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 GUUA93357031310ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003.SDR GLBA20100312HAngle · crackedDURING ROUTINE SCHEDULED MX THE RT HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FWD END OF THE ANGLE AT FS 288.0. THE CRACK IS APPROX 1.3" IN LENGTH. A CRACK AT FS 303 WAS ALSO PRESENT .5". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALLSDR GLBA2010312GAngle · crackedDURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FWD END OF THE ANGLE AT FS 288.0. THE CRACK IS APPROX 1.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W EO 10-190SDR GLBA100312002Angle · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE THE LEFT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FORWARD END OF THE ANGLE AT F.S. 288.0. THE CRACK IS APPROXIMATELY 1.5" IN LENGTH.SDR GLBA20100312FSkin · debondedDURING ROUTINE SCHEDULED MX THE AIRSTAIR DOOR AREA FROM THE TOP STEP HINGE TO THE LOWER EDGE. THE INNER SKIN IS DEBONDED. MX R & R THE AIRSTAIR DOOR BOND ASSY IAW MM 52-10-03.SDR GUUA93971031110ABracket · crackedDURING MAGNETIC PATICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. NOTE: FOUND DURING MAGNETIC PARTICLE INSP.SDR GUUA94557031110ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE MFG ACFT COMPANY KIT 118-4014-0003.SDR GUUA93332031110ACircuit Breaker · trippedFLIGHT: 9174 MIA/TPA PILOT REPORTED LANDING GEAR RELAY CIRCUIT BREAKER POPPED. TROUBLESHOT SYSTEM CHECKED LANDING GEAR RELAY CIRCUIT BREAKER COULD NOT DUPLICATE. TEST FLIGHT SATISFACTORY.SDR GUUA92752030910BDoor · stuckDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT HARD TO OPEN. LUBED RIGHT AFT EMERGENCY EXIT OPERATIONAL CHECKS GOOD.SDR GUUA92752030910ADoor · bindingDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED LEFT EMERGENCY EXIT DOOR OPERATIONAL CHECKS GOOD.SDR GUUA92752090910ADoor · bindingDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED LEFT EMERGENCY EXIT DOOR OPERATIONAL CHECKS GOOD.SDR GLBA20100309GSkin · dentedMAJOR REPAIR - DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-1900-53-008. RII INSPECTIONS COMPLIED WITH IAW EO 10-1SDR GLBA20100309FFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK IN THE FRAME RADIUS AT THE AIRSTAIR DOOR ENTRANCE FWD FRAME AT FS 177.350 AT APPROX STR 12L WAS FOUND, CRACK APPROX .5". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW SDR GLBA100307001Skin · dentedDURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-1900-53-008. RII INSPECTIONS COMPLIED WITH IAW EO10-1900-53-008. MATESDR GUUA95732030710ASwitch · out of adjustFLIGHT: 9271 FP PERCENT N1 ON LEFT ENGINE. ADJUSTED LANDING GEAR WARNING SWITCH AT LEFT ENGINE. TEST FLIGHT SATISFACTORY.SDR GUUA95652030610ACam · out of adjustFLIGHT: 9295 FKL/DUJ PILOT REPORTED WHEN LOCKING CABIN DOOR THE HANDLE IS HARD TO TURN. ADJUSTED FORWARD ECCENTRIC CAM (SECOND FROM THE BOTTOM CAM ) OPERATIONAL CHECK GOOD.SDR GUUA94252030610BGuide · bentFLIGHT: 5200 CLE/DUJ PILOT REPORTED CABIN DOOR VERY DIFFICULT TO CLOSE AND TO EXTINGUISH CABIN DOOR ANNUNCIATOR. REPLACED CABLE GUIDE AND AFT UPPER CAM SWITCH OPERATIONAL AND RIG CHECK GOOD.SDR GUUA94252030610ADoor · brokenFLIGHT: 9303 LWB/CLE PILOT REPORTED LEFT MAIN GEAR CAM DOOR ASSEMBLY ON INBOARD