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 GUUA94327071709AHorn · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR INBD TRIM TAB HORN EXFOLIATED. REPLACED RT ELEVATOR TRIM TAB.SDR GUUA94355071709CHinge Bracket · corrodedDURING ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.SDR GUUA94355071709BHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OTBD HINGE BRACKET.SDR GUUA94355071709AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CTR HINGE BRACKET.SDR GLBA20090720FSkin · crackedDURING ROUTINE SCHEDULED MX TWO CRACKS ON TOP OF FUSELAGE AT FS 150.6 WERE DISCOVERED. TOP CENTERLINE 1 RIVET HEAD SHEARED INBD OF CRACK 1.250 INCHES LONG AND A .250 INCH CRACK LT OF CENTERLINE. MX REPAIRED AFFECTED AREA IAW EO 09-1900-53-009. REPAIR AREA ASDR CA090716010Shaft · unserviceable(CAN) FLAP CABLE RT WING INBD FLAP SHEARED APPROX .2500 INCH TO .1250 INCH INSIDE THE SHEATH BODY. THE MM CALLS FOR A REPLACEMENT OF THE CABLE AT 22,500 CYCLES.SDR GUUA95057071509ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 124.25 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA95132070909ALight · inoperativeDURING APPROACH AFTER SELECTING LANDING GEAR DOWN, GEAR GREEN "H" LIGHTS DID NOT ILLUMINATE. RESEATED ANNUNCIATOR "H" LIGHTS. OPS CHECK GOOD.SDR CA100217005Elbow · fractured(CAN) DURING BOLT REPLACEMENT CAMPAIGN RGB OIL PRESSURE TRANSFER ELBOW WAS VISUALLY INSPECTED AND DISCOVERED THE OTBD MOUNTING PAD LOOP FRACTURED. (TC 20100217005)SDR GLBA200907061Engine · power lossON CLIMB THROUGH 9000 FT, NR 2 PROP RPM DROPPED TO 500 RPM & TORQUES INCREASED TO 4700 FT LBS. SUSPECTED GOVERNOR FAILURE, SET MAX PWR, PROP LEVERS FULL FWD, & VERIFIED MLG & FLAPS UP. NR 2 ENG TORQUE STAYED AT 4700 FT LBS FOR APPROX 30 SEC & RE-SET TO 2000 FSDR GUUA95552070509AClevis · bentPILOT REPORTED CABIN DOOR HARD TO OPEN FROM THE OUTSIDE. FOUND AIRSTAIR DOOR LWR FWD HANDRAIL CABLE UPPER CLEVIS BENT AND CATCHING ON STRUT COUNTER BALANCE, REPLACED LWR FWD AIRSTAIR DOOR HANDRAIL CABLE.SDR GUUA91252070409AStructure · debondedDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR UPPER FWD CORNER DEBONDED. REBONDED UPPER EDGE OF AIRSTAIR DOOR AND INSTALLED DOUBLER REPAIR.SDR GLBA20090703ATach Generator · deterioratedABORTED TAKEOFF, PILOTS REPORTED THAT AT TAKEOFF POWER THE PROPELLER RPM ON THE LT SIDE EXCEEDED 2000 RPM AND THE TAKEOFF WAS ABORTED. MX REMOVED AND REPLACED NR 1 PROPELLER TACH GENERATOR IAW 67D MM 70-00-00. OPS AND LEAK CHECKS WERE GOOD IAW MM 77-10-00.SDR GUUA95132070209AAnnunciator · inoperativeDURING APPROACH, LANDING GEAR "H" ANNUNCIATOR INOPERATIVE. RESET AND SECURED LANDING GEAR "H" ANNUNCIATOR MODULE OPS CHECK GOOD.SDR 19MA5671212O-Ring · splitAFTER SHUTDOWN, PILOT DISCOVERED OIL DRIPPING FROM NACELLE AREA ON LT ENGINE. COWLING WAS REMOVED AND OIL WAS DISCOVERED COMING FROM THE UPPER OIL SCAVENGER TUBE ON LT LWR SIDE OF ENGINE AT THE AFT SIDE OF THE "C" FLANGE COUPLING (PN 3113090-01). TUBES WHERESDR GUUA93957070109ASkin · corrodedDURING MX DISCOVERED RT FUEL LEAK AT RT WING ACCESS PANEL 632AT. REPAIRED SKIN .SDR GUUA92757070109ASkin · delaminatedDURING SCHEDULED INSP, DISCOVERED LT AND RT WING SKIN DELAMINATED AROUND FUEL ACCESS PANELS 531CB, 532CB, 531DB, 532DB, 532FB, 541AB, 632AT,632CB AND 632DB. REPAIRED WING SKIN AROUND FUEL