Boeing/Canada 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.

SDR CA190807013Proximity Sensor · failed(CAN) UPON GEAR DOWN SELECTION CREW REPORTED THREE GREEN DOWN AND LOCKED INDICATED. AT 500FT THE NOSE GEAR DOORS STARTED TO CYCLE AND CREW SAW THE RED UNSAFE LIGHT CYCLE AS WELL. CREW COULD HEAR THE DOORS/GEAR CYCLE. THEY DID A GO AROUND AND SUCCESSFULLY PREFOAug 2, 2019 · Dhav DHC8301 · Landing Gear Position and WarningSDR CA200228004Pump · malfunctioned(CAN) AUG 2019 ESN AW0212 (FEP ENGINE), TSN: 354.2 CSN: 456 CYCLES DURING APPROACH TO LANDING, AFTER SELECTING THE CONDITION LEVERS TO MAX AND ADVANCING POWER, THE #2 PROPELLER RPM WAS OVER NORMAL GOVERNING SPEED AT 1250-1280 RPM. PER QUICK REFERENCE HANDBOOAug 1, 2019 · Dhav DHC8301 · Propeller Controlling SystemSDR CA190730018Power Supply · burned(CAN) FLIGHT CREW REPORTED ELECTRICAL BURNING SMELL IN CABIN ROW 1-4. MAINTENANCE FOUND POWER SUPPLY CIRCUIT BOARD 3352-P2 BURNT. POWER SUPPLY AND EMERGENCY LIGHT BATTERY PACK REPLACED. AIRCRAFT RETURNED TO SERVICE. BATTERY PACK PN 61-0478-11, SN AAL0039, POWEJul 27, 2019 · Dhav DHC8301 · Emergency LightingSDR CA190717005Selector Valve · failed(CAN) ON APPROACH THE CREW RECEIVED 3 UNSAFE INDICATIONS WHEN GEAR SELECTED DOWN. A SUCCESSFUL ALTERNATE EXTENSION WAS CARRIED OUT AND THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE DISCOVERED THE R/H HYDRAULIC SELECTOR VALVE FAULTYJul 12, 2019 · Dhav DHC8301 · Landing Gear Retraction/Extension SystemSDR CA190628017Wire · damaged(CAN) #2 AC GENERATOR HOT LIGHT ON AT ENGINE START-UP. LIGHT STAYS ON WHEN GENERATOR SELECTED OFF. MULTIPLE DAMAGED WIRES FOUND ON HARNESS PN 82455003-005 NEAR CONNECTOR 2421-P2. HARNESS REPLACED. AC HOURS: 65750, AC CYCLES: 78979. (TC# 20190628017)Jun 28, 2019 · Dhav DHC8301 · Electrical Power System WiringSDR CA190614017Terminal Block · failed(CAN) DURING CLIMB THE CREW REPORTED THAT THE #1 AUX PUMP LIGHT WAS INOPERATIVE, AND #1 AUX FUEL PUMP WOULD NOT TRANSFER FUEL. THE WEATHER AT THE DESTINATION WAS AT APPROACH LIMITS. THE CREW ELECTED TO RETURN TO A MAINTENANCE BASE. NO EMERGENCY WAS DECLARED, AJun 13, 2019 · Dhav DHC8301 · Fuel System WiringSDR CA190509013Brake Assy · seized(CAN) DURING TAXI OUT, IT WAS REPORTED THAT SMOKE AND FLAMES WERE VISIBLE IN THE LEFT MAIN LANDING GEAR BRAKE AREA. THE CREW CONDUCTED AN EMERGENCY EVACUATION AND FIRE RESCUE ATTENDED TO THE GEAR. NO INJURIES WERE REPORTED, AND PASSENGERS WERE BUSED BACK TO THMay 8, 2019 · Dhav DHC8301 · Landing Gear Brake SystemSDR CA190425009Line · leaking(CAN) AFTER TAKE-OFF, UPON SELECTION OF GEAR UP THE FLIGHT CREW OBSERVED THAT THE #2 HYDRAULIC QUANTITY WENT TO ZERO ACCOMPANIED WITH ASSOCIATED CAUTION/WARNING LIGHTS. