Boeing DHC-8-102

Service difficulty reports · 9,272

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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 = 'DHC8102'
  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.

SDR HNAA2015030200070Connector · contaminatedABORTED TAKEOFF DUE TO AUTO FEATHER DID NOT ARM. AFTER ABORT, CREW TESTED A/F. TESTED NORMALLY. PUSHED POWER LEVERS UP, ARM LIGHT ILLUMINATED AT 76 PERCENT. INSPECTED POWER LEVER MICROSWITCHES 6121-S6, 7, 8 AND 9. NO DEFECTS NOTED. INSPECTED NR 1 AND NR 2 Mar 2, 2015 · N940HA · Dhav DHC8102 · Propeller/Propulsor System WiringSDR HNAA2015030200069Inverter · smokeWHILE DE-ICING WITH ENGINES IN START FEATHER AND BLEEDS OFF, SMOKE ODOR OBSERVED COMING FROM AVIONICS RACK BEHIND CAPTAIN'S SEAT. FOUND CIRCUIT BREAKER FOR AUX INVERTER G9 AND AUX INVERTER D8 POPPED. R & R AUX INVERTER IAW MM 24-22-00. OPS CHECKED GOOD.Mar 2, 2015 · N804EX · Dhav DHC8102 · AC InverterSDR HNAA2015030200068Brush Block · malfunctionedEMERGENCY LIGHTS FLICKERED WHEN PROP HEAT "A" PHASE ON. EITHER TIMER. R & R RT ENGINE BRUSH BLOCK DUE TO SUSPICIOUS. GROUND RAN AIRCRAFT. COULD NOT DUPLICATE EMERGENCY LIGHT DISCREPANCY ON GROUND ON ANY PHASE. PROP HEAT CHECKED GOOD.Mar 2, 2015 · N805EX · Dhav DHC8102 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HNAA2015030200067Brush Block · malfunctionedEMERGENCY LIGHTS ILLUMINATED IN FLIGHT. R & R ALL HEATER LEADS AND BOTH BUSH BLOCKS.Mar 2, 2015 · N812EX · Dhav DHC8102 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HNAA2015030200066Contactor · malfunctionedALL CABIN EMERGENCY LIGHTS FLICKERED ON TAKEOFF. PROP HEAT WAS SELECTED OFF. R & R CONTACTOR 2431-K18 USING RETAINED HARDWARE. GROUND RAN ACFT WITH NO DEFECTS NOTED. OK FOR SERVICE.Mar 2, 2015 · N812EX · Dhav DHC8102 · Ice/Rain Protection System WiringSDR CA150325004Oil System · low pressure(CAN) DURING FLIGHT THE CREW RECEIVED A LOW OIL PRESSURE INDICATION FOR THE LT ENGINE. THE CREW SHUT THE ENGINE DOWN AND RETURNED FOR A SAFE LANDING. MAINTENANCE REPLACED A LEAKING NR 1 HYDRAULIC PUMP ACCESSORY DRIVE PAD SEAL AT REDUCTION GEARBOX.Feb 28, 2015 · Dhav DHC8102 · Engine Oil Indicating SystemSDR CA150302009Line · leaking(CAN) PILOT REPORTED DEFECT, NR 1 HYD ISOLATION CAME ON WITH LOSS OF FLUID AND SYSTEM 1 QUANTITY AND PRESSURE. MAINTENANCE REPLACED THE LINE WITH SERVICEABLE PART IAW THE APPLICABLE AMM RE.Feb 27, 2015 · Dhav DHC8102 · Hydraulic System, MainSDR HNAA2015022700064Bulb · burned outF/A EMERGENCY SWITCH LIGHT GREEN BULB INOPERATIVE ON F/A SWITCH PANEL ABOVE WARDROBE. REMOVED COVER LENS R & R BULB AND REINSTALLED COVER LENS.Feb 25, 2015 · N839EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015022500063Control Box · malfunctionedEMERGENCY LIGHTS FLICKERING WITH PROP HEAT ON. R & R EMERGENCY LIGHTS CONTROL BOX IAW MM 33-51-00. OK FOR SERVICE.Feb 25, 2015 · N812EX · Dhav DHC8102 · Emergency LightingSDR HNAA2014022500062Inverter · odorSMELL FROM INVERTERS, WHEN BLEEDS ARE SELECTED OFF DURING TAKEOFF AND LANDING. R & R AUXILLARY INVERTER IAW 24-22-00. OPS CHECKED GOOD. OK FOR SERVICE.Feb 25, 2015 · N804EX · Dhav DHC8102 · AC InverterSDR HNAA2015022500061Battery Pack · no testEMERGENCY LIGHTS WILL NOT TEST. