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 29GA94032121611APressure Switch · defectiveFLIGHT: 4017 FLL/GGT PILOT REPORTED LANDING GEAR "3 GREEN" ILLUMINATED WITH GEAR HANDLE IN "UP" POSITION AIRSPEED EXCEEDED 200 KTS. REPLACED LANDING GEAR POWERPACK GEAR UP PRESSURE SWITCH. LANDING GEAR OPERATIONAL CHECK SATISFACTORY.SDR CA111216002Insulator · cracked(CAN) WHEN THE HEAT EXCHANGER WAS REMOVED FOR CLEANING, IT WAS NOTICED THAT THE ACM, INSULATOR, HAD A LARGE CRACK. THIS CRACK IS BEHIND THE COOLING FAN, ALSO THE PACKING, PN 69494J152, IN THE CONTAINMENT HOUSING WAS DETERIORATED AND COMING OUT. THE ACM WAS REPSDR GLBA20111216FFilter · leakingPILOT REPORTED THAT THERE IS A FUEL LEAK AROUND THE NR 1 ENG FUEL FILTER. MX REPLACED THE NR1 ENG FUEL FILTER.SDR GLBA20111214FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE AFT FUSELAGE FRAME AT FS 456 CRACKED AT THE FWD GAS STRUT MOUNT UPPER INBD NUT PLATE, BETWEEN STRINGER 4L AND 5L, 2 CRACKS 1" AND .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPESDR 29GA2012013000011Cable · failedFLIGHT4028, PILOT REPORTED MAIN CABIN DOOR WILL NOT OPEN. REPLACED AIRSTAIR DOOR FORWARD LOWER LATCH CABLE ASSEMBLY. OPS CHECKED GOOD.SDR CA111213005Balance Weight · damaged(CAN) AN INSPECTION OF THE LOWER CONTROL COLUMN INSTALLATION WAS CARRIED OUT AFTER BEING MADE AWARE OF ANOTHER OPERATOR SUBMITTING A SDR 20111212006 FOR THE ELEVATOR CONTROL JAMMING PRIOR TO TAKEOFF. THE INSPECTION REVEALED THAT THE STABILIZING WEIGHT, 101-52SDR GLBA20111213FWarning Light · false activationPILOT REPORTED THAT ON DPARTURE AUTOFEATHER ANNUNCIATOR ILLUMINATED. MX PERFORMED, OPS CHECKED IAW RUN WORKSHEET AND BMM 61-21-00, NO DEFECTS NOTED.SDR CA111222010Counterweight · damaged(CAN) DURING AN INTERNAL INSPECTION OF THE ELEVATOR BOB-WEIGHTS ON OUR FLEET OF 1900 ACFT IT WAS DISCOVERED THAT DAMAGE WAS PRESENT ON THE BOB-WEIGHT NEAR THE EDGE OF THE WEIGHT WHERE THE STOP BOLT CONTACTS THE WEIGHT.SDR GLBA20111212FConnector · damagedPILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATES WITH THE SWITCH ON DURING TAKEOFF, TESTED NORMAL. MX REPAIRED PIN 22 ON THE A123 PCB IAW MI 24-01, OPS CHECKED GOOD.SDR CA111212006Counterweight · damaged(CAN) THE CREW HAD CONDUCTED THE NORMAL CONTROL TRAVEL CHECKS PRIOR TO TAXING TO POSITION. DURING THE TAKEOFF ROLL THE ELEVATOR CONTROLS FELT HEAVY & APPEARED TO BE JAMMED OR STICKING, REQUIRING MORE FORCE THAN USUAL TO ROTATE. THE CREW SUBSEQUENTLY ABORTED SDR GLBA20111212JCircuit Board · malfunctionedPILOT REPORTED THAT THE RT ENGINE WILL NOT AUTOFEATHER DURING TEST. MX RESEATED THE A123 PCB, OPS CHECKED GOOD.SDR GLBA20111212GCable · brokenPILOT REPORTED THAT THE DOOR SNUBBER CABLE IS BROKEN. MX REPLACED THE CABLE IAW MM 52-10-01, OPS CHECKED