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 GLBA201206151Pump · failedLT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. TURNED ON THE STANDBY PUMP AND THE ANNUNCIATOR WENT OUT. NO FUEL LEAK NOTED ON POST FLIGHT. MX REPLACED THE LT LOW PRESSURE PUMP IAW BMM 73-10-00, OPS CHECKED GOOD.SDR 29GA94552061412ACable · brokenFLIGHT: 4052 EYW/FLL AIRSTAIR DOOR WILL NOT OPEN. REPLACED AIRSTAIR DOOR LOWER CABLE, OPERATIONAL CHECK OK.SDR 29GA2012061112Spar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED CORROSION AT FORWARD SPAR AFT FLANGE BETWEEN STRINGER 15L AND STRINGER 14L. REMOVED CORROSION DAMAGE PERFORMED EDDY CURRENT INSPECTION ON BLEND OUT AREAS NO CORROSION OR CRACKS FOUND.SDR GLBA201206123Actuator · leakingTHE CREW HEARD A LOUD POPPING NOISE COMING FROM THE NOSE AREA UPON GEAR EXTENSION. MX FOUND HYD FLUID LEAKING FROM THE NOSE GEAR ACTUATOR. R & R NLG ACTUATOR PN ON/OFF 112-380022-23, SN OFF 338, SN ON 569, REF MM 32-30-14. OPS, LEAK, AND RIG CHECKS WERE GOOD.SDR CA120621002Chip Detector · loose(CAN) DURING AN M CHECK, THE RGB CHIP DETECTOR WAS FOUND TO BE LOOSE. FURTHER INVESTIGATION REVEALED THAT THE CHIP DETECTOR ADAPTOR PN 3014580 WAS CRACKED AT THE MOUNTING FLANGES.SDR GLBA2012061211Wire · brokenLANDING GEAR RELAY CIRCUIT BREAKER TRIPPED IN FLIGHT. CREW NOTICED ROUGHLY 10 MINUTES IN TO THE FLIGHT. MX REPAIRED A BROKEN WIRE BY SEAT 2A IAW WM 20-10-00, OPS CK GOOD.SDR GLBA2012061803Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE HORIZ STAB AFT WEB AT HSS 0.00, 4 CRACKS, 1" IN LENGTH. REPAIRED IAW EO 12-1900-55-015. MAJOR REPAIRSDR GLBA2012061802Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE HORIZONAL STAB AFT WEB AT HSS 0.00, FOUR CRACKS, .5625" IN LENGTH. REPAIRED IAW EO 12-1900-55-015. MAJOR REPAIRSDR GLBA201206112Actuator · failedCREW TRIED TO EXTENDED THE GEAR NORMALLY BUT THE GEAR FAILED TO EXTEND. CREW RAN CHECKLIST AND EXTENDED THE GEAR MANUALLY. AFTER MANUAL EXTENSION THERE WERE NO ABNORMAL INDICATIONS NOTED. MX R & R RT MAIN LANDING GEAR ACTUATOR IAW TC 1900-3230.10, REV 1. OPSDR GLBA201206111Relay · failedON SELECTING GEAR DOWN ON APPROACH. LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED IMMEDIATELY. AFTER PERFORMING "FAILURE OF LANDING GEAR TO EXTEND NORMALLY" CHECKLIST, GEAR WAS DETERMINED UNSAFE. "LANDING GEAR MANUAL EXTENSION" CHECKLIST PERFORMED, LANDING GSDR GLBA201206082Spar · gougedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 0.3" LONG BY 0.040" DEEP GOUGE ON THE LT FWD BOTTOM SPAR INBD OF THE ACM EXHAUST. REPAIRED IAW EO 12-1900-55-018. MAJOR REPAIR.SDR GLBA201206081Cam · obstructedTOP LEFT LOCKING CAM IS CONTACTING THE STUD AND MOVING INWARD ON MAIN CABIN DOOR. MX R & R AIRSTAIR DOOR (DOOR SIDE) HINGE HALF IAW SRM AND RE-RIGGED THE FORWARD AND AFT UPPER LATCH POSTS IAW MM.SDR 29GA94754060512Keelbeam · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEEL BEAM UPPER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLACED RIGHT NACELLE UPPER KEEL WEB.SDR 29GA2012060594754Keelbeam · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEELBEAM LOWER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLACED RIGHT INBOARD LOWER KEEL WEB.SDR GLBA2012060401Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT SIDEWALL FS 456 AND STRINGER 10R, FRAME AT STRINGER CUTOUT, .2" IN LENGTH. REPAIRED IAW EO 12-1900-53-032. MAJOR REPAIRSDR GLBA2012053101Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 456 BETWEEN STRINGER 3 & 4L, FWD CARGO DOOR CUTOUT. REPAIRED IAW EO 12-1900-53-031. MAJOR REPAIRSDR 29GA95652053112AControl Cable · brokenFLIGHT: 4069 CLE/DUJ CABIN DOOR ANNUNCIATOR ILLUMINATED. REPLACED LOWER AFT AIRSTAIR DOOR CONTROL CABLE.SDR GLBA2012060101Turnbuckle · brokenPILOT REPORTED THAT THE INSIDE CABIN DOOR