Fairchild SA227-AC

Service difficulty reports · 2,182

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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 = 'SA227AC'
  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 CA090708007Oil Jet · broken(CAN) ACFT HAD LANDED AND WAS TAXING BACK TO HANGER WHEN RT ENG HAD SHUT ITSELF DOWN WITHOUT ANY INPUT FROM THE CAPTAIN. MAINT WAS NOTIFIED OF ISSUE AND WHEN TURNING THE PROP OVER BY HAND A LOUD CLICKING NOISE WAS NOTED. AT THAT TIME TURBINE SHOP WAS NOTIFIEDJul 7, 2009 · Swrngn SA227AC · Turbine Engine Oil SystemSDR CA090619012Shutoff Valve · inoperativeON DESCENT INTO AIRPORT, ACFT LOST PWR ON RT ENG AND FLIGHT CREW SHUT DOWN AND FEATHERED ENGINE. MX WAS CONTACTED AFTER LANDING WITHOUT INCIDENT. MX TROUBLESHOOTING WAS CARRIED OUT, FOUND THE FUEL SHUTOFF NOT OPERATING CORRECTLY. FUEL SHUTOFF WAS REPLACED AJun 14, 2009 · Swrngn SA227AC · Fuel Selector/Shut-Off ValveSDR CA090619013Retainer · crackedDURING ROUTINE PHASE INSP OF THE PROP MX, FOUND THAT THE LT ENG PROP SHAFT SEAL RETAINER HAD MULTIPLE CRACKS COMING OUT FROM UNDER EACH OF THE ATTACHMENT STUDS. PART REMOVED AND REPLACED. ACFT RETURNED TO SERVICE.Jun 10, 2009 · Swrngn SA227AC · Propeller AssemblySDR CA090519007Valve · stuck(CAN) DURING THE LANDING ROLLOUT, FLIGHT CREW ATEMPTED TO STEER ACFT USING NOSE WHEEL STEERING WHICH WAS UNRESPONSIVE. NOSE STEERING SYS INDICATED NO FAULTS AND ALL REQUIRMENTS NEEDED FOR NOSE STEERING FUNCTION WERE OBTAINED (IE GEAR DOWN, NWS ARMED, ETC). NOMay 17, 2009 · Swrngn SA227AC · Landing Gear Steering SystemSDR CA090512003Engine · surges(CAN) DURING THE DESCENT, APPROX 30NM FROM AIRPORT, RT ENGINE SURGED, THEN LOST POWER COMPLETELY, NTS LIGHT ILLUMINATED. CONFIRMED WITH POWER LEVER (NO TORQUE MOVEMENT, NOR YAW). COMPLETED ENGINE FAILURE CHECKLIST, DECLARED EMERGENCY (TRUCKS WERE DISPATCHED). May 9, 2009 · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR PNSA050902Control Cable · brokenPILOT SQUAWKED "RUDDER TRIM TAB BROKEN AND LOOSE". RUDDER TRIM TAB WAS DEFLECTED FULLY TO THE RIGHT WHEN THE AIRCRAFT ARRIVED AT MAINTENANCE BASE. PILOT REPORTED FULL RIGHT RUDDER DEFLECTION WAS REQUIRED TO CONTROL THE AIRCRAFT. MAINTENANCE FOUND BROKEN RUDMay 8, 2009 · N640PA · Swrngn SA227AC · Rudder Tab Control SystemSDR CA090506001Cooling Turbine · overserviced(CAN) FLIGHT CREW OBSERVED SMOKE IN CABIN. ACFT RETURNED TO BASE. MX WAS CALLED AND UPON INSP FOUND EXCESSIVE OIL IN UNIT AND OIL SMEARED AROUND THE PANEL BY THE AIR CYCLE MACHINE. THE OIL LEVEL WAS ADJUSTED AND THE EXCESS AMOUNT WAS REMOVED. ACFT GROUND TESTSApr 30, 2009 · Swrngn SA227AC · Cabin Cooling SystemSDR CA090407006O-Ring · split(CAN) BOTH HYDR LIGHTS CAME ON IN FLIGHT AND ACFT RETURNED TO BASE. MX