LOW PITCH SOLENOID AND OPERATIONAL CHECKS WERE SDR 20030782Truss · crackedWHILE PERFORMING OTHER NON-RELATED MAINTENANCE, THE LT ENGINE TRUSS WAS DISCOVERED TO BE COMPLETELY CRACKED THRU (360 DEGREES) ON THE LOWER LT TUBE JUST ABOVE THE ATTACH BRACKET FOR THE LOWER ENGINE AIR CAN ASSY, ADJACENT TO THE P3 BLEED LINE. NO OBVIOUS CHAFSDR S2YA05009Valve · inoperativeSHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE MLG HANDLE/SWITCH BUT OPS CHECKS WERE STILL BAD. MECHANIC REPLACED THE GROUND SERVICE VALVE AND PERSDR GUU2005F00001Brake Assy · malfunctionedDURNG TAXI, LT AND RT BRAKES FEEL SPONGY. REQUIRES ADDITIONAL PRESSURE TO APPLY BRAKES. BELD ALL FOUR BRAKES. OPERATIONAL CHECK NORMAL. (K)SDR 68374Indicator · reads lowAFTER T/O AND APPROXIMATELY 10 MINUTES INTO FLIGHT. CREW NOTICED RIGHT HAND ITT INDICATOR DROPPED TO ZERO. TOOK INSTRUCTIONS RTF ABQ LANDED AND TAXIED TO GATE WITH NO FURTHER INCIDENT.SDR 68346Master Cylinder · damagedALL FOUR BRAKE PEDALS SPONGY ON LANDING. REMOVED AND REPLACED RT SIDE OUTBOUND MASTER BRAKE CYCLINDER. P/N 90-380001-33 (OFF), S/N 7984 (ON), P/N 90-380001-33 (OFF), S/N 3119 (OFF).SDR 20030784Window Frame · crackedDURING ROUTINE STRUCTURAL INSPECTION, ALL THREE EMERGENCY EXIT WINDOW PANS WERE FOUND TO HAVE CRACKS AROUND THE RADIUS. WINDOW PANS WERE REPLACED, AIRCRAFT RETURNED TO SERVICE.SDR S2YA05004Bleed Air Sys · malfunctionedBEFORE FLIGHT, THE CREW REPORTED A RT BLEED AIR PROBLEM, THEY CONSULTED WITH MECHANIC WHO INSTRUCTED THE CREW TO RUN THE ENGINES TO LET THE SYSTEM WARM UP. AFTER RUNNING THE ENGINES THE PROBLEM COULD NOT BE DUPLICATED. WITH NO FURTHER DISCREPANCIES NOTED THESDR 68236Brake Assy · icedON TAXI OUT, A/C SLOWED TO A STOP ON THE ACTIVE TAXI WAY ENTERING THE RUNWAY AND WOULD NOT PROGRESS FWD. MX REMOVED ICE FROM THE BRAKES, A/C THEN WAS ABLE TO MOVE AND RETURNED TO GATE WITH NO FURTHER INCIDENT. CLEANED LEFT AND RIGHT BRAKES WITH DEICING FLUIDSDR 20030779Propeller · defectiveWHILE MAINTENANCE WAS PERFORMING A PRE-RELEASE AUTOFEATHER TEST, UNUSUAL VIBRATION WAS NOTED COMING FROM LT ENGINE AND PROP. ENGINE WAS SHUTDOWN WITHOUT INCIDENT AND UPON INVESTIGATION INTERNAL FAILURE WAS OBVIOUS DUE TO BLADE MOVEMENT. PROPELLER REMOVED FROSDR 0107200501Pedestal · fireFLAMES VISIBLE UNDER CENTER PEDESTAL NEAR RUDDER TRIM CONTROL KNOB.SDR S2YA05002Tube · damagedDURING FLIGHT, THE TAIL DEICE BECAME INOPERATIVE. DUE TO ENROUTE WEATHER, THE CREW PERFORMED AN AIR-TURN-BACK. THE SYSTEM WAS INSPECTED AND MECHANIC REPAIRED THE EVA TUBING IN THE LT STABILIZER ABOVE THE LOGO LIGHT. THE SYSTEM WAS INSPECTED AND WITH NO FURTSDR 20030778Axle · crackedRT MAIN GEAR LOWER STRUT AXLE ASSY LUG HAS (2) CRACKS APPROX .05 AND .06 LONG WHERE LOWER TORQUE KNEE ATTACHES TO LUG.SDR GLBA20030776Spar · crackedFOUR CRACKS .4 INCHES LONG EXTENDING FROM DEICE LINE HOLE IN HORIZ STAB MAIN SPAR CENTER WEB, REPAIRED PER EO 04/21 BEECH 1900 SRM 55-91-02SDR 68027Wheel · damagedUPON LANDING ROLLOUT, A COYOTE RAN INFRONT OF THE AIRCRAFT AND WAS STRUCK BY THE NOSE LANDING GEAR. CREW SLOWED AND STOPPED THE AIRCRAFT ON THE APRON WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY, NOSE GEAR ASSY, DRAG LEG ASSY. VISUALLY INSSDR 3651204Governor · malfunctionedLEFT AUTOFEATHER DID NOT ARM ON TAKEOFF.SDR 67974Wire · chafedDEPARTING OMA RETRACTED GEAR, C/B TRIPPED. RESET C/B, GEAR THEN RETRACTED, C/B TRIPPED AGAIN. DID NOT