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 CA110826001Inlet · cracked(CAN) REAR INLET CASE HAD A THROUGH GOING CRACK AT THE STRUT LOCATION ADJACENT TO THE FUEL PUMP/OIL PUMP DRIVE. THE CASE WAS NOT A MFG CASTING. 1 VANE OF THE LP IMPELLER HAD A DENT/BEND BEYOND REPAIR LIMITS. THE IMPELLER WAS SCRAPPED. THERE WAS NO EVIDENCESDR CA110801002Solenoid · corrodedDURING CLIMB THROUGH 1,200 FT WITH CLM PWR SETTING, RT AFTER SELECTION OF BLEED SW ON, NR 2 ENGINE TORQUE STARTED FLUCTUATING BETWEEN 50-80 PERCENT, NR 2 BLEED HOT C/L ILLUMINATED THEN NR 2 ITT EXCEEDED 800C FOR ABOUT 10 SECONDS. PILOT SELECTED BLEED SWITCH OSDR CA110609003Oil Cooler · failedDURING AN APPROACH CHECK FLIGHT, THE NR1 ENGINE OIL TEMPERATURE EXCEEDED ITS NORMAL OPERATING RANGE TO A YELLOW ARC CAUTION OF 113C. THE ACFT DID AN UNSCHEDULED LANDING. MX DETERMINED THE ROOT CAUSE TO BE A FAILED OIL COOLER - AIR OUTLET FLAP ACTUATOR. THE OSDR CA110524008Control Cable · frayedDURING SCHEDULED INSP, FOUND AILERON CABLE, PN 82700568-S001 AT RT WING STN 181 FRAYED AND STARTING TO UNRAVEL. THE POINT OF THE FAILING CABLE IS LOCATED IN A CABLE BLOCK ON THE AFT SPAR WERE ALUMINUM GUIDE ROLLERS, PN FL4C6-2 ARE IN CONTACT WITH THE CABLE. SDR CA110602001O-Ring · leakingPOWER LOSS DURING CLIMB. PILOT NOTED LEFT ENGINE LOST POWER. ENGINE SHUTDOWN AND PILOT RETURNED. AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. DURING TAXI, GROUND CREWS NOTED FUEL LEAKING FROM ENGINE DRAIN. TROUBLESHOOTING REVEALED A DAMAGED O-RING ON THE SDR CA110509002Drain · damaged(CAN) DURING REMOVAL OF THE FUEL MANIFOLD DRAIN LINE, REF, AIPC 71-70-00, FIG. 16, ITEM 250, TO FACILITATE REPLACEMENT OF NR 1 FUEL NOZZLES, IT WAS REPORTED THAT THE FLARE AT THE END OF THE LINE THAT CONNECTS TO THE FUEL NOZZLE, 6 O`CLOCK POSITION WAS COMPLETESDR CA110428005Pseu · failed(CAN) FOLLOWING SELECTION OF LANDING GEAR UP, ALL GEAR RETRACTED AND INDICATED UP AND SAFE, BUT THE NLG DOORS INDICATORS BOTH REMAINED UNSAFE. ACFT BUFFET ALSO OBSERVED. FOLLOWING ACCELERATION DRILLS, SPEED WAS KEPT AT 130KTS AND FLAPS SET TO 5. ATC WERE INFSDR CA110427005Control System · malfunctioned(CAN) UNCOMMANDED AUTOFEATHER DURING T/O ROLL, THE ENGINE HAD AN UNCOMMANDED AUTOFEATHER. THE T/O WAS ABORTED. TROUBLESHOOTING IS FOCUSING ON A FAULTY TORQUE SIGNAL CONDITIONER UNIT.SDR CA110524007Line · wornFUEL ODOR EVIDENT AFTER SHUTDOWN NOTICED IN COCKPIT