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 GLBA2013051600248Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AT THE INTERSECTION OF LONGERON UNDER RT FINGER DOUBLER, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-040. MAJOR REPAIR.SDR ERAA20130036Actuator · failedNOSE GEAR GREEN ANNUNCIATOR LIGHT DID NOT ILLUMINATE WITH GEAR CONTROL HANDLE WITH RED ILLUMINATION. CYCLED GEAR TWICE THEN USED THE MANUAL GEAR EXTENSION PROCEDURE. FOUND NLG ACTUATOR DOWNLOAD SWITCH BAD. REMOVED AND REPLACED NLG RETRACT ACTUATOR IAW B1900SDR ERAA20130035Actuator · crackedHYDRAULIC FLUID LEAKING FROM RIGHT MAIN LANDING GEAR. REMOVED AND REPLACED NR 2 MLG ACTUATOR IAW BEECH 1900D MAINTENANCE MANUAL 32-30-10. RIGGED IAW BEECH1900D MAINTENANCE MANUAL 32-30-09, OPS CHECKED GOOD.SDR 29GA0430201394721Wire · chafedFLIGHT 4082. SMOKE IN COCKPIT DURING DESCENT, DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. FOUND WIRE AT VOLTAGE TEST PORT CHAFED AND ARCING AT FORWARD RIGHT SIDE OF COCKPIT PEDASTAL. REPLACED TEST JACK AND REPAIRED WIRE, OPS CHECKED GOOD.SDR GLBA2013042600242Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS IN THE FUSELAGE FRAME AT BS 303.25 AND STRINGER 2L, ON INBD AND OTBD SIDE OF STRINGER 2L, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-039. MAJOR REPAIR.SDR GLBA2013042600243Connector · damagedPILOT REPORTED THAT THERE WAS A STRANGE ODOR IN THE COCKPIT. MX REPAIRED SEVERAL WIRES AT A CONNECTOR & CHANGED SEVERAL PCBS.SDR GLBA2013042600241Tee Fitting · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE TEE SECTION OF THE LT HORZ STAB LOWER AT HSS 5.000 AND 10.5 PERCENT CHORD BETWEEN SCREW HOLES, .25" IN LENGTH. REPAIRED IAW EO 13-1900-55-013. MAJOR REPAIR.SDR GLBA2013042600240Tee Fitting · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE TEE SECTION OF THE RT HORZ STAB LOWER AT HSS 5.000 AND 10.5 PERCENT CHORD, .75" IN LENGTH. REPAIRED IAW EO 13-1900-55-014. MAJOR REPAIR.SDR GLBA2013042600239Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 163.975 AND STRINGER 9AR AT THE STRINGER CUTOUT, .4" IN LENGTH. REPAIRED IAW EO 13-1900-53-037. MAJOR REPAIR.SDR GLBA2013042600238Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND CRACK IN THE FUSELAGE FRAME IN THE BEND RADIUS AT FS 451 AND STRINGER 10R, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-034. MAJOR REPAIR.SDR GLBA2013042600237Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT SIDEWALL FUSELAGE FRAME AT FS 107 AND JUCTION WITH LONGERON IN THE FRAME BEND RADIUS AT THE UPPER AND OF THE FRAME, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-038. MAJOR REPAIR.SDR GLBA2013042600236Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 AND STRINGER 13L IN THE BEND RADIUS, 1.1" IN LENGTH. REPAIRED IAW EO 13-1900-53-036. MAJOR REPAIR.SDR GLBA2013042600235Doubler · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME DOUBLER AT BS 177.35 S13L, 1.2" IN LENGTH. REPAIRED IAW EO 13-1900-53-035. MAJOR REPAIR.SDR GLBA2013042500234Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT WING AT BL 29.06 AND SPAR, INBD RIB ANGLE (FLANGE) AT WING SPAR, .75" IN LENGTH. REPAIRED IAW EO 13-1900-57-010. MAJOR REPAIR.SDR GLBA2013042500233Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT SPAR CAP ON THE VERT STAB AT THE SECOND HOLE DOWN FROM THE TOP, .375" IN LENGTH. REPAIRED IAW EO 13-1900-55-012. MAJOR REPAIR.SDR GLBA2013042500232Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT APPROX FS 460, 3" IN LENGTH. REPAIRED IAW EO 13-1900-53-033. MAJOR REPAIR.SDR CA130501006Oil System · low pressure(CAN) DURING CRUISE FLIGHT, CREW NOTED SOUNDS OF OUT OF SYNC PROPS, AND FLICKERING OIL PRESSURE. MASTER