HANDLE IS BROKEN, COULDN'T OPEN DOOR FROM THE INSIDE. MX REPLACED THE HANDLE TURNBUCKLE BOLT IAW MM 52-10-05, OPS CHECKED GOOD.SDR 29GA93521053012AAcm · failedON SHORT FINAL, A BUZZING NOISE WAS HEARD AND BURING ODOR COMING FROM CABIN WHEN BLEEDS TURNED OFF, ODOR AND NOISE STOPPED. REPLACED AIR CYCLE MACHINE, OPERATIONAL CHECKED GOOD. NO BURNING ODOR WAS PRESENT.SDR 29GA94357052812ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT WING ON TOP TRAILING EDGE SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR GLBA201205291Bulb · inoperativeLEFT INSTRUMENT/EMERGENCY LIGHT FLICKERS. MX REPLACED THE BULB, IAW BMM 33-10-04, OPS CHECKED GOOD.SDR 29GA95571052712AEngine · malfunctionedFLIGHT: RIGHT ENGINE OIL PRESSURE ILLUMINATED IN FLIGHT ON APPROACH ASSOCIATED SMELL OF SMOKE IN CABIN AND COCKPIT. ENGINE SECURED AND EMERGENCY DECLARED. REPLACED RIGHT ENGINE ASSEMBLY.SDR GLBA2012052901Spar · chafedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT WING MAIN SPAR CHAFED AT INBD EDGE OF LOWER ACM PANEL. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-003.SDR V0DR20120523001Bearing · brokenPROPELLER ASSY, HC-E4A-3I CAME IN FOR OVERHAUL. UPON DISASSEMBLY NR 4 BLADE LOWER AND UPPER RETENTION BEARING FOUND TO BE CRACKED. BEARING PN D-7745A & D-7745B.SDR 2012FA0000622Resistor · malfunctionedACFT VENT BLOWER WAS REPLACED BEFORE SCHEDULED MAINTENANCE PERIOD. INTERNAL MALFUNCTION OF THE VENT BLOWER RESISTOR FOUND TO BE THE PROBLEM OF COMPONENT FAILURE. REMOVED AND REPLACED RESISTOR.SDR GLBA2012052201Diaphragm · damagedPILOT REPORTED THAT DURING CLIMB OUT AND PASSING THROUGH 21,500" CABIN HIGH ANNC ILLUMINATED, DECLARED EMERGENCY, MASKS DEPLOYED, RETURNED TO DEPARTURE. MX R & R LT OUTFLOW VALUE DUE TO DAMAGE TO THE DIAPHRAM IAW BMM 21-30-01, OPS CHECKED GOOD IAW BMM 21-30-0SDR GLBA2012051601Actuator · inoperativePILOT REPORTED LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED EMERGENCY, LANDED SAFELY. MX MEGGED WIRING FROM TB150 TO ALL ACTUATORS, HANDLE TO PCB A316 AND TO SERVO VALVE, ALL CHECKED GOOD, R & R RT ACTUATOR, IAW TC 1900-3230-10SDR GLBA2012051401Actuator · inoperativePILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED AN EMERGENCY, LANDED SAFELY. MX WAS ABLE TO DUPLICATE PROBLEM, REPLACED RT MLG ACTUATOR. REF TC 1900-3230.10, OPS CHECKED GOOD.SDR GLBA2012051101Powerpack · malfunctionedPILOT REPORTED ON APPROACH, LANDING GEAR WOULD NOT EXTEND, DECLARED AN EMERGENCY, MANUALLY PUMPED GEAR DOWN, 3 GREENS, LANDED SAFELY. MX REPLACED THE HYD POWER PACK IAW BMM 32-30-04.SDR 29GA93532050912AUnknown · malfunctionedFLIGHT:4063 CLE/CLE LANDING GEAR WILL NOT RETRACT CIRCUIT BREAKER POPPED. TROUBLESHOT SYSTEM EXTENSIVELY INSPECTED WIRING TO POWER PACK, GEAR ACTUATORS AND LANDING GEAR HANDLE ALL CHECKED NORMAL. CYCLED LANDING GEAR SEVERAL TIMES NO DEFECTS NOTED.SDR 29GA93832050412ASwitch · out of adjustFLIGHT: 5201 TPA/GNV GEAR WARNING HORN AND GEAR UNSAFE LIGHT COMES ON WHEN LEFT POWER LEVER RETARDED TO 89.6 N1. ADJUSTED GEAR WARNING HORN MICRO-SWITCH OPERATIONAL CHECK GOOD. TEST FLIGHT SATISFACTORY.SDR GLBA2012050701Wire · damagedPILOT REPORTED THAT WHEN THEY TURNED ON THE MASTER PANEL LIGHT SWITCH, NOTICED AN ELECTRICAL BURNING ODOR, NO SMOKE NOTED, TURNED SWITCH OFF, ODOR WENT AWAY. MX REPAIRED A WIRE ON THE PROPELLER AMP INDICATOR, NO ODOR NOTED.SDR CA120503004Transducer · unserviceable(CAN) LEFT ENGINE RUDDER BOOST PRESSURE TRANSDUCER WAS REPLACED TO REPAIR A DEFECT WITH THE YAW DAMPER SYS. AS A RESULT OF CHANGING THIS COMPONENT THE ACFT HAS SINCE EXPERIENCED 3 REJECTED TAKEOFFS, CADOR 2012C0963, 2012C0970 AND 2012C1569. IN ADDITION TO THSDR GLBA2012050101Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE HORIZONTAL STAB AFT SPAR WEB, CRACKS RADIATE FROM LIGHTNING