AND CABIN. ON INSPECTION, FUEL WAS FOUND TO BE DRIPPING FROM THE NR 2 ENGINE BOTTOM COWL. NR 2 ENGINE FUEL PRESSURE LINE TO FLOW DIVIDER WORN THROUGH WHERE IT PASSES THROUGH FIREWALL. FUEL PRESSURE LINE TSDR CA110411003Mount · failed(CAN) DURING THE ACCEPTANCE FLIGHT OF ACFT 313, A VIBE WAS DETECTED ON NR 1 ENG & PROP. INVESTIGATION BY MTCE PERSONNEL, POST FLIGHT QUICKLY REVEALED THAT THE NR 1 ENG TOP MOUNT HAD FAILED DUE TO DISBOND. THE TOP MOUNT PN LM-431-83-V, SN LK0014 WAS INSTALLEDSDR CA110406001Computer · malfunctioned(CAN) DURING CLIMB, THE MASTER CAUTION ILLUMINATED AND PUSHER SYS FAIL AND RT STALL WARNING CAUTION LIGHTS ILLUMINATED. THE QRH WAS ACTIONED AND THE COMPANY ADVISED. RETURN TO BASE. NR 2 STALL WARNING COMPUTER REPLACED.SDR CA110308002Selector Valve · malfunctioned(CAN) PILOTS REPORT, BEGAN TO CONFIGURE ACFT FOR LANDING. ELECTED TO SELECT PROP RPM TO 1200 TO ASSIST SPEED MANAGEMENT DUE SLIGHTLY SHORTER TRACKING THAN ANTICIPATED AND A LITTLE LIGHT TURBULENCE. LANDING GEAR CALLED AND SELECTED DOWN AT APPROXIMATELY 157 KSDR CA110225011Shaft · fractured(CAN) DURING CRUISE, NR 2 PROP RPM NOTED TO HAVE INCREASED AND TORQUE SPLIT DEVELOPED. CREW DIVERTED ACFT AND WERE UNABLE TO SHUTDOWN ENGINE WITH THE CONDITION LEVER -T-HANDLE PULLED TO SHUTDOWN ENGINE. THE ENGINE CONTROL SPRING STRUT WAS FOUND TO HAVE FRACTSDR CA110228011Line · leaking(CAN) AN ACFT WAS FORCED TO MAKE AN EMERGENCY LANDING. THE ACFT WAS ENROUTE WHEN THE PILOT OBSERVED A SUDDEN AND INTERMITTENT FLASH OF HIS MASTER WARNING INDICATOR. A QUICK SCAN OF HIS ENGINE INSTRUMENTS REVEALED THAT THE RT OIL PRESSURE INDICATION WAS UNUSUALSDR CA110225012Valve · failed(CAN) "DURING CRUISE THE ICING CHECK WAS COMPLETED. AFTER DE-ICE BOOT SELECTOR SET TO OFF, THE LT SECOND FROM THE OUTERMOST OTBD DE-ICE BOOT LIGHT REMAINED ILLUMINATED. THE CORRESPONDING BOOT REMAINED INFLATED AND WAS UNABLE TO BE DEFLATED IN FLIGHT. THE CREW SDR CA110209004Landing Gear · multiple fail(CAN) NOSE WHEEL STEERING (NWS) CAUTION LIGHT ILLUMINATED ON TAXI OUT AND THE STEERING TILLER WAS INEFFECTIVE. STEERING CYCLED OFF-ON BUT THEN CAUTION LIGHT WENT OUT AND THEN CAME BACK ON AS SOON AS TILLER OPERATED. CREW APPLIED MEL (CB B6 ON RH MAIN & P6 ONSDR CA110208007Shaft · broken(CAN) DURING POST C-CHECK ENGINE GROUND RUN AT 85 PERCENT TORQUE, THE LT ENGINE TORQUE INCREASED RAPIDLY TO AN OVERTORQUE SITUATION AND ENGINE