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT LANDING WITHOApr 23, 2019 · Dhav DHC8301 · Hydraulic System, MainSDR CA190415012Ahrs · failed(CAN) PILOT REPORT THAT THE #2 EHSI AND EADI FAILED ON CLIMBOUT. MAINTENANCE ACTION: #2 AHRS REPLACED AND TESTED IAW AMM 34-20-00. AIRCRAFT HOURS: 66071:48. CYCLES: 81263. (TC# 20190415012)Apr 14, 2019 · Dhav DHC8301 · Attitude and Direction Data SystemSDR CA190410013Torque Sensor · failed(CAN) #2 PROP COMMANDED FEATHER AT TAKE OFF POWER ON TAKE OFF ROLL. TAKE OFF REJECTED AT 70KTS. CREW REPORTED THAT THE PROP UNFEATHERED ON ITS OWN AND THEY COULD NOT CONFIRM WHAT THE TORQUE GAUGE WENT TO BUT THEY DID SEE 100%. NO ASSOCIATED CAUTIONS. AUTO FEATApr 9, 2019 · Dhav DHC8301 · Propeller Feathering/ReversingSDR CA190408018Cdu · defective(CAN) ON APPROACH INTO DESTINATION THE AIRPORT, DURING IMC CONDITIONS, THE CREW HAD A POSITION UNCERTAIN STATUS MESSAGE ON BOTH FMS UNITS, THEY CONDUCTED A MISSED APPROACH AND RETURN TO THE DEPARTURE AIRPORT. THE FLIGHT LANDED SAFELY WITHOUT ANY FURTHER INCIDEApr 7, 2019 · Dhav DHC8301 · Flight Management Computing Hardware SystemSDR CA190313001Fuel Filter · bypassing(CAN) IN FLIGHT, THE FLIGHT CREW RECEIVED #2 FUEL FILTER BYPASS WARNING LIGHT. THIS RESULTED IN AN AIRBORNE RETURN TO ORIGINATING POINT. REPLACED THE #2 ENGINE FUEL FILTER IAW AMM 73-10-00-02 & TIB DH8-73-06. AIR/LEAK & VISUAL CHECK OF FILTER INSTALLATION COMMar 12, 2019 · Dhav DHC8301 · Engine Fuel DistributionSDR CA190312011Pseu · faulty(CAN) THE CREW ADVISED DISPATCH AFTER DEPARTURE THAT LANDING GEAR DID NOT RETRACT, THEY FELT GEAR COME UP AND GO BACK DOWN, HAD ALL 3 RED GEAR UNSAFE LIGHTS. THEY SELECTED GEAR DOWN AND THE GEAR WAS DOWN AND LOCKED WITH 3 GREEN LIGHTS. AFTER ENSURING THEY HAVEMar 11, 2019 · Dhav DHC8301 · Landing Gear Position and WarningSDR CA190311029Controller · defective(CAN) ON THE GROUND, WHEN BLEEDS SELECTED ON, THE AIRCRAFT BEGINS TO PRESSURIZED AT MINUS 2000 FPM, THE SAME OCCURS WHEN PRESSURIZATION SELECTED TO DUMP. THE AIRCRAFT WAS BROUGHT INTO THE HANGER FOR FURTHER TROUBLESHOOTING. MTC REPLACED THE CABIN AIR CONTROLLEMar 10, 2019 · Dhav DHC8301 · Cabin Pressure ControllerSDR CA190304011Outflow Valve · defective(CAN) DURING CRUISE, THE AIRCRAFT SUFFER UNCOMMAND LOST OF PRESSURIZATION, THE CREW DESCENDED BUT REMAINED AT FL140 FOR AN ESTIMATED 15 MINUTES DUE TO TERRAIN. THE FLIGHT DECLARED PAN PAN, RETURNS TO THE DEPARTURE AIRPORT AND LANDED SAFELY. THE AIRCRAFT WAS TAFeb 28, 2019 · Dhav DHC8301 · Pressure Regulator/Outflow ValveSDR CA190304010Outflow Valve · defective(CAN) DURING CRUISE, THE AIRCRAFT SUFFER UNCOMMAND LOST OF PRESSURIZATION, THE CREW DESCENDED BUT REMAINED AT FL140 FOR AN ESTIMATED 15 MINUTES DUE TO TERRAIN. THE FLIGHT DECLARED PAN PAN, RETURNS TO THE DEPARTURE AIRPORT AND LANDED SAFELY. THE AIRCRAFT WAS TAFeb 28, 2019 · Dhav DHC8301 · Pressure Regulator/Outflow ValveSDR CA190227012Signal Cond Unit · failed(CAN) 2961 HRS