Boeing DHC-8-301

Service difficulty reports · 571

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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 = '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 CA130125003Hose · leaking(CAN) AFTER TAKEOFF LOSS ENTIRE NR 2 HYD SYSTEM QTY. RESOLVED ON W/O: 369977, TASKCARD: NR-00001, NLG DRAG STRUT ACTUATOR HYD LINE, PN-AE2463510E0124, LEAKING. REPLACED IAW 32-20-00. INSPECTION OF ENGINE DRIVEN PUMP AFTER FLUID LOSS IAW 05-50-33 AMM, REQUIJan 24, 2013 · Dhav DHC8301 · Hydraulic System, MainSDR CA130122005Connector · damaged(CAN) FOLLOWING AN UNSUCCESSFUL ATTEMPT TO START THE RT ENGINE, TROUBLESHOOTING DISCOVERED ELECTRICAL BURN DAMAGE TO 2431-TB1 ON RT NACELLE FIREWALL. THE DAMAGE WAS CAUSED BY ARCING AT THE FORWARD SIDE OF THE 2431-TB1 TERMINAL BLOCK. THE ARCING HAS RESULTED IJan 22, 2013 · Dhav DHC8301 · Turbine Engine System WiringSDR CA130124003Sequence Valve · failed(CAN) IN FLIGHT AFTER THE LANDING GEAR WAS SELECTED DOWN THE NR 2 ENGINE HYD PUMP CAUTION LIGHT, CAME ON. WITH LOSS OF HYD PRESSURE AND QTY OF THE HYD SYSTEM NR 2. DURING POST FLIGHT INSPECTION WE FOUND SEQUENCE SOLENOID VALVE WAS BROKEN, 3 OF 4 THE COUPLING Jan 19, 2013 · Dhav DHC8301 · Landing Gear Retraction/Extension SystemSDR CA130315001Windshield · cracked(CAN) WHILE EN-ROUTE ABOUT 20 MINUTES INTO THE FLIGHT WHEN THE CREW DECIDED TO RETURN TO BASE DUE TO A CRACKED WINDSHIELD. THE ACFT LANDED SAFELY. LT WINDSHIELD REPLACED.Jan 11, 2013 · Dhav DHC8301 · Flight Compartment WindowsSDR CA121211013Oil System · low pressure(CAN) NR 1 ENGINE SELF SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE CAUTION FOLLOWED BY LOSS OF POWER. OIL PRESS INDICATION WENT TO 0PSI. LP 714634, PRELIMINARY REPORT. FURTHER INFORMATION TO FOLLOW. OFF WING PRELIMINARY INSPECTION: ENGINE SN 123056 REMOVED FRDec 10, 2012 · Dhav DHC8301 · Engine Oil Indicating SystemSDR CA121129006Line · failed(CAN) NR 2 HYDRAULIC ISOLATION VALVE CAUTION MESSAGE, QTY REMAINS STEADY AT 1.0, ALSO RECEIVED ROLL OTBD HYDRAULIC MESSAGE, CREW ACTIONED QRH AND LANDED. NOSE ACTUATOR FLEX LINE FOUND BLOWN OUT. REPLACED, FUNCTION CHECKED SEVICEABLE. ACFT RETURNED TO SEVINov 25, 2012 · Dhav DHC8301 · Hydraulic System, MainSDR CA121123003Skin · debonded(CAN) DURING INSPECTION, MECHANICAL DISBOND, AS WELL AS SOME CORROSION INDUCED DISBONDING DISCOVERED ON THE BELLY SKIN OF THE FUSELAGE BETWEEN FS 270-333. SKIN TO BE REPLACED IAW APPROVED REPAIR.Nov 22, 2012 · Dhav DHC8301 · Fuselage Main, Plate/SkinSDR CA121228009Engine · surges(CAN) AFTER T/O AT APPROX 600 FT ASL, THE CREW NOTED NR 1 ENGINE POWER SURGING, FOLLOWED BY WHAT SEEMED TO BE A FLAME OUT. THE CREW SECURED THE ENGINE AND RETURNED TO THE DEPARTURE AIRPORT FOR A SAFE SINGLE ENGINE LANDING. TROUBLESHOOTING IS ON-GOING AND