CONTROL VIA THE POWER AND CONDITION LEVERS WAS LOST. THE ENGINE WAS SHUTDOWN USING THE FUEL SHUTOFF T-HANDLE. ON INSDR CA110210003Packing · damagedDURING FLIGHT, CREW OBSERVED NR 1 LOW OIL PRESSURE WARNING LIGHT ACTUAL PRESSURE INDICATING BELOW 40 PSI. CREW FOLLOWED QRH AND SHUT DOWN NR 1 ENGINE. ACFT LANDED WITHOUT ISSUE. MECHANICS PERFORMED GROUND INSP AND FOUND OIL LEAKAGE FROM PCU ADAPTER, THEY ADVISDR CA110203002Shaft · sheared(CAN) PILOT REPORTED UPON REACHING CRUISE ALTITUDE AT FL160, NR 2 ENG HYD PUMP CAUTION LIGHT ILLUMINATED AND THE COMPANY WAS ADVISED. ACFT RETURNED TO BASE. CHECKLISTS AND INSTRUMENT READINGS INDICATED A NORMAL LANDING AND GEAR EXTENSION WOULD BE CONDUCTED. CLSDR CA110203001Proximity Sensor · out of limits(CAN) AN INTERMITTENT NOSE GEAR UNSAFE INDICATION BEGAN CYCLING PASSING 1000` AGL. THIS WAS ACCOMPANIED BY A CYCLING OF THE NOSE GEAR NOISE. A MISSED APPROACH WAS CONDUCTED AND AN ALTERNATE GEAR EXTENSION WAS COMPLETED. A NORMAL APPROACH AND LANDING WAS CONDUCSDR CA110124001Wire · chafedWHEN WING DEICE BOOTS ACTIVATED IN AUTO THEY FAILED TO INFLATE AND CB P8 WAS FOUND TO HAVE TRIPPED. RESET AND BOOTS OPERATED UNTIL L3 & R4 WHEN CB TRIPPED AGAIN. MANUAL BOOTS TRIED BUT MANUAL CONTROL CB, E8 TRIPPED. FOUND DEICE TIMER EMITTING ELECTRICAL BURSDR CA101230001Unknown · odor160 NAUTICAL MILES NORTH, FLIGHT CREW REPORTED A MIST AND AN ACRID SMELL IN THE CABIN. FLIGHT WAS THEN DECLARED AN EMERGENCY AND IS DIVERTING. ENGINE INSTALL IN PROGRESS IAW SHEETS. ON ENGINE INSTALL CONNECTED SPRING STRUT TO ENGINE TORQUED AND SAFTIED. COMSDR CA110210010Actuator · failed(CAN) RT MLG FAILED TO RETRACT WITH CREW NOTING AN AUDIBLE BANG AND A JOLT WAS FELT THROUGH THE ACFT POST TAKEOFF. NO ADDITIONAL INFORMATION IS YET AVAILABLE AS TO HOW GEAR WAS EXTENDED AND CIRCUMSTANCES SURROUNDING AN IMMEDIATE LANDING. SUBSEQUENT TO A GEARSDR CA101213011Window · delaminated(CAN) REF: DEFECT-955009. 561475-THE CAPTAINS FRONT WINDOW HAS CRACKS ALL THE WAY AROUND THE PERIMETER. THE A/C PRESSURIZES NORMALLY. (RESOLVED ON W/O: 265017 TASKCARD: NR-00002) VISUAL INSPECTION COMPLETED AND FOUND WINDOW TO HAVE CRACKLING DELAMINATION DAMSDR CA101202009Bearing · failedOPERATOR ADVICED THAT THEIR AIRCRAFT STARBOARD INBOARD MAIN-WHEEL ASSY EXPERIENCED A WHEEL BEARING FAILURE WHICH CAUSED THE MAIN-WHEEL ASSEMBLY TO MIGRATE OFF THE AXLE DURING TAKEOFF TODAY THURSDAY 2ND DECEMBER 