FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N203LG and the event date: up to this one’s cancellation.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CIEA201303260003Access Door · inoperativeON DESCENT FROM FL250, THE CABIN PRESSURE SPIKED TO 12500, THE CABIN LIGHTS ILLUMINATED AND THE NO SMOKING/SEATBELT SIGNS ILLUMINATED. THE POWER LEVERS WERE AT IDLE DUE TO TURBULENCE. THE ALT WARN ANNUNCIATOR DID NOT ILLUMINATE AND THE PAX O2 MASKS DID NOT SDR CIEA201303260002Warning Switch · inaccurateON DESCENT FROM FL250, THE CABIN PRESSURE SPIKED TO 12500, THE CABIN LIGHTS ILLUMINATED AND THE NO SMOKING/SEATBELT SIGNS ILLUMINATED. THE POWER LEVERS WERE AT IDLE DUE TO TURBULENCE. THE ALT WARN ANNUNCIATOR DID NOT ILLUMINATE AND THE PAX O2 MASKS DID NOT DSDR CIEA201303260001Controller · erraticON DESCENT FROM FL250, CABIN PRESSURE SPIKED TO 12500, CABIN LIGHTS ILLUMINATED AND NO SMOKING/SEATBELT SIGNS ILLUMINATED. POWER LEVERS WERE AT IDLE DUE TO TURBULENCE. ALTITUDE WARN ANNUNCIATOR DID NOT ILLUMINATE AND PAX O2 MASKS DID NOT DEPLOY. WHEN POWERSDR CIEA200900008Bracket · crackedDURING THE 10000 CYCLE STRUCTURAL INSP, FOUND THE FWD DOOR SUPPORT CABLE EXTRUSION INSIDE THE DOOR IS CRACKED IN TWO PLACES. GAINED ACCESS TO THE FWD HANDRAIL BRACKET ON THE MAIN CABIN DOOR UNDER THE HANDRAIL SUPPORT BRACKET, REMOVED THE CRACKED BRACKET AND ISDR CIEA200900006Stringer · crackedDURING COMPLIANCE WITH MFG MANDATORY SB 53-2472, REVISION 4, DATED JULY 2003 AND AD 2005-01-18, AMENDMENT 39-13943, EFFECTIVE DATE MARCH 01, 2005 THE LT STRINGER NR 9 AT AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED. REPAIRED THE NR 9 AFT FUSELAGE STRINGER ONSDR CIEA200500013Downlock Switch · failedDURING APPROACH, RT MAIN GEAR DID NOT INDICATE IT WAS DOWN AND LOCKED. DUE TO SERV AT DESTINATION AIRPORT, A/C RETURNED TO ORIG AIRPORT. PILOT CYCLED GEAR SEVERAL TIMES, UNABLE TO GET A DOWN AND LOCK IND ON RT MAIN GEAR. PILOT DID A MANUAL EXTENSION OF GEARSDR CIEA200500008Hinge · crackedAFT LANDING ATTEMPTED TO CLOSE MAIN CABIN ENTRY DOOR & HAD DIFFICULTY. A 5 INCH CRACK NEAR AFT, BOTTOM END OF DOOR, WHERE HINGE IS ATTACHED. DAMAGED - ENTRY DOOR HINGE HALF FOUND 8 INCH CRACK RESULTING IN CRACK GOING THRU 8 RIVETS AFT OF DOOR FWD. DOOR CHANSDR CIEA200500007Oxygen Mask · mismanufacturedDURING THE CLIMB THE CABIN LOST PRESSURIZATION. (NOTE: SEE SEPARATE SDR ON THE PRESSURIZATION ISSUE). AS A RESULT OF THE PRESSURIZATION LOSS THE OXYGEN MASKS DROPPED. ONE OF THE PASSENGERS HAD AN ALLERGIC REACTION SIMILAR TO A LATEX ALLERGIC REACTION. IF THSDR CIEA200500006Door Seal · inoperativeDURING CLIMB, PAX HEARD WIND NOISE FROM AFT CABIN. BROUGHT TO ATTENTION OF PILOT, NOTICED CABIN PRESSURIZATION WAS DROPPING, RESULTING IN CABIN ALTITUDE CLIMBING. PILOT ATTEMPTED TO ADJUST PRESSURIZATION CONTROLLER, CABIN LOST PRESSURIZATION. OXYGEN MASKS DSDR CIEA200500005Strut · corrodedDURING SCHEDULED LG INSP, NLG UPPER STRUT HSG WAS FOUND TO BE CORRODED. CORROSION WAS IN 2 AREAS OF STRUT, NEAR TOP CROSS BRACE. CORROSION IN EXCESS OF 70 PERCENT AROUND STRUT. IT WAS IN SHAPE OF VALLEY, MORE THAN 50 PERCENT OF CORROSION WAS MORE THAN 50 PESDR 0026Windshield · crackedDURING CRUISE THE COPILOTS WINDSHIELD INNER PANE SHATTERED. NO DEBRIS FELL INTO THE CABIN OTHER THAN DUST. THE OUTER PANE STAYED IN TACT. THE PILOT DESENDED TO A LOWER ALTITUDE AS RECOMMANDED BY THE AIRCRAFT FLIGHT MANUAL. THE AIRCRAFT LANDED WITHOUT INCIDSDR 0021Sprocket · defectiveDURING COMPLIANCE, THE AILERON SPROCKET WAS FOUND TO HAVE A POSSIBLE DEFECT. DOING A VISUAL INSPECTION BETWEEN THE TWO GEARS OF THE AILERON SPROCKET, ON THE LARGE GEAR NEAR THE SHAFT AREA, IT APPEARS THE WELDING MAY NOT HAVE BEEN COMPLETED IN A SMALL AREA, AP