HOLE AT 2, 5, 7& 10 O'CLOCK POSITIONS, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1SDR 29GA93532042812ARelay · shortedPILOT REPORTED LANDING GEAR CIRCUIT BREAKER POPPED DURING LANDING GEAR EXTENSION. RESET BREAKER MOTOR RAN LONG ENOUGH TO GIVE US 3 GREEN LIGHTS FOR GEAR EXTENSION AND THEN CIRCUIT BREAKER POPPED AGAIN. DID LOW APPROACH AND TOWER VISUAL CONFIRMED GEAR WAS DOWSDR GLBA2012042701Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FWD PRESSURE BULKHEAD ALONG THE OTBD ROW OF FASTENERS NEXT TO THE RT NOSE GEAR WEB AT FS 84.00, .375" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1SDR GLBA2012042605Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150 AND STRINGER 9AL, AT NUTPLATE FOR A/S DOOR STRUT LWR MOUNT, .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-028. MAJOR REPAIRSDR GLBA2012042604Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 164 AND STRINGER 9AR AT CUTOUT, .35" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-026. MAJOR REPAIR.SDR GLBA2012042603Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME AT FS 509 AND AFT GAS STRUT MOUNT AREA FROM CENTER OF THE UPPER INBD GAS STRUT NUTPLACE SCREW HOLES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. ESDR GLBA2012042602Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FWD PRESSURE BULKHEAD ALONG ROW OR FASTENERS NEXT TO THE LT NOSE GEAR WEB, FS 84.00, 7.25" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-029. MASDR 29GA95132042512APosition Switch · out of adjustFLIGHT:3967 GNV/MCO PILOT REPORTED UNSAFE RED GEAR HANDLE LIGHT INFLIGHT. ADJUSTED RIGHT UP POSITION SWITCH, OPERATIONAL CHECK GOOD.SDR 29GA95132042512Position Switch · out of adjustFLIGHT:3967 GNV/MCO PILOT REPORTED UNSAFE RED GEAR HANDLE LIGHT INFLIGHT. ADJUSTED RIGHT UP POSITION SWITCH, OPERATIONAL CHECK GOOD.SDR GLBA2012042601Pressure Switch · malfunctionedPILOT REPORTED THAT THE LT ENGINE ATTEMPTED TO FEATHER IN FLIGHT AT APPROX 1000 FT/LBS OF TORQUE ON THE LT AND RT SIDE. MT TROUBLESHOT LEFT LP SWITCH, R & R LT AFX LOW PRESSURE SWITCH IAW BMM 61-21-01, OPS CHECKED GOOD.SDR 2012FA0000625Resistor · malfunctionedACFT VENT BLOWER REPLACED BEFORE SCHEDULED MAINTENANCE PERIOD. INTERNAL MALFUNCTION OF THE VENT BLOWERS RESISTORS FOUND TO BE THE PROBLEM OF COMPONENT FAILURE. REMOVED AND REPLACED RESISTORS.SDR GLBA2012042301Circuit Board · damagedPILOT REPORTED THAT THE LT AUTOFEATHER SYS DISARMED AND REARMED REPEATEDLY DURING FLIGHT. MX REPLACED THE PCB A123, OPS CHECKED GOOD.SDR GLBA2012041803Support · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACKED ON THE LT SIDEWALL FLANGE AT FS 327 STRINGER 9A LT IN THE FLANGE BEND RADIUS, 1.8" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-025. MAJOR REPAIR.SDR GLBA2012041802Support · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT SIDEWALL FLANGE AT FS 288 & STRINGER 9AR IN THE BEND RADIUS OF THE FWD FLANGE, 1.4" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-024. MAJOR SDR GLBA2012041801Support · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT SIDEWALL FLANGE AT FS 327 & STRINGER 9AR, 1.2" IN LENGTH AT THE AFT FLANGE BEND RADIUS. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-023. MAJOR REPAIR.SDR CA120416007Skin · corroded(CAN) RIGHT WING DE-ICE BOOT REQUIRED REPLACEMENT. UPON REMOVAL OF DE-ICE BOOT, CORROSION WAS NOTED THROUGHOUT THE LEADING EDGE SKIN, OTBD WING CENTER SECTION FROM WS 147.735-WS 223.485, CORROSION WAS NOTED TO BE ALMOST THROUGH THE SKIN IN SEVERAL AREAS. THIS SDR GLBA2012041202Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 BETWEEN STRINGERS 3L & 4L, AT THE CARGO DOOR STRUT MOUNT, UPPER INBD NUTPLATE, 2" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1
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