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-03Q. OPS CHECKED GOOD.Feb 25, 2015 · N941HA · Dhav DHC8102 · Emergency LightingSDR HNAA2015022300059Control Box · malfunctionedEMERGENCY LIGHTS FLICKERING WHEN PROP HEAT SELECTED ON. R & R EMERGENCY LIGHTS CONTROL BOX IAW MM 33-51-00. OK FOR SERVICE.Feb 23, 2015 · N812EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015022300058Apu · fireFUELER REPORTED FLAMES AND SMOKE COMING FROM APU EXHAUST, APU HUNG START. DISCHARGED APU FIRE BOTTLE. R & R APU FIRE BOTTLE IAW WC, 26-20-09X, 26-20-04F AND 26-21-01. RAN APU AND FOUND TO BE HUNG START. R & R FORWARD PURGER VALVE IAW HS 49-20M, THEN START NOFeb 23, 2015 · N940HA · Dhav DHC8102 · Airborne Auxiliary Power Unit (APU) SystemSDR CA150223010Ring · dislodged(CAN) DURING SCHEDULED LUBRICATION OF THE FLAP ACTUATORS, IT WAS NOTICED THAT THE ICE SCRAPER RING WAS PARTIALLY DISLODGED FROM THE LT NR 4 FLAP ACTUATOR. IT WAS NOTICED DUE TO THE EXCESSIVE PLAY BETWEEN THE BALL SCREW SHAFT AND ACTUATOR HOUSING ASSEMBLY.Feb 22, 2015 · Dhav DHC8102 · Trailing Edge Flap ActuatorSDR CA150223006Inverter · failed(CAN) DURING CLIMB, FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE PRESENCE OF SMOKE IN THE COCKPIT. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. BEFORE TAXING TO THE GATE, THE AIRCRAFT WAS CHECKED/CLEARED BY LOCAL EMERGENCY RESPONSE SERVICES ON THE RUFeb 20, 2015 · Dhav DHC8102 · DC Generating SystemSDR HNAA2015022000057Battery · inoperativeCEILING EMERGENCY LIGHT AT ROW 3 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IN ROW 3 CEILING LIGHT. OPS CHECKED GOOD.Feb 20, 2015 · N815EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015022000056Battery · inoperativeLEFT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R POWER SUPPLY 3351, PS3 IAW MM 33-51-00.Feb 20, 2015 · N815EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015022000053Lead · unknownRIGHT A PHASE ON PROP HEAT CAUSE EMERGENCY LIGHTS TO COME ON R & R HEATER LEADS ON NR 2 PROP, NR 1 AND NR 2 BLADES. GROUND RAN ACFT. OPS CHECKED GOOD.Feb 20, 2015 · N812EX · Dhav DHC8102 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HNAA2015021600051Bulb · inoperativeEMERGENCY LIGHT IS INOPERATIVE AT ROWS 1AC-1DC. R & R THE BULB . OPS CHECKED GOOD.Feb 16, 2015 · N805EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015021600048Unknown · smokeAPU BLEED AIR SMOKE NOTICED IN COCKPIT. INSPECTED APU AND BLEED, GROUND RAN ENGINE. RAN APU WITH BLEEDS SELECTED ON FOR OVER 30 MINUTES WITH NO SMOKE OR ODOR. CYCLED BLEEDS MULTIPLE