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 GLBA20111116GUplock Switch · inoperativeWITH THE AUTOFEATHER SWITCH OFF, AUTOFEATHER OFF ANNUNCIATOR AND MAST CAUTION ANNUNCIATOR DO NOT ILLUMINATE. MX REPLACED THE LT UPLOCK SWITCH IAW EO 11-1900-32-002, OPS CHECKED GOOD.SDR GLBA20111115GSkin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE BELLY SKIN, FWD OF THE FWD DME ANTENNA AT FS 228.25, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-065. MATERIALS UTILIZED ARE INCLUDED IN SDR 29GA95557111411ASkin · corrodedREPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING OUTBOARD TRAILING EDGE UPPER SKIN HAS CORROSION DAMAGE. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER.SDR 29GA95527111411ASkin · damagedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING OUTBOARD TRAILING EDGE UPPER SKIN HAS CORROSION DAMAGE. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER.SDR GLBA20111114LFrame · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 288 AND STRINGER 4R, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-064. MATERIALS UTILIZED ARE INCLUDED IN THE ENGISDR GLBA20111114KFrame · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE AT FS 150 AND STRINGER 9AL AT THE AS DOOR STRUT LWR MOUNT UPPER AFT INNER NUTPLATE AREA, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSSDR GLBA20111116FPlacard · missingTHE SEAT BACK UPRIGHT FOR TAKEOFF AND LANDING, & THE EMERGENCY EVACUATION PLACARD IS MISSING FROM SEAT 5A. MX REPLACED THE PLACARD IAW AIM 5-16-0.SDR V0DR20111114018O-Ring · deterioratedCUSTOMER REPORTED OIL LEAKING AROUND BULKHEAD OF PROPELLER ASSY. TECH REPORTED DURING DISASSEMBLY, A PITCH CHANGE ROD O-RING WAS BAD. THE O-RING APPEARS TO HAVE DETERIATED (OUTER LAYER OF RUBBER TO PEEL). NO OTHER DISCREPANCIES WITH THE PROPELLER HAVE BEEN SDR V0DR20111114017Bearing · failedTECH REPORTED THAT DURING DISSASEMBLY, FOUND THAT THE COMM END BEARING HAD FAILED.SDR V0DR20111114016Bearing · failedBLOWER WAS REPORTED TO CAUSE CURRENT LIMITER TO BLOW ON CUSTOMER'S ACFT. DURING DISASSEMBLY OF THE VENT BLOWER TECHNICIAN FOUND COMM END BEARING TO HAVE FAILED AND COME APART.SDR V0DR20111114015Bearing · failedTHE VENT BLOWER WAS REMOVED FOR MAINTENANCE. TECH REPORTED DURING DISASSEMBLY COM END BEARING HAD FAILED. INSPECTION OF THE BEARING REVEALED THE BEARING CAGE HAD LET GO.SDR 29GA95653111311ASkin · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED TWO SPIDER WEB CRACKS LEFT AND RIGHT OF STRINGER 1 AS SEEN FROM EXTERIOR CRACKS ARE LESS THAN 1.0 INCH IN LENGTH AT FS 163.975. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GLBA20111114JCable · inoperativeDOOR WAS EXTREMELY HARD TO OPEN. MX INSTALLED NEW UPPER AND LOWER DOOR CABLES IAW BMM 52-10-02, OPS CHECKED GOOD.SDR GLBA20111114HSelector Valve · inoperativeAFTER SWINGING GEAR 11 TIMES, THE INTRANSIT LIGHT DID NOT ILLUMINATE, DID NOT HEAR HYD PUMP. MX REPLACED THE SELECTOR VALVE IAW AMM 32-30-03, OPS CHECKED GOOD.SDR GLBA20111114FPressure Switch · inoperativeRIGHT AUTOFEATHER WILL NOT TEST DURING RUN UP. MX REPLACED THE RT ENGINE AUTOFEATHER LOW PRESSURE SWITCH.SDR 29GA93553111011ASkin · damagedDURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED SEVERAL LOCATIONS OF DAMAGE TO AREAS WITHIN A BAND APPROXIMATELY 1.0 INCH WIDER THAN WINDOW 8F OPENING INTERIOR SURFACE OF FUSELAGE SKIN. REMOVED BAND OF DAMAGED SKIN 1.0 INCH WIDE FROM AROUND WINDOW OPENING FSDR GLBA20111111HConnector · unsecurePILOT REPORTED THAT THE AUTOFEATHER IS INOPERATIVE. MX RESECURED THE