FOUND THE LT HYDR PUMP PRESSURE FITTING LEAKING. THE FITTING WAS REMOVED AND AND THE O-RING WAS FOUND DAMAGED. O-RING REPLACED - SYS SERVICED AND RETURNED TO SERVICE.Mar 29, 2009 · Swrngn SA227AC · Hydraulic Pump (Electric/Engine), MainSDR CA090331003Accumulator · fractured(CAN) ACFT DEPARTED AND WHILE IN CLIMB WHEN FLAPS WERE SELECTED UP A LOUD "POP" WAS HEARD AND THEN ALL HYDR PRESSURE WAS LOST AND BOTH LT/RT LIGHTS ILLUMINATED. ACFT TURNED AROUND, CARRIED OUT AN EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCIDENT. MX INVESTIMar 25, 2009 · Swrngn SA227AC · Hydraulic Accumulator, AuxiliarySDR CA090202003Windshield · crackedIN CRUISE AT FL230 SOUTHBOUND, A LOUD BANG HEARD BY BOTH CREW AND SAW F/O SIDE WINDSHIELD SHATTER, BUT REMAINED INTACT. NO LOSS OF PRESSURIZATION. FLIGHT DESCENDED TO FL100 AND CREW INFORMED ATC BUT DID NOT DECLARE AN EMERGENCY. LANDED WITHOUT FURTHER INCIDEFeb 1, 2009 · Swrngn SA227AC · Flight Compartment WindowsSDR 2009FA0000237Impeller · damagedDURING TAKEOFF (ASCENT), ACFT SUFFERED A BIRD STRIKE IN THE RT ENGINE. THE PILOT VERIFIED HIS PARAMETERS AND THEY DID NOT HAVE ANY VIBRATION. HOWEVER, HE SMELLED BURNED BIRD AND DECIDED TO RETURN TO DEPARTURE AIRPORT. DURING THE WALK AROUND INSP, THE PILOT Dec 2, 2008 · N239LC · Swrngn SA227AC · Turbine Engine Compressor SectionSDR DUFA20080003Overheat Sensor · false activationWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE RT WING OVERHEAT LIGHT ILLUMINATED. THE RT GENERATOR WAS SHUT DOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FOR ENGINE SHUT DOWNov 26, 2008 · N158MC · Swrngn SA227AC · Overheat DetectionSDR CA081117003Ignition Switch · cracked(CAN) ACFT DEPARTED AIRPORT AND CREW NOTICED SMOKE IN THE CABIN. THE CREW TURNED THE TEMP CONTROLLER OFF - THE BLEEDS WERE TURNED OFF WHICH DUMPED THE CABIN PRESSURIZATION. THE LOW OIL PRESSURE LIGHT CAME ON ALONG WITH THE EGT STARTING TO RISE. ENGINE WAS THNov 13, 2008 · Swrngn SA227AC · Engine Start Valves/ControlsSDR CA081114005Impeller · cracked(CAN) HOT SECTION INSPECTION WAS BEING CARRIED OUT BY ENGINE SHOP ON ENGINE SN P44659C AND IT WAS NOTED THAT THE IMPELLER WAS CRACKED. THIS IMPELLER IS NOT TRACKED. THE TIMES ON THE IMPELLER SINCE INSTALL ARE 2407.0 AND 3434 CYCLES. THIS IS NOT THE 1ST INSTANCNov 4, 2008 · Swrngn SA227AC · Turbine Engine Compressor SectionSDR MT92008F00007Wire · brokenON TUESDAY 11/4/08, FLIGHT RETURNED TO RAMP AFTER DEPARTURE. PILOT IN COMMAND STATED THAT AFTER ROTATION AND STANDARD DEPARTURE, HE SELECTED FLAPS UP. NO CHANGE IN ACFT CONFIGURATION WAS NOTED AND NO MOVEMENT ON THE FLAP INDICATOR. HYDR PRESSURE AND ALL CIRNov 4, 2008 · N592BA · Swrngn SA227AC · Flight Control System WiringSDR CA081103005Ignition Switch · cracked(CAN) OIL