Garrett TPE331-10UA

Service difficulty reports · 375

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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 engine_model_key = 'TPE33110UA'
  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 CA190801009Solenoid · malfunctioned(CAN) CREW WERE LINED UP FOR TAKEOFF, AS THEY ADVANCED THE SPEED LEVERS THE L/H ENGINE SHUT DOWN. THE AIRCRAFT TAXIED BACK TO THE MAINTENANCE HANGAR ON ONE ENGINE AND MAINTENANCE INVESTIGATION FOUND THE PRIMARY ONLY SOLENOID VALVE ON THE L/H ENGINE HAD FAILED,Jul 31, 2019 · Swrngn SA226TC · Fuel Controlling SystemSDR CA190614012Carrier Assy · damaged(CAN) ENGINE HAD A SOAP SAMPLE COME BACK THAT INDICATED MAJOR ALLOY STEAL, MANUFACTURER INDICATED ON THE SOAP IT REQUIRED INSPECTION RIGHT AWAY DUE TO THE FINDINGS OF THE SOAP SAMPLE. THE ENGINE WAS FORWARDED TO AN ENGINE SHOP FOR EVALUATION AND THE PART THATJun 10, 2019 · Swrngn SA226TC · Turbine Engine Reduction GearSDR CA190508001O-Ring · chafed(CAN) LOWER ENGINE COWLING OIL COOLER INTAKE IS HEATED WITH ENGINE OIL. ABOVE THE OIL RING (INTAKE LIP) THERE IS A RUBBER TRANSITION DUCT THAT CONNECTS THE INTAKE LIP TO THE OIL COOLER SHROUD.THE RUBBER DUCT IS REINFORCED WITH METAL WIRE TO RETAIN SHAPE. THE RFeb 12, 2019 · Swrngn SA226TC · Engine Oil CoolerSDR CA180207026Gear · damaged(CAN) THE AIRCRAFT WAS IN FIGHT AND THE PILOTS NOTICED A CHIP LIGHT CAME ON FOR THE RT ENGINE. THE AIRCRAFT CAME TO BASE AND MAINTENANCE DID A OIL SAMPLE AND INDICATED TO THE TURBINE SHOP THAT THERE SEEMED TO BE A BUNCH OF METAL ON THE CHIP DETECTOR. THE OILFeb 17, 2017 · Swrngn SA226TC · Accessory GearboxesSDR CA160314011Turbine Blades · broken(CAN) THE ACFT WAS IN THE HANGER FOR A ROUTINE DAILY INSPECTION WHEN MAINTENANCE NOTICED THAT WHEN HE LOOKED UP THE EXHAUST PIPE ON THE ENGINE THAT HE COULD SEE THE NR 3 TURBINE ROTOR HAD DAMAGE ON IT. THE TURBINE SHOP WAS NOTIFIED OF THE PROBLEM AND THE MAINMar 10, 2016 · Swrngn SA226TC · Turbine SectionSDR CA160311004Window Frame · corroded(CAN) DURING AN AIRFRAME STRUCTURE INSPECTION REQUIRED, ST-UN-M002, 5-2, WHICH IS ON A 25000 TTAF INSPECTION CYCLE, THE BOTTOM OF THE LT OTBD WINDSHIELD POST WAS FOUND TO BE SIGNIFICANTLY CORRODED. THE PORTION THAT IS CORRODED IS SANDWICHED BETWEEN A STEEL BMar 9, 2016 · Swrngn SA226TC · Fuselage Main, StructureSDR CA160127008Indicator · shorted(CAN) 5 MINUTES AFTER TAKEOFF, CREW NOTED BOTH AC BUSS LIGHTS ILLUMINATED AND SMOKE BEGAN TO COME FROM THE RT FUEL QUANTITY GAUGE. THE NR 1 AC BUSS CIRCUIT BREAKER HAD TRIPPED. THEY TURNED THE INVERTER SWITCH OFF AND CONTINUED TO DESTINATION AND LANDED SAFELJan 23, 2016 · Swrngn SA226TC · Fuel Quantity IndicatorSDR CA150910008Windshield · cracked(CAN) AT CRUISING ALTITUDE FL20 THE LT WINDSHIELD DEVELOPED SUDDEN SUBSTANTIAL CRACKING. PILOT