RESET 2ND TIME PER CHECK LIST. DIVERTED TO HON MANUAL EXTENSION. MX THEN SECURED LANDING GEAR AND TOWED A/C TO GATE. REPAIRED CHAFED WIRE ON HYDRO GROUNDSDR 67971Annunciator · failedTAIL DE-ICE ANNUNCIATOR FAILED IN FLIGHT DURING ICING CONDITIONS, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED TAIL DE-ICE SENSOR AND SERVICED TUBES, OPS CHECK GOOD.SDR 67819Brake Assy · smokeAFTER LANDING IN MIA CREW NOTICED LEFT BRAKES SMOKING. CLEANED LEFT MAIN GEAR BRAKE ASSY. CHECK OK AT THIS TIME.SDR CA041220003Relay · shorted(CAN) DURING LANDING PROCESS, GEAR REQUIRED 2 ATTEMPTS FOR EXTENSION. MAINTENANCE FOUND THE LANDING GEAR RELAY, WAS PITTED INTERNALLY PROVIDING INTERMITTENT CONTACTS.THIS OPERATOR HAS EXPERIENCED NUMEROUS FAILURES AT OR ABOVE 8000 HOURS TSN ON THESE RELAYS. ASSDR CA041221004Windshield · cracked(CAN) WHILE IN THE CLIMB, PASSING THROUGH 15000 FT THE CAPTAINS WINDSHIELD CRACKED.THE CREW CARRIED OUT THE APPLICABLE FLIGHT MANUAL PROCEDURES AND RETURNED BACKTO AIRPORT. THE AIRCRAFT WAS LATER FERRIED TO THE MAINTENANCE BASE WHERE THE WINDSHIELD WAS REPLACESDR CA041220002Switch · not closed(CAN) DURING LANDING PROCESS, THE CREW NOTED THAT THE NOSE GEAR DOWN GREEN INDICATION WAS NOT ILLUMINATING. MAINTENANCE FOUND THE INTERNAL SWITCH ON THE ACTUATOR WAS NOT CLOSING PROPERLY AND THE ACTUATOR WAS REPLACED.SDR 67556Brake Assy · weakCREW EXPERIENCED WEAK BRAKING ACTION ON RIGHT SIDE ON TAXI IN WITH NO FURTHER INCIDENT. BLED BRAKES.SDR 67554Yaw Damper · malfunctionedWHEN YAW DAMPER SYS ON, CREW EXPERIENCED A MOMENTARY STIFFNESS IN THE RUDDER PEDALS. CREW SHUT OFF THE YAW DAMPER AND CONTINUED FLIGHT WITH NO FURTHER INCIDENT. PERFORMED TAXI TEST. INSPECTED, OPS CHECK NORMAL AT THIS TIME.SDR GUU2005F00000Warning Light · intermittentDURING FLIGHT, LT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. CHECKED SYSTEM AND PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE. OPS CHECK NORMAL. (K)SDR GLBA20030769Pump · malfunctionedLT FUEL LOW PRESSURE ANNUN CAME ON IN FLT. REMOVED AND REPLACED LP FUEL PUMP.SDR S2YA04046Annunciator · false activationSHORTLY AFTER TAKEOFF, THE CREW NOTICED AN AIR STAIR DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. AFTER MX CONSULTATION, THE ANNUNCIATOR WAS MEL`D AND THE AC RETURNED TO SERVICE. MX CLEANED AND INSPECTSDR CA041206006Engine · malfunctioned(CAN) ON APPRAOCH THE ENGINE EXPERIENCED A POWER LOSS ACCOMPANIED BY LOW OIL AND FUEL PRESSURE WARNINGS. THE AIRCRAFT LANDED AT POINT OF DESTINATION. THE EVENT WAS NOT REPRODUCED DURING SUBSEQUENT GROUND AND FLT TESTS. THE FUEL CONTROL UNIT HAS BEEN REPLACED.SDR 341024Engine · failedRIGHT ENGINE FAILURE INFLIGHT.SDR CA041208002Tube · cracked(CAN) WHILE INSPECTING ONE OF THE FLEETS 1900D AIRCRAFT BLEED AIR TUBE PN 129-910033-63 FOUND TO BE CRACKED ALONG THE WELD. TIME OF THIS ACRFT 21,691.6 HOURS. A PRECAUTIONARY INSPECTION WAS COMPLETED ON AN OTHER AIRCRAFT TOTAL TIME 6291.9. THE SAME PN TUBE WASDR GUU2004F00043Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET.SDR GUU2004F00042Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.SDR GUU2004F00041Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.SDR 66896Circuit Board · burned outON TAKEOFF ROLL, CREW SMELLED ELECTRICAL FUMES IN COCKPIT, ABORTED TAKEOFF, RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED 11/21/04-REPLACED A127 PCB GOOD P/N 101-364580-1.
Back to Beech 1900D