Fairchild SA227-AC

Service difficulty reports · 2,182

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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 = '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 HKGA20160118001Rib · crackedWHILE PERFORMING A FUEL LEAK REPAIR, TWO CRACKS WERE NOTICED ON A LT WING RIB, AT WS 131.889. CRACKED RIB REPAIRED IAW LAR 16-BRY-006 REVISION A, BY CUTTING OUT THE DAMAGED SECTION OF RIB 131.889 & SPLICING IN A NEW SECTION.Jan 18, 2016 · N175SW · Swrngn SA227AC · Wing, Rib/BulkheadSDR CA160113012Bolt · sheared(CAN) A METRO III WAS CONDUCTING A TAKE OFF WHEN THE CREW FELT THE AIRCRAFT PULL TO THE RIGHT IMMEDIATELY AFTER APPLICATION OF POWER. THEY REJECTED THE TAKEOFF, AND ATTEMPTED ANOTHER. ON THE SECOND ATTEMPT THE AIRCRAFT ACHIEVED MORE SPEED UNTIL AT APPROX. 40 KJan 4, 2016 · Swrngn SA227AC · Rudder Control SystemSDR CA160113003Scavenge Pump · failed(CAN) DURING FLIGHT THE PILOT NOTED THAT THE LT OIL PRESSURE INDICATION WAS FLUCTUATING. WHEN THE AIRCRAFT LANDED WITH NO ISSUES THERE WAS OIL NOTED ON THE GROUND BEHIND THE EXHAUST ON THE GROUND. THE MAINTENANCE DEPARTMENT WAS NOTIFIED OF THE ISSUE AND WHEN TJan 4, 2016 · Swrngn SA227AC · Turbine Engine Oil SystemSDR JIKA2015121401Hydraulic Line · leakingON APPROACH, THE PILOT REPORTED THAT THE LT & RT HYD SYS WARNING ANNUNCIATORS ILLUMINATED. THE PILOT SELECTED THE LG HANDLE TO THE EXTEND POSITION, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE PILOT PERFORMED AN EMER LG EXTENSION. FOLLOWING A SUCCESSFUL Dec 14, 2015 · N152AF · Swrngn SA227AC · Hydraulic System, MainSDR CA151222002Line · chafed(CAN) RIGHT HYDRAULIC FAILURE ALERT FOLLOWING FLAP RETRACTION. UPON SELECTING GEAR DOWN COMPLETE HYDRAULIC SYSTEM FAILURE. TOTAL SYSTEM PRESSURE WAS LOST. THE GEAR TOOK A LONGER THAN NORMAL TO EXTEND AND ALTERNATE GEAR DOWN WAS USED FOR HYDRAULIC LOCKS. NR 2 Dec 12, 2015 · Swrngn SA227AC · Hydraulic System, MainSDR HKGA2016F00044Skin · corrodedAN AREA OF CORROSION ON THE RT LOWER WING SKIN JUST INBD OF THE ENGINE NACELLE WAS IDENTIFIED. IT IS LOCATED ON THE AFT SKIN EDGE WERE IT IS SECURED TO THE SPAR, IN THE DRY AREA, AROUND WS 72.548 AND APPROXIMATELY 1.0" IN DIAMETER.Dec 3, 2015 · N697AX · Swrngn SA227AC · Wing, Plate/SkinSDR JIKA2015111201Duct · contaminatedDURING CLIMB OUT, THE PILOT REPORTED THE SMELL OF SMOKE, THE PILOT WAS UNABLE TO LOCATE SOURCE OF THE SMOKE SMELL & RETURNED & LANDED WITHOUT INCIDENT. INSPECTION REVEALED THREE BOXES IN D BAY WITH MELTED PLASTIC LABELS ON THE BLEED AIR DUCT WAS THE CAUSE OF Nov 12, 2015 · N473AF · Swrngn SA227AC · Pneumatic Distribution SystemSDR CA151021008Impeller · damaged(CAN) ENGINE CAME INTO THE TURBINE SHOP FOR A ROUTINE 7000 HR CAM INSPECTION AND WHEN THE ENGINE WAS BEING DISMANTLED TO START