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.

SDR CA001207024Fuel Control · failed(CAN) DURING THE TAKEOFF ROLL, THE NR 1 ENGINE ROLLED BACK TO 65% TORQUE WITH NO MANUAL LIGHT. NR 1 MFC AND FUEL PUMP REPLACED WITH GROUND RUNS CARRIED OUT SERVICEABLE.Nov 15, 2000 · Dhav DHC8301 · Fuel Control/Turbine EnginesSDR CA001228024Trim Switch · faulty(CAN) PILOT REPORT): OPERATION OF RUDDER TRIM CAUSED TRIM MOTOR FULL DEFLECTION RIGHT. YAW CORRECTED WITH RUDDER INPUT - ABLE TO RE-CENTRE TRIM, BUT SUBSEQUENT OPERATION OF TRIM CAUSED FAULT TO RETURN. (INITIAL IDENTIFICATION OF FAULT HINDERED BY DEFECTIVE RUDNov 8, 2000 · Dhav DHC8301 · Rudder Tab Control SystemSDR CA001128004Valve · seized(CAN) FORWARD EMERGENCY EXIT SEAL FAILED TO DEFLATE, EXIT UNABLE TO OPEN. LOTS OF WATER FOUND IN EXIT DOOR SHELL, SEAL INFLATION VALVE REPLACED AND LUBRICATED. OLD VALVE SHOWED NO SIGNS OF LUBRICATION. OPERATOR INFORMED OF LUBRICATION TASKS AT PER ISAR 97-09 (Oct 19, 2000 · Dhav DHC8301 · Emergency ExitsSDR CA001128002Warning Light · illuminated(CAN) NR 2 SPU AUXILIARY POWER CAUTION LIGHT ILLUMINATED. PILOT REPORTED CAUTION LIGHT CYCLED ON & OFF FOR 3 MINS. PILOT REPORTED THERE WAS NO DRILL IN THE EMERGENCY CHECK LIST (DEHAVILLAND QRH PSM 1-83-1B ITEM 12.8 IDENTIFIES PROCEDURE FOR THIS EVENT). LT REMOct 14, 2000 · Dhav DHC8301 · Drag Control SystemSDR CA001207005Nut · loose(CAN) DURING TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS THE PILOT IN CONTROL WAS ALERTED TO A CONTROL PROBLEM. APPROXIMATELY 90 KG BACK PRESSURE WAS REQUIRED TO MOVE THE CONTROLS. TAKEOFF WAS ABORTED. INSPECTION FOUND RT ELEVATOR SPRING TAB WAS IN A FULL UP POSITIOct 9, 2000 · Dhav DHC8301 · Elevator Tab Control SystemSDR CA001031022Warning System · activated(CAN) THE FOLLOWING WAS REPORTED TO US (FROM BRYMON SAFETY REPORT 213R/00/DH8): TAKEOFF ABORTED SHORTLY AFTER POWER APPLICATION, DUE TO INTERMITTENT SERVICE DOOR WARNING LIGHT ILLUMINATION. PILOT LIAISON WITH CABIN ATTENDANT WHO ADVISED SERVICE DOOR HANDLE NOTOct 9, 2000 · Dhav DHC8301 · Door Warning SystemSDR CA001026006Line · leaking(CAN) DURING ROUTINE INSPECTION, A HYDRAULIC LEAK WAS DISCOVERED IN THE NR 2 SYSTEM HYDRAULIC LINE FROM THE RESERVOIR TO THE AC PUMP. THE LINE WAS REPLACED AND HE AIRCRAFT WAS RETURNED TO SERVICE.Oct 3, 2000 · Dhav DHC8301 · Hydraulic System, MainSDR CA001031016Pressure Switch · failed(CAN) BWIA MCC REPORT FROM GEORGETOWN, BARBADOS: NR 2 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED (SWITCHES SWAPPED FOR TROUBLESHOOTING), PROBLEM TRANSFERRED TO NR 1 SIDE. NR 1 PRESSURE SWITCH ON RUDDER DAMPER REPLACED (SWITCH