SLOWED THE ACFT REDUCED PRESSURIZATION AND DESCENDED TO 10000 FT AND RETURNED. LANDING UNEVENTFUL.Sep 9, 2015 · Swrngn SA226T · Flight Compartment WindowsSDR CA150910007Wire · broken(CAN) ALL 3 GEAR LIGHTS FAILED TO ILLUMINATE ON GEAR DOWN SELECTION AND GEAR LIGHTS FAILED TO TEST WHEN TESTED IN FLIGHT. AFTER 2 GEAR CYCLES AND WHEN INDICATOR BOX TAPPED ALL 3 LIGHTS ILLUMINATED AND ACFT LANDED UNEVENTFULLY. SYS INSPECTED AND A BROKEN WIRESep 7, 2015 · Swrngn SA226T · Landing Gear System WiringSDR CA150123003Exhaust Duct · cracked(CAN) WHILE PERFORMING NR 1 PHASE INSPECTION, FOUND NR 1 ENGINE AFT TURBINE EXHAUST HOUSING HAS A CRACK AT 1:00 POSITION ALONG SIDE A WELDED REPAIRED AREA.Jan 23, 2015 · Swrngn SA226TC · Engine Collector/Tailpipe/NozzleSDR CA141110012Bolt · damaged(CAN) DURING ROUTINE MAINTENANCE A PORTION OF BOLT 6924B1 WAS FOUND IN THE COWLING MISSING ITS HEAD (9 O CLOCK POSITION BOLT). THIS BOLT IS ONE OF 3 THAT LOCATE THE COMBUSTION CHAMBER IN THE COMBUSTION CASE ASSEMBLY. UPON REMOVAL OF THE 2 REMAINING BOLTS, ONE Nov 7, 2014 · Swrngn SA226TC · Turbine Engine Combustion SectionSDR CA140904010Screw · damaged(CAN) FOLLOWING NORMAL TAKEOFF, ON CLIMBOUT PASSING 7500FT THE FLIGHT CREW EXPERIENCED AN OVERSPEED ON THE RT ENGINE, THE PROPELLER SPEED LEVER WAS PULLED BACK TO REDUCE PROPELLER RPM WITH NO EFFECT. THE END RESULT WAS THE FCU OVERSPEED GOVERNOR HELD THE ENGISep 3, 2014 · Swrngn SA226TC · Propeller AssemblySDR CA140702011Fuel Control · malfunctioned(CAN) ON THE FIRST OCCURRENCE, THE ACFT LANDED AND WHEN FULL REVERSE WAS SELECTED, THE ENGINE APPEARED TO LOSE POWER. THE STOP AND FEATHER WAS PULLED AND THE ACFT WAS INSPECTED BY AN AME. AFTER SOME RIGGING ADJUSTMENTS THAT APPEARED TO FIX THE PROBLEMS THE AJun 3, 2014 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA140723002Sun Gear · damaged(CAN) UPON HAVING A CHIP LIGHT IN THE COCKPIT THERE WAS A OIL SAMPLE TAKEN THAT VERIFIED THERE WAS AN ISSUE WITH THE ENGINE. THE ENGINE WAS REMOVED AND FORWARDED TO THE TURBINE SHOP AND WAS DISMANTLED TO THE AREA OF THE NOTED DAMAGE OF THE SUN GEAR TOOTH. THMay 20, 2014 · Swrngn SA226TC · Turbine Engine Reduction GearSDR CA140303020Switch · failed(CAN) DURING PRE-FLIGHT CHECKS, THE PILOT CHECKED THE ANNUNCIATOR PANEL WITH THE PRESS TO TEST SWITCH AND SEVERAL LIGHTS DID NOT ILLUMINATE. MAINTENANCE WAS CALLED TO LOOK INTO THE PROBLEM AND DETERMINED THAT THE LIGHTS THAT WOULD NOT TEST WERE ASSOCIATED WITHMar 1, 2014 · Swrngn SA226TC · DC Power Distribution SystemSDR CA140212007Bolt · failed(CAN) AIRCRAFT EXPERIENCED AN ELEVATOR MALFUNCTION ON LANDING. IN THE FLARE THE CREW LOST ALL ABILITY TO MANEUVER THE ELEVATOR LEAVING THE CONTROL COLUMN WITH NO RESISTANCE AT ALL. THIS HAPPENED ON TOUCHDOWN WITH THE RESULT OF THE ACTUAL LANDING UNAFFECTED. Feb 