GEAR DOOR BROKEN. INSTALLED NEW CAM DOOR ASSEMBLY ON LEFT MAIN GEAR INBOARD GEAR DOOR.SDR GLBA20100308FDoor · corrodedMAJOR REPAIR - DURING ROUTINE FOLLOW UP MX, CORROSION WAS FOUND ON THE AIRSTAIR DOOR UNDERNEATH AND JUST BEYOND THE HINGE APPROX 12" BY 5". MX R & R THE AIRSTAIR DOOR ASSY IAW MM 52-10-03 & 52-10-00 AND RIGGED DOOR IAW 52-10-00.SDR GUUA93357030210BAccess Panel · debondedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING FUEL ACCESS PANEL 632 AT INNER RING DEBONDED. FABRICATED AND INSTALLED RING DOUBLER REPAIR AT ACCESS PANEL 632AT.SDR GUUA93357030210AAccess Panel · debondedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING FUEL ACCESS PANEL 531DB INTERNAL RING DEBONDED. FABRICATED AND INSTALLED RING DOUBLERS AT WING FUEL ACCESS PANEL 531DB.SDR GLBA20100302GFrame · crackedUPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L CRACK IS APPROX 2" LONG. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-007. MATERIALS UTILIZED ARE INCLUDED IN THESDR GLBA20100302FASpar · damagedMAJOR REPAIR - UPON ROUTINE SCHEDULED MX A LOCK FASTENER HOLE IN THE LT WING SPAR AT APPROX WS 93.250 WAS FOUND STEPPED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-57-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.SDR GLBA20100302FFrame · crackedMAJOR REPAIR - UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L. CRACK IS APPROX 2" LONG.SDR GUUA93957022810ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE MFG ACFT COMPANY KIT 118-4014-0003.SDR GUUA95255022810BTorque Tube · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED RIGHT ELEVATOR TORQUE TUBE.SDR GUUA95255022810AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR OUTBOARD HINGE BRACKET HAS CORROSION. REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET.SDR GUUA95652022710BDoor · bindingDURING SCHEDULED ROUTINE INSPECTION DISCOVERED EMERGENCY EXIT DOOR AT SEAT 6A WILL NOT SEAT AND LATCH. ADJUSTED UPHOLSTERY ON EMERGENCY EXIT DOOR AT SEAT 6A. OPERATIONAL CHECK GOOD.SDR GUUA95652022710ADoor · bindingDURING SCHEDULED ROUTINE INSPECTION DISCOVERED EMERGENCY EXIT AT SEAT 4F WILL NOT LATCH. ADJUSTED INTERIOR WINDOW UPHOLSTERY ON EMERGENCY EXIT AT SEAT 4F. OPERATIONAL CHECK GOOD.SDR GUUA93352022510ADoor · inoperativeFLIGHT: 9167 MCO/PNS PILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN. REPOSITIONED AIRSTAIR DOOR HANDRAIL CABLE OPERATIONAL CHECK GOOD.SDR GUUA95052022510BDoor · stiffDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT LATCH HARD TO OPERATE. CLEANED AND LUBRICATED ENTIRE LATCH SYSTEM.SDR GUUA95052022510ADoor · stiffDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT HARD TO OPEN. CLEANED AND LUBRICATED ENTIRE LATCH MECHANISM.SDR GUUA95652022410ACable · wornDURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR UPPER FORWARD CONTROL CABLE WORN. REPLACED AIRSTAIR DOOR UPPER FORWARD CONTROL CABLE. OPERATIONAL CHECK GOOD. AIRCRAFT DOWN FOR STRUCTURAL INSPECTION.SDR GUUA94627022410BTorque Tube · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED RT ELEVATOR TORQUE TUBE.SDR GUUA94627022410AHinge · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED SURFACE CORROSION AT RT ELEVATOR OTBD HINGE. REPLACED RT ELEVATOR OTBD HINGE.SDR 2010FA0000220Motor · seizedELECTRIC FLAP MOTOR