WAS SWAPPED).AIRCRAFT FUNCTIONALLYSep 26, 2000 · Dhav DHC8301 · Rudder Control SystemSDR CA001031015Pressure Switch · failed(CAN) FROM BWIA MAINTENANCE REPORT: NR 2 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED, SWITCHES SWAPPED FOR TROUBLESHOOTING. PROBLEM TRANSFEREE TO NR 1 SIDE. NR 1 PRESSURE SWITCH ON RUDDER DAMPER REPLACED (SWITCH WAS SWAPPED).AIRCRAFT FUNCTIONALLY TESTED SATISFASep 24, 2000 · Dhav DHC8301 · Rudder Control SystemSDR CA001018009Indicator · failed(CAN) DURING DESCENT THE FLIGHT CREW NOTICED SMOKE COMING FROM THE RADAR INDICATOR. THE RADAR WAS TURNED OFF AND THE SMOKE DISAPPEARED. THE RADAR INDICATOR WAS REPLACED.Sep 12, 2000 · Dhav DHC8301 · Weather Radar SystemSDR CA000926004Panel · shorted(CAN) FLIGHT NR1179DURING REFUELING A FUEL VALVE CIRCUIT BREAKER POPPED. RESETTING WAS NOT SUCCESSFUL (C/B POPPED AFTER VERY SHORT TIME). MAINTENANCE REPLACED L/H REFUEL/DEFUEL SHUTOFF VALVE, S/N ON AV24B1318D-1, S/N OFF RN20152. AIRCRAFT GROUND CHECKED SERVICSep 5, 2000 · Dhav DHC8301 · Aircraft Fuel SystemSDR UHLA002468Indicator · intermittentFLT 24 - TTN-BED - DURING LEVEL FLIGHT, NOTED AILERON TRIM INDICATOR SHOWING FULL DEFECTION TO THE LEFT. PILOT REPORTED UNABLE TO RECENTER. AIRCRAFT ROLLED TO THE RIGHT WHEN AUTOPILOT WAS DISENGAGED WHILE AIRCRAFT WAS TRIMMED FULL RIGHT WHICH WAS INDUCED BY Sep 3, 2000 · N806SA · Dhav DHC8301 · Aileron Tab Control SystemSDR CA000901003Actuator · leaking(CAN) TIME SINCE REPAIR 4379. RIGHT PROP LEAKING OIL. RT PROP ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE.Aug 22, 2000 · Dhav DHC8301 · Propeller Controlling SystemSDR CA000907020Pump · malfunctioned(CAN) AT 4 MILES FINAL FLAPS SELECTED TO 15 DEGREES NR1 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED TOGETHER WITH ROD PRESSURE NR1 AND ROD HYDRAULIC NR1 AND MASTER CAUTION.STANDBY AND MAIN PRESSURES OBSERVED TO BE 1500 PSI FLAPS CONTINUED TO TRAVEL TO 15 DEGREEAug 21, 2000 · Dhav DHC8301 · Hydraulic Pump (Electric/Engine), MainSDR CA000907022Proximity Switch · out of adj(CAN) DURING THE CRUISE THE FORWARD EMERGENCY EXIT ILLUMINATED EMERGENCY CHECK LIST ENTERED AND AIRCRAFT DIVERTED TO MANCHESTER, UNEVENTFUL LANDING MADE AT MANCHESTER AIRPORT. ENGINEERS FOUND THAT THE PROXIMITY SENSOR WAS NOT WIRE LOCKED LARGER THAN NORMAL OPEAug 11, 2000 · Dhav DHC8301 · Door Warning SystemSDR CA001031017O-Ring · deteriorated(CAN) THE FOLLOWING REPORTED TO US (BRYMON MAINT CTL): DURING CRUISE AT 16,000 FT ON ROUTE TO GLASGOW SPARE CAUTION LIGHT ILLUMINATED (LIGHT ABOVE FUEL TANK LOW LEVEL) THEN EXTINGUISHED FOLLOWED BY HYDRAULIC CAUTION LIGHTS. HYDRAULIC CONTENTS