GOOD.SDR GLBA20111212HConnector · dirtyPILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATED. MX CLEANED P277 CONNECTOR AT A123 PCB REF AIM 14.2.0, SYS OPS CHECKED GOOD.SDR GLBA20111208FActuator · inoperativePILOT REPORTED THAT THE LEFT GEAR INDICATION DID NOT SHOW DOWN AND LOCKED UNTIL APPROX 25 SECONDS AFTER THE HANGLE WAS PLACED IN THE DOWN POSITION. MX REPLACED THE LT MLG ACTUATOR IAW TC 1900-3230.10, PN: 114-300041-15, SN: 0561A, OPS CK GOOD.SDR GLBA20111207JCable · brokenPILOT REPORTED THAT THE DOOR SNUBBER CABLE IS BROKEN. MX REPLACED THE DOOR CABLE IAW 52-10-00, OPS CHECKED GOOD.SDR 29GA95527120611ATrim System · out of rigFLIGHT: 3998 FLL/FLL DURING FLIGHT THE ADDITION OF RIGHT AILERON TRIM DOES NOT ALTER THE CONTROL WHEEL FORCES NECESSARY TO MAINTAIN ATTITUDE. DECLARED AN EMERGECNY RETURNED TO FLL LANDED WITHOUT INCIDENT. PERFORMED AIRCRAFT AILERON AND RUDDER INTERCONNECT SYSDR GLBA20111204BBulb · inoperativeEMERGENCY LIGHTS ON THE CAPTAIN'S SIDE INOP. MX RELAMPED CAPT EMERGENCY LIGHT IAW B-1900 33-60-00-801, ALL CHECKED GOOD.SDR GLBA20111204ABlower · failedPILOT REPORTED THAT SMOKE IN CABIN AND COCKPIT. MX REPLACED THE FORWARD VENT BLOWER, IAW AIM 21-02, ALL CHECKED GOOD.SDR GLBA20111207GWire · damagedPILOT REPORTED THAT WHEN TAKEOFF POWER WAS APPLIED THE AUTOFEATHER DID NOT ARM ON EITHER SIDE. MX R & R HIGH PRESSURE SWITCH, R & R AFX ARMING SWITCH, REPAIRED BROKEN WIRE ON SWITCH IN PEDESTAL AND ADJUSTED SWITCH REF AIM 12.15.0 & 61-21-02-201, OPS CHECKED SDR GLBA20111207FCable · brokenPILOT REPORTED THAT THE AIRSTAIR DOOR CABLE TO THE SNUBBER IS BROKEN. MX REPLACED THE CABLE.SDR GLBA201112053Downlock Switch · failedPILOT REPORTED THAT THE LANDING GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT WITH TORQUE AT 3000LB AND AIRSPEED 210KNOTS SLOWED TO 170 AND PUT GEAR DOWN NORMAL APPROPRIATED CHECKK LIST RAN FOR UNSAFE GEAR EVEN WITH ALL INDICATIONS OF GEAR DOWN EXCEPT FOR HANDLE SDR GLBA201112052Door · openDURING THE PASSENGER BRIEFING (WITH ENGINES NOT RUNNING), A PASSENGER OPENED UP THE 6C EMERGENCY EXIT DOOR. MX REINSTALLED THE EMERGENCY EXIT DOOR.SDR 29GA95153120111ASkin · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED 1.0 INCH CRACK THROUGH FASTENER AT APPROXIMATELY FS 294 RBL 30 EXTERNAL. REMOVED DAMAGE SKIN AND INSTALLED A 4.5 X 9.5 INCH EXTERNAL DOUBLER REPAIR.SDR GLBA201112022Switch · unsecureCABIN DOOR ANNUNCIATOR WILL NOT EXTINGUISH. IT WAS ACTUALLY THE CARGO DOOR ANNUNCIATOR, SHOULDN'T HAVE BEEN AN SDR. MAINTENANCE RESECURED THE CARGO DOOR SWITCH ROLLER IAW BMM 52-30-00, OPS CK GOOD. ORIGINAL SUBMISSION DATE: 12-02-2011SDR GLBA201112023Placard · dislodgedLANDING GEAR EMERGENCY EXTENSION PLACARD FELL OFF. MX REINSTALLED PLACARD.SDR GLBA201112024Pump · leakingFUEL