LEAK ON THE ENG FROM LWR ENG COWL FOUND. TROUBLESHOOTING REVEALED THE PROBLEM AS A AUTO IGNITION PRESSURE SWITCH LEAKING AT THE BASE WELD. INSP WITH A MAGNIFYING GLASS FOUND A CRACK APR .7500 AROUND THE CIRCUMFERENCE OF THE WELD.Oct 30, 2008 · Swrngn SA227AC · Engine Starting SystemSDR CA081020009Tire · separated(CAN) DURING GROUND HANDLING PROCEDURES THE NR2 MAIN WHEEL WAS FOUND TO BE SHREDDED AND THE TREAD PORTION OF THE TIRE MISSING. THIS TIRE WAS A RECAPPED TIRE RECEIVED FROM A CERTIFIED FAA REPAIR STATION. THE TIRE WHEN IT SHREDDED CAUSED DAMAGE TO THE ACFT FLAPOct 7, 2008 · Swrngn SA227AC · TireSDR CA081007010Disc · worn(CAN) THIS BRAKE ASSEMBLY WAS REMOVED FROM ACFT ON THE RT - O/B GEAR FOR BRAKE WEAR BEYOND LIMITS. UPON TEAR DOWN THE LUGS WERE FOUND TO HAVE WORN APPROXIMATELY 40% WHILE THE RIM SIDE HAD MINIMAL WEAR AND THE RIM WAS RETURNED TO SERVICE. THIS TYPE OF WEAR ISOct 2, 2008 · Swrngn SA227AC · Landing Gear Brake SystemSDR CA080912006Tube · cracked(CAN) DURING THE PREFLIGHT WALKAROUND, THE FLIGHT CREW NOTICED OIL DRIPPING FROM THE RT ENGINE. MX WAS DISPATCHED TO THE LOCATION WHERE THE STAINLESS STEEL TUBE ASSY FROM THE ENGINE PROP GOVERNOR TO THE NEGATIVE TORQUE SENSING (NTS)MANIFOLD WAS FOUND LEAKING. Sep 8, 2008 · Swrngn SA227AC · Engine Oil Distribution (Airframe Furnished)SDR CA080819011Tube · fractured(CAN) TUBE HAD BROKEN AT WELDMENT THAT ATTACHES THE TUBE TO THE FLANGE THAT BOLTS IT TO THE ENGINE BLEED. AIR PORT WAS CRACKED 90% OF THE WAY AROUND WELD. THIS CAUSED THE ENGINE TO NOT REACH TARGET TORQUES UNLESS WATER METH WAS USED. UNIT WAS REPLACED AND AAug 10, 2008 · Swrngn SA227AC · Engine Bleed Air SystemSDR CA080728008Fitting · cracked(CAN) ON INSPECTION, IT WAS DISCOVERED THAT THERE WAS AN OIL LEAK AROUND THE RT ENGINE PROP GOVERNOR. UPON FURTHER INSPECTION IT WAS FOUND THAT THE FITTING WAS CRACKED HALF WAY AROUND THE FITTING. FITTING REPLACED AND ACFT RETURNED TO SERVICE.Jul 22, 2008 · Swrngn SA227AC · Propeller GovernorSDR CA080728007Structure · bent(CAN) ON APPROACH PILOT EXTENDED GEAR AND HAD GREEN INDICATION FOR NOSE AND LT MAIN GEAR ONLY, INTRANSIT LIGHT WAS ON FOR RT GEAR. PILOT RECYCLED GEAR AND ALL 3 GREEN INDICATIONS WERE NOW PRESENT. ACFT LANDED WITHOUT FURTHER PROBLEMS. MAINT WAS CALLED AS THE RJul 22, 2008 · Swrngn SA227AC · Landing Gear DoorsSDR CA080724003Bearing · spalled(CAN) SN OF THE PART IS MS030633106124 WAS UNABLE TO PUT THIS INTO SN FIELD. A/C WAS DOWN FOR A ROUTINE OIL SAMPLE. AT THIS TIME THE OIL SAMPLE WAS NOTED TO HAVE A UNUSUAL AMOUNT OF METAL IN THE OIL SAMPLE. THE ENGINE SHOP WAS INFORMED TO HAVE A LOOK AT THE MJul 17, 2008 · Swrngn SA227AC · Turbine Engine Compressor SectionSDR DUF2008F00000O-Ring · crackedWHILE ENROUTE, THE PILOT