I INDICATED NR 2 Aug 4, 2000 · Dhav DHC8301 · Hydraulic System, MainSDR CA000829009Fuel Line · leaking(CAN) FSR WAS CALLED INTO ASSIST. BW1A MAINTENANCE CONTROL ON AOG WITH AIRCRAFT 9Y-WIN, WITH A LEAKING FUEL LINE ON THE NR2 ENGINE. THE AIRCRAFT WAS IN BARBADOS WITH NO PARTS. PRELIMINARY REPORTS WAS THE LINE FROM THE FUEL COOLED OIL COOLER HAS PIN HOLE, LEAKIAug 4, 2000 · Dhav DHC8301 · Engine Fuel DistributionSDR CA000829008Windshield · failed(CAN) BW1A AIRCRAFT MSN-489, LANDED WITH THE FIRST OFFICERS WINDSHIELD SHATTERED. INFORMATION FROM JOURNEY LOG: CLIMBING OUT OF 17,500 FT, RIGHT WINDSHIELD (OUTER GLASS) SHATTERED WITH LOUD BANG. AIRCRAFT WAS DESCENDED TO 10,000 PLUS PROCEDURES CARRIED OUT. ATAug 2, 2000 · Dhav DHC8301 · Flight Compartment WindowsSDR CA000829007Bearing · worn(CAN) ON APPROACH INTO BRISTOL PILOT REPORTED LOOSE & FLOPPY ELEVATOR CONTROL.NOTE: ELEVATOR TENSION CARRIED OUT AND RIG CHECK. INSPECTION OF ELEVATORS REVEALED INPUT LEVER BEARINGS WORN. BEARINGS REPLACED AND FUNCTIONS COMPLETED SATISFACTORY.Aug 2, 2000 · Dhav DHC8301 · Elevator Control SystemSDR CA000907018Starter Gen · inoperative(CAN) AIRCRAFT ARRIVED IN GEORGETOWN (GGO) WITH THE " NR 1 DC GEN HOT" CAUTION LIGHT & HEATER CAUTION LIGHT. THE STARTER GENERATOR AND AREA AROUND IT INSPECTED AS PER MEL 24-1, STARTER GENERATOR FUNCTIONED CHECKED. OK.AIRCRAFT ARRIVED LATER AT PORT OF SPAIN (PAug 1, 2000 · Dhav DHC8301 · Starter-GeneratorSDR CA000829004Slide · deployed(CAN) CABIN CREW INFORMED. FLIGHT CREW F USUAL NOISE IN VICINITY OF ROW 11, SUSPECT, LEFT HAND DITCHING DAM DEPLYMENT, VISUALLY CONFIRMED BY THE CABIN CREW. FLIGHT CONTINUED TO DESTINATION AIRPORT AT REDUCED AIRSPEED 190 KTS. 26 MAY 2000 LEFT HAND DITCHING DAMJul 31, 2000 · Dhav DHC8301 · Escape SlideSDR CA000905009Fuel Control · malfunctioned(CAN) FLIGHT NR1170ONJULY 20/2000, CRA AIRCRAFT C-GSTA, S/N 182 REJECTED TAKE OFF OUT OF WINDSOR, ONTARIO (YQG) BECAUSE OF A LARGE POWER LEVER STAGGER. THE CREW REPORTED THE NR1 ENGINE AT 30% TORQUE AND THE NR2 ENGINE AT 70%. THE CREW ELECTED TO RETURN TO THE Jul 28, 2000 · Dhav DHC8301 · Fuel Control/Reciprocating EnginesSDR CA000907021Windshield · failed(CAN) DURING A FLIGHT THE CAPTAIN NOTICED A SMELL & SOME SMOKE COMING FROM THE TOP OF HIS WINDSHIELD. WINDSHIELD DE-ICING WAS TURNED OFF AND THE SMELL WENT AWAY. AIRCRAFT CONTINUED WITH DE-ICE OFF. MAINTENANCE NOTICED THAT THE STUD FOR THE GROUND AT THE WINDOWJul 20, 2000 · Dhav DHC8301 · Windshield/Door Rain/Ice RemovalSDR CA000706016Line · leaking(CAN) DURING WALK AROUND INSPECTION, THE FLIGHT CREW OBSERVED A FLUID LEAK IN THE ARMPIT AREA