THE INSPECTION OF THE ENGINE THE NR 2 IMPELLER WAS NOTICED TO HAVE A BROKEN BLADE ON IT.Oct 20, 2015 · Swrngn SA227AC · Turbine Engine Compressor SectionSDR JIKA2015100801Unknown · smokeAFTER TAKEOFF, PILOT NOTICED THE RT WING OVERHEAT LIGHT ILLUMINATED & OBSERVED SMOKE IN THE COCKPIT. PILOT DECLARED AN EMER & RETURNED, LANDED WITHOUT INCIDENT. PERFORMED HIGH POWER ENG RUNS WITH THE RT BLEED AIR SYS ON & OFF, BUT COULD NOT DUPLICATE THE DISOct 8, 2015 · N422MA · Swrngn SA227AC · Air Distribution SystemSDR JIKA2015091001Hydraulic Line · chafedON VISUAL APPROACH, PILOT SELECTED LG TO THE EXTENDED POSITION. THE LG POSITION INDICATORS LIGHTS FOR THE MLG REMAINED RED & THE LIGHT FOR NLG DID NOT ILLUMINATE. THE PILOT CYCLED THE LG & RECEIVED TWO GREEN INDICATOR LIGHTS FOR THE MLG, BUT NO LIGHT FOR THESep 10, 2015 · N424MA · Swrngn SA227AC · Hydraulic System, MainSDR CA150820011Frame · cracked(CAN) DURING SCHEDULED MAINTENANCE, THE CABIN FUSELAGE LT AND RT FLOORBOARDS WERE REMOVED AND CRACKS WERE FOUND AT VARIOUS LOCATIONS IN THE FUSELAGE BELT FRAME ASSEMBLIES IN THE AREA OF THE BEND RELIEF CUT-OUT AT THE FLOORBOARD LEVEL (BOTH LT AND RT SIDES). THAug 20, 2015 · Swrngn SA227AC · Fuselage Main, FrameSDR JIKA2015081001Wire Harness · damagedEN-ROUTE THE PILOT NOTICED THE RT ENG EGT SPIKED 100 DEGREES CELSIUS, THE RT ENG FUEL BYPASS LIGHT ALSO ILLUMINATED. THE PILOT FOLLOWED THE EMER CHECKLIST & PERFORMED A PRECAUTIONARY RT ENG SHUTDOWN. DECLARED AN EMER & DIVERTED. THE PILOT LANDED WITHOUT FURAug 10, 2015 · N424MA · Swrngn SA227AC · Turbine Engine System WiringSDR JIKA2015072401Actuator · failedON APPROACH, PILOT SELECTED LG HANDLE TO THE RETRACT POSITION, LG WOULD NOT RETRACT. PILOT NOTICED LOW HYD PRESSURE & FOLLOWED ESTABLISHED EMER PROCEDURES IN THE PILOT POH. MANUALLY EXTENDED LG, RECEIVED THREE GREEN DOWN & LOCKED INDICATION LIGHTS & LANDED WJul 24, 2015 · N698AF · Swrngn SA227AC · Landing Gear ActuatorSDR JIKA2015062401Latch · unsecureDURING TAKEOFF, THE RT ENG COWLING OPENED & THE TOP COWLING DEPARTED THE ACFT. THE PILOT WAS NOTIFIED & RETURNED. THE PILOT LANDED WITHOUT INCIDENT. MX INVESTIGATION IS STILL ON GOING, PRELIMINARY FINDINGS REVEALED INBD LATCHES WERE NOT SECURED. OPENJun 24, 2015 · N362AE · Swrngn SA227AC · Engine Cowling SystemSDR KY7A20150622001Uplock Switch · defectiveFLIGHT CREW REPORTED LG WOULD NOT RETRACT AFTER TAKEOFF. FOUND DEFECTIVE UPLOCK SWITCH & REPLACED.Jun 22, 2015 · N31171 · Swrngn SA227AC · Landing Gear Position and WarningSDR JIKA2015042201Accumulator · crackedAFTER TAKEOFF, PILOT NOTICED BOTH LT & RT HYD FAIL ANNUNCIATORS ILLUMINATED, VERIFIED FAILURE HYD PRESS INDICATOR WAS READING ZERO PRESSURE. PILOT INFORMED ATC OF THE SITUATION & PERFORMED A MANUAL EXTENSION OF THE LG. PILOT RECEIVED THREE