FOCUNov 19, 2012 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA121126001Autofeather Sys · malfunctioned(CAN) AFTER TAKE OFF AT APPROXIMATELY 600 FT ASL, THE CREW NOTED NR 1 ENGINE POWER SURGING, FOLLOWED BY WHAT SEEMED TO BE A FLAMEOUT. THE CREW SECURED THE ENGINE AND RETURNED TO THE DEPARTURE AIRPORT FOR A SAFE SINGLE ENGINE LANDING. TROUBLESHOOTING IS ON-GNov 19, 2012 · Dhav DHC8301 · Propeller Feathering/ReversingSDR CA121217002Blade · distorted(CAN) DURING PREFLIGHT INSPECTION, ENGINEERS NOTICED THAT THE LT ENGINE, NR 4 PROPELLER BLADE WAS DEFORMED. THE BLADE WAS IMMEDIATELY REMOVED FROM THE ACFT AND SENT FOR ANALYSIS.Nov 15, 2012 · Dhav DHC8301 · Propeller Blade SectionSDR CA121115007Connector · damaged(CAN) BACKSHELL FOR LT ELEVATOR HORN HEAT CONNECTOR/WIRING LOCATED ON TOP CENTER OF THE HORIZONTAL STABILIZER SEVERELY CORRODED/CRACKED. BACKSHELL REPLACED.Nov 15, 2012 · Dhav DHC8301 · Flight Control System WiringSDR CA121114004Bearing · seized(CAN) 2 AILERON CIRCUIT PULLEYS IN THE RT SIDE OF THE CENTER WING AREA WERE FOUND TO HAVE SEIZED BEARINGS. DISCOVERED DURING AILERON CABLE REPLACEMENT. REPLACED WITH NEW.Nov 14, 2012 · Dhav DHC8301 · Aileron Control SystemSDR CA121114010Line · chafed(CAN) ACFT HAD HIGH OIL CONSUMPTION SNAG AND THE OIL COOLER LINE WAS FOUND TO BE CHAFED THROUGH AND LEAKING OIL. REFER TO CHAFED AREA CAUSED BY BRAIDED ENGINE DRAIN LINE RUBBING ON OIL COOLER LINE. POOR CLAMPING IN THE AREA PROBABLY CAUSED THE PROBLEM. AFTENov 13, 2012 · Dhav DHC8301 · Turbine Engine Oil SystemSDR CA121113002Attach Angle · cracked(CAN) DURING INSPECTION, CRACKS WERE FOUND IN THE FORWARD PORTION OF THE NR 2 NACELLE OTBD ATTACHMENT ANGLE. SECTION CONTAINING CRACKS WAS REPLACED IAW RD 8-57-1053. SIMILAR FINDINGS ON THE AFT PORTION OF THE NR 1 NACELLE INBD DRAG ANGLE FWD PORTION OF THE Nov 13, 2012 · Dhav DHC8301 · Nacelle/Pylon, Main FrameSDR CA121121004Connector · miswired(CAN) DURING A FLIGHT TEST, THE NR 1 ENGINE WAS INTENTIONAL SHUTDOWN IN THE AIR. ENGINE COULD NOT BE RESTARTED. DURING T/S, OPERATOR FOUND WIRES CROSSED AT SPLICE 2931-E6 REF. WM 29-30-01.Nov 7, 2012 · Dhav DHC8301 · Electrical Power System WiringSDR CA121019007Union · sheared(CAN) DURING APPROACH, THE NR 2 ENGINE HYDRAULIC PUMP, CAUTION LIGHT ILLUMINATED. CREW CLIMBED AND ENTERED THE HOLDING PATTERN AND ACTIONED THE QRH CHECKLIST, SUBSEQUENTLY WITH NO HYDRAULIC FLUID IN NR 2 SYS, AN ALTERNATE GEAR EXTENSION PROCEDURE WAS CARRIED OOct 15, 2012 · Dhav DHC8301 · Hydraulic System, MainSDR CA121003011Control Box · malfunctioned(CAN) PROP AUTOFEATHER ARM LIGHT DID NOT COME ON WHEN THE PILOT ADVANCED POWER FOR TAKEOFF, THE CREW REJECTED T/O AT OR AROUND 20KT. AUTOFEATHER CONTROL BOX WAS REPLACED, THE ACFT RETURNED TO SERVICE AFTER OPS CHECK OF AUTOFEATHER SYS BY HIGH POWER