OF THE LT FUSELAGE. MAINTENANCE REPLACED A LEAKING LANDING GEAR DOWN PRESSURE LINE IN THE WING CENTRE SECTION, AND THE AIRCRAFT RETURNED TO SERVICE.Jul 5, 2000 · Dhav DHC8301 · Hydraulic System, MainSDR CA000706015Wire · chafed(CAN) THE FLIGHT CREW REPORTED THAT THE NR 1 BLEED SYSTEM CONTROL CIRCUIT BREAKER POPPED. MAINTENANCE INVESTIGATION REVALED A CHAFED WIRE AT THE NR 1 HGIH PRESSUE BLEED VALVE CONNECTOR PLUG 2121-P9. THE WIRE WAS REPAIRED AND THE AIRCRAFT WAS RETURNED TO SERVICJul 5, 2000 · Dhav DHC8301 · Compressor Bleed ValveSDR UHLA002193Gasket · failedFLT 35 - BED-TTN - AFTER TAKEOFF AT ABOUT APPROXIMATELY 300 FT, NR 1 ENGINE TORQUE WENT TO 40 PERCENT. ENGINE FAILURE CALLED AND AT 400 FT, TORQUE RAISED THEN WENT TO ZERO ON AFFECTED ENGINE. SECURED ENGINE. WENT THROUGH CHECKLIST/QRH, DECLARED EMERGENCY, LJun 17, 2000 · N806SA · Dhav DHC8301 · Engine Bleed Air SystemSDR UHLA001928Pseu · failedDURING CLIMB-OUT, ALL THREE GEAR DOORS OPENED ACCOMPANIED BY GEAR DOOR OPEN LIGHTS. AIRCRAFT RETURNED TO BUF. WHEN GEAR WAS SELECTED GEAR DOWN, GEAR DOWN AND LOCKED INDICATORS DID NOT SHOW GEAR DOWN. ALTERNATE GEAR EXTENSION DID NOT INDICATE DOWN AND LOCKEDApr 24, 2000 · N806SA · Dhav DHC8301 · Landing Gear Retraction/Extension SystemSDR UHLA001896Sensor · inoperativeFLT 31 - BED-BUF - AFTER TAKEOFF WITH GEAR UP, CREW NOTICED RIGHT MAIN GEAR RED AND YELLOW DOOR LIGHTS FLASHING OFF AND ON. FLIGHT ATTENDANT VERIFIED RIGHT AFT GEAR DOOR WERE OPENING AND CLOSING. CREW RETURNED TO FIELD AND MAINTENANCE WAS CALLED AND PROXIMITApr 21, 2000 · N806SA · Dhav DHC8301 · Landing Gear Retraction/Extension SystemSDR CA000404019Controller · failed(CAN) CREW REPORTED THAT PRESSURIZATION WAS ERRATIC IN-FLIGHT PLUS OR MINUS 700 FEET. MAINT UNABLE TO DUPLICATE AND TEST FLIGHT CONFIRMED THE PRESSURE CONTROLLER WAS UNSERVICEABLE.Apr 3, 2000 · Dhav DHC8301 · Cabin Pressure ControllerSDR CA000317004Indicator · false indication(CAN) JUST AFTER TAKEOFF, PILOTS REPORTED 31 ENG OIL TEMP INDICATION WAS IN THE RED ARC. INDICATION REMAINED IN THE RED ARC AFTER POWER REDUCTION. BOTH FUEL TEMP WAS AT 25 DEGREES. CIRCUIT BREAKER FOR OIL TEMP WAS RESET WITH NO CHANGE. A/C RETURNED TO YVR. TEMar 15, 2000 · Dhav DHC8301 · Engine Oil Indicating SystemSDR CA001106010Bolt · loose(CAN) THE FOLLOWING WAS REPORTED TO US (FROM BRYMON MAINTENANCE CONTROL): AFTER LANDING IN ABERDEEN THE NR 1 CABIN ATTENDANT WAS UNABLE TO OPEN PASSENGER AIRSTAIR DOOR. ENGINEERS WERE CALLED TO ASSIST WITH OPENING THE DOOR USING THE EXTERNAL MECHANISM.AIRCRAFMar 12, 2000 · Dhav DHC8301 · Entrance StairsSDR CA000322011Connector · failed(CAN) DURING