SINCE REPAIR DURING T/O ROLL AS THE LH ENGINE TORQUE WAS RISING TO APPROX 70% THE TORQUE SURGED TO OVER 100% AND PROP RPM DROPPED TO APPOX 600-800 RPM. CAPT SAID IT SOUNDED LIKE THE PROP WAS PARTIALLY FEATHERING.TAKE OFF WAS REJECTED AT OR BELOWFeb 23, 2019 · Dhav DHC8301 · Propeller Feathering/ReversingSDR CA190218006Fcu · failed(CAN) NO1 ENG ON FINAL AT 20 TQ , RPM DROPPED , ABLE TO GET 1030 RPM WITH COND LEVER AT MAX , OTHER REMAINED AT 1050 GROUND RUNS CARRIED OUT#1 PWR LEVER DOES NOT INCREASE WITH PLA INCREASE. #1 ENGINE LAGS IN PWR. #1 ENGINE IS AT 786 RPM WHEN IT SHOULD BE AT 90Feb 17, 2019 · Dhav DHC8301 · Fuel Control/Turbine EnginesSDR CA180618003Indicator · malfunctioned(CAN) AT FL200, DURING CRUISE IN ICING CONDITIONS, THE CAPTAIN`S ASI DROPPED FROM 190 KIAS TO 120 KIAS. MAINTENANCE ACTION INITIALLY HAD THE SYSTEM PURGED WITH NO MOISTURE FOUND. THEN THE CAPTAIN`S ASI WAS REPLACED, IAW AMM 34-11-33. A LEAK CHECK WAS CARRIEJun 17, 2018 · Dhav DHC8301 · Airspeed/Mach IndicatorSDR CA180423017Bracket · cracked(CAN) IN CLIMB UPON GEAR RETRACTION, FLIGHT CREW RECEIVED A LEFT GEAR UNSAFE RED WARNING LIGHT AND A LT DOOR AMBER CAUTION LIGHT. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT AFTER PERFORMING AN ALTERNATE GEAR EXTENSION. FLIGHT CREW VISUAL INSPECTION Apr 21, 2018 · Dhav DHC8301 · Nacelle/Pylon Miscellaneous StructureSDR CA160307004Housing · cracked(CAN) WHILE REPLACING THE ACM FOR AN UNRELATED ISSUE, IT WAS FOUND TO HAVE A CRACK INTERNALLY IN THE HOUSING CAUSING AN OIL LEAK WITH SMOKE IN THE CABIN.Mar 5, 2016 · Dhav DHC8301 · Cabin Cooling SystemSDR CA160301020Windshield · burned(CAN) ON APPROACH THE CREW EXPERIENCED ARCING AND SMOKE FROM THE FO WINDSHIELD AT THE LOCATION OF THE TERMINAL LUGS. THERE WERE NO ASSOCIATED CAUTION LIGHTS. MAINTENANCE FOUND EVIDENCE OF ARCING AT THE TERMINAL LUG LOCATION. ALL TERMINALS WERE FOUND TIGHT AND Feb 26, 2016 · Dhav DHC8301 · Flight Compartment WindowsSDR CA160301010Oil System · leaking(CAN) AFTER START BLEED AIR WAS SELECTED ON AND THERE WAS A MILD ODOR OF OIL THROUGHOUT THE ENTIRE AIRCRAFT. THE OIL ODOR INTENSIFIED AFTER 30-40 SECONDS. BLEED AIR WAS THEN SELECTED OFF AND MISSION CANCELLED. BORESCOPE INSPECTION CARRIED OUT ON BOTH ENGINES. Feb 19, 2016 · Dhav DHC8301 · Turbine Engine Oil SystemSDR CA160216009Bleed Air Sys · malfunctioned(CAN) LIGHT BLUE SMOKE REPORTED IN COCKPIT AFTER ENGINE START. BOTH NR 1 & NR 2 ENGINE BLEEDS SWITCHED WERE ON WITH RECIRCULATION FAN ON. ENGINES WERE SUBSEQUENTLY SHUTDOWN AND A REPORT OF MILD OIL SMELL REPORTED BY THE CREW. NO MEDICAL ACTION WAS REQUIRED Feb 10, 2016 · Dhav DHC8301 · Compressor Bleed ControlSDR CA160120015Housing · cracked(CAN) BOTH ENGINES HAD BEEN STARTED AND AND AT LEAST THE NR 2 BLEED HAS BEEN SELECTED, THEY WERE JUST ABOUT TO CALL FOR THE GROUND POWER TO BE DISCONNECTED WHEN THE THE FA CALLED THE COCKPIT ABOUT VISIBLE SMOKE IN THE CABIN. CREW CONFIRM THE ENTIRE CABIN WAS FJan 20, 2016 · Dhav DHC8301 · Cabin Cooling SystemSDR CA160121021Wire Harness · burned(CAN) NR 2 RUDDER ISOLATION CAUTION LIGHT CAME ON, WITH NO OTHER ASSOCIATED CAUTION LIGHTS. 