GREEN DOWN & LOCK Apr 22, 2015 · N529AF · Swrngn SA227AC · Hydraulic Power Accumulator, MainSDR KY7A20150421001Trunnion · brokenPILOT FOUND RT MLG UPLOCK ROLLER BROKEN. RT MLG TRUNNION ASSEMBLY REPLACED.Apr 21, 2015 · N788KL · Swrngn SA227AC · Main Landing Gear Attach SectionSDR KY7A20150416001Disk · failedE2 SUFFERED UNCONTAINED ENG FAILURE ON CLIMB OUT. 2ND STAGE TURBINE DISK FAILED & WAS THROWN FROM THE ENG THROUGH THE LT & RT SIDES OF THE ENG. APPROX 1/4 OF THE 2ND STAGE TURBINE DISK PENETRATED THE CABIN & WAS FOUND ON THE CARGO FLOOR.Apr 16, 2015 · N2691W · Swrngn SA227AC · Turbine SectionSDR JIKA2015030801Hydraulic Line · chafedDURING APPROACH, THE PILOT REPORTED THAT THE LT & RT HYD PRESS ANNUNCIATORS ILLUMINATED & THE HYD PRESS GAUGE INDICATED 0 PSI. THE PILOT NOTIFIED ATC OF THE CONDITION & DECLARED AN EMER. PERFORMED A MANUAL EXTENSION OF THE LG IAW THE EMER PROCEDURES IN QRH, Mar 8, 2015 · N488AF · Swrngn SA227AC · Hydraulic System, MainSDR HKGA2015F00036Truss · corrodedRIGHT ENGINE TRUSS OTBD TOP TUBE HAS CORROSION PITTING PAST LIMITS.Feb 12, 2015 · N26959 · Swrngn SA227AC · Engine Mount SectionSDR 2015FA0000031Oil System · lowAPPROXIMATLY 100 MILES FROM THE DESTINATION OF THE FLIGHT, THE PILOT NOTICED A OIL PRESSURE LOW CAUTION LIGHT FOR THE LT ENGINE. THE PILOT SECURED THE ENGINE AND FEATHERED THE PROPELLER, ACFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE FOUND THE ENGIJan 27, 2015 · N320MC · Swrngn SA227AC · Turbine Engine Oil SystemSDR CA150126003Bracket · cracked(CAN) DURING AN ENGINE REPLACEMENT INSTALL PROCESS, IT WAS FOUND THAT THE LH POWER LEVER WAS HITTING THE UPPER QUADRANT AND FOUND THAT THE ENGINE CONTROL CABLE SUPPORT BRACKET TO BE BROKEN OFF AND FREELY MOVING. THE BRACKET HAS REMOVED AND REPLACED. (TC# 20150Jan 24, 2015 · Swrngn SA227AC · Engine ControlsSDR MCCA201501050019Antenna · damagedENROUTE, EXPERIENCED A LIGHTING STRIKE APPROXIMATELY 70-80 MILES FROM DESTINATION. THIS STRIKE KNOCKED OUT BOTH COMMS. PLACED CORRECT CODE ON THE TRANSPONDER AND CONTINUED ON AND MADE AN UNEVENTFUL LANDING. MAINTENANCE DISCOVERED THAT THE NR 1 COMM ONE COAX,Jan 5, 2015 · N211RH · Swrngn SA227AC · VHF Communications SystemSDR JIKA2014122201Uplock Roller · frozenJUST AFTER TAKEOFF, PILOT SELECTED LG IN RETRACT POSITION, GEAR INTRANSIENT LIGHT REMAINED ILLUMINATED. THE PILOT TRIED TO CYCLE GEAR TWO ADDITIONAL TIMES WITH THE SAME RESULT. THE PILOT NOTIFIED TOWER OF THE SITUATION & RETURNED. THE TOWER DECLARED AN EMERDec 22, 2014 · N473AF · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR CA141126002Housing · damaged(CAN) ENGINE P-44016 WAS BROUGHT INTO THE TURBINE SHOP FOR ROUTINE OVERHAUL AND WHEN THE ENGINE WAS TAKEN APART THE COMPRESSOR HOUSING WAS DAMAGED IN THE AREA WERE THE NR 2 IMPELLER SITS AND RIDES