CONNECTOR PLUG ON THE AUTOFEATHER RELAY AND CLEANED, OPS CK GOOD.SDR GLBA20111111GPcb · inoperativePILOT REPORTED THAT UPON RAISING THE GEAR HANDLE THE GEAR REMAINED DOWN WITH 3 GREEN AND RED INTRANSIT LIGHTS EXTINGUISHED. MX REPLACED THE TIME DELAY PCB PN: 68-10GLA SN: 506I96, IAW MI 28-01, OPS CHECKED GOOD.SDR GLBA20111111FCable · frayedPILOT REPORTED THAT THE TOP AFT AIRSTAIR DOOR CABLE IS FRAYED. MX REPLACED THE TOP AFT DOOR CABLE, OPS CHECKED GOOD.SDR 29GA93552110911ADoor · dirtyREPORT: DURING SCHEDULE ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT HARD TO OPEN. CLEANED AND LUBED LEFT EMERGENCY EXIT OPERATIONAL CHECK GOOD.SDR 29GA95231110811AWarning System · false activationFLIGHT: 3998 TLH/FLL PILOT REPORTED BLANK RED ANNUNCIATOR WARNING PANEL ILLUMINATES IN TANDEM WITH LANDING GEAR HANDLE ANNUNCIATOR LIGHT. PERFORMED SEVERAL LANDING GEAR OPERATIONAL CHECKS COULD NOT DUPLICATE.SDR GLBA20111109JWire · damagedPILOT REPORTED THAT UPON GEAR RETRACTION THE INTRANSIT LIGHT STAYED ILLUMINATED AND THE LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR WITH ALL NORMAL INDICATIONS. MX REPAIRED A WIRE AT THE LANDING GEAR SERVICE VALVE, OPS CHECKED GOOD.SDR GLBA20111109GPcb · inoperative"SUP" - PILOT REPORTED THAT THE AFX DISABLE WILL NOT ILLUMINATE DURING AUTOFEATHER TEST. MX REPLACED PCB 129-364091-9 SN: 559895, REF MM 61-21-00, OPS CK GOOD.SDR GLBA20111109FWire · damagedPILOT REPORTED THEAT THE CABIN DOOR ANNUNCIATOR EXTINGUISHES WHEN DOOR IS OPEN AND HANDLE IS CLOSED. MX REPAIRED SPLICE D436, OPS CHECKED GOOD.SDR 29GA93553110711AStringer · debondedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED 4.0 INCH DEBOND AT INTERIOR STRINGER 14L APPROXIMATELY AT FS 402 TO 406. REPAIRED STRINGER 14L BY REMOVING OLD ADHESIVE AND REBONDED 4.0 INCH SECTION OF STRINGER TO SKIN WITH NEW ADHESIVE IAW EA9309.SDR GLBA20111108FLanding Gear · malfunctionedPILOT REPORTED THAT ON GEAR RETRACTION THE INTRANSIT LIGHT STAYED ILLUMINATED AND LDG GEAR RELAY CB TRIPPED, MANUALLY EXTENDED GEAR WITH ALL NORMAL INDICATIONS. MX MEGGED WIRES 66A22, 66C22, & 66F22 NFF, INSPECTED WIRING IN BEAVER TAIL, NFF, RAN ALL APPLICABLSDR 29GA201111060611Frame · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED 1.0 INCH CRACK AT STRINGER 9AR CUTOUT ON FORMER AT FS 177.350. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER.SDR GLBA20111106APcb · inoperativeUPON SELECTING LANDING GEAR HANDLE DOWN, CB LANDING GEAR RELAY POPPED IMMEDIATELY. GEAR PUMP NOT HEARD. MANUAL GEAR EXTENSION SUCCESSFUL. MX WAS ABLE TO DUPLICATE, REPLACED THE PCB IAW AIM MI 24-01, GEAR SWUNG 3 TIMES IAW AIM MI 32-01, OPS CHECKED GOOD.SDR GLBA20111104GFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE CARGO DOOR AFT FUSELAGE FRAME OF FS 509 AT THE GAS STRUT MOUNT BETWEEN STRINGERS 4L & 5L, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-SDR GLBA20111104FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS IN CARGO BAY FRAME FS 456 AT GAS STRUT MOUNT, 1" AND 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-062. MATERIALS UTILIZED ARE INCLUDED IN THE SDR GLBA20111107GSwitch · inoperativePILOT REPORTED THAT THE AUTOFEATHER IS DISARMING WHEN THE NR 1 POWER LEVER IS REDUCED TO 93 PERCENT. MX REPLACED THE HP SWITCH.SDR 29GA94752110411ACable · defectiveFLIGHT: 4069 CLE/DUJ PILOT REPORTED AFT CABIN DOOR LATCHES INOPERATIVE. REPLACED CABIN DOOR AFT LOWER CABLE OPERATIONAL CHECK GOOD.SDR CA111113001Engine · malfunctioned(CAN) WHILE ON T/O ROLL, THE ENGINE STARTED TO "RUNAWAY" AND REACHED 