1. FOUND CONNECTOR 2921-P12 TO NR 2 HYDRAULIC RESERVOR LEVEL SWITCH SHORTING INTERNALLY. 2. CONNECTOR 2921-P12 REPLACED AS PER WMM 29-25-01. POWER CHECK DONE AT 292Jan 9, 2016 · Dhav DHC8301 · Hydraulic Power System WiringSDR CA160119018Autofeather Sys · malfunctioned(CAN) THERE WAS AN ABORTED TAKEOFF DUE TO A NR 1 ENGINE AUTO-FEATHER FAILED TO ARM. THE HIGH PRESSURE COMPRESSOR SPEED DROPPED BUT THE PROPELLER DID NOT FEATHER. DURING TROUBLESHOOTING, THE AUTO-FEATHER DID NOT ARM. THE NR 1 ENGINE TORQUE SIGNAL CONDITIONER UNDec 30, 2015 · Dhav DHC8301 · Propeller Feathering/ReversingSDR CA151229007Autofeather Sys · malfunctioned(CAN) THE FLIGHT CREW HAVE REPORTED 3 EVENTS OVER THREE WEEKS OF AUTO-FEATHER (AF) FAIL TO ARM INDICATIONS DURING TAKE-OFF AND HAVE REJECTED THE TAKE-OFFS AS A RESULT. AIRCRAFT OPERATED ON MINIMUM EQUIPMENT LIST (MEL) WITH RESTRICTIONS TO ALLOW RETURN TO MAIN Dec 21, 2015 · Dhav DHC8301 · Propeller Feathering/ReversingSDR CA151208011Selector Valve · failed(CAN) ON LANDING GEAR EXTENSION , CREW GOT 3 RED UNSAFE , UNABLE TO TELL IF GEAR DOWN , RETURNED TO AIRPORT FOR SUCCESSFUL ALTERNATE GEAR SELECTION , PREVIOUS RETRACTION WAS NORMAL , HYD PX NORMAL , ALL DOORS NORMAL FOUND GEAR SELECTER VALVE U/S REPLACED I.A.Dec 5, 2015 · Dhav DHC8301 · Landing Gear SelectorSDR CA151118007Terminal · burned(CAN) SPARKS OBSERVED FROM RIGHT WINDSHIELD DURING CLIMB AND DISSIPATED ONCE SELECTED OFF. EXCESSIVE HEAT NOTED AT TERMINAL ON WINDOW, MASKING TAPE TO IDENTIFY WIRES LEFT ON AFTER LAST WINDOW INSTALL WAS BURNT CAUSING FLAME OBSERVED BY FLIGHT CREW WIRES BURNT Nov 15, 2015 · Dhav DHC8301 · Windshield/Door Rain/Ice RemovalSDR CA151022004Relay · failed(CAN) NR 2 DC GEN HAD BEEN PLACED ON MEL JUST PRIOR TO DEPARTURE. INBOUND TO AIRPORT CREW LOST MANY F/O INSTRUMENTS: ADI, HSI, ALTIMITER STARTED GOING WAY UP AND DOWN, F/D FAILURES. CREW SUSPECTED THAT THEY WERE ON BATTERY POWER. BATTERY TEMP INDICATOR SHOWS BOct 19, 2015 · Dhav DHC8301 · DC Generating SystemSDR CA151022006Actuator · failed(CAN) ON FINAL WHEN GEAR WAS SELECTED DOWN A/C LOST NO2 HYD FLUID AND ISO VALVE LIGHT CAME ON. MAINTENANCE FOUND THE LEAK WAS SOURCE WAS A CRACK IN THE RT GEAR AFT AND CENTER DOOR ACTUATOR HOUSING. REMOVED AND REPLACED DOOR ACTUATOR WITH NEW IAW AMM 32-10-36 AOct 17, 2015 · Dhav DHC8301 · Landing Gear Door ActuatorSDR CA151015013Engine · smoke(CAN) AFTER DEPARTING AIRPORT, PILOT NOTICED SMOKE IN THE CABIN. PILOT ELECTED TO SHUT DOWN ONE ENGINE AND RETURN AIRCRAFT BACK TO DEPARTURE AIRPORT WHERE IT LANDED WITHOUT