Boeing DHC-8-301
Service difficulty reports · 571
Newest first. General aviation reporting is voluntary.
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 = 'DHC8301' 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 = 'DHC8301' 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 CA960709010Drain Line · chafed(CAN) CREW ON WALKAROUND FOUND A FUEL LEAK IN #1 ENGINE NACELLE. SOURCE WAS A DRAIN LINE WHICH HAD CHAFED THROUGH.SDR CA961018005Connector · burnt(CAN) AT START OF POST ENGINE START CHECKS, THE CREW NOTICED AN ELECTRICAL BURNING SMELL, FOLLOWED BY SMOKE FROM BEHIND THE COPILOT SEAT. ONCE THE ENGINES SHUTDOWN, DC POWER REMOVED AND THE PASSENGER DOOR OPENED THE SMOKE SUBSIDED. OVERHEAD BIN CONNECTOR HAD BSDR CA960703018Clamp · loose(CAN) #2 ENGINE INDICATED FIRE DETECTION ON TAXI-OUT. ENGINE SHUTDOWN AND FIRE BOTTLE USED. INVESTIGATION REVEALED EXHAUST PIPE HAD SEPARATED OFF REAR ENGINE AT POWER TURBINE. THE 'V' CLAMP HAD BECOME LOOSE.SDR CA960614002Drive · damaged(CAN)AFTER TAKEOFF FLAPS FAILED TO RETRACT FROM 10 DEGREES. FLEX SECONDARY DRIVE REPLACED.SDR CA960619040Micro Switch · failed(CAN) ON #1 ENGINE SHUTDOWN, ENGINE OVERTORQUE OCCURRED, ENGINE SHUTDOWN WITH "T" HANDLE. NP UNDERSPEED GOVERNING MICROSWITCH FAILED.SDR CA960620004Ahrs · failed(CAN) #2 ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS) FAILED IN FLIGHT. EADI ATTITUDE INFO TOPPLES. CYCLING THE #2 AHRS AND #2 AHRS CIRCUIT BREAKERS WOULD BRING AHRS BACK ON LINE. UNIT REPLACED.SDR CA960524025Socket · shorted(CAN) RIGHT WING INSPECTION LIGHT CIRCUIT BREAKER FOUND POPPED. INVESTIGATION REVEALED A SHORT IN RIGHT LOWER NACELLE COWLING WING INSPECTION LIGHT SOCKET. SOLDER FROM CONTACT ASSEMBLY CENTRE CONTACT FOUND MELTED AND HAD FLOWED ACROSS TO SOCKET BASE ASSEMBLY GSDR CA960515010Rib · cracked(CAN)DURING REPAIR OF RUDDER TO REPLACE CENTRE HINGE FITTING, FOUND UPPER ADJACENT RIB CRACKED BETWEEN TWO RIVETS ALONG FORWARD RIVET ROW. REPAIR ACCOMPLISHED AS PER STRUCTURAL REPAIR MANUAL (SRM).SDR CA960419009Fuel Control · malfunction(CAN)POWER EXCURSION REPORTED ON TAXI-OUT CONFIRMED BY FDR THAT MAXIMUM TORQUE EXCEEDED. PROPELLER ASSEMBLY REPLACED. MFC, ECU AND HARNESS REPLACED PENDING RESULTS OF PWC INVESTIGATION.SDR CA960524020Control Cable · frayed(CAN)ON DAILY INSPECTION OF ENGINE, #1 ENGINE PROP/CONDITION CABLE CHAFED AND FRAYED AT ENGINE FIRE WALL PULLEY. LOWER CABLE P/N 87600518-001 REPLACED.SDR CA960429009Turbine Case · punctured(CAN)AFTER TAKEOFF, VIBRATION FROM #2 ENGINE FOLLOWED BY ENGINE FIRE. AFM PROCEDURES CARRIED OUT, BOTH BOTTLES DISCHARGED. FIRE EXTINGUISHED BUT LATER REIGNITED AFTER LANDING, AIRPORT FIRE CREW EXTINGUISHED FIRE. A LARGE QUANTITY OF RESIDUAL OIL NOTED IN THESDR CA960315006Spring · broken(CAN)CAPTAIN'S SEAT ASSEMBLY NOT POSITIVELY LOCKING IN FORE/AFT POSITION. SEAT UNLOCKED A COUPLE OF TIMES AND HAD TO BE SHAKEN BACK INTO POSITION IN TRACK. COMBINATION OF BOTH SEAT TRACK LOCKING PIN SPRING S BROKEN AND SEAT TRACK LOCKING HOLES FILLED WITH DUSTSDR CA960311006Pc Board · burnt(CAN)ADVISORY LIGHT CONTROL BOX SHORTED OUT CAUSING A STRONG ELECTRICAL BURNING SMELL IN COCKPIT CAUTION LIGHTS SWITCHED FROM DIM TO BRIGHT ON THEIR OWN JUST PRIOR CREW COULD NOT SWITCH LIGHTS BACK TO DI M. ADVISORY LIGHT BOX PC BOARD 'B' FOUND BURNT.SDR CA960214005Blade · failed test(CAN) BLADE FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95.SDR CA960306001Selector Valve · failed(CAN)ON APPROACH THREE RED WARNING LIGHTS ON WITH NO GEAR MOVEMENT WHEN GEAR SELECTED DOWN. CREW DID GO AROUND. ALTERNATE GEAR EXTENSION, OK. ALSO NOSE WHEEL STEERING FAILED DURING TAXI. LANDING GEAR SELECTOR VALVE REPLACED.SDR CA960306002O-Ring · ruptured(CAN) ON APPROACH, THE CREW EXPERIENCED COMPLETE LOSS OF HYDRAULIC FLUID ON THE NUMBER TWO SYSTEM. THE CREW CARRIED OUT AN ALTERNATE GEAR EXTENSION. MAINTENANCE DISCOVERED THE PROBLEM TO BE CAUSED BY A RUPTURED 'O' RING ON A FITTING LEADING TO THE #2 ENGINE DRSDR CA960212010Carbon Seal · leaking(CAN) ON TAKEOFF ROLL, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ON. TAKEOFF REJECTED. ENGINE OIL LEVEL FOUND DOWN 7 LITRES.SDR CA960129003Blade · failed ndt test(CAN)PROPELLER BLADE FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95.SDR CA960123010Torque Probe · faulty(CAN)ON DEPARTURE #2 ENGINE HAD AN UNCOMMANDED AUTOFEATHER. CREW SHUTDOWN THE ENGINE AND RETURNED TO BASE. MAINTENANCE REPLACED THE TORQUE PROBE. ENGINE RUN AND PROP CHECKS CARRIED OUT SERVICEABLE. AIRCRAF T RETURNED TO SERVICE.SDR CA951114004Line · leaking(CAN)HYDRAULIC LEAK FROUND IN NOSE LANDING GEAR BAY FROM GEAR EXTEND RETRACT LINE TO NLG DOOR.SDR CA960102003Connector · corroded(CAN)DURING SIO 8-61-03 INSPECTION, THE LEFT HAND CONNECTOR (9811-P13) WAS FOUND HEAVILY CORRODED. BACKSHELL AND CANNONN PLUG SHOWING SEVERE 'POWDERING' DUE TO EXCESSIVE CORROSION. THIS CORROSION POSSIBLY CAUSING LOSS OF CIRCUIT INTEGRITY IN AUTO-FEATHER SYST
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