128 PERCENT TORQUE AND POSSIBLY OVER 1000 DEGREES TEMPERATURE BEFORE THE T/O WAS ABORTED. POST EVENT INSPECTION FOUND NO ISSUES WITH THE RIGGING. TROUBLESHOOTING IS ON-GOING WITH VERIFICATIOSDR GLBA20111101GPump · leakingPILOT REPORTED THAT THERE WAS A FUEL LEAK ON THE LT ENGINE. MX REPLACED THE LP FUEL PUMP.SDR GLBA20111028FUnknown · odorPILOT REPORTED A BURNED RUBBER ODOR IN COCKPIT. MX INSPECTED AND FOUND NO ODORS IN THE COCKPIT OR CABIN, INSPECTED WINDSHIELD HEAT SYS, NO DEFECTS FOUND, RAN ACFT, NO DEFECTS FOUND, OK FOR SERVICE.SDR GLBA201110281Unknown · odorBURNED RUBBER SMELL IN COCKPIT.SDR GLBA20111027GSeal · dirtyPILOT REPORTED THAT THE CABIN DOOR WAS SQUEELING IN FLIGHT. MX CLEANED THE DOOR SEAL, PRESSURIZATION CHECKS GOOD, OK FOR SERVICE.SDR GLBA20111025GVentral Fin · debondedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE LT VENTRAL FIN DEBONDED BETWEEN FS 570 AND FS 605, 9.5" ALONG LWR T/E AND INWARD FROM EDGE 3" ON BOTH INBD & OTBD SKINS. MX REPLACED THE VENTRAL.SDR GLBA20111024HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L CRACKED AT CARGO DOOR GAS STRUT MOUNT AREA, (UPPER INBD NUTPLATE), 3 CRACKS ABOUT .5" EACH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSDR GLBA20111024GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND 3 CRACKS AT FUSELAGE FRAME AT FS 456 BETWEEN STRINGER 3L & 4L AT THE UPPER INBD NUTPLATE ON THE CARGO DOOR GAS STRUT MOUNT AREA, ABOUT .5" LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RISDR GLBA20111025FPlacard · dislodgedPILOT REPORTED THAT THE EMERGENCY PLACARD FELL OFF AT 3C. MX REPLACED THE PLACARD IAW AIM 5-16-0.SDR 29GA94353102211ASkin · corrodedREPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED BELLY SKIN CORROSION AFT OF LOWER BEACON AT FS 378.25. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLER REPAIR.SDR GLBA20111024FAnnunciator · inoperativePILOT REPORTED THAT THE LT AND RT LANDING GEAR INDICATION IS INTERMITTENT. MX REPLACED THE ANNUNCIATOR ASSY PN: 90-42291-2, GEAR SWING OPS CKS GOOD, NO DEFECTS NOTED.SDR GLBA20111020GPropeller · malfunctionedPILOT REPORTED THAT THE LT PROP WON'T MANUALLY FEATHER. MX INSPECTED THE LINKAGE AND RAN ENG, NO DEFECTS NOTED.SDR GLBA201110181Bulb · burned outEMERGENCY LIGHT UNDER GLARESHIELD ON CAPT SIDE INOPERATIVE FOUND DURING PREFLIGHT INSPECTION BY CREW. MX DETERMINED BULB WAS BURNED OUT AND REPLACED THE BULB.SDR GLBA20111019FFcu · leakingPILOT REPORTED THAT THERE IS A LEAK COMING FROM THE SMALL DRAIN ON THE LT ENGINE. MX REPLACED THE LT HP FUEL PUMP AND FCU, OPS AND LEAK CHECKED GOOD.SDR 29GA95773101711ATransfer Tube · leakingFLIGHT: 4017 BIM/FLL PILOT REPORTED STRONG FUEL SMELL IN CABIN NOTICED WHEN BOTH ENGINES RUNNING AND LEFT BLEED OPEN. REPLACED FOUR TRANSFER TUBES AND ORINGS ON NUMBER ONE ENGINE FUEL NOZZLES AT SIX O`CLOCK POSITION LEAK CHECK GOOD.SDR CA111019020Cooling Fan · damaged(CAN) DURING RE-INSTALL OF THE HEAT EXCHANGER, AFTER CLEANING, NOTICED THAT THE FAN BLADES OF THE ACM WERE DAMAGED. A FUTHER INVESTIGATION FOUND THAT THE BLADES ALSO DAMAGED THE CASE AND THERE WAS PLAY IN SUPPORT BEARING. REF CMM 21-51-33, FIG ITEM 59.SDR GLBA20111017FSwitch · out of adjustPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE RIGGED CABIN DOOR ANNUNCIATOR CENTER LATCH SWITCH IAW BMM 52-70-02, OPS CHECKED GOOD.SDR GLBA20111017HLine · leakingPILOT REPORTED THAT FUEL WAS LEAKING FROM THE BOTTOM OF THE ENGINE. MX TIGHTED A LOOSE FUEL LINE, LEAK AND OPS CHECKED GOOD.
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