IN. THIS AREA HAS A SPRAY METAL REPAIR THAT IS DONE TO BUILD UPNov 26, 2014 · Swrngn SA227AC · Turbine Engine Compressor SectionSDR HKGA20141113001Angle · crackedA CRACK WAS FOUND IN THE RT BATTERY BOX LOWER ANGLE DURING THE ABCD INSPECTION. FABRICATED A DOUBLER, FILLERS & ANGLE FOR REPAIR. ALL WORK WAS PERFORMED IAW SA227 SRM 57-90-10.Oct 31, 2014 · N175SW · Swrngn SA227AC · Battery Box StructureSDR JIKA2014102501Hydraulic Line · crackedON APPROACH, PILOT SELECTED FLAP DOWN, PILOT NOTICED HYD FAILED LIGHT ILLUMINATED. THE HYD PRESS GAUGE INDICATED 0. PILOT DECIDED THAT THE WINDS WERE TOO HIGH TO PERFORM A LANDING WITHOUT FLAPS AT THAT POINT, PILOT DIVERTED BACK. DURING APPROACH PILOT PERFOOct 25, 2014 · N152AF · Swrngn SA227AC · Hydraulic System, MainSDR CA141020005Spar · cracked(CAN) DURING THE COMPLETION OF A SCHEDULED MAINTENANCE INSPECTION CRACKS WERE DISCOVERED ON BOTH THE LT & RT AILERONS. EACH AILERON SPAR HAD CRACKS WHERE THE HINGE BRACKET ATTACHES TO THE AILERON. THE AILERON SPARS WERE REPLACED TO RECTIFY THIS DISCREPANCY.Oct 14, 2014 · Swrngn SA227AC · AileronsSDR CA141104006Indicator · reads high(CAN) COPILOTS ASI READS 85 KTS HIGHER THAN PILOTS ASI. INDICATOR REPLACED AND GROUND CHECKER SERVICEABLE. ACFT RETURN TO SERVICE.Oct 7, 2014 · Swrngn SA227AC · Airspeed/Mach IndicatorSDR JIKA2014093001Duct · looseDURING CRUISE FLIGHT AT 12,000 PILOT NOTICED HAZE & SMOKE WAS PRESENT IN COCKPIT ALONG WITH SMOKE ODOR. PILOT DONNED OXYGEN MASK & SMOKE GOGGLES IAW GOM PROCEDURES. PILOT FOLLOWING PILOT QRH TURNED OFF BLEED AIR, DUMPED CABIN PRESSURIZATION & TURNED FAN ON OSep 30, 2014 · N698AF · Swrngn SA227AC · Pneumatic Distribution SystemSDR CA140926005Uplock Switch · false indication(CAN) ON LOWERING THE LANDING GEAR THE CREW HAD NO NOSE DOWN GREEN INDICATION, GEAR RECYCLED WITH SAME RESULT AND EMERGENCY GEAR LOWERING PROCEDURE CARRIED OUT WITH SAME RESULT. WARNING HORN WAS OUT AND VISUAL OF GEAR ON FLYBY INDICATED IT WAS DOWN. EMERGENCY Sep 23, 2014 · Swrngn SA227AC · Landing Gear Position and WarningSDR JIKA2014081901Connector · dirtyDURING CLIMB OUT THE STALL AVOIDANCE SYSTEM, SAS, FAULT ANNUNCIATOR ILLUMINATED. THE PILOT NOTIFIED TOWER OF CONDITION & RECEIVED VECTORS TO RETURN. PILOT LANDED WITHOUT FURTHER INCIDENT. DISCONNECTED THE CONNECTOR AT THE SAS SYS SPEED SWITCH. CLEANED & REAug 19, 2014 · N578AF · Swrngn SA227AC · Navigation System WiringSDR JIKA2014081101Strut · malfunctionedAFTER ROTATION PILOT SELECTED LG HANDLE IN THE RETRACT POSITION. LG REMAINED EXTENDED & LOCKED WITH THREE GREEN INDICATOR LIGHTS ILLUMINATED. PILOT SWITCHED THE GEAR CONTROL & INDICATOR TO RT BUS & VERIFIED THE EMER GEAR RELEASE SYS WAS PROPERLY STOWED, GEARAug 11, 2014 · N422MA · Swrngn SA227AC · Nose/Tail Landing Gear Strut/AxleSDR 