NOTICED HIS LT ENGINE OIL PRESSURE GAUGE FLUCTUATING. SHORTLY THERE AFTER THE "LOW OIL PRESSURE" LIGHT ILLUMINATED. SINCE HE WAS VERY CLOSE TO HIS DESTINATION, THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND SECURE IT AS A PRECAUTION. PJul 10, 2008 · N3108B · Swrngn SA227AC · Turbine Engine Oil SystemSDR CA080711002Indicator · burned(CAN) ON APPROACH THE CREW REPORTED A LOUD POP WHICH WAS FOLLOWED BY AN ELECTRICAL ODOR AND THE DME WENT OFF LINE. THE CREW SHUT DOWN ALL NON-ESSENTIAL AVIONICS AND CONTINUED WITHOUT INCIDENT. THE ACFT WAS THEN POSITIONED AT THE HANGAR WHERE MX REMOVED AND CARJul 9, 2008 · Swrngn SA227AC · DME/TACAN SystemSDR JIK2008F00003Accumulator · failedAFTER TAKEOFF, BOTH HYDRAULIC PRESSURE LIGHTS CAME ON RIGHT AFTER GEAR RETRACTION. PILOT DECLARED AN EMERGENCY, CONDUCTED AN EMERGENCY GEAR EXTENSION PROCEDURE, AND MADE A LANDING WITHOUT FURTHER INCIDENT. UPON EXAMINATION, IT WAS DISCOVERED THAT THE HYDRAULICJul 3, 2008 · N423MA · Swrngn SA227AC · Hydraulic Power Accumulator, MainSDR JIK2008F00002Accumulator · failedFOLLOWING TAKEOFF, BOTH HYDR PRESSURE LIGHTS CAME ON RIGHT AFTER GEAR RETRACTION. PILOT DECLARED AN EMERGENCY, CONDUCTED AN EMERGENCY GEAR EXTENSION PROCEDURE, MADE A LANDING WITHOUT FURTHER INCIDENT. UPON EXAMINATION, IT WAS DISCOVERED THAT HYDR ACCUMULATOR Jul 3, 2008 · N423MA · Swrngn SA227AC · Hydraulic System, MainSDR MT92008F00004Spacer · misinstalledIN FLIGHT, THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO THE LT ENGINE. THIS FORCED THEM TO DO AN INFLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND SPACER THAT SECURES TJun 19, 2008 · N26932 · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR MT92008F00003Screw · misinstalledIN FLIGHT, THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO THE LT ENGINE. THIS FORCED THEM TO DO AN INFLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND SPACER THAT SECURES TJun 19, 2008 · N26932 · Swrngn SA227AC · Powerplant SystemSDR MT9A0000001Screw · missingIN FLIGHT THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO THE LEFT ENGINE. THIS FORCED THEM TO DO AN IN-FLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND SPACER THAT SECURES TJun 19, 2008 · N26932 · Swrngn SA227AC · Power LeverSDR CA080625004Line · cracked(CAN) ON APPROACH, CREW NOTED A DROP IN HYDR PRESSURE FOLLOWED BY THE ILLUMINATION OF THE HYDR WARNING LIGHTS. THE HYDR PRESSURE WENT TO ZERO AND CREW CREW CONSULTED TO APPROPRIATE CHECKED LIST AND COMPLETED A MANUAL EXTENSION OF THE LANDING GEAR USING THE ALTJun 18, 2008 · Swrngn SA227AC · Hydraulic System, MainSDR CA080611010Bearing Race · damaged(CAN) THE INNER SEAL WAS NOTED TO BE PROTRUDING MORE THAN NORMAL. WHEEL ASSY WAS REMOVED AND THE INNER RACE WAS FOUND