2, 2014 · Swrngn SA226TC · Elevator StructureSDR CA130925005Master Cylinder · leaking(CAN) THE FLIGHT CREW NEEDED TO APPLY FULL RT RUDDER TO KEEP ACFT STRAIGHT DURING TAKE-OFF. THE TAKEOFF WAS REJECTED AND DURING TAXI A FIRE WAS OBSERVED AT THE LT MLG FROM THE CABIN. THE CREW STOPPED THE ACFT, ENGINES WERE SHUTDOWN AND ATC ADVISED OF FIRE. Sep 22, 2013 · Swrngn SA226TC · Master Cylinder/Brake ValveSDR CA130621006Mixing Valve · failed(CAN) ACFT EXPERIENCED A WING OVERHEAT LIGHT IN CRUISE. DURING THE INVESTIGATION INTO THE CAUSE OF THE OVERHEAT LIGHT INDICATION, MAINTENANCE DISCOVERED THE CONDITIONED AIR MIXING VALVE FOR THE AFFECTED SIDE TO HAVE ITS BUTTERFLY VALVE STRIPPED ABOUT ITS SPLIJun 19, 2013 · Swrngn SA226TC · Pneumatic Distribution SystemSDR KY7A20130304001Fcu · intermittentFLIGHT CREW REPORTED THAT AFTER DEPARTING, THEY EXPERIENCED A MOMNENTARY "SURGE" OF E1 TORQUE ON CLIMBOUT AT 12000 FT MSL, FOLLOWED BY STABILIZATION OF ENGINE OPERATION. MX ADVISED PILOT TO RETURN TO DEPARTURE. RE-ROUTED. ON FINAL APPROACH, PILOT WAS UNABLE TFeb 27, 2013 · N276CA · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA120615004Turbine Wheel · cracked(CAN) THE ENGINE WAS REMOVED FROM THE ACFT FOR A SCHEDULED O/H. WHEN THE ENGINE WAS TORN DOWN FOR INSPECTION OF ALL COMPONENTS, THE NR1 T-WHEEL WAS SENT TO THE NDT DEPARTMENT FOR AN FPI INSPECTION WHICH IS ROUTINE TO THE ENGINE INSPECTION REPAIR MANUAL. THEJun 15, 2012 · Turbine SectionSDR 2012FA0000356Downlock Switch · defectiveON LANDING THE PILOT NOTICE THE LT DOWNLOCK FAILED TO ILLUMINATE. A FLY BY WAS PERFORMED AND A NORMAL LANDING WAS PERFORMED WITH NO OTHER PROBLEMS.Jun 6, 2012 · N841BC · Swrngn SA226TC · Landing Gear Position and WarningSDR CA120223004Attach Fitting · cracked(CAN) DURING A BLOCK INSPECTION IT WAS NOTICED VISUALY THAT THE FRONT SPAR REAR WING ATTACH FITTING WAS CRACKED. ONCE THE FITTING WAS REMOVED, ADDITIONAL DEFECTS WERE NOTICED ON THE UNDER SIDE. THE ADDITIONAL DEFECT COULD ONLY BE DETECTED BY EDDY CURRENT.Dec 30, 2011 · Swrngn SA226TC · Wing, Fuselage Attach FittingsSDR CA111024009Spur Gear · damaged(CAN) MX NOTIFIED OF A CHIP LIGHT ON THE ACFT AND WHEN THEY INSPECTED THE CHIP DETECTOR IT WAS NOTICED TO HAVE ALOT OF METAL ON THE DETECTOR. THE OIL FILTER WAS PULLED AND GEARCASE DRAINED. THE ENGINE WAS THEN REMOVED DUE TO THE AMOUNT OF METAL PRESENT. THE Sep 24, 2011 · Accessory GearboxesSDR CA110812004Attach Fitting · crackedDURING REMOVAL OF THE CRACKED AFT WING TO FUSELAGE ATTACH FITTING THE FORWARD HALF OF THE ASSY WAS DAMAGED. ON REMOVAL, IT WAS DISCOVERED THAT THE FITTING WAS CRACKED. THE FLAW COULD NOT BE SEEN WITHOUT REMOVING THE SEALANT.Aug 2, 2011 · Swrngn SA226TC · Wing, Fuselage Attach FittingsSDR CA110803028Fuel Control · leakingMX WAS TROUBLESHOOTING A DEFECT RELATED TO