ENGINE RUNSep 30, 2012 · Dhav DHC8301 · Propeller Feathering/ReversingSDR CA121003005Engine · low torque(CAN) DURING CLIMB, APPROACHING 3000 FT, NR 2 ENGINE TORQUE SUDDENLY DROPPED TO ZERO. LOW OIL PRESSURE LIGHT ILLUMINATED. PILOT VERIFIED OIL PRESSURE ON THE OIL PRESSURE GAUGE AND IT WAS AT ZERO. FLIGHT CREW STOPPED THE ENGINE OPERATION. THE ACFT DIVERTED ASep 26, 2012 · Dhav DHC8301 · Engine BMEP/Torque IndicatingSDR CA120927006Socket · burned(CAN) BURNING ODOR IN FRONT FOUR ROWS. NO SMOKE, NO LIGHTS OUT, NO BURNED COFFEE. F/A SEEMS TO THINK ITS A PLASTIC ODOR. FOUND NR 2 COFFEE URN SOCKET BADLY BURNED, FORWARD GALLEY. REPLACED NR 2 COFFEE URN OUTLET. CHECKED SERVICEABLE, PN AC16371.Sep 26, 2012 · Dhav DHC8301 · Buffet/GalleysSDR CA121010001Display · odor(CAN) ACFT DIVERTED TO AN AIRPORT DUE AFTER THE CREW OBSERVED A BURNING ODOR IN THE FLIGHT DECK. MAINTENANCE PERSONNEL WERE DISPATCHED, INVESTIGATION FOUND THE WEATHER RADAR DISPLAY WAS THE CAUSE OF THE BURNING ODOR. THE WEATHER RADAR DISPLAY WAS REPLACED, ASep 25, 2012 · Dhav DHC8301 · Weather Radar SystemSDR CA120926003Fuel Nozzle · leaking(CAN) CREW REPORTED WHILE CLIMBING THROUGH 3000 FT, THE TORQUE OF NR 2 ENGINE DROPPED TO ZERO WITH ILLUMINATION OF OIL PRESSURE CAUTION SHORTLY THEREAFTER. ENGINE WAS SHUTDOWN IAW QRH AND DIVERTED TO NEAREST AIRPORT. ACFT LANDED SAFELY WITHOUT INCIDENT. ROOTSep 25, 2012 · Dhav DHC8301 · Fuel Injector NozzleSDR CA120925006Housing · damaged(CAN) RT OTBD SECONDARY DRIVE CABLE OUT HOUSING FOUND SHEARED OFF AT CABLE SWAGGED END. SWAGGED FITTING SEPARATED FROM CABLE SHEATH. RESOLVED ON W/O: 354198, TASKCARD: NR-00008, REPLACED RT OTBD SECONDARY FLEX DRIVE SHAFT, PN-745581A IAW AMM.Sep 23, 2012 · Dhav DHC8301 · Trailing Edge FlapsSDR CA120829007Handle · detached(CAN) HANDLE WAS DISCOVERED, DETACHED FROM ACFT. HANDLE WAS ROUTED TO SHOPS FOR REPAIR, VISUAL INSPECTION SHOWS BEARINGS FAILED DUE TO LACK OF LUBRICATION AND CORROSION. WHEN THE BEARINGS FAILED IT ALLOWED THE HANDLE TO BECOME DETACHED FORM THE OUTER HOUSINGAug 25, 2012 · Dhav DHC8301 · Passenger/Crew DoorsSDR CA120815006Pump · failed(CAN) NLG DID NOT EXTEND ON NORMAL GEAR EXTENSION EMERGENCY GEAR EXTENSION CARRIED OUT, GEAR EXTENSION SUCESSFUL ACFT LANDED WITH NO FURTHER ISSUES. DURING SWINGS WITH NR 2 HYDRAULICS, NOSE DOOR`S WOULD NOT OPEN DURING GEAR UP. SEQUENCE STOPED BEFORE DAMMAGEAug 14, 2012 · Dhav DHC8301 · Hydraulic Pump (Electric/Engine), MainSDR JJBA20120730019Skin · damagedON LANDING, CREW OBSERVED THE TOUCHED RUNWAY LIGHT ILLUMINATE. CREW NOTIFIED MX OF THE ILLUMINATED LIGHT. GROUND MX CREW INSPECTED THE ACFT AND FOUND DAMAGE TO THE TAIL BUMPER AREA. ACFT REMOVED FROM SERVICE. PERFORMED A HARD LANDING INSPECTION, A TOUCHED Jul 30, 2012 · N857CA · Dhav DHC8301 · Fuselage Main, Plate/SkinSDR