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 GUUA94953120809ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON ACFT BELLY SKIN AT FS 243.280 TO 258.280. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA95552120409AStrut · dischargedPILOT REPORTED PASSENGER DOOR VERY HEAVY TO OPERATE GAUGE READS 1,000 PSI. SERVICED PASSENGER DOOR STRUT TO 1,400 PSI OPS CHECK GOOD.SDR GUUA95432120409ACircuit Board · malfunctionedDURING FLIGHT, LANDING GEAR HANDLE LIGHT WITH HORN REMAINED ILLUMINATED FOR THE ENTIRE DURATION OF THE FLIGHT. REPLACED PC BOARD A406. LANDING GEAR OPERATIONAL CHECK GOOD.SDR GLBA20091202BTransmitter · malfunctionedRT ENG WENT INTO AND OUT OF FEATHER ON SHORT FINAL. MX TROUBLESHOT THE SYS AND FOUND THE TORQUE INDICATION BAD. MX REMOVED AND REPLACED THE TORQUE TRANSMITTER IAW MM 77-10-00. OPS CHECK OF THE AUTOFEATHER SYS WAS GOOD IAW MM 61-20-00.SDR GUUA94957120109BStringer · corrodedDURING SCHEDULED RT WING X-RAY INSP, DISCOVERED SPOTS OF CORROSION ON FWD BONDED STRINGER OTBD OF WS 124.25. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR STRAP.SDR GUUA94957120109ASpar · corrodedDURING SCHEDULED LT WING X-RAY INSP, DISCOVERED SURFACE CORROSION ON MAIN SPAR AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION AND INSTALLED AN INTERNAL REPAIR STRAP AND EXTERNAL DOUBLER REPAIR.SDR GLBA20091130JFrame · crackedDURING ROUTINE SCHEDULED MX A CRACK IN THE FRAME AT THE STR CUTOUT OF STR 10 R WAS FOUND AT FS 456.0 CRACK APPROX .563" IN LENGTH. MAINTENANCE REPAIRED THE STRINGER SPLICE AT F.S. 451.0 STRINGER 10R AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1SDR GLBA20091130HStringer · crackedDURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN STR 10R SPLICE AT FS 451.0. CRACK LENGTH IS APPROX.5" IN LENGTH. MAINTENANCE REPAIRED THE STRINGER SPLICE AT F.S. 451.0 STRINGER 10R AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-53-039. MASDR GLBA20091130KStringer · crackedDURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT FS 451.0 ON THE RELIEF CUTOUT OF STR 10R CRACK APPROX .625" IN LENGTH. MAINTENANCE REPAIRED THE CRACK IN THE FRAME RADIUS AT F.S. 451.0 AND STRINGER 10R AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. SDR GLBA20091130FSkin · corrodedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX CORROSION ON THE BELLY SKIN WAS FOUND AT FS 213.25 5 INCHES TO THE RT OF STRI GER 16R CORROSION BETWEEN STRINGERS 15R AND 16R. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED A FILLER /REPAIR DOUBLER AT F.S. 213.25 BESDR GUUA94957113009ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WS 133.86 TO WS 173.50. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR GUUA93532112909ALight · inoperativePILOT REPORTED LANDING GEAR HANDLE LIGHT WILL NOT ILLUMINATE WITH PWR BELOW 90 PERCENT N1 AND PULLED ALL THE WAY BACK. PERFORMED LANDING GEAR OPS CHECK. TEST FLIGHT SATISFACTORY.SDR GUUA94132112909APressure Switch · out of adjustPILOT REPORTED DELAY IN NOSE WHEEL EXTENSION 4 SECONDS AFTER MAINS. REPLACED HYD PRESSURE SWITCH AND ADJUSTED NLG DOWN POSITION SWITCH. LANDING GEAR OPS CHECK NORMAL.SDR GLBA20091130GAutofeather Sys · malfunctionedSUSPECTED AUTOFEATHER - PILOTS REPORTED THE RT PROP AUTOFEATHERED IN FLIGHT WHILE REDUCING TORQUE FROM 2500 LBS TO 500 LBS. TOR4QUE LEVELS WERE EVEN THROUGHOUT PWR REDUCTION. MX ADJUSTED THE FLIGHT IDLE TORQUES ON THE RT AND LT ENG IAW MM 76-10-00. OPS CHECSDR GLBA200911301Linkage · out of adjustRT AUTO FEATHER ENGAGED ON APPROACH TO LANDING AT 780 FT AGL AS PWR WAS INCREASED FROM IDLE THROUGH 600LBS OF TORQUE. WHEN THE AUTO FEATHER ENGAGED IT WENT IN AND OUT OF FEATHER SEVERAL TIMES BEFORE MORE PWR WAS APPLIED AND THE AUTO FEATHERING CYCLE STOPPED OSDR GUUA93652112809BCable · frayedPILOT REPORTED CABIN DOOR CABLES APPEAR TO BE BINDING AND VERY DIFFICULT TO CLOSE AND LOCK CABIN DOOR. REPLACED CABIN DOOR FWD BOTTOM CABLE ASSY.SDR GUUA93652112809ACamlock · stuckPILOT REPORTED UNABLE TO CLOSE CABIN DOOR APPEARS CAMLOCKS ON AFT SIDE OF DOOR ARE NOT ROTATING. REPLACED AFT UPPER AND LOWER CABIN DOOR CABLES. OPS CHECK NORMAL.SDR GLBA20091127091Autofeather Sys · malfunctionedSUSPECTED AUTOFEATHER - UPON APPROACH, THE PILOTS REPORTED THAT THE RT PROPELLER AUTOFEATHERED WITH TORQUE AT APPROX 1000 LBS. MX PERFORMED THE AUTOFEATHER OPERATIONAL CHECK 5 TIMES AND ALL INDICATIONS WERE WELL WITHIN LIMITS. NO DEFECTS NOTINE IN DURING THE SDR GLBA20091127FAngle · crackedDURING ROUTINE SCHEDULED MX, THE LT HEAVY ANGLE WAS FOUND CRACKED AT FS 303.25. ONE CRACK EXTENDING APPROX 1.3" ON EITHER SIDE OF 303.25. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-036. RII INSPECTIONS COMPLIED WITH IAW EO 09-1900-53-036. MATERIALS UTILISDR GLBA20091127HSkin · crackedDURING ROUTINE SCHEDULED MX CRACKS WERE FOUND AROUND RIVETS ON THE FUSELAGE SKIN ABOVE THE AIRSTAIR DOOR AT FS 163.975. 3 CRACKS NOTED TOTALING APPROX .875". MAINTENANCE REMOVED DAMAGED PATCH AND INTALLED FILLER AT F.S. 163.975 STRINGER 1 AND PERFORMED THE SDR GLBA20091127GSkin · crackedDURING ROUTINE SCHEDULED MX CRACKS WERE FOUND AROUND RIVETS ON THE FUSELAGE SKIN ABOVE THE AIRSTAIR DOOR AT FS 150.6. MAINTENANCE REMOVED DAMAGED SKIN AND INTALLED PATCH AT F.S. 150.6 STRINGER 1 AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-SDR GUUA94357112409ASpar · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED RT WING LWR AFT SPAR ON COLLECTOR TANK HAS SMALL SPOT OF SURFACE CORROSION BETWEEN WS 114.25 TO 124.25. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP. NOTE: PREVIOUSLY SUBMITTED, OPEN.SDR GUUA93557112409AStringer · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED RT WING BONDED STR HAS AREA OF CORROSION AT WS 125. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR DOUBLER.SDR GLBA20091124GFrame · crackedDURING ROUTINE SCHEDULED MX, A CRACK ON FRAME AT STR 9R AND FS 163.975 WAS FOUND AT THE RELIEF CUTOUT. CRACK LENGTH APPROX .375 ". MAINTENANCE REPLACED THE RIGHT HAND HEAVY ANGLE/CLOSING ANGLE AT F.S. 303.25 AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.SDR GLBA20091124FSkin · damagedDURING ROUTINE SCHEDULED MX, SEVERAL DAMAGED FASTNER HOLES ON THE RT WING ON THE AFT SPAR LOWER CAP. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-57-007. RII INSPECTIONS COMPLIED IAW EO 09-1900-57-007. MATERIALS UTILIZED ARE INCLUDED IN THE EO INSTRUCTIONS.SDR CA100217003Elbow · fractured(CAN) DURING BOLT REPLACEMENT CAMPAIGN RGB OIL PRESSURE TRANSFER ELBOW PN 3100470-01 WAS VISUALLY INSPECTED AND FOUND THE OTBD MOUNTING PAD ATTACHMENT LOOP FRACTURED. (TC 20100217003)SDR GUUA95452112209BDoor · stiffDURING SCHEDULED ROUTINE INSP, DISCOVERED SEAT 6A EMERGENCY EXIT DOOR HARD TO OPEN. LUBRICATED SEAT 6A EMERGENCY EXIT DOOR INNER AND OUTER HANDLES, OPS CHECK OK.SDR GUUA95452112209ADoor · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED SEAT 4F EMERGENCY DOOR HARD TO OPEN. LUBRICATED SEAT 4F EMERGENCY EXIT DOOR INNER AND OUTER HANDLES, OPS CHECK OK.SDR GLBA200911221Indicator · inoperativeUPON APPLICATION OF TAKEOFF POWER ON RUNWAY, THE NR 2 PROP GAUGE WENT TO ZERO.SDR GLBA20091120AGauge · inoperativeABORTED TAKEOFF - UPON APPLYING TAKEOFF POWER ON THE RUNWAY, PILOTS REPORTED THAT THE NR 2 PROPELLER GAUGE WENT TO ZERO. MX REMOVED AND REPLACED THE NR 2 PROPELLER GAUGE IAW MM 31-10-00 AND OPERATIONALLY CHECKED THE SYS WHICH WAS GOOD.SDR GLBA1123GSpar · damagedDURING ROUTINE SCHEDULED MX SIX FASTNER HOLES WERE FOUND DAMAGED AT THE LT INBD FLAP TRACK AREA. WS 46.500. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-57-007. RII INSPECTIONS COMPLIED WITH IAW EO 09-1900-57-007. MATERIALS UTILIZED ARE INCLUDED IN THE EO INSDR GLBA20091123FAngle · crackedDURING ROUTINE SCHEDULED MX, THE RT HEAVY ANGLE WAS FOUND CRACKED AT FS 303.25. MAINTENANCE REPLACED THE RIGHT HAND HEAVY ANGLE/CLOSING ANGLE AT F.S. 303.25 AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-53-031. MATERIALS UTILIZED FOR THE RSDR GLBA20091120FBleed Air Sys · contaminatedSMOKE/SMELL - PILOTS REPORTED THAT BURNING ODOR WAS PRESENT FROM THE CAPTAINS SIDE THAT SMELLED LIKE PLASTIC. NO SMOKE WAS OBSERVED. MX CLEANED GLYCOL FROM WINDOW DRIP TRAY AND INSPECTED THE FUEL PANEL FOR ANY EVIDENCE OF GLYCOL. NONE NOTED. MX RAN THE ACSDR GUUA93932111709AHose · leakingDURING CRUISE FLIGHT LANDING GEAR LIGHT ILLUMINATED AND GEAR CIRCUIT BREAKER POPPED. DIVERTED, MANUALLY EXTENDED LANDING GEAR, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ACTUATOR HOSES, OPS CHECK GOOD.SDR GUUA95753111609ASkin · damagedDURING SCHEDULED ROUTINE MX, DISCOVERED EMERGENCY EXIT 6F HAS SKIN DAMAGE UNDER WINDOW PAN. BLENDED DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR GUUA93721111509ALine · leakingPILOT REPORTED VERY STRONG CHEMICAL ODOR INSIDE PLANE. REPLACED RT ENGINE PRESSURE FUEL LINE, OPS CHECK OK.SDR GLBA200911141Wire · chafedAIR RETURN - THE PILOTS REPORTED THAT LANDING GEAR CIRCUIT BREAKER POPPED IN CRUISE AND