TIMES AND RAN BLEEDS FULL HOT AGAIN WITH NO SMOKE. INSPECTED COCKPIT FOR ANFeb 16, 2015 · N805EX · Dhav DHC8102 · Air Distribution SystemSDR HNAA2015021600046Display · inoperativeDURING TAKEOFF, WEATHER RADAR SCREEN WENT BLANK, TCAS OFF MESSAGE AND FDR CAUTION LIGHT ILLUMINATED. SUSPECT RT TRU FAILURE. LOAD AT .07 POWERED DOWN AND POWERED UP ACFT. GROUND RAN ACFT. OPERATED AC AND DC SYSTEMS AND TRU'S IAW DASH 8 RUN UP MANUAL. NO DFeb 16, 2015 · N809EX · Dhav DHC8102 · Weather Radar SystemSDR HNAA2015021300045Switch · inoperativeEMERGENCY LIGHT SWITCH ON F/A PANEL IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.Feb 13, 2015 · N809EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015021300043Feeder Cable · arcedDC FEEDER CABLE DAMAGE FROM ARCING AT ROW 4 TERMINAL CONNECTION. R & R DC FEEDER CABLE.Feb 13, 2015 · N805EX · Dhav DHC8102 · Electrical Power System WiringSDR HNAA2015021300041Inverter · odorROTTEN FISH ODOR IN COCKPIT. R & R SECONDARY INVERTER IAW MM 24-22-00. OPS CHECKED GOOD. NO OTHER SOURCE OF ODOR FOUND. OK FOR SERVICE.Feb 13, 2015 · N804EX · Dhav DHC8102 · AC Generator-AlternatorSDR HNAA2015021300039Brush Block · failedRIGHT PROPELLER PHASE "B" CIRCUIT BREAKER TRIPPED IN FLIGHT. R & R NR 200 PROPELLER BRUSH BLOCK. FOUND HEATER LEADS AT 2 AND 3 BLADES CHAFED. R & R SAID LEADS IAW H/S MM61-10-00. OPS CHECKED GOOD. OK FOR SERVICE.Feb 13, 2015 · N940HA · Dhav DHC8102 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HNAA2015020900038Brush Block · failedEMERGENCY LIGHTS FLICKERING WITH PROPELLER HEAT ON. R & R BOTH LT AND RT PROPELLER HEAT BUSH BLOCKS IAW 61-10-11. GROUND RAN AT SEVERAL SETTINGS. OPS CHECKED GOOD.Feb 9, 2015 · N812EX · Dhav DHC8102 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HNAA2015020600034Indicator · malfunctionedREJECTED T/O DUE TO NR 2 PROPELLER REACHED 1243 RPM FOR APPROX 5-10 SEC. R &R NR 2 PROP INDICATOR & NR 2 NP PROBE AS REQUIRED. R & R NR 2 HORSECOLLAR PANEL. RAN ENGINES PERFORMED ALL REQUIRED OPS CHECKS. OPS CHECK GOOD AT THIS TIME.Feb 5, 2015 · N934HA · Dhav DHC8102 · Propeller Indication SystemSDR HNAA2015020600033Valve · inoperativeNR 1 ENGINE INTAKE BOOT DOES NOT APPEAR TO INFLATE WITH LT NR 3 WING BOOT ADVISORY LIGHT NO ILLUMINATING. R & R DISTRIBUTOR VALVE & PRESSURE SWITCHES IN REF TO D8MM 30-10-16. OPS CHECK GOOD AT THIS TIME. HA300 SEQ NR 4 FOR L/E R & R.Feb 5, 2015 · N809EX · Dhav DHC8102 · Air Intake Anti/De-Ice SystemSDR HNAA2015020200030Window · burnedEVIDENCE OF HEATING ELEMENT BURNED ON CAPTAIN'S WINDOW. VISIBILITY WAS OBSCURED WITH HEAT APPLIED. REPLACED CAPTAINS SIDE WINDOW REF W/C 56-00-01R.Jan 30, 2015 · N809EX · Dhav DHC8102 · Flight Compartment WindowsSDR HNAA2015020200029Lamp · inoperativeEMERGENCY LIGHTS SWITCH NORMAL GREEN LIGHT INOPERATIVE. R & R LAMP, OPS CHECKED GOOD.Jan 30, 2015 · N815EX · Dhav DHC8102 · Emergency LightingSDR CA150204010Engine · failed(CAN) THE ENG WAS RECEIVED FOR REPAIR & INVESTIGATION AFTER THE OPERATOR REPORTED A FLAME OUT DURING CRUISE & INFLIGHT SHUTDOWN. DURING THE OPERATOR TROUBLESHOOTING A LOUD MECHANICAL GRINDING NOISE WAS NOTED TO BE COMING FROM THE ANGLE DRIVE AREA OF THE TURBOJan 29, 2015 · Dhav DHC8102 · Engine (Turbine/Turboprop)SDR HNAA2015012800028Bulb · inoperativeEMERGENCY LIGHT IS INOPERATIVE AT ROW 1. R & R THE BULB. OPS CHECKED GOOD.Jan 28, 2015 · N815EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015012800027Bulb · inoperativeEMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.Jan 28, 2015 · N815EX · Dhav DHC8102 · Emergency LightingSDR HNAA2015012600026Bulb · inoperativeEMERGENCY LIGHT IS INOPERATIVE AT ROW 1. R & R THE BULB. OPS CHECKED GOOD.Jan 26, 2015 · N938HA · Dhav DHC8102 · Emergency LightingSDR CA150126004Smoke Detector · defective(CAN) FLIGHT CREW RECEIVED A RED SMOKE WARNING MESSAGE IN CLIMB. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED/LANDED WITHOUT FURTHER INCIDENT. INSPECTION OF THE CARGO COMPARTMENT REVEALED NO TRACE OF FIRE OR SMOKE. THE CARGO COMPARTMENT SMOKE DETECTOR SJan 25, 2015 · Dhav DHC8102 · Smoke DetectionSDR HNAA2015012000025Bulb · inoperativeEMERGENCY EXIT KNEE SIN IS INOPERATIVE AT ROWS 1DF AND 4DF. REMOVED LENS COVER, R & R BULBS. OPS CHECKED GOOD. REINSTALLED LENS COVER.Jan 20, 2015 · N941HA · Dhav DHC8102 · Emergency LightingSDR HNAA2015012000024Generator · failedLEFT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT. GROUND RAN ACFT AND LT AC BUSS FAULT CLEARED AND LEFT AC GENERATOR CAUTION LIGHT ILLUMINATED. R & R NR 1 AC GENERATOR AND GCU IAW 24-20-11R LEAKED AND OPS CHECKED GOOD.Jan 20, 2015 · N814EX · Dhav DHC8102 · AC Generator-AlternatorSDR HNAA2015012000023Lens · meltedODOR FOUND IN WARDROBE. WARDROBE COURTESY LIGHT LENS WAS FOUND TO BE MELTED. R & R BULB AND LENS IAW 25-28-00. OPS CHECKED GOOD.Jan 20, 2015 · N805EX · Dhav DHC8102 · Passenger Compartment LightingSDR HNAA2015011600020Indication Sys · inoperativeF/O'S VSI/TRA IS BLANK. R & R VISI/TRA SYSTEM. OPS CHECKED GOOD IAW MM 34-52-10 AND MAINTENANCE BULLETIN 34-68.Jan 16, 2015 · N808EX · Dhav DHC8102 · Navigation SystemSDR HNAA2015011600022Power Supply · inoperativeDURING EMERGENCY LIGHT SYS OPS CHECKED, FOUND RT FORWARD EGRESS LIGHT AND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY AT POSITION PS-2. OPS CHECKED GOOD.Jan 16, 2015 · N931HA · Dhav DHC8102 · Emergency LightingSDR HNAA2015011600021Control Box · failedEMERGENCY LIGHTS FLICKERING IN FLIGHT. R & R EMERGENCY LIGHT CONTROL BOX AND SECURED WITH RETAINING HARDWARE. INSPECTED CONTROL BOX CONNECTOR PLUG. NO DEFECTS NOTED.Jan 16, 2015 · N931HA · Dhav DHC8102 · Emergency LightingSDR HNAA2015011600019Connector · dirtyRIGHT AC BUSS CAUTION LIGHTS ILLUMINATED IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. CLEANED CONNECTOR ON NR 2 AC