ACCESS PANELS.SDR GUUA95753062709ASeat Track · damagedDURING SCHEDULED INSP, HOLE FOUND IN LT SEAT TRACK INBD FWD CABIN SEAT BETWEEN FS 258.25 AND FS 273.25. REPAIRED LT SEAT TRACK BY INSTALLING A RIVET.SDR GUUA93557062509AAccess Panel · damagedPILOT REPORTED FUEL LEAK FOUND UNDER LT WING INSP PANEL OTBD OF ENGINE. ACCOMPLISHED EXTERNAL REPAIR DOUBLER ON LT WING FUEL PANEL 531EB.SDR GUUA93757062409ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT UPPER WING SKIN T/E CORROSION AND DEBOND BETWEEN WING STA 136.036 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.SDR GLBA20090629FShaft · corrodedDURING MX IT WAS DISCOVERED THAT THE LT EXIT DOOR AT ROW 6A WOULD NOT LATCH SHUT PROPERLY. MX REMOVED AND REPLACED THE EXIT DOOR WHICH WAS REMOVED FROM ACFT IN SERVICEABLE CONDITION IAW 52-20-00. LEAK CHECK IAW 21-30-00 AND OPS CHECK WERE GOOD. THE ORIGINAL DSDR CA090626005Engine · seized(CAN) RT ENG OIL PRESSURE GAUGE VARIES BETWEEN 80 AND 90 PSI IN FLIGHT WITH A MAX FLUCTUATION BETWEEN 100 TO 105 PSI. RT ENG IS A RENTAL ENG FROM MFG. IRREGULARITY SMS REPORT STATES, "DURING CRUISE ACFT QUICKLY AND SLIGHTLY YAWED TO LT. FELT SIMILAR TO YAW SDR ERAA200900002Fitting · crackedWHILE INSPECTING IAW SB27-3928, FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON THE RT AILERON.SDR ERAA200900001Fitting · crackedWHILE INSPECTING IAW SB27-3928 FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON LT AILERON.SDR GUUA94155062209AHinge Bracket · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. C/A: REPLACED RT ELEVATOR OTBD HINGE BRACKET.SDR GUUA941062209AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.SDR GLBA200906231Hose · damagedPILOTS REPORTED THAT AFTER TAKEOFF THE GEAR HANDLE WAS MOVED TO THE UP POSITION AND 3 GREEN LIGHTS EXTINGUISHED AND THE INTRANSIT LIGHTS STAYED ILLUMINATED. PILOTS CONFIRMED GEAR DID NOT COME UP. PILOTS MANUALLY PUMPED THE GEAR DOWN. MX FOUND DAMAGED HOSES SDR GLBA200906221Switch · out of adjustPILOTS REPORTED THE NR 1 ENGINE WAS GOING IN AND OUT OF FEATHER WHEN APPLYING POWER ON DESCENT. MX COMPLIED WITH FLEET CAMPAIGN DIRECTIVE 1900-08-61-01. MX ADJUSTED THE NR 1 AUTOFEATHER SWITCH IAW FLEET CAMPAIGN DIRECTIVE 1900-08-61-01. OPS CHECK WAS GOOD.SDR GUUA93357062009AFuel Tank · leakingDURING SCHEDULED ROUTINE INSP DISCOVERED RT AUX TANK HAS A LEAK AT AUX PUMP MOUNT RING. REBONDED AROUND BOOST PUMP RING AND INSTALLED REPAIR DOUBLER.SDR GUUA92757062009AAccess Panel · corrodedDURING INSP OF LT WING FUEL LEAK, FOUND FUEL ACCESS PANEL 532AB HAS CORROSION AND DEBOND ON INTERNAL RING. INSTALLED REPAIR RINGS AT LT FUEL ACCESS PANEL 532AB.SDR GUUA92757061809AStringer · corrodedDURING INSP FOR FUEL LEAK ON LT WING DISCOVERED CORROSION AT LT STRINGER INSIDE COLLECTOR TANK. CLEANED CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA93757061709AStringer · corrodedDURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 J STRINGER HAS CORROSION.SDR GUUA95732061709AActuator · inoperativeAFTER TAKEOFF WHEN GEAR SELECTED UP NOTHING HAPPENS ( NO RED HANDLE LIGHT NO GEAR MOTOR) FOR APPROX 2 SECONDS THEN LOUD NOISE JUST BEFORE GEAR STARTS TO RETRACT. REPLACED NOSE GEAR ACTUATOR, OPS CHECK NORMAL.SDR GUUA93757061709DSpar · corrodedDURING SCHEDULED INSP DISCOVERED LT WING FWD SPAR AFT FLANGE AREA 3 