WHICH RESULTED IN A RETURN TO "DEN". MX REPAIRED 4 CHAFED WIRES THAT WERE FOUND AT THE LT UPLOCK SWITCH HARNESS IAW AC 43-13-1B CHAPTER 11 SECTION 13. GROUND POWER WAS APSDR GUUA93721111409AIntake · contaminatedPILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE CLEANED AREA OF OIL. PREVIOUSLY SUBMITTED CORRECTED DATE.SDR GUUA93721110409AIntake · contaminatedPILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE. CLEANED AREA OF OIL.SDR GUUA94157111409AAccess Panel · delaminatedDURING SCHEDULED ROUTINE MX DISCOVERED RT WING FUEL ACCESS PANEL 631DB LEAKING FUEL. INSTALLED EXTERNAL RING DOUBLER ON WING SKIN AT FUEL ACCESS PANEL 631DB, NO LEAKS NOTED.SDR GLBA20091116FBrace · chafedMX DISCOVERED THAT THERE WAS CHAFING ON THE FWD RT SIDE OF THE RT MLG BRACE CTR TUBE APPROX 11 INCHES FROM TOP. CHAFE IS APPROX AT A 45 DEGREE ANGLE AND MEASURES .5 INCHES LONG, .310 INCHES WIDE AND .020 INCHES MAX DEPTH. CHAFE ON FWD RT SIDE OF THE MLG BRACSDR CA091112002Actuator · cracked(CAN) ON PILOTS WALK AROUND AT NON MX STA. PILOT FOUND HYD FLUID COMING FROM THE NOSE GEAR AREA. ON INSP FOUND FLUID LEAKING FROM ACTUATOR END CAP.SDR GUUA94652111109ADoor · obstructedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. ADJUSTED RT AFT EMERGENCY EXIT DOOR UPHOLSTRY, DOOR OPERATES SMOOTHLY.SDR GLBA20091111FSpar · damagedDURING ROUTINE SCHEDULED MX, DISCOVERED 2 LOCK FASTENER HOLES MISDRILLED (HOLES ARE STEPPED) AT/ON THE LT WING, AFT WING SPAR ON THE FWD SIDE OF THE SPAR AT WS 127.288 AND 129.588. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTSDR GUUA95753111009ASkin · corrodedDURING SCHEDULED ROUTINE MX, DISCOVERED CORROSION ON FUSELAGE BELLY SKIN AT FS 228, STRINGER 14L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR GUUA94532111009AUplock Switch · out of adjustDURING CLIMB, RED GEAR WARNING LIGHT IN HANDLE STAYS ILLUMINATED IN FLIGHT WITH GEAR IN THE UP POSITION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR UPLOCK SWITCH. LANDING GEAR OPS CHECK GOOD.SDR GUUA91221110809ALine · leakingDURING TAKEOFF CRUISE AND DESCENT, SAME DISGUSTING ODOR COMES THROUGH EYEBALL VENTS. REPLACED RT ENGINE HIGH PRESSURE FUEL LINE.SDR GUUA92752110809AStructure · loosePILOT REPORTED PLASTIC CASING ON INSIDE AIRSTAIR DOOR GETS CAUGHT ON DOOR JAM WHEN TRYING TO OPEN DOOR. SECURED AIRSTAIR DOOR FWD TRIM PANEL AND HARDWARE. OPS CHECKS GOOD.SDR GLBA20091110HSpar · damagedDURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, A HOLE WAS FOUND TO BE STEPPED AND OVERSIZED AT THE LEFT HAND WING SPAR W.S. 104.0. APPROXIMATE DIAMETER OF .230". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIOSDR GLBA20091110GSpar · damagedDURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, PART OF AN EXISTING RIVET WAS IN THE HOLE UPON REMOVING THE RIVET THE DIAMETER OF THE HOLE WAS FOUND TO BE APPROXIMATELY .230" ACROSS AT LEFT HAND WING SPAR W.S. 114.250. MAINTENANCE REPAIRED
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