2014FA0000571Retainer · chafedPERIMETER EDGE OF CABIN WINDOWS HAVE CHAFED INTO CABIN WINDOW RETAINERS ON RT CABIN WINDOWS. THIS DISCREPANCY OCCURRED UNDER NORMAL WEAR AND UTILIZATION, MATERIAL IS 0.040 THICK. DEEPEST CHAFE DAMAGE MEASURES 0.020 THICK.Jul 23, 2014 · Swrngn SA227AC · Fuselage Main, StructureSDR 2014FA0000448Sprocket · brokenCAPTAIN`S CONTROL COLUMN SPROCKET WAS FOUND TO HAVE A BROKEN TOOTH. APPEARS TO HAVE BEEN CRACKED/BROKEN FOR SOME TIME.Jul 1, 2014 · Swrngn SA227AC · Control Column SectionSDR JIKA2014070101Hydraulic Line · puncturedON APPROACH PILOT NOTICED HYD PRESS BOUNCING BETWEEN 1800 & 1000 PSI. SHORTLY THEREAFTER RT HYD PRESS ANNUNCIATOR ILLUMINATED. PILOT DECIDED TO PERFORM A MANUAL EXTENSION OF LG, PILOT RECEIVED THREE GREEN DOWN & LOCKED INDICATOR LIGHTS. LANDED WITHOUT FURTJul 1, 2014 · N426MA · Swrngn SA227AC · Hydraulic System, MainSDR JIKA2014062201Hydraulic Line · crackedON APPROACH THE PILOT NOTICED A HIGH PITCH WHINE COMING FROM WHERE HE BELIEVED TO BE THE RT ENG. AFTER THREE SECONDS THE PILOT NOTICED BOTH HYD LOW PRESS ANNUNCIATORS ILLUMINATED. CHECKED HYD QTY GAUGE & READING WAS 0. PILOT STARTED EMER PROCEDURES OUTLINEDJun 22, 2014 · N424MA · Swrngn SA227AC · Hydraulic System, MainSDR CA140602021Engine · overheated(CAN) THE PILOT SHUTDOWN NR 1 ENGINE FOR HIGH OIL TEMPERATURE AND THEN THE NR 2 ENGINE RUN IN OEI. THE ON GROUND PRELIMINARY FINDINGS FROM THE TROUBLESHOOTING REVEALED THAT NR 1 ENGINE OIL TEMPERATURE PEAKED AT 132.375 OC AND WAS ABOVE 130OC FOR 2 MINUTES 41 May 23, 2014 · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR DUFA20140502001Hydraulic Line · chafedAPPROX 200 FT AGL, THE PILOT BEGAN TO SEE & SMELL SMOKE IN THE COCKPIT. CONTACTED ATC & DECLARED AN EMER, MADE A SAFE LANDING. WHILE EXITING THE ACFT, NOTICED THE SMOKE WAS MUCH THICKER IN THE MID CABIN AREA. AN INSPECTION OF THE ENGS REVEALED NO EVIDENCE OFApr 30, 2014 · N572GW · Swrngn SA227AC · Hydraulic System, MainSDR HKGA20140423001Aileron · crackedA CRACK WAS FOUND ON THE RT AILERON OTBD HINGE LOCATION WHEN PERFORMING INSPECTION IAW SA227 SERVICE LETTER 227-SL-060. R & R RT AILERON WITH A SERVICEABLE AILERON.Apr 19, 2014 · N680AX · Swrngn SA227AC · AileronsSDR JIKA2014040101Switch · failedAPPROXIMATELY 10 MINUTES AFTER DEPARTURE, DURING CLIMB, LT WING OVERHEAT ANNUNCIATOR ILLUMINATED. PILOT & CO-PILOT FOLLOWED EMERGENCY PROCEDURES & RETURNED TO DEPARTURE. AFTER ONE MINUTE WHILE ON APPROACH, THE LIGHT EXTINGUISHED. REPLACED THE 350 & 450 DEGMar 28, 2014 · N698AF · Swrngn SA227AC · Airfoil Anti/De-ice SystemSDR OWFR2014040400231Spar · crackedCRACK IN AILERON SPAR ADJACENT TO OTBD HINGE FITTING. THIS DISCREPANCY OCCURRED UNDER NORMAL WEAR AND UTILIZATION.Mar 25, 2014 · N680AX · Swrngn SA227AC · AileronsSDR CA140226005Smoke