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA93757061709CSpar · corrodedDURING SCHEDULE INSP DISCOVERED LT WING FWD FRONT SPAR AREA 2 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA93757061709BSpar · corrodedDURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 FWD SPAR AFT FLANGE HAS CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.SDR GUUA95027061509AHorn · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR INBD TRIM TAB HORN EXFOLIATED. REPLACED RT ELEVATOR TRIM TAB.SDR GUUA95055061509BHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET.SDR GUUA95055061509ASpar Cap · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED SURFACE CORROSION ON VERTICAL STABILIZER LT AND RT SPAR CAPS, LT CAP BETWEEN CSS 39.289 AND 46.289 AND RT CAP BETWEEN CSS 53.026 AND 55.026. CLEANED CORROSION AND INSTALLED REPAIR STRAP IN CORRODED AREA BETWEEN CSS 53.SDR GUUA93757061409BSkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FUSELAGE BELLY EXFOLIATED AT FS 303.25. REMOVED EXFOLIATED SKIN AND INSTALLED FILLER AND DOUBLER REPAIR.SDR GUUA93757061409ASkin · crackedDURING SCHEDULED ROUTINE MX 2.25 INCH CRACK ON RT FUSELAGE BELLY AT FS 310.00. INSTALLED FILLER AND DOUBLER REPAIR.SDR GUUA94752060909AScrew · out of adjustDURING SCHEDULED ROUTINE MX DISCOVERED EMERGENCY DOOR AT SEAT 6A WILL NOT PULL OUT OF SEAT FREELY. ADJUSTED EMERGENCY EXIT INTERIOR LINING CONTOUR SCREW. OPS CHECK NORMAL.SDR GUUA93657060909AAccess Panel · delaminatedPILOT REPORTED FUEL LEAK FROM PANEL UNDER RT WING OTBD SIDE OF THE ENGINE. REPAIRED LOWER WING SKIN AROUND FUEL ACCESS PANELS 631DB AND 631CB.SDR GLBA20090606AValve · inoperativePILOTS REPORTED THAT THE RT ENVIRO FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. MX REMOVED AND REPLACED THE RT PRE-COOLER VALVE IAW MM 21-11-00. THE OPS CHECK WAS GOOD.SDR GLBA20090606BBlower · smokePILOTS REPORTED THAT ENVIRONMENTAL SMOKE AND FUMES WERE PRESENT IN THE COCKPIT. THE BLOWERS SEEMED TO MAKE THE SITUATION WORSE. PILOTS DECLARED AN EMERGENCY. THE CAPTAINS O2 MASK MIC WAS NOT WORKING WHEN SWITCHING TO THE O2 MASK. MX TROUBLESHOT THE ISSUE AND FSDR GUUA95557060509ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT WING UPPER SKIN HAD CORROSION AT LWS 147.74. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.SDR GLBA200906051Annunciator · illuminatedLT ENVIRO FAIL ANNUNCIATOR ILLUMINATED ON TAKE OFF.SDR GUUA93672060409AGas Generator · fodDURING CLIMBOUT, SPARKS COMING OUT OF THE NR 1 ENGINE. ALL INSTRUMENT INDICATIONS READING NORMAL AND NO ANNUNCIATOR ILLUMINATED. FOUND NR ONE ENGINE GAS GENERATOR FIRST STAGE COMPRESSOR BLADE DAMAGE DUE TO FOREIGN OBJECT DEBRIS, REPLACED GAS GENERATOR.SDR GLBA20090605GSkin · crackedMAJOR REPAIR, DURING ROUTINE MX A CRACK WAS FOUND ON THE RUDDER TRIM ROD CUT OUT. APPROX RUDDER STA CSS 31.20. CRACK APPROX .375 INCH LONG. MX REMOVED DAMAGED AND REPAIRED THE AFFECTED AREA IAW EO-09-1900-27-001. RII INSPECTIONS COMPLIED WITH AND RUDDER BALANSDR GLBA20090605FSkin · dentedMAJOR REPAIR, DURING NORMAL LINE OPERATIONS A DENT WAS FOUND JUST FWD AND UNDER THE CARGO DOOR AT FS 446.5 1 INCH ABOVE WATERLINE MEASURING APPROX 1.2 INCH LONG, .250 INCH WIDE AND .063” DEEP. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-006. RII INSP COMPL
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