LEAKING OUT OF MAIN DRAIN LT NACELLE. MX R & R LT LOW PRESSURE FUEL PUMP.SDR GLBA20111130FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE LT BELLY SKIN AT FS 300, 2.2" FROM BELLY SKIN LT OTBD EDGE, 1.1" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-066. MATERIALS SDR GLBA20111130GSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE AS DOOR INNER SKIN DEBONDED FROM FWD EDGE TO AFT EDGE INWARD FROM LWR EDGE 1.2", DEBONDED 3" AT THE FWD & AFT EDGES. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW SDR GLBA201112012Terminal · brokenALL THE INSPECTION LIGHTS IN THE AIRSTAIR DOOR SYS ARE INOPERATIVE. MX FOUND A BROKEN TERMINAL WIRE ON THE DOOR, MX REPLACED THE TERMINAL AND OPS CHECKED GOOD.SDR GLBA20111130KWheel · out of balancePILOT REPORTED THAT WHEN THE GEAR WAS RETRACTED, A STRONG VIBRATION WAS FELT FOR ABOUT 10 SECONDS. MX PERFORMED GEAR SWINGS IAW AIM CHAP 10 32-01, NO DEFECTS NOTED, REPLACED NOSE WHEEL PN: 114-8001-35, SN: 2345 IAW TC. 1900-3240.00 R2, OPS CK GOOD.SDR GLBA201112011Wire · damagedCABIN DOOR LIGHT ANNUNCIATOR CAME ON WHILE TAXIING. MX REPAIRED SMASHED WIRE IN DOOR.SDR 29GA94152112811AHandle · lack of lubeDURING SCHEDULED ROUTINE C-1 INSPECTION DISCOVERED LEFT EMERGECNY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED LEFT EMERGENCY EXIT OUTER HANDLE. OUTER HANDLE OPEN AND CLOSED NORMALLY.SDR GLBA20111128FSolenoid · dirtyPILOT REPORTED THAT THE ACFT YAWED TO THE LT IN THE LANDING FLARE. MX CLEANED THE LOW PITCH SOLENOID, OPS CHECKED GOOD.SDR CA111201001Engine · malfunctioned(CAN) TWO MIN. AFTER T/O, THE CABIN FILLED WITH SMOKE AND AN EMERGENCY WAS DECLARED. THE CREW RETURNED TO THE DEPARTURE AIRPORT WHERE ON SHORT FINAL AT 100` ALTITUDE, THE LOW OIL PRESSURE WARNING CAME ON ENGINE NR 2. THE A/C LANDED SAFELY AND BOTH ENGINE WERE SDR 29GA95432112511ATerminal · looseFLIGHT: 3565 SDY/BIL PILOT REPORTED LANDING GEAR WARNING HORN SILENCE BUTTON INOPERATIVE. TIGHTENED TERMINAL END ON THE BACK OF GEAR HORN OPERATIONAL CHECKED GOOD.SDR ERAA201100010Controller · inoperativeTCAS CONTROLLER AND TRANSPONDER CONTROLLER DISPLAY WENT BLANK ON SHORT FINAL INTO ANC. REPLACED CONTROLLER AND SYSTEM OPERATES OK.SDR V0DR20111123019Strut · damagedNLG LEAKING. DURING DISASSEMBLY, NOTED SIGNIFICANT SCRATCHES IN THE CHROME PLATING OF THE PISTON TUBE. FURTHER DISASSEMBLY REVEALED THAT THE INTERNAL BEARING COATING OF THE NOSE CYLINDER WAS DETERIORATED TO THE POINT THE MATERIAL WAS FLAKING OFF. THE TECH SDR RMIA2011112200056Bulkhead · crackedLOWER PORTION OF FUSELAGE CANTED BULKHEAD AT FS 570 BUCKLED. THE LT SIDE OF THE BULKHEAD HAS SMALL CRACKS AROUND RIVET HOLES AT STRINGER 8L. EARLIER SN OF THIS MODEL ACFT HAD 0.032" BULKHEADS WITH A KIT TO UPSIZE THE SIDES OF THE BULKHEAD TO 0.050".SDR