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 GLBA2015092200547Skin · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT BELLY SKIN AT APPROX FS 303.25 & BL 29.06, 1.25" IN LENGTH. REPAIRED IAW EO 15-1900-53-017.SDR GLBA2015092200546Skin · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND 3 CRACKS IN THE LT FUSELAGE SKIN, AT THE LT VORTEX GENERATOR, LOCATED BETWEEN FS 232.25 & 248.25, LOCATED AT THE BOTTOM OF STRINGER 12L, TOTAL 3.35" IN LENGTH. REPAIRED IAW EO 15-1900-53-016.SDR GLBA2015092200545Skin · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK AT THE EMERGENCY EXIT 6A SKIN, AT THE INNER LOWER FWD CORNER, .55" IN LENGTH. REPAIRED IAW EO 15-1900-52-001.SDR GLBA2015092200544Skin · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE SKIN CRACKED AT FS 100.500, JUST BELOW FIRST OFFICERS WINDSHIELD, BOTTOM OTBD CORNER, .625" IN LENGTH. REPAIRED IAW EO 15-1900-53-15.SDR GLBA2015092200543Skin · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EMERGENCY EXIT 6C SKIN, CRACKED AT THE INNER LOWER AFT CORNER, .8" INCHES LENGTH. REPAIRED IAW EO 15-1900-52-002.SDR V0DR20150922003Cover · wornFUEL NOZZLE SHEATHS HAVE SIGNS OF CONTACTING THE TOP OF THE FUEL NOZZLE & THE SHEATH DOME AREA.SDR CA150922008Wire · shorted(CAN) CREW REPORTED ISSUES WITH THE NR 2 COMM SYSTEM. TROUBLESHOOTING REVEALED WIRE J298001 AT A107 CIRCUIT CARD SHORTED IN THE NOSE AVIONICS COMPARTMENT ON THE RT SIDE. WIRE WAS FOR THE SWITCH POWER OUTPUT FROM THE COM CONTROL HEAD AND WAS CAUSING THE CONTRSDR GLBA2015092100542Bulkhead · dentedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND DENTS AT BULKHEAD AT FS 84.00, BETWEEN THE FIRST & SECOND DOUBLER FROM THE LT OTBD EDGE. DENT AREA IS 4" FROM LT TO RT & 6.7" UP & DOWN, DEEPEST DENTED AREA MEASURES AT APPROX .23". ALSO FOUND TWO SMALL DENTSDR GLBA2015091800541Door Frame · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THAT THE AIRSTAIR DOOR FRAME LOWER FWD CORNER AREA, FS 150 & STRINGER 11L, IS CRACKED APPROX .50 INCHES IN LENGTH. CRACK RADIATES OTBD FROM THE CUT OUT. THE CUT OUT IS APPROX 3 INCHES UPWARD FROM THE LOWER ESDR GLBA2015091800540Angle · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THAT THE ANGLE LOCATED AT FS 150.60 IS CRACKED IN AN AREA AT THE AIRSTAIR DOOR STRUT UPPER MOUNT BRACKETS, LOWER AFT SCREW HOLE. REPAIRED IAW EO 15-1900-53-009.SDR GLBA2015091800539Skin · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE INNER SKIN AT FS 150.60, BETWEEN STRINGERS 7L & 6L IS CRACKED, APPROX 1.5" IN LENGTH AT THE AIR STAIR DOOR STRUT'S UPPER MOUNT BRACKETS, LOWER AFT ATTACHING SCREW HOLE ACCESS. SUPPLEMENTAL INFORMATION WILSDR GLBA2015091800538Pin · out of positionSIGNIFICANT EVENT, PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER PIN CAME OUT. INSTALLED SAME AIR STAIR DOOR SNUBBER & COUNTER BALANCED ASSEMBLY. REPLACED STUD, PN 129-514123-1, NO FURTHER DEFECTS NOTED AT THIS TIME.SDR GLBA2015091600537Tire · blownTHE NR 1 TIRE BLEW ON LANDING. THE TIRE DEVELOPED A FLAT SPOT DURING BRAKING THAT RESULTED IN LOSS OF TIRE PRESS. R & R THE NR 1 WHEEL ASSEMBLY IAW TC 1900-3240.00. PN 5006028-5, SN ON 1325, SN OFF 1681. OK FOR CONTINUED