FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N352SK and the event date: up to this one’s cancellation.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR S2YA06007Bracket · brokenIMMEDIATELY AFTER TAKEOFF OF FLIGHT 2343, THE RT GROUND SPOILER DEPLOYED. THE CREW DECLARED AN EMERGENCY AND IMMEDIATELY RETURNED TO DEPARTURE. OUTSTATION MX FOUND THE RT GROUND SPOILER’S ACTUATING BRACKET BROKEN.SDR S2YA05031Connector · failedDURING APPROACH, CREW REPORTED A CAS MESSAGE (NWS POWER UP FAIL) AND EXECUTED A MISSED APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT WITH FREE CASTERING NOSE WHEEL. OUTSTATION MECHANIC VISUALLY INSPECTED THE NOSE GEAR, RERACKED THE NWS ECUSDR S2YA05011Rod · shearedFLT 2343 - MKE-CMH - AFTER TAKEOFF, THE CREW NOTICED A NOSE VIBRATION BELIEVING THAT THE GEAR DOOR MIGHT NOT BE FULLY CLOSE. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE A/C AND REPLACED THE LEFT FORWARD NOSE LANDING GEAR DOOR SHEAR ROD. SDR S2YA04042Controller · malfunctionedDURING CLIMB OUT, THE CREW WAS UNABLE TO PRESSURIZE THE AC AND RECEIVED INTERMITTENT DOOR OPEN INDICATION. THE CREW PERFORMED AND AIR-TURN-BACK. MX INSPECTED THE AC INCLUDING PRESSURIZATION AND DOOR INDICATION. THE AC WAS PRESSURIZED TO MAXIMUM PRESSURE DIFSDR S2YA04038Wheel · separatedAFTER FLIGHT, THE CREW DISCOVERED A DAMAGE TO THE NR 3 TIRE AND THE RT HYDRAULIC DOOR. MX INSPECTED THE ACAND FOUND NO OTHER DAMAGE. INSPECTION OF THE TIRE REVILED EVEN THOUGH IT WAS STILL INFLATED, PART OF THE RECAPPED TREAD HAD LET GO AND DAMAGED THE DOOR.SDR S2YA04032Valve · brokenDURING FLIGHT, THE CREW REPORTED LOAD VIBRATION THAT SOUNDED LIKE IT WAS OUTSIDE OF THE AC. THE CREW MADE AN AIR-TURN-BACK. THE AC WAS INSPECTED BY MX WHO FOUND THE LT PACK VALVE WAS BROKEN. MX REPLACED THE LT PACK VALVE. THE AC WAS RETURNED TO SERVICE WITSDR S2YA04027Proximity Sensor · inoperativeDURING FLIGHT, THE CREW REPORTED CARGO DOOR OPEN INDICATION. THE CREW MADE AN AIR-TURN-BACK. THE AC WAS INSPECTED BY MECHANIC WHO CHECKED THE PSEU`S MEMORY AND FOUND THE CARGO DOOR OVER-CENTER PROXIMITY SENSOR HAD LOGGED SEVERAL FAULTS. MECHANIC REPLACED THSDR S2YA04020Sensor · inoperativeDURING TAKEOFF, THE CREW NOTED A WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW RETURNED TO THE GATE AND CONSULTED WITH MX. SINCE THE SPARE WINDSHIELD SENSOR WAS ALREADY ON MCO, MX REPLACEDTHE WINDSHIELD AND RETURNED THE AC TO SERVICE. (K)SDR S2YA04013Warning Light · false indicationDURING FLIGHT, WHILE ENCOUNTERING SOME LIGHT TURBULANCE THE CREW NOTED A (L/R ELEVATOR HORN HEAT FAIL). THE CREW PERFORMED AN AIR-TURN-BACK AND MADE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM, REMOVED THE LT AND RT RUDDER HORNS BUT DID NOT FIND ANY DISCRSDR S2YA04012Control Panel · false indicationDURING FLIGHT, THE CREW NOTED A FIRE INDICATION FOR THE RT ENGINE. THE CREW SHUT THE RT ENGINE DOWN IN FLIGHT AND MADE AN SUCCESSFUL SINGLE ENGINE LANDING. MX INSPECTED THE AC AND FOUND NO INIDCATION OF FIRE. MX SWAPPED FIRE EXTINGUISHER/APU PANELS. MX RETSDR S2YA02030Engine · failedSHORTLY AFTER TAKEOFF, THE CREW HEARD A THUD ON THE SIDE OF THE PLANE. THIS WAS FOLLOWED BY A RISE IN ITT AND FUEL FLOW BUT A DROP IN OIL PRESSURE. THE CREW MADE AN AIR TURN BACK. MECHANIC INSPECTED THE RIGHT ENGINE AND FOUND DAMAGE TO THE HP TURBINE. MECH