PREP FOR SCHEDULED FLIGHT, A BURNING SMELL WAS NOTICED IN THE CABIN AREA. INVESTIGATION REVEALED THE CONNECTOR 3320 J39/P39 HAD OVERHEATED AND WAS PRODUCING FUMES. CONNECTOR CONTAINED CABIN OVERHEAD, CABIN SIDEWALL AND PSU WIING. BRYMON ENGINEEFeb 27, 2000 · Dhav DHC8301 · Passenger Compartment EquipmentSDR CA000307003Valve · failed(CAN) OPERATORS HAVE NOTED PROBLEMS WITH DASH 8 300 FORWARD EMERG TYPE 1 DOOR FAILING TO OPEN DURING THE WINTER MONTHS. SEVERAL OCCURRENCES HAVE BEEN REPORTED BUT ARE DIFFICULT TO DUPLICATE DUE TO THE DOOR FUNCTIONS NORMALLY AFTER THE A/C WARMS UP. SERVICE EFeb 17, 2000 · Dhav DHC8301 · Emergency ExitsSDR CA000224018Doubler · corroded(CAN) DURING ULTRASONIC INSPECTION FOR DISBONDING OF FUSELAGE SKIN IAW DHC 8 SIP TASK 5300/1, A SIGNIFICANT AREA OF DISBONDING FOUND IN RT FUSEALAGE SKIN BETWEEN STATIONS X531.50 AND X550.50, AND BETWEEN STRINGERS 26S AND 28S. BOMBARDIER WAS CONTACTED FOR REFeb 17, 2000 · Dhav DHC8301 · Fuselage Main, Plate/SkinSDR CA000224019Valve · failed(CAN) AFTER DEPARTURE, CREW REPORTED LOSS OF NR 2 HYDRAULIC QUANTITY, ASSOCIATED WITH ENGINE DRIVEN PUMP CAUTION LIGHT ILLUMINATING AND ALSO LOSS OF NR 2 HYDRAULIC PRESSURE. MAINTENANCE REVEALED THAT OUTBOARD RT FLIGHT SPOILER VALVE HAD FAILED WHICH RESULTED Feb 9, 2000 · Dhav DHC8301 · Drag Control SystemSDR CA000110015Oxygen Mask · leaking(CAN) DURING PREFLIGHT INSPECTION, THE CAPTAINS OXYGEN MASK WAS FOUND TO BE LEAKING.Jan 2, 2000 · Dhav DHC8301 · Crew Oxygen SystemSDR CA991230034Display · failed(CAN) THE CAPTAINS EADI SCREEN HAD NO DISPLAY AND SMELLED BURNED.Dec 3, 1999 · Dhav DHC8301 · Integrated Flight SystemSDR CA991208029Valve · stuck(CAN) MIST IN CABIN REPORTED AFTER SELECTING NR 1 BLEED ON. ENG P2.5-3 AIR SWITCH STUCK IN P3 POSITION CAUSING OIL TO BE FORCED PAST THE SEALS AND INTO COMPRESSOR.Nov 28, 1999 · Dhav DHC8301 · Compressor Bleed ControlSDR CA991208028Coffee Warmer · failed(CAN) THE FLIGHT CREW REPORTED AN ELECTRICAL SMELL IN THE CABIN DURING TAKEOFF AND RETURNED TO THE AIRPORT. MAINTENANCE INVESTIGATION REVEALED THE COFFEE WARMER TO BE MALFUNCTIONING AND REPLACED IT.Nov 23, 1999 · Dhav DHC8301 · Buffet/GalleysSDR CA991208027Switch · stuck(CAN) DURING THE TAKEOFF ROLL, THE CREW NOTICED THE BAG DOOR WARNING LIGHT COME ON AND ABORTED THE TAKEOFF. MAINTENANCE DETERMINED THE BAGGAGE DOOR PROXIMITY SWITCHES TO STICK (COMPRESSED) BEYOND THEIR NORMAL DOOR CLOSED POSITION, EVEN WHEN THE DOOR WAS OPENENov 7, 1999 · Dhav DHC8301 · Cargo/Baggage DoorsSDR CA991209014Fuel Control · failed(CAN) AFTER TAKEOFF THE NR 2 ENGINE PARAMETERS BEGAN TO FLUCTUATE WITH