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 GLBA20110405HStringer · bentMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND STRINGER 12L BENT AT FS 47.5, STRINGER 12L BENT 5" FROM FS 47.5 GOING AFT ALONG STRINGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-19SDR GLBA20110405GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FWD FUSELAGE FRAME AT F.S. 456 CRACKED AT THE GAS STRUT MOUNT UPPER IB NUTPLATE AREA, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSSDR GLBA20110405JSkin · chafed"SUP" - MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND RH OB FWD CORNER OF FUSELAGE BELLY SKIN AT F.S. 258.25 CHAFFED THROUGH, AREA OF CHAFE 2.2" BY .6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSSDR GUUA94955040511BStringer · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STAB RT SIDE APPEARS TO HAVE CRACKS AT EACH OF THE 3 CHORD STRINGERS AT CSS 54.026. STOP DRILLED CRACKS AND INSTALLED REPAIR STRAPS THREE EACH.SDR GUUA94955040511ARib · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER LT SIDE, 1 CRACK AT CSS 54.026. STOP DRILLED CRACK AND INSTALLED REPAIR STRAP.SDR GUUA93852040511ACable · brokenPILOT REPORTED MAIN CABIN DOOR UPPER RT CAM LOCK WILL NOT ROTATE. DOOR WILL NOT OPEN OR LOCK PROPERLY. REPLACED AIRSTAIR DOOR FWD UPPER AND LOWER CABLES. OPS CHECK GOOD.SDR GLBA20110404FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CUTOUT IS CRACKED AT THE IB LWR CORNER OF THE COUTOUT, CRACK IS .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUSDR ERAA201100003Actuator · crackedAFTER LANDING FLIGHT CREW NOTED HYDRAULIC FLUID LEAKING FROM LEFT MAIN LANDING GEAR. MAINTENANCE FOUND LMLG ACTUATOR END CAP CRACKED AND LEAKING. REPLACED ACTUATOR WITH OVERHAULED. FAILED UNIT SUBJECT TO 1200 CYCLE REPETITIVE ULTRASONIC INSPECTION OF THE ENSDR GUUA94276040411APropeller · malfunctionedPILOT REPORTED WHEN PULLING PROPS BACK FROM 1550 RPM ON THE DESCENT TO 1400 RT PROP LAGGED ABOUT A KNOB AND HALF FROM LT SIDE PROPS WERE OUT OF SYNC AND COULD NOT GET INTO SYNC. WHEN PROPS PUSHED FULL FWD LT PROP REACHED ABOUT 1700 RPM WHILE RT PROP INCREASEDSDR GUUA93653040311ABulkhead · crackedDURING SCHEDULED ROUTINE OXYGEN INSP DISCOVERED A CRACK ON INBD LT PRESSURE BULKHEAD AT FS 84.00. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER AT LT PRESSURE BULKHEAD F/A 84.00.SDR GUUA94732032811AControl Handle · stiffPILOT REPORTED LANDING GEAR HANDLE STIFF TO LOWER IT FEELS LIKE ITS CATCHING. INSPECTED CLEANED J HOOK AND HANDLE SLIDE, ASSY CYCLED GEAR SEVERAL TIMES LANDING GEAR OPS CHECK GOOD, NO DEFECTS NOTED.SDR CA110413001Gas Generator · seized(CAN) UNCOMMANDED SHUTDOWN DURING FLIGHT TEST FOR CERTIFICATE OF APPROVAL PURPOSES, THE ENGINE WAS SHUTDOWN AND RELIT IAW OPERATING HANDBOOK. 2 MIN AFTER RE-LIGHT, THE ENGINE SHUTDOWN UNCOMMANDED AND COULD NOT BE RE-STARTED. AN UNEVENTFUL SINGLE ENGINE LANSDR ERAA201100002Reservoir · lowON LANDING APPROACH PILOT REPORTED "NOSE GEAR LIGHT FAILED TO ILLUMINATE & RED HANDLE LIGHT REMAINED ILLUMINATED UPON GEAR SELECTED DOWN". REPLENISHED RESEVOIR & PERFORMED MULTIPLE GEAR SWINGS SATISFACTORY REF HB 1900D MM 32-30.SDR GUUA94761032711ACircuit Board · looseLT AUTOFEATHER-INOPERATIVE. FLASHES AFX ON TAKEOFF THEN GOES OUT. R & R PCB A123. OPS CHECKS NORMAL.SDR GUUA92756032711AWindshield · crackedAS ACFT CROSS THE COASTLINE ON THE APPROACH FOR 10L THE CAPTAIN SIDE WINDSHIELD CRACKED. THE INNER WINDOW PANE MADE NUMEROUS CRACK LINES BUT STAYED INTACT. DECLARED AN EMERGENCY, RECEIVED PRIORITY AND LANDED WITHOUT FURTHER INCIDENT. R & R CAPTAINS WINDSHIELSDR GUUA94553032511ASkin · corrodedDURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON EXTERIOR SKIN AT STRINGER 15R, APPROX FS 258. REMOVED CORROSION AND INSTALLED 3 X 5 INCH INSERTION PATCH AND 5 X 8 INCH COVER PATCH.SDR GUUA94553032411DStringer · debondedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 