INCIDENT.Oct 8, 2015 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA150921008Pulley · seized(CAN) ELEVATOR TRIM WHEEL IS EXTREMELY STIFF TO OPERATE MAINTENANCE FOUND 2 PULLEYS IN AFT SECTION AT STA X773.00 TO BE SEIZED. PULLEYS REPLACED, CABLE TENSIONS ADJUSTED IAW AMM 27-00-00. FUNCTION CHECKED SERVICEABLE AND SMOOTH OPERATION VERIFIED.Sep 17, 2015 · Dhav DHC8301 · Elevator Tab Control SystemSDR CA150828005Engine · failed(CAN) CREW REPORTED "LEFT HAND ENGINE FAILED ON TAKE OFF" FOLLOWED BY UP-TRIM ON RIGHT HAND ENGINE AND LEFT HAND ENGINE FEATHERED, LH ENGINE TSCU WAS REPLACED AND WILL BE SENT TO P&WC FOR TESTING. AIRCRAFT RETURN TO SERVICEAug 17, 2015 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA150804003Selector Valve · faulty(CAN) ON GEAR SELECTION, GEAR DOORS DID NOT OPEN. GEAR UNLOCKED BUT DID NOT COME DOWN. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE AS PER AMM 32-30-41. GEAR SWINGS COMPLETED AND OPERATIONAL CHECKED SERVICEBLE.Aug 4, 2015 · Dhav DHC8301 · Landing Gear SelectorSDR CA150727010Blade · fractured(CAN) PILOT REPORTED VIBRATION IN FLIGHT WITH STRANGE RATTLING SOUND AND VIBRATION IN CONDITION LEVER ON NR 2 ENGINE. AFTER AND ADDITIONAL GROUND RUNS AND INVESTIGATION, ONE PT BLADE WAS FOUND FRACTURED.Jul 17, 2015 · Dhav DHC8301 · Turbine SectionSDR CA150708006Precooler · cracked(CAN) ENGINE TEMPS FOUND 90 DEGREES HOTTER ON ONE SIDE THAN THE OTHER UPON INVESTIGATION, THE PRE- COOLER ON THAT SIDE WAS FOUND CRACKED AND WITH PIECES MISSING. CRACKS FOUND ON WELDS AND LOOKS LIKE GENERAL FATIGUE, AS A SIDE NOTE THE LAST REPAIR DONE ON THISJul 7, 2015 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA150629005Oil System · unknown(CAN) A CONTINUOUS SMELL OF OIL OCCURRED AFTER SETTING CLIMB POWER UPON TAKEOFF & CONTINUED FOR APPROX 2 - 3 MINUTES. SMELL WAS CONFIRMED BY ALL 4 CREW MEMBERS. CREW PUT ON OXYGEN MASKS & THE RAM VENTILATION, BLEEDS OFF. CHECKLIST WAS RUN. SHORTLY THEREAFTJun 20, 2015 · Dhav DHC8301 · Turbine Engine Oil SystemSDR CA150617012Wire Harness · damaged(CAN) DURING AVIONICS SHOP REPAIRS, QTY 3 OF THESE DASH 8-300 ACFT EMER LIGHT CONTROL BOXES, ALL HAD THE SAME FAULT FINDINGS. THE DIODES INSIDE WERE EXCESSIVELY HOT & CAUSED PC BOARD OVERHEAT DAMAGE RESULTING IN THE SOLDERS TO CRACK. PLEASE SEE PICTURES ATTAJun 16, 2015 · Dhav DHC8301 · Light System WiringSDR CA150615014Fuel Control · leaking(CAN) FROM ROTATION THE CREW NOTICED FUEL LEAK FROM RT NACA VENT FOR 18 MIN, STOPPED JUST BEFORE LANDING. WHEN CREW NOTICED THAT WHEN SELECT OFF, THE AUX PUMPS AFTER 1000FT, THE RT AUX PUMP LIGHT REMAINED ON. FUEL LOSS WAS ABOUT 30LBS PER MIN. REPLACED THE Jun 11, 2015 · Dhav DHC8301 · Fuel Control/Turbine EnginesSDR CA150612008Ahrs · failed(CAN) PITCH ROLL MISMATCH, NO FD NO YD. NR 2 AHRS FAILED SHORTLY AFTER TAKEOFF. CREW ELECTED TO RETURN