SERVICE.SDR CA150915006Switch · out of adjust(CAN) DURING A FLIGHT THE CREW NOTICED THAT THE CARGO DOOR LIGHT WAS ILLUMINATED. DECISION WAS MADE TO DIVERT TO THE MAINTENANCE BASE TO ASSESS SITUATION. THE ACFT LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE DISCOVERED THAT THE CARGO DOOR UPPER FORWSDR CA150914011Handle · cracked(CAN) DURING GROUND HANDLING OPERATIONS THE RAMP AGENT REPORTED TO THE CREW THAT THE CARGO DOOR WAS NOT FUNCTIONING PROPERLY. MAINTENANCE WAS CONTACTED AND INSPECTION OF THE DOOR REVEALED THAT THE DOOR HANDLE ASSEMBLY P/N: 114-514035-29 WAS FOUND CRACKED. RESDR GLBA2015091000535Skin · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 243.25 & STRINGER 15L. REPAIRED IAW EO 15-1900-52-012.SDR GLBA2015091100536Autofeather Sys · unknownSIG EVENT, PILOT REPORTED THAT THE LT PROP AUTO FEATHERED WHEN INTRODUCING POWER FROM FLIGHT IDLE. TESTED AUTO FEATHER SYS SEVERAL TIMES IAW MM 61-21-00, SYS OPERATED NORMAL.SDR GLBA2015091000534Frame · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK ON THE FWD FRAME FLANGE AT FS 177.35 BETWEEN STRINGER 14L & 13L, 1" IN LENGTH. REPAIRED IAW EO 15-1900-53-011.SDR GLBA2015082600532Skin · crackedFOUND THE LT INBD LE INSIDE SKIN HAS SEVERAL AREAS OF CHAFING FROM THE CONTROL CABLES RUBBING & HOLES, A .5" SHALLOW HOLE & CHAFE MARKS, A .375", .125" HOLES IN SKIN ONLY, SHALLOW HOLE, SMALL .25" WEAR HOLE, .75" TEAR IN THE EDGE OF THE SKIN & A CRACK, .25" INSDR GLBA2015082000531Snubber · detachedSIG EVENT, PILOT NOTED THAT THE CABIN DOOR SNUBBER DETACHED IN FLIGHT. LOCATED THE UPPER BOLT FOR THE AIRSTAIR DOOR SNUBBER ON THE FLOORBOARD. INSPECTED THREADS ON THE BOLT & RECEPTACLE, NO DEFECTS NOTED. REINSTALLED UPPER BOLT IAW AIM 12 15 0, NO FURTHER DSDR CA150724006Relay · failed(CAN) ON TAKEOFF, THE CREW HAD THE NR 2 AC BUS FAIL IN FLIGHT. THE CREW ELECTED TO RETURN TO DEPARTURE WHERE MAINTENANCE COULD ASSESS THE ISSUE. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED DURING TROUBLESHOOTING THAT THE NR 2 INVERTER PSDR V0DR20150722002Retainer · detachedUPON WALK AROUND ONE OF THE PILOTS REPORTED THAT A ORING WAS LOCATED IN THE MIDDLE OF THE LANDING GEAR STRUT. MAINTENANCE DETERMINED THE ORING IN QUESTION WAS THE STRUT AXLE ASSY SCRAPER RING HAD COME LOOSE FROM ITS RETAINER. NO REPORT OF THE LANDING GEAR LOSDR CA150811003Fitting · cracked(CAN) DURING ABC STRUCTURAL INSPECTION SECTION UNDER CABIN FLOOR, ITEM 37, FIGURE 27 THE RT FRAME BS 288 AT LOWER TUB FITTING ON WING SPAR WAS FOUND CRACKED. REPAIR CARRIED OUT IAW CAS ENGINEERING EA B1900-53-008. DAMAGE REMOVED. NDT CARRIED, CIRCULAR PLUG ISDR CA150720003Spar · corroded(CAN) CORROSION FOUND ON RH WING SPAR AT WS 24.025 DURING INSPECTION. RECTIFICATION: REPAIR CARRIED OUT IAW FR-CO-105218 REV 2. CORROSION BLENDED OUT. NDT CARRIED OUT TO ENSURE NO FURTHER DAMAGE. INTERNAL STRAP OF 7075-T3511 MADE & INSTALLED WET USING 9309.3NSDR CA150714001Wire · chafed(CAN) AFTER TAKEOFF DURING THE INITIAL CLIMB, THE CREW COULD NOT GET THE FLAPS TO RETRACT. THE CREW RETURNED TO ORIGIN & CONTACTED MX. THE FLAPS WERE RESET TO ZERO & THE ACFT WAS RELEASED UNDER THE MEL PROTOCOL & THE ACFT CONTINUED ITS RUN. ONCE THE ACFT WASDR CA150713020Wire Harness · chafed(CAN) LANDING GEAR CIRCUIT RELAY POPPED AFTER TAKEOFF. UNABLE TO DUPLICATE FAULT IN HANGAR. TROUBLESHOOTING CARRIED OUT BY MX & FOUND WIRES G15E22, G16C22, D10A22 & D21J22 AT RT MLG ACTUATOR CONNECTOR J198 CHAFED & ARCING AGAINST PANEL 622BT. WIRES WERE REPSDR GLBA2015071400526Angle · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A 2.8" CRACK IN AN ANGLE AT FS 456.0, AT FWD CARGO FLOOR LEVEL. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-008.SDR CA150710004Powerpack · malfunctioned(CAN) ON APPROACH THE CREW SELECTED LANDING GEAR TO THE DOWN POSITION AND THE CB POPPED AND GEAR DID NOT EXTEND. CB WAS RESET AND THE CB POPPED AGAIN. CREW DECIDED TO RETURN TO MAINTENANCE BASE. ON APPROACH THE GEAR WAS MANUALLY LOWERED AS PER CHECKLIST AND THSDR 7C7A201506080054Skin · damagedDAMAGE THROUGH RT ICE SHIELD & DENT IN FUSELAGE SKIN WITH STRINGER DAMAGE AT FS 195, WS 101. REPAIRED IAW ECO 190 53 15 04.SDR 7C7A201507080053Skin · dentedDENT FROM PROP THROWN ROCK, RT SIDE FUSELAGE STATION 178, WL 100. REPAIRED DENT DAMAGE IAW ECO 190 53 15 05.SDR CA150708008Light · inoperative(CAN) CREW PERFORMED A MISSED APPROACH DUE TO A GEAR ISSUE. THE CREW CANCELLED IFR AND COMPLETED ONE VFR CIRCUIT TO TROUBLE SHOOT THE GEAR ISSUE. AFTER TROUBLE SHOOTING WAS CARRIED OUT BY THE CREW IT WAS DETERMINED THAT A BURNT OUT BULB WAS AT FAULT. THE CRESDR GLBA2015070100525Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME AT FS 107 BY STRINGER 8L, PROTRUDING OUT OF RIVET ON EITHER SIDE, .25" IN LENGTH. REPAIRED IAW EO 15-1900-53-007. MAJOR REPAIR.SDR CA150713003Turbine Blades · fractured(CAN) DURING DESCENT FROM 15,000 FT, THE CREW REDUCED POWER & THE LT ENG BEGAN TO SURGE. POWER WAS FURTHER REDUCED TO IDLE & ENG CONTINUED TO SURGE. THE CREW ELECTED TO PERFORM A PRECAUTIONARY SHUTDOWN & ACTIVATE THEIR EMER PROCEDURES. THE ACFT LANDED UNEVESDR GLBA2015062300524Door Frame · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME AT FS 509.5, AFT SIDE OF CARGO DOOR FRAME AT MID-CARGO FLOOR LEVEL, .7" IN LENGTH. REPAIRED THE AFFECTED AREA. PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-006.SDR CA150720009Rib · corroded(CAN) DEFECT: CORROSION FOUND ON LH WS124 RIB FORWARD OF FORWARD WING SPAR.. RECTIFICATION: REPAIR CARRIED OUT IAW BEECHCRAFT FR-CO-105158. A ONE INCH RADIUS CUTOUT MADE ON LOWER FLANGE TO REMOVE ALL CORROSION. NDT CARRIED OUT TO ENSURE NO FURTHER DAMAGE WAS SDR CA150713011Hydraulic Line · ruptured(CAN) AFTER ENG SHUTDOWN, OBSERVED HYD FLUID DRIPPING FROM LT WW. INSPECTED LT GEAR WELL, FOUND RUPTURED EXTEND HYD LINE. LT MLG EXTEND, RETRACT & EMER EXTEND LINES REPLACED WITH NEW. AS A PRECAUTIONARY MEASURE RT MLG EXTEND, RETRACT & EMER EXTEND LINES REPSDR 7C7A201507090055Skin · dentedDENT ON LT WING OUTER LE AT WS 304.625. REPAIRED IAW SRM 57-94-02 & ECO 190 57 15 02.SDR CA150616007Wire · chafed(CAN) CREW REPORTED THAT THE ELEC TRIM WAS UNSERVICEABLE ON BOTH SIDES. DURING INVESTIGATION MX FOUND WIRES AT ELEC TRIM MOTOR CHAFED & ARCHING ON RT SIDE COVER. PREVIOUSLY WRAPPED IN SPIRAL WRAP BUT CUT THROUGH. WIRES WERE REPAIRED & PROTECTED, AS A