SEIZED CAUSING ODOR IN THE CABIN AREA. FOUND THE FLAP MOTOR SEIZED AND REPLACED FLAP MOTOR/GEAR BOX WITH AN O/H UNIT IAW MM 27-50-03 AND 27-50-05.SDR GUUA95052022210ADoor · stuckDURING SCHEDULED ROUTINE MX, DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT FWD EMERGENCY EXIT OPS CK GOOD.SDR GUUA94052022210ADoor · stuckDURING SCHEDULED ROUTINE MX DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. REPOSITIONED RT FWD EMERGENCY EXIT INTERIOR PANEL.SDR GLBA201002181Relay · failedUPON APPROACH THE PILOTS REPORTED THAT THE LANDING GEAR DID NOT EXTEND AND THE CIRCUIT BREAKER POPPED. THEY THEN PERFORMED A MANUAL EXTENSION. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE HYDRAULIC POWER PACK WOULD NOT SHUT OFF CAUSING THE CIRCUIT BREASDR GUUA94152021810APanel · out of limitsPILOT REPORTED CABIN DOOR HARD TO OPEN AFTER LANDING. TRIMMED CABIN DOOR INTERIOR PANEL AROUND PUSH BUTTON OPS CHECK GOOD.SDR CA100224009Fastener · missing(CAN) ACFT WAS ON SCHEDULED CHECK AND DURING INCORPORATION OF SB 57-3815/16 TO COMPLY WITH AD 2009-23-03. IT WAS DISCOVERED THAT THERE WAS A CONFLICT WITH THE SB DWG AND THERE WERE SOME MISSING FASTENERS (QTY 7) AT RWS 123 ON THE RT AFT WING SPAR THAT WERE MISDR CA100216015Downlock Switch · burned(CAN) SELECTING GEAR DOWN, NEGATIVE ON ALL 3 GREEN INDICATION AND GEAR HANDLE INTRANSIT LIGHT DID NOT ILLUMINATE, GEAR C/B POPPED. C/B WAS PUSHED IN AFTER MX CALL. GOT 2 GREEN MAIN AND NEGATIVE NOSE, INTRANSIT HANDLE LIGHT WENT OUT AFTER EXTENSION. PERFORMSDR GUUA93861021410APressure Switch · failedDURING FINAL APPROACH RT ENGINE GOES IN AND OUT OF FEATHER MULTIPLE TIMES. REPLACED AUTOFEATHER HIGH PRESSURE SWITCH.SDR GUUA95432021010ASwitch · brokenPILOT REPORTED LANDING GEAR WARNING HORN SILENCE BUTTON INTERMITTENT NEED TO WIGGLE AROUND TO SILENCE. REPLACED LANDING GEAR WARNING HORN SILENCE SWITCH S14. OPS CK NORMAL.SDR 19MA201002086413Drain · cloggedWHILE PERFORMING 36 MONTH FUEL COLLECTOR TANK INSP, INSPECTOR WAS UNABLE TO LOCATE THE COLLECTOR TANK AFT DRAIN OPENING IN LT COLLECTOR TANK. REMOVED DRAIL LINES FROM LOWER NACELLE AREA TO INSERT PIN UP THROUGH DRAIN FITTING TO TANK AREA TO LOCATE HOLES BUT FOSDR GUUA93757020710ASkin · puncturedDURING SCHEDULED ROUTINE INSP DISCOVERED RT STUB WING TOP OF L/E HAS A DENT AND PUNTURED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR.SDR GUUA93352020610ACam · dirtyPILOT REPORTED CABIN DOOR HARD TO CLOSE. CLEANED CABIN DOOR CAMS, OPS CHECK GOOD.SDR GUUA94232020410AActuator · malfunctionedDURING APPROACH LANDING GEAR MAINS TAKE LONGER 10-15 SECONDS TO LOCK INTO POSITION. REPLACED RT MLG ACTUATOR. OPS CHECK NORMAL.SDR GUUA95432020410AWire · chafedDURING APPROACH, LANDING GEAR WARNING HORN AND GEAR HANDLE ILLUMINATED WITH GEAR HANDLE IN THE DOWN POSITION 3 GREEN WAS ILLUMINATED BEFORE GEAR HANDLE ILLUMINATED AND HORN SOUNDED. REPAIRED CHAFED WIRES TO LT GEAR UPLOCK SWITCH, OPS CHECK NORMAL.SDR CA100204008Blower · failed(CAN) PILOT REPORTED SMOKE AND BAD SMELL IN CABIN. BLOWER (AFT) ASSY WAS REMOVED AND INSPECTED. INSP FOUND ARCING AT THE BRUSH COVER ATTACH SCREWS, AND ON BRUSH COVER WHERE 1 BRUSH LEAD WAS HUNG UP ON BRUSH HOLDER. THE LEAD WAS CLEARLY SQUASHED DOWN TO CLEAR C
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