FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N13234 and the event date: up to this one’s cancellation.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CALA9700538Return Hyd Line · leakingTHE AIRCRAFT LOST A-HYDRAULIC SYSTEM QUANTITY ON APPROACH. CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT WING SPOILER HYDRAULIC RETURN LINE ABOVE LEFT GEAR LEAKING. THE HYDRAULIC LINE WAS REMOVED ASDR CALA9600940Hyd Line · leakingTHE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM RDU. ALL GEAR WERE LOWERED AND VERIFIED DOWN. THE AIRCRAFT WAS RETURNED TO RDU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR LOCK ACTUATOR HYDRAULIC FLEX LINE LEAKING. THE LINE SDR CAL960282Hyd Pump · leakingFLT NR 1160 - EWR - THE AIRCRAFT LOST ALL PRESSURE AND FLUID FROM THE 'A' HYDRAULIC SYSTEM DURING FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVE HYDRAULIC PUMP AT FAULT. THE NR 2 HYDRAULIC PUMP WAS REMOVSDR CAL950788Harness · chafedFLT NR 1588 - EWR - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON APPROACH TO EWR. THE NR 2 ENGINE WAS SHUT DOWN AND BOTH LEFT AND RIGHT FIRE BOTTLES WERE DISCHARGED. THE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY ANOTHER EIGHT MINUTES AND THEN EXTINGUISHESDR CAL950802Web · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN NOSE WHEELWELL UPPER WEB AT THE INBOARD AFT CORNER ON LT SIDE AND CORROSION FOUND AT THE INBOARD FORWARD CORNER ON LT SIDE. THE WEB AREA WAS REPAIRED IAW EA 5310-02452 AND BAC DRAWING 65C35749. (X)SDR CAL950801Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN FUSELAGE FRAME AT RIGHT BS 664, WL 191.5, STRINGER 18A SHEAR BEAM. THE AREA WAS REPAIRED IAW ECRA 5310-03156 AND IAW BAC SERVICE BULLETIN 737-53-1082, REV 3, FIG 1. (M)SDR CAL950798Blkhd Chord · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD LEFT OUTBOARD CHORD AT STRINGER 18A. THE CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638, OPERATION NR 2. (M)SDR CAL950797Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON FORWARD LOWER AND UPPER AFT END OF STRINGER 26R AT STATION 1006. THE STRINGER WAS REMOVED AND A NEW STRINGER AND SPLICE WERE INSTALLED IAW SRM 53-10-3, FIGURE 1. (M)SDR CAL950796Beam · corrodedGSO - INSPECTION FOUND THE RIGHT NOSE WHEEL WELL STATION 251.6 VERTICAL SUPPORT BEAM AND ATTACHING WEB CORRODED. THE RIGHT VERTICAL BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. THE CORRODED ANGLES AND FRAME WEB WERE REPAIRED IAW SRM 51-40-1 AND 51-40-2. (SDR CAL950795Blkhd Chord · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD RIGHT OUTBOARD CHORD AT STRINGER 18A. THE RIGHT OUTBOARD CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638. (M)SDR CAL950553Battery · failedGSO - FLT 1551 - A FAINT ELECTRICAL SMELL WAS OBSERVED IN THE COCKPIT AND CABIN DURING TAXI IN AT GSO. THE AIR STARTED TO CLEAR AFTER THE PACKS AND BLEEDS WERE TURNED OFF. MAINTENANCE FOUND ACFT BATTERY BURNED. THE BATTERY WAS REMOVED AND REPLACED. THE BATSDR CAL950548Battery · failedGSO - FLT 1551 - A FAINT ELECTRICAL SMELL WAS OBSERVED IN THE COCKPIT AND CABIN DURING TAXI IN AT GSO. THE AIR STARTED TO CLEAR AFTER THE PACKS AND BLEEDS WERE TURNED OFF. MAINTNANCE FOUND THE ACFT BATTERY BURNED. THE BATTERY WAS REMOVED AND REPLACED. THE SDR CAL950431Line · rupturedMCO - FLT 1594 - THE A-SYSTEM HYDRAULIC FLUID QUANTITY WAS LOST IN-FLIGHT. THE LANDING GEAR AND FLAPS WERE EXTENDED MANUALLY AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED HYDRAULIC LINE AT THE LT REAR SPA