POWER LEVER SPLIT IN CRUISE, THE MAX POWER ADJUSTMENT CAP WAS REMOVED FROM THE BACK OF THE FCU. THE BACK OF THE FUEL CONTROL, WHICH IS NORMALLY DRY, WAS COMPLETELY FULL OF FUEL. AN INTERNAL LEAK WAS SUSPECTED AND THEAug 1, 2011 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA110812003Attach Fitting · crackedDURING THE 6750 BLOCK INSP, A TECH THOUGHT THAT NOTICED A CRACK ON THE AFT WING TO FUSELAGE ATTACH FITTING. THE CRACK WAS CONFIRMED BY EDDY CURRENT PRIOR TO PART REMOVAL.Aug 1, 2011 · Swrngn SA226TC · Fuselage Main, Attach FittingsSDR 2011FA0000779Fuel · inadequateWHILE DEMONSTRATING EXTERNAL LOAD CAPABILITY DIRECTLY ABOVE A JUNGLE HELIPAD, THE ENGINE BEGAN TO LOOSE RPM AND THE ACFT LANDED BACK ON THE PAD. THE LANDING WAS CONTROLLED AND TOUCHDOWN WAS CUSHIONED SO AS TO AVOID ANY DAMAGE. POSTFLIGHT INSPECTION REVEALED Jun 26, 2011 · N17756 · Skrsky S55 · Aircraft Fuel SystemSDR CA110404004Pinion Gear · damaged(CAN) ENG TPE331-10UA-511G, SN P-54019 WAS IN THE TURBINE SHOP FOR ITS SCHEDULED OVERHAUL. WHEN THE INSPECTION WAS CARRIED OUT ON THE HIGH SPEED PINION IT WAS NOTED THAT ONE OF THE GEAR TEETH WAS DAMAGED. THE HELICAL TOOTH ON ONE GEAR HAD A CHIP ON THE TOOTHApr 4, 2011 · Turbine Engine Reduction GearSDR CA101028004Truss · damaged(CAN) MAINTENANCE FOUND THAT THE ANTI-ICE VALVE HAD BEEN RUBBING UP AGAINST THE ENGINE TRUSS, CAUSING A SCREW ON THE ELECTROMAGNETIC RECEPTACLE ASSEMBLY TO COME LOOSE, WHICH THEN WORE A HOLE THROUGH THE ENGINE TRUSS. THE IPC LISTS 319980-6-1 (PRE SB 75-009) AOct 27, 2010 · Swrngn SA226TC · Engine Mount SectionSDR CA101007014Mount · crackedUPON ROUTINE SERVICING, MX FOUND LT LOWER ENGINE FRAME TO BE CRACKED THROUGH BOTH INBD AND OTBD, PART WAS REMOVED FOR REPAIR. ALMOST IDENTICAL TO INCIDENT ON SEPT 30TH, 2010. REF SDR 20101007013.Oct 7, 2010 · Swrngn SA226AT · Engine Mount SectionSDR CA101012004Housing · crackedOUTPUT HSG CRACK LINE MX WAS DOING A ROUTINE INSP ON ENGINE, WHEN ONE OF THE MECHANICS NOTICED A CRACK ON THE SIDE OF THE ACCY DRIVE HSOUSING. THE TURBINE SHOP WAS NOTIFIED OF THE ISSUE AND UPON FURTHER INSP, THE ENG WAS DETERMINED TO HAVE TO COME OFF TO BE ROct 6, 2010 · Swrngn SA226TC · Turbine Engine Accessory DriveSDR CA101007013Frame · crackedUPON ROUTINE ENG SERVICING, FOUND RT LOWER ENGINE FRAME ASSY TO BE CRACKED THROUGH MAIN BAR ON BOTH INBD AND OTBD.Sep 30, 2010 · Swrngn SA226TC · Engine Mount SectionSDR CA100929007Windshield · crackedON APPROACH, THE CREW NOTICED THE CAPTAINS HEATED WINDSHIELD HAD CRACKED. THE CREW RETURNED TO DEPARTURE. THE ACFT WAS FERRIED TO MAIN BASE AND THE WINDOW WAS REPLACED.Sep 16, 2010 · Swrngn SA226TC · Flight Compartment WindowsSDR DALA1022685507Wire · damagedDURING L CHECK, MX FOUND SEAT EMERGENCY LIGHTS AT ROWS 21-23ABC INOPERATIVE. MX REPAIRED WIRES BY SEATS 22C & 23C, AND REPLACED THE FUSE ON M11612 POWER SUPPLY. OPS CHECK WAS GOOD.Sep 12, 2010 · N507US · Boeing 757251 · Light System WiringSDR CA101207005Windshield · failed(CAN) DURING DESCENT THROUGH 14000 ASL AIRCRAFT EXPERIENCED MOMENTARY MODERATE TURBULENCE FOLLOWED BY A DEEP `POP` SOUND, DRAWING ATTENTION TO THE RIGHT WINDSHIELD. IT APPEARED THE OUTER LAYER COMPLETELY CRACKED OVER ENTIRE SURFACE. (TC NR 20101207005)May 5, 2010 · Swrngn SA226TC · Flight Compartment WindowsSDR CA100114006Windshield · cracked(CAN) WHILE IN CRUISE, RT WINDSHIELD CRACKED. CREW DIVERTED TO MAIN BASE. REPLACED WINDSHIELD. TOTAL TIME 944.3 HOURS, 2 YEARS IN SERVICE APPROX. NUMEROUS FAILURES OF THIS TYPE, BUT NOT MANY WITH THIS LOW OF HOURS ON IT.Jan 12, 2010 · Swrngn SA226TC · Flight Compartment WindowsSDR CA091222007Windshield · cracked(CAN) APROX 60 NM NORTH WEST, IN CRUISE THE CREW HEARD A LOUD CRACKING NOISE AND NOTICED THE LT HEATED WINDSHIELD HAD SHATTERED. THE CREW IMMEDIATELY STARTED DECENT AND DECREASING THE CABIN DIFFERENTIAL TO ZERO. THESE WINDOWS ON THE METRO ACFT CONTINUE TO FAIDec 11, 2009 · Swrngn SA226TC · Flight Compartment WindowsSDR CA091222006Windshield · cracked(CAN) ON DECENT FOR LANDING. THE CREW NOTICED THE CAPTAINS HEATED FRONT WINDSHIELD HAD A LARGE CRACK THAT SPIDERED DOWN THE WINDOW.Dec 10, 2009 · Swrngn SA226TC · Flight Compartment WindowsSDR CA091210008Switch · failed(CAN) AFTER TAKE-OFF, GEAR WAS SELECTED UP AND 3 GREEN LIGHTS REMAINED, THERE WAS NO APPARENT MOVEMENT OF GEAR. GEAR WAS THEN CYCLED SEVERAL TIMES, AND LANDING GEAR CB PULLED AND RESET. NO IN TRANSIT LIGHTS WERE ILLUMINATED AT ANY POINT AND HYD PRESSURE WAS NODec 8, 2009 · Swrngn SA226TC · Landing Gear Position and WarningSDR CA091202011Relay · malfunctioned(CAN) CREW ARRIVED AFTER ONE HOUR FLIGHT REPORTING ABNORMAL LT GENERATOR VOLT METER INDICATION. THE GEN FAIL LIGHT FUNCTIONED NORMALLY WITH THE GENERATOR OFF OR ON, HOWEVER, THE GENERATOR WOULD NOT SUPPLY THE BUS, THIS WAS CONFIRMED ON A GROUND RUN CHECK. AFDec 1, 2009 · Swrngn SA226TC · DC Generating SystemSDR CA091125007Trunnion · corroded(CAN) FOUND CORROSION PITTING IN TRUNNION BORES ON BOTH SIDES OF NLG TRUNNION, WHICH HOUSE THE DRAG BRACE PINS. PITTING IS 0.030 INCHES DEEP LONGITUDINALLY IN END OF BORE AND 0.045 INCHES DEEP LATERALLY AT END OF BORE, AROUND THE BORE RADIUS FOR APPROXIMATELYNov 21, 2009 · Swrngn SA226TC · Fuselage, Landing Gear Attach FittingsSDR CA091209003Bearing Race · failed(CAN) THE ACFT CAME IN FOR A CHIP LIGHT SNAG AND WHEN THE MX DEPARTMENT INSPECTED CHIP DETECTOR IT WAS NOTED TO HAVE QUITE A BIT OF METAL ON THE DETECTOR. ENG SHOP WAS NOTIFIED AND IT WAS DETERMINED THAT A REPAIR WAS NECESSARY AT THAT TIME. GEARBOX WAS REMOVNov 17, 2009 · Swrngn SA226TC · Engine (Turbine/Turboprop)SDR CA091118009Stop · broken(CAN) ON APPROACH WHEN THE GEAR WAS SELECTED DOWN ONLY 2 MAINS WENT GREEN. CREW DIDN’T GET THE RED IN TRANSIT ON NOSE GEAR EITHER, THEY RECYCLED THE GEAR SEVERAL TIMES, WITH NO LUCK. AFTER TROUBLESHOOTING SELECTED GEAR DOWN AGAIN AND NOTHING HAPPENED. THEY PUNov 10, 2009 · Swrngn SA226TC · Landing Gear Retraction/Extension SystemSDR CA091113005Bearing Race · failed(CAN) ACFT SUFFERED A RT GENERATOR FAILURE ON DECENT. THE GENERATOR FAIL LIGHT ILLUMINATED IN THE COCKPIT BUT NO ADVERSE RESULTS FROM THE FAILURE OCCURED. MX REPLACED THE GENERATOR FOR INSP AND FOUND THAT THE REAR SUPPORT BRG HAD FAILED, MOST LIKLEY DUE TO OVNov 6, 2009 · Swrngn SA226TC · Starter-GeneratorSDR CA091117006Line · cracked(CAN) UPON SELECTING GEAR DOWN ON FINAL, ACFT EXPERIENCED 2 HYD WARNING LIGHTS, CREW DECLARED AN EMERGENCY. ON THE INITIAL GEAR EXTENSION THE ACFT INDICATED ALL 3 LANDING GEARS DOWN AND LOCKED BUT JUST IN CASE THE CREW ELECTED TO DO THE EMERGENCY GEAR EXTENSIONov 5, 2009 · Swrngn SA226TC · Hydraulic System, MainSDR CA091015006Windshield · cracked(CAN) A LOUD THUD WAS HEARD AND THE CREW NOTICED THE COPILOTS WINDOW WAS SHATTERED. THEY DECENDED AND ASKED FOR PRIORITY HANDLING, BUT DID NOT DECLARE AN EMERGENCY. THEY NOTICED IT WAS THE OUTER PAIN OF GLASS, THEY LANDED UNEVENTFULLY 20 MIN LATER. MX HAS SINOct 14, 2009 · Swrngn SA226TC · Flight Compartment WindowsSDR CA090925005Line · chafed(CAN) ON APPROACH THE CREW HAD JUST SELECTED FULL FLAP ON THE FINAL LANDING CHECKS WHEN THEY NOTICED SMOKE IN THE COCKPIT. SINCE THEY WERE LESS THAN 3 MILE FINAL THEY ELECTED NOT TO ATTEMPT TO PUT ON THEIR OXYGEN MASKS. THE CREW DUMPED CABIN PRESSURE, TURNED TSep 22, 2009 · Swrngn SA226TC · Hydraulic System, MainSDR CA090917004Shutoff Valve · failed(CAN) AFTER THE ENGINE WAS OVERHAULED AND WAS INSTALLED IN THE TEST CELL, WHEN TRYING TO DO A START, ENG WOULD NOT LIGHT OFF. IT WAS NOTED THAT THERE WAS NO FUEL GOING TO THE ENG WHEN STARTING. AFTER TROUBLESHOOTING THE STARTING ISSUES IT WAS FOUND TO BE A FASep 17, 2009 · Fuel Selector/Shut-Off ValveSDR CA090918004Hose · ruptured(CAN) UPON CLIMBOUT THE AIRCRAFT HYDRAULIC WARNING LIGHTS ILLUMINATED AND HYDRAULIC PRESSURE WAS LOST. THE AIRCRAFT RETURNED TO THE AIRPORT AND PERFORMED A FLAPLESS LANDING WITH THE EMERGENCY GEAR HANDLE ACTIVATED. MAINTENANCE DISCOVERED THE HYDRAULIC FLEXIBLSep 15, 2009 · Swrngn SA226TC · Hydraulic System, MainSDR CA090918011Switch · failed(CAN) UPON TAXI THE FLIGHT CREW NOTED THAT THE NOSE WHEEL STEERING WAS UNRESPONSIVE. THE TEST FUNCTION WORKED FINE. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REPLACED THE FAILED POWER LEVER NOSE STEERING MICROSWITCH. NO WARNING INDICATIONS WERE GIVESep 13, 2009 · Swrngn SA226TC · Landing Gear Steering System
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