2010. AFTER TAKEOFF, AIRCRAFT RETURNED AND MADE ASDR CA101126002Line · leakingSHORTLY AFTER TAKEOFF, THE LANDING GEARS WERE SELECTED UP, THEN A LOUD WHOOSHING SOUND WAS HEARD AND WHAT APPEARED AT THE TIME AS DESCRIBED BY THE PILOTS TO BE SMOKE COMING FROM BEHIND THE INSTRUMENT PANEL IN THE FLIGHT COMPARTMENT. SOON THEREAFTER IT WAS REASDR CA101110002Dadc · malfunctioned(CAN) PILOTS REPORT: "DURING CLIMB, "OFF" FLAG APPEARED ON NUMBER ONE ALTIMETER AND INERTIAL VERTICAL SPEED INDICATOR WITH TCAS FAIL BOTH SIDES. MAINTENANCE WATCH REQUESTED RETURN TO BASE." "NR 1 ADC REPLACED. ADJUSTMENT/TEST C/O. SELF TEST AND PITOT STATICSDR CA101111001Pump · malfunctioned(CAN) LATE DOWNWIND SELECTED FLAP 15. "NR 1 ENG HYD PUMP" CAUTION LIGHT ILLUMINATED. REMAINED IN THE CIRCUIT AND WENT THROUGH THE QRH CHECKLIST. SYSTEM PRESSURE INDICATED NORMAL SO THEN CONTINUED THE CIRCUIT AND LANDED NORMALLY IN MT ISA. ON FLAP RETRACTIONSDR CA101027008Terminal · overheated(CAN) REF: DEFECT 946604 SMOKE COMING FROM THE RT WINDSCREEN AT TOP OF DESCENT, WINDSHIELD SWITCHED OFF AND SMOKE STOPPED IMMEDIATELY. FOUND TERMINAL STRIP LUG L2 DISCOLORED FROM EXCESS HEAT. CO PILOTS WINDSHIELD REPLACED AND FUNCTION CHECKED IAW MM 56-10-1SDR CA101019015Hose · leakingNR 1 ENG HAD AN IN-FLIGHT ENG SHUTDOWN DUE TO LOW OIL PRESSURE WARNING LIGHT DURING CRUSE, PILOT REPORTED THE OIL PRESSURE HAS BEEN CONFIRMED BELOW 40 PSI AND THEN SHUTDOWN THE ENGINE, FOLLOWED QRH PROCEDURE. AFTER A GROUND INSP, THE MECHANICS FOUND THE OIL WSDR CA101012001Windshield · crackedCREW RETURNED TO DEPARTURE, DUE TO THEIR RT WINDSHIELD HEAT ELEMENT BURNED OUT. CREW REPORT WAS NO FIRE OR SMOKE SMELL, JUST A SMALL GLOW AND THEN A HAIRLINE CRACK IN THE WINDSHIELD. INCIDENT REPORT ON JAZZ SAFETY IRREGULARITY REPORT 101011/08. DEFECT 94385SDR CA110209003Actuator · malfunctioned(CAN) LANDING GEAR SELECTED DOWN DURING APPROACH AND TWO GREENS INDICATED FOR MLG BUT A RED GEAR UNSAFE AND DOOR AMBER FOR NLG, PLUS GEAR IN TRANSIT LIGHT IN SELECTOR HANDLE. LANDING ABORTED AND DURING CIRCUIT CREW CHECKED THE ALTERNATE INDICATION AND CONFIRMESDR CA100903012G Switch · failedAN OPERATOR PERFORMING ELT G-SWITCH FUNCTIONAL CHECKS AS REQUIRED BY NZCAA AD DCA/RAD/54 FOUND TO DATE, 4 OUT OF 6 SWITCHES HAVE FAILED THE CMM CHECK. UNIT SERIAL NR`S,13601 (EX A/C 621) 11619 (EX A/C 615) 15389 (EX A/C 630) 11212 (EX A/C 611).SDR CA100902004Anti-Skid