TO NOT BE SEATED ALL THE WAY. SERVICEABLE WHEEL ASSY WAS INSTALLED ON THE ACFT AND ACFT RETURNED TO SERVICE.Jun 10, 2008 · Swrngn SA227AC · Wheel/Ski/FloatSDR SIMA200816501Floorbeam · corrodedDURING A HMBV INSPECTION, THE L ANGLE ON FRAME 225 AT THE GALLEY FLOOR AREA WAS FOUND TO HAVE LEVEL TWO CORROSION. FABRICATED A FILLER, SHIM AND REPAIR ANGLE. TREATED ALL PARTS AND INSTALLED IN AIRCRAFT. REPAIR DONW IAW SAAB 340 SRM (SRM 72LKS 3079 REV 50) Jun 5, 2008 · N340AE · Swrngn SA227AC · Fuselage Main, Floor BeamSDR CA080403003Tube · crackedDURING TAKEOFF, THE CREW NOTED THE LT ENGINE WAS A LITTLE LOW ON POWER. DECIDED TO RETURN TO THE AIRPORT AS THE FUEL FLOW INDICATION FOR THAT ENGINE WAS ERRATIC. THE LANDING WAS UNEVENTFUL. ONCE ON THE GROUND THE AIRCRAFT WAS INSPECTED BY MAINTENANCE AND THMar 31, 2008 · Swrngn SA227AC · Engine Fuel DistributionSDR CA080319007Switch · intermittentON APPROACH, THE CREW NOTICED THAT THE LT GEAR HAD NO "GREEN" SAFE LIGHT. FLY BY WAS CARRIED OUT CONFIRMED GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. SWITCH WAS FOUND STICKY. SWITCH REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20080319007)Mar 6, 2008 · Swrngn SA227AC · Landing Gear Position and WarningSDR 2008FA0000250Engine · overheatedIN CRUISE TO 8000 FT, INDICATION OF RED LIGHT OF OIL PRESSURE WITH 870 DEGREE TEMPERATURE. LIGHT TURNS OFF. AFTER 15 SECONDS, THE LIGHT TURNS ON AGAIN WITH 870 DEGREE TEMPERATURE, BUT THE PRESSURE DOWN NEAR ZERO. THE CREW MADE THE SHUTDOWN ENGINE PROCEDUREMar 5, 2008 · N139LC · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR CA080228011Bellcrank · missingDURING MAINTENANCE GEAR RETRACTION A "CLICKING" NOISE WAS HEARD FROM THE NOSE GEAR WHEELWELL. THE ROLLER BEARING ON THE RT NOSE GEAR BELLCRANK WAS BROKEN AND ONLY THE INNER RACE REMAINED ON THE BOLT. THE BELLCRANK WAS REPLACED, GEARSWINGS CARRIED OUT AND AIRCFeb 27, 2008 · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MCC2008F00001Engine · leakingON DESCENT TO DESTINATION, ENGINE BYPASS LIGHT ILLUMINATED, ATTEMPTED TO PULL POWER BACK, BUT ENGINE SEEMED TO NOT RESPOND AND TEMP STARTED TO RISE. ENGINE SECURED AND UNEVENTFUL LANDING MADE. ON GROUND, NOTICED OIL LEAKING FROM ENGINE. FOUND ENGINE WOULD NFeb 26, 2008 · N2699Y · Swrngn SA227AC · Turbine Engine Oil SystemSDR MT92008F00000Actuator · crackedAC WAS ON A TRAINING FLIGHT IN THE LANDING PATTERN AT AROUND 2130 HOURS. THE TRAINING OFFICER NOTICED THE HYD PRESSURE GOING BETWEEN 400 AND 1800 PSI. HE SELECTED GEAR DOWN AND VERIFIED 3 GREENS BUT MINIMUM PRESSURE WAS LOW. THE CREW SELECTED EMERGENCY GEARFeb 22, 2008 · N370AE · Swrngn SA227AC · Trailing Edge Flap ActuatorSDR MCC2008F00000Governor · failedWHILE TRAINING FOR A CHECK RIDE, POWER WAS PULLED