SEVERE ASSOCIATED YAW. THE AIRCRAFT RETURNED FOR LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL UNIT.Nov 4, 1999 · Dhav DHC8301 · Fuel Control/Reciprocating EnginesSDR CA991103003Line · leaking(CAN) WHILE INVESTIGATING A HYDRAULIC LEAK IN THE NR 2 ENGINE NACELLE AREA, MAINTENANCE FOUND A DAMAGED FLARE ON THE HYDRAULIC LINE TO THE SPOILER UNLOADING VALVE. THE LINE WAS REPLACED.Oct 24, 1999 · Dhav DHC8301 · Hydraulic System, MainSDR CA991027028Cable · damaged(CAN) DURING INSPECTION, NR 1 ENGINE LOWER CONDITION LEVER CABLE WAS BLENDED TO LIMITS AT THE STEEL PULLEY FORWARD OF THE FIREWALL. CABLE REPLACED.Oct 16, 1999 · Dhav DHC8301 · Mixture ControlSDR CA991027027Contactor · malfunctioned(CAN) WHEN MAINTENANCE APPLIED GROUND POWER TO THE AIRCRAFT, THE NR 2 ENGINE BEGAN TO ROTATE. STARTER CONTACTOR 2431-K2 WAS REPLACED AS WELL AS STARTER/GENERATOR WHICH HAD EXCEEDED DUTY LIMITS.Oct 10, 1999 · Dhav DHC8301 · Starter-GeneratorSDR CA991007088Selector Valve · failed(CAN) DURING TAXI, THE NWS FAILED. AFTER TAKEOFF, GEAR RETRACTED NORMALLY, BUT FAILED TO EXTEND WHEN SELECTED.Sep 26, 1999 · Dhav DHC8301 · Landing Gear SelectorSDR CA991007072Rod · failed(CAN) THE LATCH ASSY IS COMPOSED OF 3 SHOOTBOLTS THAT ARE INTERCONNECTED BY ACTUATOR RODS. ON THREE OCCASIONS ACTUATION ROD WAS FOUND BROKEN (DUE TO FATIGUE). FAILURE MAY PREVENT ACCESS FROM THE CABIN TO THE CARGO AREA. SUBMITTER STATED MANUFACTURER IS CONSep 18, 1999 · Dhav DHC8301 · Cargo/Baggage DoorsSDR CA991004014Pipe · leaking(CAN) WHILE INVESTIGATING A HIGHER THAN AMBIENT OAT INDICATION, MAINTENANCE FOUND A LEAKING BLEED AIR PIPE. THE PIPE WAS REPLACED WITH A POST MOD 8/2613 PIPE ASSEMBLY PN 16032-511.Sep 18, 1999 · Dhav DHC8301 · Engine Bleed Air SystemSDR CA991103046Indicator · failed(CAN) NR 2 AIRSPEED INDICATOR FAILED DURING CRUISE FLIGHT AT FL 210. A/P AND Y/D ALSO FAILED. INDICATOR OPERATED ERRATICALLY FOR 1/2 HOUR BEFORE RETURNING TO NORMAL. UNEVENTFUL LANDING CARRIED OUT AT DESTINATION.Sep 17, 1999 · Dhav DHC8301 · Airspeed/Mach IndicatorSDR CA991004013Coupling · leaking(CAN) FLIGHT CREW REPORTED OXYGEN SYSTEM LOSING PRESSURE. MAINTENANCE TRACED PROBLEM TO A LEAKING OXYGEN MASK HOSE COUPLING.Sep 16, 1999 · Dhav DHC8301 · Crew Oxygen SystemSDR CA990927038Manifold · leaking(CAN) DURING CRUISE FLIGHT, THE CREW GOT A HYDRAULICS ISOLATION VALVE CAUTION LIGHT. THE NR 2 HYDRAULIC SYSTEM SHOWED A QUANTITY OF ONLY 1 QUART OF FLUID REMAINING. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE AND MADE A SAFE LANDING AFTER MAKING AN ALTERSep 16, 1999 · Dhav DHC8301 · Landing Gear Steering System
Back to Boeing DHC-8-301