Valve · leakingDURING CLIMB, FLIGHT REPORTED THAT NR 1 HYD SYS WAS LOW. FLIGHT RETURN TO DEPARTURE. ON THE WAY BACK- CREW REPORTED FLAPS WERE INOPERATIVE AT FL060 IN A HOLD SOUTH OF DEPARTURE. CREW DECLARED EMERGENCY. LANDED WITHOUT FURTHER INCIDENT. ACFT TOWED TO GATE.SDR CA100720004Line · chafed(CAN) NR 1 NACELLE FUEL LEAK TAKEN TO THE HANGER. UPON OPENING COWL AT THE HANGER , EVIDENCE OF A FIRE WAS FOUND. WAS ORIGINALLY REPORTED AS A POSSIBLE HYDRAULIC LEAK NR 1 NACELLE. PRELIMINARY INVESTIGATION FOUND RESIDUAL FUEL ON INBOARD SIDE OF LEFT ENGINESDR CA100617001Bracket · damagedWHILE CARRYING OUT AN INSP IN THE RT CABIN UNDERFLOOR, 1 OF THE RUDDER CABLES HAD CUT THROUGH THE PULLEY BRACKET AT STN X396.00. CABLE WAS INSPECTED AND FOUND SERVICEABLE AND BRACKET WILL NEED TO BE REPLACED. REF IPC 27-20-00, FIG 45, ITEM 180.SDR CA100611005Wheel Half · broken(CAN) NR 3 MAIN TIRE CAME OFF THE RIM DUE TO RIM FAILURE DURING TAXI. PIECE OF RIM FLEW OFF AND HIT THE FUSELAGE IN TWO PLACES CAUSING DENTS, RESOLVED ON W/O: 240470 TASKCARD: NR-00001 NR 3 AND NR 4 MAINWHEEL ASSEMBLIES REPLACED. AXLES VISUALLY INSPECTED FORSDR CA100601002Control Rod · damaged(CAN) DURING REPLACEMENT OF THE NR 2 MECHANICAL FUEL CONTROL (MFC), THE NR 2 ENGINE CONDITION LEVER CONTROL ROD THAT GOES TO THE MFC FROM THE NACELLE QUADRANT (REF. IPC 76-20-00, FIG 5-150, P/N 87620102-011) WAS FOUND TO BE MISSING THE SOLID RIVET AT THE TOP ESDR CA100520001Retaining Ring · leaking(CAN) DURING ROUTINE INSP OF THE (NLG) IAW TASK 3230/07 VISUAL INSP OF NLG RETRACTION ACTUATOR PART OF A1 CHECK, A HYD LEAK WAS NOTICED FROM THE ACTUATOR. FURTHER INVESTIGATION REVEALED THAT THE RING RETAINER (45) ON THE GLAND NUT (70) WAS PARTIALLY ENGAGED, SDR CA100211004Latch · worn(CAN) THE RT LOWER COWLING, INBD, FWD LATCH PIN (FOR HORSE COLLAR) FOUND WORN HALF WAY THROUGH THE DIAMETER OF THE PIN. THE WEAR ON THE BOLT PIN WAS FACING OUTWARD IN FULL VIEW. (TC 20100211004)SDR CA100219001Shutoff Valve · failed(CAN) DURING 3A CHECK, THE LT EMERGENCY HYD SHUTOFF VALVE DID NOT OPERATE TO THE `SHUTOFF` POSITION WHEN TESTED. THE MOTOR PORTION OF THE VALVE ASSY WAS CONFIRMED TO BE FAULTY AND REPLACED. THE SYS WAS THEN TESTED AND OPERATED NORMALLY. NB: VALVE ASSY WAS ORISDR CA100127002Hinge Fitting · cracked(CAN) UPON INSP, IT WAS FOUND THAT THE LT AILERON HINGE FITTING NR4 WAS CRACKED. ACCORDING TO EXPERIENCED AMES ON THE