15R DEBONDED AT APPROXIMATELY FS 235. INSTALLED EXTERNAL REPAIR DOUBLER STRINGER 15R FROM FS 229 TO FS 241.SDR GUUA94553032411CStringer · debondedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 15R DEBONDED AT APPROXIMATELY FS 378 AND FS 398. INSTALLED EXTERNAL REPAIR DOUBLER STRINGER 15R FROM FS 478 TO FS 400.SDR GUUA94553032411BStringer · debondedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 15L DEBONDED AT APPROXIMATELY FS 412. INSTALLED EXTERNAL REPAIR DOUBLER STRINGER 15L FROM FS 404 TO FS 421.SDR GUUA94553032411AStringer · debondedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 14L DEBONDED AT APPROXIMATELY FS 412 AND FS 398. INSTALLED EXTERNAL REPAIR DOUBLER FROM FS 392 TO FS 412.SDR GUUA95755032411BRib · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL CANTED STABILIZER RIB CRACKS AT RIGHT NR 4 STRINGER AT STATION 89.184. STOP DIRILLED CRACK AT RIGHT VERTICAL STABILIZER RIB NR 4 STRINGER AND INSTALLED REPAIR DOUBLERS.SDR GUUA95755032411ARib · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL CANTED STABILIZER RIB CRACKS AT LEFT NR 2, 3 AND 4 STRINGERS AND RIGHT NR 3 STRINGER AT STATION 54.026. STOP DIRILLED ALL CRACKS VERTICAL STABILIZER RIBS LEFT AND RIGHT SIDE AND INSTALLED REPAIR DOUBLESDR GUUA95752032411BHandle · stiffDURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT INNER HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT INNER AND OUTER HANDLES.SDR GUUA95752032411AHandle · bindingDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT OUTER HANDLE STICKS WHEN OPERATED. LUBRICATED RT FWD EMERGECNY EXIT DOOR INNER AND OUTER HANDLES.SDR GUUA93521032411AController · malfunctionedPILOT REPORTED CABIN PRESSURIZATION 5.2 PSID UNTIL REACHING 17,000 FT AT LEVEL OFF CABIN BEGAN A 6,000 FPM CLIMB UNTIL REACHING AROUND 1 PSID AT THAT TIME CABIN PRESSURIZED AT 1-1.5 PSID THE REMAINDER OF THE FLIGHT NO NOISE OR RUSH OF AIR WAS OBSERVED. CLEANESDR GUUA94932032411ARelay · shortedPILOT REPORTED LANDING GEAR WILL NOT RETRACT. CONTINUED, LANDED WITHOUT INCIDENT. REPLACED K3 RELAY LANDING GEAR OPS CHECK GOOD.SDR GUUA93652032311AHandle · lack of lubeDURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT WILL NOT OPEN FROM INSIDE HANDLE. LUBRICATED RT AFT EMERGENCY EXIT DOOR. ACFT DOWN FOR MAJOR REPAIR.SDR GUUA94553032311ADoor Frame · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED CRACK 5.0 INCHES INTERIOR UPPER CARGO DOOR FRAME APPROX AT FS 496 TO 501. STOP DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR GUUA93653032311ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED FUSELAGE SKIN SHOWS SIGNS OF CORROSION AT FS 408.25 BL 0.00. REMOVED DAMAGED SECTION OF STRINGER AND SKIN AND INSTALLED STRINGER SPLICE REPAIR AND AN EXTERNAL DOUBLER REPAIR.SDR GUUA94053032211ASkin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUSELAGE BELLY SKIN EXFOLIATED IN ONE SPOT AT FS 349.00 JUST AFT OF VCS SERVICE DOOR. REMOVED DAMAGE SKIN AND STRINGER AND INSTALLED STRINGER REPAIR AND AN EXTERNAL DOUBLER REPAIR.SDR GLBA20110322FSkin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND CORROSION ON THE BELLY SKIN JUST AFT OF THE ADF ANTENNA MEASURING .75". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-018. MATERIALS UTILIZED ARESDR GUUA93357031611CSkin · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED CORROSION RT WING LOWER SKIN NR 2 STRINGER IN COLLECTOR TANK INBD OF MAIN DRAIN. REMOVED SURFACE CORROSION PERFORMED FLOURESCENT PENETRANT INSPECTION NO FURTHER CORROSION FOUND.SDR GUUA93357031611BSkin · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED CORROSION RIGHT WING LOWER SKIN RIB IN COLLECTOR TANK FORWARD OF MAIN SPAR OUTBOARD WS 125.25. REMOVED SURFACE CORROSION PERFORMED FLOURESCENT PENETRANT INSPECTION NO FURTHER CORROSION FOUND.SDR GUUA93357031611AStringer · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED MINOR CORROSION ON