WARNING LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED FOLLOWED BY A CREW SHUTDOWN OF THE L/H ENGINE. MAINTENANCE REVEALED, REDUCTION GEARBOX CHIP DETECTOR COVERESDR 29GA93553041613Skin · damagedDURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED LEFT FUSELAGE SKIN DAMAGE AT FS 250.00 WL 130. REMOVED DAMAGED SKIN AND INSTALLED COVER PATCH.SDR CA130412004Hinge Bracket · worn(CAN) DURING INSPECTION, RT ELEVATOR OTBD HINGE BRACKETS WERE FOUND WORN.SDR GLBA2013041100229Door · misinstalledPILOT REPORTED THAT THE EMERGENCY DOOR AT 6C WAS NOT PROPERLY SEATED. MX REINSTALLED THE EMER DOOR.SDR GLBA2013040900228Cable · brokenPILOT REPORTED THAT THE AIRSTAIR DOOR INTERNAL LOCK CABLE IS BROKEN AND THE DOOR WON'T OPEN. MX REPLACED THE LOWER FWD AIRSTAIR DOOR ACTUATOR CABLE, OPS CHECKED GOOD.SDR GLBA2013040800228Cable · brokenPILOT REPORTED THAT THE AIRSTAIR DOOR INTERNAL LOCK CABLE IS BROKEN AND THE DOOR WON'T OPEN. OPENSDR GLBA2013040800227Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE FRAME FLANGE AT FS 177.35 AND STRINGER 13L, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-031. MAJOR REPAIR.SDR GLBA2013040800226Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDEWALL LONGERON AT FS 107, AT JUNCTION WITH SIDEWALL FRAME, .75" IN LENGTH. REPAIRED IAW EO 13-1900-53-030. MAJOR REPAIR.SDR GLBA2013040800225Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDE WALL FRAME AT FS 107 AT THE UPPER 2 FASTENER HOLES, RADIATES FROM EACH HOLE UPWARD, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-030. MAJOR REPAIR.SDR GLBA2013040800224Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FUSELAGE SKIN AT THE UPPER FWD AREA OF A/S DOOR CUTOUT, RADIATES FROM FASTENER UPWARD & DOWNWARD AT FS 150 AND BELOW STRINGER 4L, .55" IN LENGTH. REPAIRED IAW EO 13-1900-53-031. MAJOR REPAIR.SDR GLBA2013040800223Skin · crackedDURING A SCHEDULED ROUTINE INSP FOUND 2 CRACKS IN THE UPPER FUSELAGE SKIN AT FS 150 AND STRINGER 1 ON THE LT & RT SIDE OF STRINGER 1, .7" IN LENGTH. REPAIRED IAW EO 13-1900-53-029. MAJOR REPAIR.SDR CA130405001Duct · cracked(CAN) BLEED AIR PIPE CRACKED AROUND WELDED AREA ON MOUNTING FLANGE. CAUSED BLEED AIR FAILURE.SDR GLBA2013040100222Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE TEE SECTION OF THE LT HORIZONTAL STAB LOWER AT HSS 5.000 AND 10.5 PERCENT AT A SCREW HOLE, .5" IN LENGTH. REPAIRED IAW EO 13-1900-55-011. MAJOR REPAIR.SDR A8OA2013040200004Pressure Switch · defectiveWITH AUTOFEATHER ARMED AND POWERED AND PASSING APPROX 93-94 PERCENT THE AFX ANNUNCIATOR ILLUMINATES. AFTER TROUBLESHOOTING, REMOVED DEFECTIVE RT HIGH OIL PRESSURE SWITCH, INSTALLED NEW SWITCH IAW MM CHAPTER 61-21-01. GROUND RUN UP OPERATED WITHIN SPECIFICATISDR GLBA2013040100221Handle · dislodgedPILOT REPORT THAT THE MAIN DOOR HANDLE FELL OFF. MX REPLACED THE DOOR HANDLE, OPS CHECKED GOOD.SDR GLBA2013040100220Circuit Breaker · trippedPILOT REPORTED THAT UPON EXTENDING THE GEAR THE LANDING GEAR CIRCUIT BREAKER TRIPPED, RAN MANUAL GEAR EXTENTION CHECKLIST, GEAR EXTENDED NORMALLY, A HIGH PITCH NOISE WAS HEARD FROM THE WHEEL WELL AFTER PARKING AT THE GATE. MX FOUND THE POWER PACK RUNNING, REPLSDR GLBA2013032900219Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK EXTENDING FROM A SCREW HOLE ON THE TOP SIDE OF THE LT HORIZONTAL STAB AT HSS 5.000 AND 10.5 PERCENT CHORD, ON THE FLANGE FOR PANEL 332 BTC ON THE FORWARD LT CORNER, .25" IN LENGTH. REPAIRED IAW EO 13-1900-55SDR GLBA2013032900218Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT HORIZONTAL STAB LOWER TEE SECTION AT HSS 5.000 AND 10.5 PERCENT CHORD, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-010. MAJOR