FLOOR, THIS IS NOT A PROBLEM THAT THEY HAVE SEEN BEFORE AND THEREFORE SHOULD BE DOCUMENTED.SDR CA091130005Pump · malfunctioned(CAN) NR 1 STBY HYD PUMP NOT COMING ON LINE. (RESOLVED ON W/O: 216586 TASKCARD: NR-00001) FOUND BURNT WIRES ON THE UPPER AFT CORNER OF NR 2 AC CONTACTOR BOX, (CB POPPED AS WELL) WIRES ON TOP OF BOX HAVE ARCED AND BURNED A HOLE IN THE AC CONTACTOR BOX AS WELL SDR CA090929002Torque Tube · sheared(CAN) ON APPROACH, FLT CREW NOTICED "FLAP DRIVE" CAUTION LIGHT ILLUMINATE. FLAPS HAD ALREADY BEEN EXTENDED, SO CREW CARRIED OUT A NORMAL LANDING. AFTER LANDING, MX CREW PERFORMED AN INSPECTION OF VISIBLE SECTIONS OF FLAP DRIVE TRAIN & DISCOVERED A SHEARED RT NSDR CA090925001Tube · cracked(CAN) ON APPROACH, AFTER GEAR DOWN SELECTION, THE CREW NOTICED MIST WITH A STRONG SCENT OF HYDRAULIC FLUID. MAINTENANCE INSPECTION PERFORMED AND A SMALL CRACK WAS FOUND IN A HYDRAULIC TUBE UNDER THE COCKPIT FLOOR (PRESSURIZED ZONE). TUBE REPLACED AND AIRCRSDR CA090903002Access Door · separatedDURING ROUTINE FLIGHT REFUEL/DEFUEL ACCESS DOOR CAME OFF. ISAR Q123-2008-09 AND REPAIR DWG RD8-54-2335 AND IN-SERVICE MODSUM IS8Q5200012 WERE RAISED TO ADDRESS THIS ISSUE.SDR CA090908004Rod End · brokenAILERON TRIM INOP AND AP MISTRIM MESSAGE. AP DISCONNECTED AND MISTRIM CONFIRMED. FOUND TRIM TAB FULL UP (LWD) DEFLECTED AND MOVEABLE WITH FINGER. TRIMMING WITH ACTUATOR ONLY IN UP DEFLECTION POSSIBLE. FOUND AILERON TRIM ACTUATOR ROD END BOKEN OFF. TRIM TAB SDR CA091016001Pcu · malfunctioned(CAN) "ENGINE NR 1 PROP AND ITT DROPPED ON FINAL APPROACH TORQUE LOGGED ON 40% PROP (RPM) 910, ITT - 350 DEG TO 400 DEG. REMOVED AND REPLACED PCU AND PERFORMED FUNCTIONAL AND OPERATIONAL TEST, FOUND SATISFACTORY IN ACCORDANCE WITH CMM 71-00-02 AND AMM 71-00-00SDR CA090625002Control Panel · inoperative(CAN) ON APPROACH, UPON LDG DOWN SELECTION, ALL LDG POSITION INDICATORS ARE IN RED AND THE TRANSIT LIGHT IS ON. RECYCLED LDG = SAME. ALTERNATE EXTENSION PERFORMED. ON LDG SELECTOR PANEL, INDICATION IS STILL THE SAME. ALTERNATE EXTENSION DOWN AND LOCKED ADVISDR CA090416001Switch · seized(CAN) ON DESCENT, THE ACFT FELT AS THOUGH IT WERE SLIDING SIDEWAYS. CREW CONFIRMED NO RUDDER TRIM. MANUAL TRIM WAS USED. ACFT LANDED AT DESTINATION AIRPORT UNEVENTFULLY. MX INVESTIGATION DETERMINED THE RUDDER TRIM SWITCH WAS JAMMED IN THE FULL LT POSITION.
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