FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N59207 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 CALA9700537Accessory Unit · inoperativeTHE LEFT GEAR GREEN DOWN AND LOCKED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. ALL OTHER INDICATIONS WERE NORMAL. THE GEAR WAS VISUALLY INSPECTED WHILE IT WAS EXTENDED AND RETRACTED, BUT THE GREEN LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO EWR WSDR CALA9700504Actuator · leakingTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST AFTER TAKEOFF. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 SPOILER ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-61-11, PAGE 401. LEAK AND OPERATSDR CALA9700067Gcu · inoperativeSMOKE AND FUMES MOMENTARILY APPEARED IN THE COCKPIT DURING A STANDBY POWER CHECK WHILE AIRCRAFT WAS AT GATE. MAINTENANCE FOUND THE APU GENERATOR CONTROL UNIT AT FAULT. THE APU GCU WAS REMOVED AND REPLACED, GROUND CHECK WAS GOOD.SDR CALA9601713Hyd Line · leakingTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC PRESSURE LINE ON TOP OF NR 2 ENGINE LEAKING. THE LINE WAS REPLACED USING A FLEX LINE ANSDR CALA9601445Line · leakingLOSS OF A-SYSTEM HYD ON SHORT FINAL. A-SYSTEM PUMPS TURNED OFF. FOUND BLOWN PRESSURE LINE AT FORWARD WHEEL WELL WALL. REMOVED AND REPLACED LINE AND NR 1 ENGINE HYD PUMP PER MM 29-11-32 AND REPLACED SYSTEM CASE DRAIN FILTERS PER MM 29-11-41.SDR CALA9601305Hyd Line · rupturedTHE AIRCRAFT LOST A-SYSTEM HYDRAULICS AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC PRESSURE LINE FROM NR 1 ENGINE PYLON TO WING ROOT RUPTURED. THE HYDRAULIC PRESSURE LINE WAS REPLSDR CALA9601251Hyd Line · chafedTHE AIRCRAFT WAS RETURNED TO EWR AFTER LOSS OF THE A-HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM RETURN LINE IN LT MLG WHEEL WELL CHAFED AGAINST ANOTHER HYDRAULIC LINE. BOTH HYDRAULIC LINES WERE REMOVED AND REPLACED ANSDR CALA9600859Gearbox · leakingTHE NR 1 ENGINE OIL PRESSURE ROSE TO OVER 60 PSI AFTER TAKEOFF. WHEN THE NR 1 THROTTLE WAS RETARDED, THE OIL TEMPERATURE ROSE BEYOND THE RED LINE. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ESDR CALA9600858Fuel Heat Valve · inoperativeTHE NR 1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW BAND AFTER DEPARTURE FROM EWR. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FUEL HEAT VALVE NOT SEATING PROPERLY. THE FUEL HEAT VALSDR CAL951036Eel · inoperativeGSO - INSPECTION FOUND THE RT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE RT AFT EXTERIOR LIGHT ASSY WAS REMOVED AND REPLACED IAW MM 33-51-01. (X)SDR CAL951035Battery Pack · dischargedGSO - INSPECTION FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACKS FOR THE LT AND RT OVERWING EMERGENCY LIGHTS WERE REMOVED AND REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X)SDR CAL950630Circuit Breaker · poppedEWR - FLT 1482 - WHEN LANDING GEAR WAS EXTENDED ON FINAL APPROACH TO EWR, THE GEAR 'DOWN AND LOCKED' LIGHTS DID NOT ILLUMINATE. A 'GO AROUND' WAS INITIATED AND THE CREW OBSERVED THE CIRCUIT BREAKER ON P6-3 PANEL LABELED 'SECT 5' POPPED. THE CIRCUIT BREAKER WSDR CAL950152Hyd Line · chafedFLT NR 1484 - EWR - THE 'A' HYDRAULIC SYSTEM WAS LOST APPROXIMATELY 20 MINUTES BEFORE ARRIVING IN EWR. THE HYDRAULIC QUANTITY INDICATED ZERO. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM AILERON PCU HYDRAULIC PRESSURE LINE C