CA121019001Turbine Blades · fractured(CAN) UNUSUAL NOISE DURING START. PILOT REPORTED UNUSUAL NOISE DURING NR 1 ENGINE START, WHEN PROPELLER PITCH CHANGED FROM FEATHER TO UN-FEATHER POSITION. PILOT SHUTDOWN THE ENGINE. MECHANIC PERFORMED ENGINE RUN AND FOUND ENGINE SUFFERED SERIOUS VIBRATION WHJul 23, 2012 · Dhav DHC8301 · Turbine SectionSDR JJBA20120717013Skin · damagedON LANDING, THE CREW OBSERVED THE TOUCHED RUNWAY LIGHT ILLUMINATE. THE CREW NOTIFIED MX OF THE ILLUMINATED LIGHT. GROUND MX CREW INSPECTED ACFT AND FOUND DAMAGE TO THE TAIL BUMPER AREA. THE ACFT WAS REMOVED FROM SERVICE IMMEDIATELY. THE FDR WAS ANALYZED ANJul 17, 2012 · N876CA · Dhav DHC8301 · Fuselage Main, Plate/SkinSDR JJBA20120704003Battery Pack · dischargedDURING PRE-FLIGHT, CREW NOTICED SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MX RECHARGED THE EMERGENCY LIGHT BATTERIES. AN OPS CHECK PRODUCED SATISFACTORY RESULTS AFTER BATTERIES HAD CHARGED. THE ACFT WAS RELEASED TO SERVICE.Jul 4, 2012 · N838CA · Dhav DHC8301 · Emergency LightingSDR JJBA20120703001Power Supply · inoperativeDURING PRE-FLIGHT, CREW NOTICED EMERGENCY LIGHTS WERE INOPERATIVE. GROUND MX CREW R & R THE EMERGENCY LIGHTS AND ESCAPE PATH POWER SUPPLY UNITS. OPS CHECKED SATISFACTORY. ACFT RETURNED TO SERVICE.Jul 3, 2012 · N857CA · Dhav DHC8301 · Emergency LightingSDR CA120704001Ditching Dam · malfunctioned(CAN) AN OPERATOR HAD AN INCIDENT WHERE THE RT DITCHING DAM COVER OPENED DURING DESCENT. THE DAM DID NOT INFLATE BUT THE BAG SUFFERED DAMAGE AND THE AFT SECTION OF THE ALUMINUM DAM COVER IS MISSING. NEW ITEMS WERE FITTED AND TESTED. THE ACFT HAS RETURNED TOJun 29, 2012 · Dhav DHC8301 · Emergency EquipmentSDR CA120626007Wire Harness · broken(CAN) LANDING GEAR RETRACTION CARRIED OUT NORMAL AFTER T/O. 5 TO 6 SECONDS AFTER ALL 3 GEARS WERE RETRACTED, NLG DOOR AMBER LIGHT AND GEAR UNSAFE LIGHT ILLUMINATED WITHOUT ANY PILOT COMMAND. THE CREW ALSO HEARD SOUND AND SHAKE OF THE NLG AND ITS DOORS WERE ACJun 21, 2012 · Dhav DHC8301 · Landing Gear System WiringSDR CA120531005Heater · burned(CAN) DEFECT-1057146, NR 1 ENGINE, ONE PROPELLER HEATER ELEMENT LOOKS BURNED NEAR THE ROOT. REPLACED RELAY 3061-K1, PN KC-D4N IAW TIB DH8-30-2. LEFT PROP NR 3 BLADE ASSY REPLACED IAW CMM 61-13-06. LEFT ENGINE BRUSHBLOCK ASSY REPLACED IAW CMM 61-26-00. LEAMay 29, 2012 · Dhav DHC8301 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA120704003Generator · malfunctioned(CAN) CREW REPORT OF ENGINE TORQUE FLUCTUATIONS OF 10 PERCENT IN FLIGHT. THE ACFT WAS REPOSITIONED TO BASE AND THEN THE FOLLOWING WORK WAS COMPLETED. ENGINE GROUND RUNS AND FAULT CONFIRMED. ENGINE BLEED POINTS BLANKED AND EGR C/O WITH ELECTRICAL PLUG OFF MFCMay 14, 2012 · Dhav DHC8301 · AC Generator-AlternatorSDR CA120514003Computer · failed(CAN) ON CLIMB OUT, THE FLIGHT