TO THE DEPARTED AIRPORT. NR 2 AHRS COMPUTER REPLACED, OPERATION & FUNCTION CHECKS C/W ON GND & SYSTEM CHECKS SERVICEABLE. ACFT RETURNED TO SERVICE.Jun 8, 2015 · Dhav DHC8301 · Integrated Flight SystemSDR CA150603008Housing · damaged(CAN) CABIN DUCT HOT CAUTION LIGHT ILLUMINATED WHILE CLIMBING THROUGH 11,000 FT. CREW COULD NOT COOL DUCT IN AUTO OR MANUAL MODE, SO FOLLOWED QRH AND SELECTED PACK OFF. DUCT TEMP CAME DOWN GRADUALLY. ACM MAINTENANCE ACTIONS: RECIRC DIVERTER DUCT HOUSING REPLJun 1, 2015 · Dhav DHC8301 · Air Distribution SystemSDR CA150511002Unknown · malfunctioned(CAN) AIRCRAFT AN AUTO FEATHER EVENT UPON TAKEOFF. EVENT RESULTING IN 120%+ TORQUE READING. PROCEEDED TO SHUT DOWN THE ENG. ACFT LANDED UNEVENTFULLY. FDR DATA IS BEING SENT FOR CONVERSION.Apr 15, 2015 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA150415009Feeder Cable · burned(CAN) PILOT DEFECT NR 1 ITT WORKED FINE IN THE START UP WITH ALL INDICATIONS BUT WHEN AIRBORNE AND CLIMBING TO 17,000 FT HAVE DIGITAL READING ONLY WITH AMBER ITT OVERHEAT LIGHT ILLUMINATED. DIGITAL ITT READS 632, THE ANALOG READS 0. WHEN THE PWR WAS ADVANCEDApr 11, 2015 · Dhav DHC8301 · Engine Starting System WiringSDR CA150410019Indicator · false indication(CAN) NR 1 ENGINE TORQUE INDICATION BOTH ANALOGUE AND DIGITAL WENT TO TO ZERO AND NR 1 ECU WENT TO MANUAL MODE IN CLIMB. THE ANALOGUE TORQUE INDICATION WENT TO ZERO AND THE DIGITAL PORTION WENT TO DASHES. CLIMB POWER WAS SET TQ WAS 90 PERCENT BEFORE GUAGE WENApr 9, 2015 · Dhav DHC8301 · Engine BMEP/Torque IndicatingSDR CA150406003Bushing · migrated(CAN) DURING LT, INBD FLAP REMOVAL, FOUND THE INBD ACTUATOR SCREW BUSHING MIGRATED OUT OF ACTUATOR.Apr 6, 2015 · Dhav DHC8301 · Trailing Edge Flap ActuatorSDR CA150408023Engine · power loss(CAN) DURING APPROACH, AT 3000 FT, THE NR 1 ENGINE MANUAL LIGHT ILLUMINATED. A SUDDEN DROP OF THE NR 1 ENGINE PARAMETERS WERE OBSERVED. IT THEN WENT INTO THE AUTO-FEATHER MODE AND THE NR 2 ENGINE EXPERIENCED AN AUTOTRIM UP. FLIGHT CREW THEN ELECTED TO SHUTDOApr 2, 2015 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA150306004Oil System · faulty(CAN) BEFORE FLIGHT THE CUSTOMER REPORTED THAT OIL SMOKE OCCURRED AFTER RIGHT HAND ENGINE START. SMOKE DETECTOR IN LAVATORY WAS ACTIVATED & THE REVENUE FLIGHT WAS CANCELLED AS A RESULT OF THE SMOKE. GROUND RUN WAS PERFORMED & THE SYMPTOMS WERE DUPLICATED. TFeb 23, 2015 · Dhav DHC8301 · Turbine Engine Oil SystemSDR CA150220007Wire · melted(CAN) DURING CRUISE, AN A/C EXPERIENCED A DUAL LOST OF AC GENERATOR POWER AFTER 25 MINUTES OF FLIGHT. THE AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT OF DEPARTURE SAFELY. THE INVESTIGATION DISCOVERED DAMAGED WIRES IN THE AC VARIABLE FREQUENCY WIFeb 17, 2015 · Dhav DHC8301 · Electrical Power System Wiring
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