Detector · failed(CAN) LAV FIRE LIGHT ILLUMINATED ON TAXI PRIOR TO TAKEOFF. UPON ENGINE SHUTDOWN LIGHT EXTINGUISHED AND ILLUMINATED UPON RESTART OF ENGINES. REMOVED LAV DETECTOR CAUSING FALSE FIRE INDICATION AS IT WAS NOT REQUIRED FOR CURRENT ACFT CONFIGURATION.Feb 22, 2014 · Swrngn SA227AC · Smoke DetectionSDR JIKA2014022101Regulator · defectiveABOUT 10 MINUTES AFTER DEPARTURE, THE PILOT NOTICED A STEADY LT WING OVERHEAT ANNUNCIATOR. THE PILOT IMMEDIATELY RAN THE EMERGENCY CHECKLIST. PILOT DECLARED AN EMERGENCY & LANDED WITH NO FURTHER PROBLEM. MX TROUBLESHOOTING REVEALED LT BLEED AIR REGULATOR WAFeb 21, 2014 · N698AF · Swrngn SA227AC · Pneumatic Distribution SystemSDR CA140226006Fire Detector · intermittent(CAN) ON APPROACH, FLIGHT CREW TURNED ON THE LT INTAKE HEAT, WITHIN SECONDS THE LT FIRE LIGHT ILLUMINATED. FLIGHT CREW SELECTED ANTIICE OFF AND THE FIRE LIGHT WENT OUT A FEW SECONDS LATER. FLIGHT CREW LT ANTI-ICE OFF FOR THE REMAINER OF THE FLIGHT WITH NO FUFeb 14, 2014 · Swrngn SA227AC · Fire DetectionSDR CA140210006Unknown · smoke(CAN) FLIGHT CREW SAW AND SMELLED SMOKE IN THE CABIN 5 MINUTES AFTER TAKEOFF FROM AIRPORT. ACFT RETURNED TO AIRPORT. MAINTENANCE CREW RAN ACFT WITH NO FAULTS FOUND. DUST WAS REMOVED FROM CABIN TEMP CONTROLLER. TEST FLIGHT COMPLETED WITH NO FAULTS FOUNDS. MFeb 10, 2014 · Swrngn SA227AC · Air Distribution SystemSDR CA140205001Sensor · inaccurate(CAN) RT ANNUCIATOR ILLUMINATED AND RT EGT FLUCTUATING. SYSTEM GROUND FAULTED BY MAINTENANCE WITH SRL ON AND OFF. WIRES REPAIRED AT RT SRL COMPUTER FOR SRL ON AND OFF FOR EGT FLUCTUATION. GROUND RUNS CHECKED CHECKS SERVICEABLE FOR RT EGT T2 SENSOR. REPLACFeb 2, 2014 · Swrngn SA227AC · Engine Temperature Indicating SystemSDR MCCA2014011300017Engine · flamed outDURING APPROACH, TURNED ON THE ENGINE INTAKE HEAT. RT ENGINE THEN INGESTED ICE AND FLAMED OUT. PILOT WENT AROUND, RESTARTED ENGINE AND LANDED WITHOUT FURTHER INCIDENT.Jan 10, 2014 · N2699Y · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR HKGA20131224001Hydraulic Line · rupturedLEFT & RT HYD PRESS WARNING LIGHTS ILLUMINATED IN FLIGHT. LOSS OF HYD PRESS WAS CONFIRMED BY A ZERO PSI INDICATION ON THE HYD PRESS INDICATOR. THE CAPTAIN DECLARED AN EMERGENCY, PERFORMED AN EMERGENCY LANDING GEAR EXTENSION & MADE A SAFE LANDING. UPON INSPECDec 23, 2013 · N227LJ · Swrngn SA227AC · Hydraulic System, MainSDR JIKA2013120901Hydraulic Line · crackedDURING CRUISE FLIGHT FROM SLC, BOTH LOW HYD PRESS LIGHTS CAME ON. PILOT DECLARED AN EMERGENCY & LANDED AT JAC WITHOUT FURTHER INCIDENT. MX INSPECTION REVEALED CRACK IN BEND RADIUS OF HYD LINE FOR NOSE GEAR EXTENSION ACTUATOR. HYD LINE WAS R & R WITH NEW FABDec 9, 2013 · N672AV · Swrngn SA227AC · Hydraulic System, Main
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