PREVENSDR CA150616006Connector · corroded(CAN) ON TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR 2 AMP CIRCUIT BREAKER POPPED & THE GEAR WOULD NOT RETRACT. THE CREW DECIDED TO DIVERT TO MX BASE FOR MX TO ASSESS. THE ACFT LANDED WITHOUT INCIDENT & THE ACFT WAS HANDED OVER TO MX. DURING TROUBLESHOOSDR CA150626002Protector · unsecure(CAN) ON CLIMB OUT CREW NOTICED THEY COULD NO LONGER USE THE MANUAL TRIM. IT WAS JAMMED AT THE BOTTOM OF THE GREEN ARC. THE CREW CONTINUED THE CLIMB WHILE TROUBLE SHOOTING THE ISSUE. THE ELEC TRIM WAS TURNED ON & OFF WITH NO CHANGE. THE MANUAL TRIM WAS ATTSDR CA150603009Relay · faulted(CAN) WHILE ENROUTE AND IN CRUISE FLIGHT, THE CREW NOTICED THAT THE LANDING GEAR CONTROL 2A, CB2, CIRCUIT BREAKER HAD POPPED. AFTER CONSULTATION WITH MAINTENANCE THE DECISION WAS MADE TO ATTEMPT TO RESET THE CB ONCE. UPON ATTEMPTING TO RESET THE CB, IT POPPESDR CA150605005Connector · corroded(CAN) ON FINAL APPROACH THE CREW SELECTED GEAR DOWN IAW SOP AND DID NOT HEAR THE GEAR EXTEND, AS WELL THE GEAR IN TRANSIT LIGHT DID NOT ILLUMINATE. THE CREW BOTH VISUALLY CONFIRMED OUT THE WINDOW THAT BOTH MAINS WERE NOT DOWN AND THE LANDING GEAR RELAY CIRCUISDR CA150720010Spar · damaged(CAN) DAMAGED LT SPAR ABOVE LT FENDER BRACKET. REPAIR CARRIED OUT IAW FR-CO-104134. COLD WORKING PROCESS CARRIED OUT USING 8-0-N COLD WORKING KIT. NDT CARRIED OUT TO ENSURE NO FURTHER CRACKING WAS EVIDENT. ALL AFFECTED AREAS PREPPED/EPOXY PRIMED TO MEET MILSDR GLBA2015050800519Fastener · looseSIG EVENT, MX REPORTED THAT THE CABIN DOOR WILL NOT CLOSE FROM THE OUTSIDE OF ACFT. FOUND LOOSE HARDWARE AT THE INTERNAL HANDLE BELL CRANK. SECURED HARDWARE IAW AIM 12.15.0. OPERATIONS CHECKED GOOD.SDR CA150505009Blade · cracked(CAN) DURING 300 HOUR SCHEDULED COIN TAP TEST ON PROPELLER, IT WAS FOUND BY INTERPRETING THE SOUND DURING THE TEST THAT A SIGNIFICANT PORTION OF THE LEADING EDGE OF ONE OF THE PROPELLER BLADES WAS INDICATING A DELAMINATION & DEBONDING. THE LEADING EDGE JUST OSDR CA150506010Windscreen · cracked(CAN) WINDSCREEN CRACKED IN MULTIPLE LOCATIONS DURING FLIGHT.SDR GLBA2015042700515Check Valve · leakingSIG EVENT, PILOT REPORTED THAT THERE WAS A STRONG SMELL OF FUEL IN CABIN. REMOVED FLOORBOARDS & INSPECTED FUEL TRANSFER LINES, PRESSURIZED & LEAK CHECKED FUEL LINES, NO DISCREPANCIES NOTED. INOPERATIVE LT & RT ENG ACCESSORIES FOR FUEL LEAKS, NO LEAKS NOTED ASDR CA150420001Wire · chafed(CAN) CREW REPORTED TRANSPONDER NR 1 & NR 2 WAS TRANSMITTING INCORRECT ALTITUDES. THESE ERRORS STOPPED FOR A SHORT TIME AFTER TURNING TRANSPONDER OFF THEN ON AGAIN. ERROR READINGS SUCH AS: INDICATED 7600, TRANSMITTING 10000 INDICATED 8400, TRANSMITTING 9600 ASDR 7C7A201505270051Fastener · looseNUMEROUS LOOSE FASTENERS WERE FOUND IMMEDIATELY OUTBOARD OF WS 136 IN LOWER SPAR CAP DURING ROUTINE INSPECTION. DISCREPANT FASTENERS ARE REMOVED HOLES DRILLED OUT AND NDT INSPECTED AND REPAIRS ARE APPLIED IAW BEECHCRAFT FIELD REPAIR FR-CO-104153R1.SDR 7C7A2015041500003Skin · crackedSKIN CRACK FROM EXTRUDING RIVET FA 163.95 JUST BELOW STR 9AR. REPAIRED USING BEECHCRAFT SRM. DATED 4/15/2015
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