FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N605GC and the event date: up to this one’s cancellation.
Incident 20041226032429IOther Ground Ops · Miami, FL(-23) "Industrial incident-no intent to fly" aircraft was being serviced with fuel. The fuel truck was positioned under the wing. During the servicing the aircraft settled downward onto the truck with the right hand outboard flap track fairing due to weight…Incident 20041011027469IOther Ground Ops · Miami, FL(-23) During walk around found a hole in the side of the right forward fuselage near cargo door. Found paint from aircraft on loader that was loading the aircraft. No witness or person who caused the accident. Hole was through skin only, the size was about 1…
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR G6OA071Bolt · wornAIRCRAFT PERFORMED AN AIR RETURN SAFELY DUE TO UNABLE TO PRESSURIZE AFTER TAKE OFF. DURING TROUBLESHOOTINGFOUND GROUND SENSE ROD LOOSE. R/R UPPER BOLT PER MM 32-21-01SDR G6OA059Bellcrank · wornELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BELLCRANK ASSEMBLIES ON LEFT INBOARD ELEVATOR ACTUATOR. REMOVED AND REPLACED BELLCRANK ASSEMBLY IAW MM 20-50-02. OPS CHECKS GOOD IAW MM 27-30-00. (M)SDR G6OA060Bracket · wornFOUND ELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BRACKET ASSEMBLIES ON LEFT INBOARD ELEVATOR. REMOVED AND REPLACED BRACKET ASSY IAW MM 20-50-02. OPS CHECKS GOOD IAW MM 27-30-00. (M)SDR G60A040Seal · leakingCABIN ALTITUDE COULD NOT BE CONTROLLED IN AUTO, SEMI-AUTO, STANDBY, OR MANUAL POSITION. PERFORMED RAPID DEPRESSURIZATION/EMERGENCY DESCENT TO 11,000 FT, DUMPED FUEL AND RETURNED TO SBKP. DURING TROUBLESHOOTING, FOUND MAIN CARGO DOOR SEAL AFT AND FORWARD OF TSDR GTOAA036Battery · dischargedEMERGENCY LIGHT TEST DOES NOT COME ON WITH TEST. REMOVED AND REPLACED EMERGENCY BATTERY IAW MM 24-24-00. OPS CHECKED GOOD. (M)SDR G6OA043Bolt · looseNR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON, HAS SIX LOOSE PYLON BOX BOLTS ON LOWER FORWARD SIDE, AND THREE HI-LOCKS ON LOWER FORWARD SHOWS EVIDENCE OF SPINNING. INSPECTED FWD MOUNT TRUSS FITTINGS AS PER DRAWING AVB 7000-503 AND 504 PER BOEING JAC GC 116SDR G60A044Bolt · looseNR 3 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON LOWER FORWARD SIDE ATTACH BOLTS LOOSE. INSPECTED FORWARD MOUNT TRUSS FITTINGS AS PER DRAWING AVB 7011 '2' AND PER BOEING JAC GC 116-02 AND S/B A54-99. REFER TO SINGLE ITEM SQUAWK NUMBERS 237887 AND 228931. COSDR G6OA024Connector · looseTHE FLIGHT CREW REPORTED THE NR 2 ENGINE PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURES PER AOM VOL 1. GROUND MAINTENANCE TROUBLESHOT THE SYSTEM. PERFORMED MANIFOLD DETECTION TEST PER MM 36-23-00. TESTED WITH NO FAULTS FOUNSDR G6OA006Computer · malfunctionedGVA - AFTER TAKEOFF, CREW REPORTED STALL SPEED WARNING ACCOMPANIED BY AUTO SLAT EXTENSION. CREW ACCOMPLISHED IRREGULAR PROCEDURES AND PULLED AUTO SLAT EXTEND CIRCUIT BREAKERS. AIRCRAFT DIVERTED TO FCO AND LANDED WITHOUT FURTHER INCIDENTS. NO EMERGENCY WAS SDR G6OA005Garloc Seal · damagedGVA - APPROXIMATELY 90 MINUTES AFTER TAKEOFF, CREW REPORTED LOSS OF NR 1 ENGINE OIL QUANTITY AND OIL PRESSURE FLUCTUATION OF 30-40 PSIG. ENGINE NR 1 WAS SHUT DOWN AND AIRCRAFT DIVERTED TO LYS AND LANDED WITHOUT FURTHER INCIDENTS. NO EMERGENCY WAS DECLARED. SDR G60A004Tr Mount · brokeNR 3 ENGINE THRUST REVERSER RHS CENTER BALL ACTUATOR ASSEMBLY FAILED TO RETRACT AFTER LANDING. THE BALL SCREW ACTUATOR MOUNT BRACKET BROKE OFF AND DAMAGED THE LEADING EDGE OF TRANSLATING COWL. (X)