GENERATOR AND GCU. INSPECTED AC CONTACTOR BOX. GROUND RAN NR 2 ENGINE. OPERATED AC SYSTEMS, PROP HEAT AND WINDSHIELD HEAT. OPS CHECKED GOOD.Jan 16, 2015 · N931HA · Dhav DHC8102 · Electrical Power System WiringSDR HNAA2015011400017Wire Harness · burnedDURING CRUISE, APPROXIMATELY 6,000 FT, NR 1 ECU CIRCUIT BREAKER TRIPPED WITH NR 1 FUEL CAUTION LIGHT ILLUMINATED. NR 1 TORQUE FELL TO 3.8. CONFIRMED LOSS OF POWER PULLING BACK NR 1 POWER LEVER. SHUTDOWN NR 1 ENGINE. NR 1 ENGINE TORQUE CONDITION CIRCUIT BREAJan 14, 2015 · N807EX · Dhav DHC8102 · Turbine Engine System WiringSDR HNAA2015011200014Pressure Switch · failedNR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. R & R NR 1 ENGINE PRESSURE WARNING SWITCH IAW 71-00-02. LEAKED CHECKED GOOD.Jan 12, 2015 · N942HA · Dhav DHC8102 · Engine Oil Indicating SystemSDR HNAA2015011200013Warning Light · false activationNR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. CHECKED OIL LEVEL, FOUND TO BE AT ACCEPTABLE LIMIT. INSPECTED, CLEANED AND RESEATED OIL PRESSURE SWITCH AND TRANSMITTER. PERFORMED SIMULATED TAKEOFF ROLL WITH CREW. NO DEFECTS NOTED AT TJan 12, 2015 · N942HA · Dhav DHC8102 · Turbine Engine Oil SystemSDR HNAA2015011200012Connector · contaminatedAFTER TAKEOFF, APPROXIMATELY 50-300 FT, NR 2 ENGINE/PROP CYCLING BETWEEN 100-70 TORQUE AND 1218-900 RPM. AFTER CREW COMPLIED WITH PROCEDURES, CONDITION LEVERS AT 900 RPM, ENGINE/PROP OPERATIONS RETURNED TO NORMAL. NO WARNING HORNS. CLEANED AND DRIED PCU CONNJan 12, 2015 · N812EX · Dhav DHC8102 · Propeller/Propulsor System WiringSDR HNAA2015010900009Propeller · fluctuatesNR 2 PROPELLER FLUCTUATED BETWEEN 1300 AND 1400 RPM DURING CLIMBOUT. ALL OTHER STAGES OF FLIGHT FLUCTUATED 100-200 RPM. FLUCTUATION CONTINUED ON LANDING. RESET BETA LOCK OUT CIRCUIT BREAKER AND CLEANED CONNECTOR PLUGS ON ECU AND OVER SPEED GOV GROUND RAN NRJan 9, 2015 · N804EX · Dhav DHC8102 · Propeller AssemblySDR HNAA2015010900008Propeller · vibrationMODERATE PROPELLER VIBRATION AT 1050 N/P. OK AT 900N/P. R & R NR 2 PROPELLER ASSY IAW MM 61-10-06. PERFORMED -8 RUN UPS IAW START RUN TAXI MANUAL. NO PROPELLER VIBRATION NOTED AT THIS TIME.Jan 9, 2015 · N940HA · Dhav DHC8102 · Propeller AssemblySDR CA150109006Target · missing(CAN) SHORTLY AFTER TAKE OFF, THE WEIGHT ON WHEELS CAUTION LIGHT ILLUMINATED. ON APPROACH THE NLG AND THE MLG, RT FAILED TO EXTEND. THE ALTERNATE GEAR EXTENSION PROCEDURE WAS USED TO EXTEND THE GEARS. TROUBLESHOOTING THE NLG, THE RT TARGET WAS FOUND TO BE MISJan 8, 2015 · Dhav DHC8102 · Landing Gear Position and WarningSDR CA150108010Blade · cracked(CAN) DURING PRE-FLIGHT INSPECTION THE NR 1 PROPELLOR BLADE ON THE NR 2 PROPELLOR ASSY WAS FOUND TO HAVE A LARGE CRACK ON THE LEADING EDGE, AT APPROXIMATELY THE CENTER OF THE PROPELLOR BLADE.Jan 7, 2015 · Dhav DHC8102 · Propeller Blade Section
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