CREW EXPERIENCED A DOUBLE, ATTITUDE AND REF SYS FAILURE. FLIGHT RETURNED TO DEPARTURE AND LANDED SAFELY. BOTH UNITS REPLACED WERE REPLACED AND TESTED SERVICEABLE. NOTE: THE 2ND UNIT, TSN: 39786, TSO: 39786.May 12, 2012 · Dhav DHC8301 · Attitude and Direction Data SystemSDR CA120522003Engine · power loss(CAN) DURING FLIGHT AT FL250 IN LIGHT ICING CONDITIONS, THE ENGINE POWER DROPPED OFF FROM THE SELECTED 65 PERCENT TORQUE TO 17 PERCENT. THE ENGINE REMAINED IN AUTO MODE AND AS THE ACFT DESCENDED TO FL220, THE TORQUE INCREASED TO 26 PERCENT BUT NEVER INCREASEDMay 5, 2012 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA120522010Check Valve · malfunctioned(CAN) ON CLIMB TO FL120 AND PASSING 8000 FT THE, RUDDER PRESSURE, NR 2 RUDDER HYD AND RUDDER FULL PRESSURE LIGHTS ILLUMINATED. A PAN WAS DECLARED AND RADAR VECTORED BACK TO BASE. APPROPRIATE CHECKLISTS WERE COMPLETED, FINISHING WITH AN ALT GEAR EXTENSION. Apr 22, 2012 · Dhav DHC8301 · Hydraulic System, MainSDR CA120412002Pressure Switch · failed(CAN) DURING CRUISE, FLIGHT CREW NOTED THAT THE NR 2 ENG FUEL PRESSURE LIGHT ILLUMINATED ON THE CAUTION AND WARNING PANEL. CABIN CREW ALSO ADVISED THAT FUEL LEAK IS SEEN ON THE NR 2 ENGINE. IAW QRH, IF ILLUMINATION OF THE ENG FUEL PRESSURE COUPLED WITH PRESEApr 6, 2012 · Dhav DHC8301 · Fuel Pressure IndicatorSDR CA120406003Switch · inoperative(CAN) WHEN BUMPING POWER UP TO START TAXIING, THE NR 1 PROP SPEED DROPPED TO 450 RPM & TQ INCREASED TO 90 PERCENT +. CREW COULD NOT CONFIRM ACTUAL MAX TORQUE P/L WAS IN FLT IDLE & C/L AT MIN. NR 1 PCU LOW PITCH SWITCH FOUND AT FAULT, CONN P2. SWITCH STICKINGApr 5, 2012 · Dhav DHC8301 · Propeller Controlling SystemSDR CA120330001Bearing · failed(CAN) ACFT WAS TAXIING INTO TO GATE WHEN NR 3 WHEEL BEARING FAILED, DAMAGE TO WHEEL, GEAR SHOCK STRUT AND AXLE OCCURED MORE DETAILS TO FOLLOW WHEN INVESTIGATION COMPLETED, 212 HRS SINCE INSPECTION, 258 CYCLES FEB 20 TO MAR 28, 2012.Mar 28, 2012 · Dhav DHC8301 · Wheel/Ski/FloatSDR CA120327001Lug · broken(CAN) DURING HEAVY MAINTENANCE, THE NOSE GEAR BELLCRANK HAD BEEN FOUND WITH A BROKEN LUG.Mar 24, 2012 · Dhav DHC8301 · Fuselage, Landing Gear Attach FittingsSDR CA120312025Actuator · detached(CAN) AFTER TAKEOFF, THE CREW ADVISED MAINTENANCE CONTROL THAT THE LT MLG WOULD NOT RETRACT. MAINTENANCE ADVISED TO GO THROUGH THEIR QRH, SHORTLY AFTER THE CREW ADVISED THEY HAD 3 GREEN LIGHTS. UPON ARRIVAL AT DESTINATION, MAINTENANCE INSPECTED AND FOUND THEMar 11, 2012 · Dhav DHC8301 · Landing Gear ActuatorSDR CA120312009Drive Shaft · failed(CAN) THE ENGINE FLAMEOUT DURING CRUISE WITHOUT ANY PRE-WARNING. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED AT POINT OF ORIGIN. TROUBLESHOOTING IS POINTING AT THE AGB DRIVE, TOWERSHAFT.Mar 7, 2012 · Dhav DHC8301 · Accessory GearboxesSDR CA120228008Rotor · seized(CAN) DURING A FLIGHT THE CREW NOTED NR 2 ENGINE OIL PRESSURE LOSSES. THE CREW SHUTDOWN AND SECURED THE ENGINE AND CARRIED OUT A SINGLE ENGINE LANDING. A PRELIMINARY INSPECTION REVEALED A LARGE QUANTITY OF METALLIC DEBRIS ON THE TM CHIP DETECTOR. NH ROTOR DFeb 23, 2012 · Dhav DHC8301 · Turbine SectionSDR CA120125004Terminal Block · arced(CAN) DURING DESCENT, THE FLIGHT CREW NOTICED ELECTRICAL ARCING, BURNING SMELL AND SMOKE ORIGINATING FROM THE FIRST OFFICER WINDSHIELD TOP LEFT CORNER. FLIGHT CREW CONSULTED THEIR QUICK REFERENCE HANDBOOK, DONNED OXYGEN MASKS AND DECLARED AN EMERGENCY. THE AIRJan 22, 2012 · Dhav DHC8301 · Window System WiringSDR CA120119003Signal Cond Unit · failed(CAN) APPLICATION OF TAKE OFF POWER - SLIGHT REDUCTION TO TRIM POWER REQUIRED ON NO.1 (96 TO 92%) ,SIMULTANEOUSLY FLICKER OF AUTOFEATHER ARM AND SELECT LIGHTS, SOUND LIKE A FEATHERING, SLIGHT SENSE OF YAW -SPIKE OFF TORQUE ON NR 2 (105% OBSERVED) AND PROP RPM Dec 30, 2011 · Dhav DHC8301 · Engine BMEP/Torque IndicatingSDR CA120115005Signal Cond Unit · malfunctioned(CAN) DURING T/O ROLL, AN UNCOMMANDED AUTOFEATHER OCCURRED RESULTING IN AN OVERTORQUE. THE FDR DATA CONFIRMED THE OVERTORQUE AND THE TORQUE SIGNAL CONDITIONER UNIT FAULT INDICATOR WAS TRIGGERED. TROUBLESHOOTING IS ON-GOING.Dec 30, 2011 · Dhav DHC8301 · Engine (Turbine/Turboprop)SDR CA120104007Link · obstructed(CAN) DURING SCHEDULED MAINTENANCE, THE COCKPIT ALTERNATE NLG RELEASE HANDLE WAS PULLED TO OPEN THE NOSE LANDING GEAR (NLG) DOORS, HOWEVER THE DOORS FAILED TO FULLY OPEN. BOTH FORWARD DOORS OPENED APPROXIMATELY ONE INCH AND JAMMED. A SMALL HAND PRESSURE WAS APDec 29, 2011 · Dhav DHC8301 · Landing Gear Door Retract SectionSDR CA111220003Wire · damaged(CAN) ON APPLICATION OF ACFT EXTERNAL POWER IN THE HANGAR, SMOKE WAS REPORTEDLY FOUND IN LOWER CONTACTOR BOX AREA, RT AC CONTACTOR BOX. RESOLVED ON W/O: 316378 TASKCARD: NR-00004, ON INSPECTION OF LIMITER BOX, ATTATCHED TO BOTTOM OF CONTACTOR BOX, HEAVY ARCINDec 19, 2011 · Dhav DHC8301 · Electrical Power System WiringSDR CA111104001Line · cracked(CAN) DURING CRUISE AT 13,000 FT, THE CREW HEARD STRANGE SOUND LIKE HOWLING MICROPHONE FOR ABOUT 2 MINUTES FOLLOWED BY NR 1 ENG HYD PUMP, NR 1 RUD HYD, ROLL SPOILER INBD HYD AND RUD PRESS CAUTION LIGHTS. THEY ALSO CONFIRMED ZERO INDICATION OF NR 1 HYD FLUID QNov 2, 2011 · Dhav DHC8301 · Hydraulic System, MainSDR CA110921005Engine · shutdown(CAN) AIR RETURN NR 1 ENG SHUTDOWN IN FLT CREW HEARD A LOUD BANG AT V1, UNCOMMANDED FEATHER OF THE NR 1 ENGINE ON ROTATION, (TOWER REPORTED SEEING SMOKE). CREW CONTINUED THE FEATHER PROCEDURE, AND AT 1000" SHUTDOWN & SECURED THE ENGINE. ENGINE, PROP AND OIL CSep 19, 2011 · Dhav DHC8301 · Engine (Turbine/Turboprop)
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