CA111124002Bearing · failed(CAN) LT GENERATOR FAIL LIGHT CAME ON IN FLIGHT. ACFT CONTINUED TO DESTINATION. MAINTENANCE DISPATCHED TO LOCATION FOR TROUBLESHOOTING/REPAIR. UPON INSPECTION OF STARTER/GENERATOR, IT WAS NOTED THAT THERE WAS DAMAGE TO THE COOLING FAN, AND A LARGE AMOUNT OF SDR GLBA20111122FDrain · leakingTHE FUEL PUMP FCU DRAIN IS DRIPPING ON THE LT ENGINE. MX BAGGED ALL DRAINS ON THE LEFT ENGINE, NO LEAKS NOTED.SDR 29GA94272112011AEngine · malfunctionedFLIGHT: 4073 CLE/LWB DURING TAKEOFF ROLL HEARD A LOUD BANG COMING FROM THE LEFT ENGINE A LOSS OF POWER AND A HUMMING NOISE AFTER ENGINE SHUTDOWN AND VISUAL INSPECTION SEVERAL BUMPS ARE FOUND ON THE LEFT ENGINE EXHAUST. REPLACED LEFT ENGINE ASSEMBLY.SDR 29GA95732112011ACircuit Breaker · inoperativeFLIGHT: TLH/FLL PILOT REPORTED LANDING GEAR WARNING HORN YOU CANNOT SILENCE IT. REPLACED CIRCUIT BREAKER (CB-1) ON RIGHT CIRCUIT BREAKER PANEL OPERATIONAL CHECK GOOD.SDR 29GA95153111911ASkin · corrodedREPORT: DURING SCHEDULED ROUTINE INSPECTION FOUND TWO SPOTS OF CORROSION OUT OF LIMITS ON AIRCRAFT BELLY NEXT TO NUMBER 3 FLAP. REMOVED CORROSION AND INSTALLED FILLER AND AN EXTERNAL DOUBLER REPAIR.SDR 29GA93632111811AActuator · bypassingFLIGHT:3536 SDY/BIL DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY PERFORMED MANUAL GEAR EXTENSION. REPLACED NUMBER ONE AND NUMBER TWO MAIN LANDING GEAR ACTUATORS OPERATIONAL CHECK GOOD.SDR GLBA20111121FB-Nut · looseEVIDENCE OF FUEL LEAKING FROM UNDER THE ENGINE INLET. MX TIGHTENED THE B-NUT ON THE FLOW DIVIDER, LEAK CHECKED GOOD.SDR GLBA20111117GPcb · inoperativeON LANDING, THE GEAR HANDLE ILLUMINATED FOR A SPLIT SECOND AND THE LANDING WARNING HORN SOUNDED AT THE SAME TIME, 3 GREEN GEAR DOWN ILLUMINATED THE WHOLE TIME. MX REPLACED PCB A119, IAW AIM 10-24-01.SDR GLBA20111117FOxygen Mask · brokenTHE F/A O2 MASK IS BROKEN. MX REPLACED F/A'S O2 MASK.SDR CA111117010Pump · unserviceable(CAN) LT ENGINE NOT GOING PAST 30 PERCENT NG ON START. THIS WAS AN INTERMITTENT SNAG ON FIRST START OF DAY WOULD BE DIFFICULT TO START THEN WOULD HAVE NO ISSUES. AFTER SOME TROUBLESHOOTING THAT DID NOT FIX THE ISSUE, THE LT ENGINE HIGH PRESSURE FUEL PUMP WAS SDR CA111117002Strut · corroded(CAN) DURING MAINTENANCE, A SHOCK STRUT FLUID LEAK WAS NOTED ON THE NOSE GEAR OF A SN UE79. THE LOWER SHOCK ABSORBER TUBE WAS REMOVED TO FACILIATE SEAL REPLACEMENT. DURING THE PROCESS TO REPLACE THE SEAL, SEVERE CORROSION WAS NOTED AT THE LOWER END OF THE UPSDR 29GA93679111511AOil Cooler · defectiveFLIGHT: 3564 BIL/BIL AIR RETURN DUE TO HIGH OIL TEMPERATURE ON LEFT ENGINE, LEFT ENGINE WAS SHUT DOWN AS A PRECAUTION IN FLIGHT. REPLACED NUMBER ONE OIL COOLER LEAK CHECK AND OPERATIONAL CHECK GOOD.
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