BACK TO SIMULATE ENGINE AT CONDITION. WHEN POWER WAS REAPPLIED, ENGINE FAILED TO RESPOND ENGINE WAS SECURED, TROUBLESHOOTING DECIDED PROP GOV FAILED. PROP GOV WAS REPALCED WITH OVERHAULED UNIT, ALL CHECK SAT.Feb 21, 2008 · N26991 · Swrngn SA227AC · Propeller GovernorSDR CA080228012Pin · damagedPIVOT PIN FOR RT MAIN GEAR TORQUE KNEE WAS PROTRUDING FROM THE TORQUE KNEE. SPRING PIN REMOVED AND INSPECTED. NO DAMAGE FOUND. NEW SPRING PIN INSTALLED. NO FURTHER PROBLEMS SINCE REPLACEMENT OF SPRING PIN (TC NR 20080228012)Feb 20, 2008 · Swrngn SA227AC · Nose/Tail Landing Gear Strut/AxleSDR PNSA080202Unknown · dirtyDURING A CHECK FLIGHT FOR A RT ENGINE CHANGE THE NOSE GEAR WOULD NOT STAY IN THE UPLOCK POSITION. AFTER THE CHECK FLIGHT THE MX DEPARTMENT CLEANED AND LUBED THE NOSE GEAR AND PERFORMED AN OP CHECK, NORMAL.Feb 19, 2008 · N640PA · Swrngn SA227AC · Nose/Tail Landing GearSDR CA080205007Bearing · worn(CAN) TACH/GEN IDLER ASSY DUAL SPUR GEAR, CENTER ANTI FRICTION BEARING FOUND WITH AN UNUSUALLY HIGH AMOUNT OF RADIAL PLAY AND WAS EXTREMELY ROUGH WHEN TURNED OVER BY HAND. THE ENGINE WAS REMOVED DUE TO CARBON STEEL PLATELETS FOUND IN THE OIL SAMPLE.Jan 29, 2008 · Swrngn SA227AC · Turbine Engine Accessory DriveSDR CA080124008Fuel Nozzle · cracked(CAN) DURING SCHEDULED FUEL NOZZLE CHANGE A NOZZLE WAS FOUND TO BE CRACKED IN THE AREA, SECONDARY MANIFOLD FITTING THAT MFG SAYS TO INSPECT. (TC NR 20080124008)Jan 21, 2008 · Swrngn SA227AC · Fuel Injector NozzleSDR CA080124009Fuel Nozzle · cracked(CAN) FUEL NOZZLE FOUND CRACKED ON SECONDARY MANIFOLD DURING SCHEDULED NOZZLE CHANGE IN THE AREA THAT MFG SAYS TO INSPECT FOR CRACKS.Jan 20, 2008 · Swrngn SA227AC · Engine Fuel DistributionSDR PNSA080103Unknown · malfunctionedON CLIMBOUT REALIZED HAD LITTLE IF NO LT RUDDER. DECLARED EMERGENCY BECAUSE OF FLIGHT CONTROL MALFUNCTION. LANDING WAS UNEVENTFUL.Jan 18, 2008 · N41NE · Swrngn SA227AC · Rudder Control SystemSDR DUFA20080001Overheat Sensor · defectiveWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FJan 3, 2008 · N159MC · Swrngn SA227AC · Overheat DetectionSDR DUFA20080002Overheat Sensor · defectiveWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE RT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER APPROXIMATELY ONE MINUTE THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUJan 3, 2008 · N3116N · Swrngn SA227AC · Overheat DetectionSDR EAC0705Overheat Sensor · defectiveWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FJan 3, 2008 · N159MC · Swrngn SA227AC · Overheat DetectionSDR DUFA010308001Warning Light · false activationWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FJan 3, 2008 · N159MC · Swrngn SA227AC · Overheat Detection
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