LEFT WING NR 1 STRINGER IN THE COLLECTOR TANK WS 124.25-114.25. REMOVED CORROSION AND INSTALLED REPAIR STRINGER AND REPAIR DOUBLERS.SDR GLBA201103171Wire · chafedPILOT REPORTED THAT THE #1 FIRE BOTTLE "DISCH" ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND FOUND A CHAFFED WIRE GOING TO THE LH FIRE BOTTLE, REPAIRED WIRE AND SPLICED IAW AIM 12.8.0, OPS CK GOOD.SDR GUUA94531031511AEngine · malfunctionedPILOT REPORTED NR 1 ENG N1 AND TORQUE DECREASED CONTINUOUSLY IN FLIGHT WHEN TORQUE REACHED 0 ENGINE SECURED. DIVERTED, LANDED WITHOUT INCIDENT. (OPEN)SDR GUUA94577031511AHeater · damagedPILOT REPORTED LT ENGINE N1 AND TORQUE DECREASED CONTINUOUSLY IN FLIGHT TORQUE, WHEN TORQUE REACHED ZERO. DIVERTED, SECURED THE LT ENGINE, LANDED WITHOUT INCIDENT. REPLACED LT ENGINE FUEL TO OIL HEATER. OPS CHECKED GOOD, TEST FLIGHT SATISFACTORY. PREVIOUSLYSDR GUUA94531031411AFuel Control · failedPILOT REPORTED INFLIGHT THE LEFT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED, DECLARED AN EMERGENCY DIVERTED TO JAX SECURED THE ENGINE LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL CONTROL AND HIGH PRESSURE FUEL PUMP GROUND PERFORMANCE CHECK WITH POWER ASDR GUUA95557031211BStringer · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED LT WING CORROSION ON STRINGER FWD OF SPAR 1.270 X 0.30 INCHES AT WS 124.25. REMOVED CORROSION FROM LEFT WING LOWER FORWARD SPAR FORWARD FLANGE COMPLIED WITH FLOURESCENT PENETRANT INSPECTION NO SIGNS OF CORROSION FOUND.SDR GUUA95557031211ASpar · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED RT WING CORROSION ON MAIN SPAR 1.3 X 0.06 INCHES AT WS 124.25. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT PENETRANT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND ALL ARESDR GUUA95152030711AHandle · stickingDURING SCHEDULED ROUTINE MX DISCOVERED LT EMERGENCY EXIT HANDLES STICKING. LUBRICATED LT EMERGENCY EXIT HANDLES, OPS CHECK NORMAL.SDR GUUA93371030711ATruss · crackedDURING MAG PARTICLE INSP, DISCOVERED ENGINE TRUSS TUBE WELD AREA CRACK. (OPEN)SDR GLBA20110307GSpar · wornMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE LH WING REAR SPAR BOTTOM LEADING EDGE CHAFFED AT 2 LOCATIONS BY EXT PWR CABLE, OB CHAFF .4" IN LENGTH .1" DEEP, IB CHAFFR .3" IN LENGTH .05" DEEP. MAINTENANCE REPAIRED THE AFFECTED ARESDR GLBA20110307FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT STABILON OB TIP DAMAGED WHILE PARKING IN HANGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-55-005. MATERIALS UTILIZED ARE INCLSDR GLBA20110308GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME CRACKED 1.5" IN LENGTH AT THE GAS STRUT MOUNT UPPER IB NUT PLATE, FS 509 BETWEEN STRINGERS 4L & 5L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED ASDR GLBA20110308HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FRAME AT THE FWD GAS STRUT MOUNT CRACKED IN TWO PLACES 1.5" IN LENGTH AT FS 456 BETWEEN STRINGERS 3L & 4L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFSDR GLBA20110304FStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT OB WHEEL WELL KEEL ATTACHING HOLES FOR OB FENDER BRACKET HAS ELONGATED HOLES. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-54SDR GLBA20110304JSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER FUSELAGE SKIN AT F.S. 288 AND STRINGER 1 IS CRACKED, CRACK RADIATES FORWARD FROM FASTENER .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSSDR GLBA20110304KSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER SKIN CRACKED AROUND (7) FASTENERS AT FS 273 BETWEEN STRINGER 1 AND 2R, CRACKS RANGE FROM .4" TO .2" IN LENGTH. SOME FOUND WITH EDDY CURRENT. MAINTENANCE REPAIRED THE AFFECTED ARESDR GLBA20110304HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME CRACKED .3" IN LENGTH AT STRINGER 9AR CUTOUT AT F.S. 177. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-014. MAT
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