REPAIR.SDR GLBA2013032700217Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 164 AND STRINGER 10R, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-53-028. MAJOR REPAIR.SDR GLBA2013032700216Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R FRAME, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-027. MAJOR REPAIR.SDR GLBA2013032500215Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT SPAR CAP AT THE SECOND FASTENER, FWD VERT STAB, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-008. MAJOR REPAIR.SDR CA130412002Hinge · loose(CAN) DURING INSPECTION, LT ELEVATOR OTBD HINGE FASTENERS LOOSE. SMOKING RIVETS AND DISCOVERED DURING SHAKE CHECK AT ELEVATOR TIP. ALSO, FOUND 1 OTHER ACFT IN FLEET WITH THE SAME PROBLEM.SDR ERAA201303210031Gauge · inoperativeRIGHT ITT BECAME INOPERATIVE IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE ITT GAUGE, RAN ENGINE, OPS CHECK GOOD. OK FOR SERVICE.SDR CA130320011Oil Cooler · cracked(CAN) AFTER LANDING, PILOTS CARRIED OUT A PREFLIGHT INSPECTION AND NOTICED THAT THERE WAS OIL ON THE RT ENGINE COWLS. COWLS WERE REMOVED AND ENGINE INSPECTED. OIL LEAK WAS FROM A CRACKED OIL COOLER, MAINTENANCE WAS NOTIFIED AND AN O/H COOLER WAS INSTALLED. SDR GLBA2013031900214Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE HORIZONTAL STAB AFT WEB AT THE 10 & 2 O'CLOCK POSITION AROUND THE ACCESS HOLE, .15" IN LENGTH. REPAIRED IAW EO 13-1900-55-007. MAJOR REPAIR.SDR GLBA2013031800213Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STABILIZER LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT FSS 84.10, GOING THROUGH THE THIRD FASTENER FROM THE TOP (SECOND FASTENER BELOW THE HAT SECTION) IN THE AREA OF THE HORIZONTAL STAB ATTACH SDR GLBA2013031500211Clamp · loosePILOT REPORTED THAT AT ALTITUDE 18500, CABIN ALTITUDE HIGH ANNUCICATOR ILLUMINATED. CABIN ALTITUDE INDICATED 10000 FT AND CABIN INDICATED 800 FT IAW MIN WITH INCREASE IN TRENDS, PASS O2 MASK DEPLOYED, CLIMB DIFFERENTIAL PRESSURE AT 2.8 AT TIME OF CLIMB ALTITSDR GLBA2013031300202Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT FS 107, LT SIDEWALL LONGERON AT FINGER DOUBLER AREA "M" JUNCTION WITH SIDEWALL FRAME, RADIATES UPWARD FROM A FASTENER HOLE AND TERMINATES BELOW LONGERON BEND RADIUS, .4" IN LENGTH. REPAIRED IAW EO 13-1SDR GLBA2013031300206Doubler · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SIDEWALL FINGER DOUBLER AT FS 107, .25" IN LENGTH. REPAIRED IAW EO 13-1900-53-026. MAJOR REPAIR.SDR GLBA2013031300205Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 177.35 BETWEEN STR 13 - 14L AFT SIDE, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-023. MAJOR REPAIR.SDR GLBA2013031300204Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SIDEWALL AT FS 107 AT THE UPPER END OF THE FRAME AT THE LAST ATTACHING FASTENER AREA, .75" IN LENGTH. REPAIRED IAW EO 13-1900-53-024. MAJOR REPAIR.SDR GLBA2013031300203Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SIDEWALL FRAME AT FS 107 IN THE BEND RADIUS (UPPER END OF FRAME) AND AT UPPER FASTENER AREA, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-025. MAJOR REPAIR.SDR GLBA2013031200201Controller · malfunctionedCABIN OXYGEN CONTROL PULLED DUE TO CABIN ALTITUDE EXCEEDING 10000FT AND CABIN ALTITUDE INCREASING AT 4000FT IAW MIN CREW TRIED TO RESET SYS, ADJ CABIN HEAT, RAN CHECKLIST, DEPLOYED MASKS AND DESCENDED. AT 5000FT ALTITUDE, ACFT BEGAN TO PRESSURIZE. OUTFLOW VSDR GLBA2013030700200Skin · dentedDURING A SCHEDULED ROUTINE INSPECTION, FOUND DENT ON THE RT WING OTBD L/E AT WS 290.06, DAMAGE APPROX 17.5". REPAIRED IAW EO 13-1900-57-001. MAJOR REPAIR.
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