NTSB investigations · 1
Matched to this aircraft by N602GC and the event date: up to this one’s cancellation.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N602GC 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 G6OA042704Coalescer Bag · contaminatedSMOKE IN COCKPIT FROM PILOT AND COPILOT FOOT WELL.SDR G60A046Valve · failedAT FL33, AC PACK NR 1 FLOW VALVE WAS SURGING WITH PACK SELECT SWITCH IN AUTO. COCKPIT FILLED WITH SMOKE. RAN PROCEDURES FROM FOM VOLUME I, PAGE I-110 AND SECURED THE NR 1 AC PACK. SMOKE STOPPED AS SOON AS PACK WAS TURNED OFF. ENTERED IN MEL LOG AS MEL 21-1SDR G60A038Elevators · damagedTCAS MADE CONTACT WHILE FLT GCO7580 WAS DEPARTING PHNL, AT APPROXIMATELY 3800 FT. FLIGHT CREW INITIATED EVASIVE MANEUVER WHICH RESULTED IN STRUCTURAL DAMAGE TO BOTH LT AND RT ELEVATORS. (M)SDR 2000ZZZM12Elevators · damagedTCAS MADE CONTACT WHILE FLT GCO7580 WAS DEPARTING PHNL, AT APPROXIMATELY 3800 FT. FLIGHT CREW INITIATED EVASIVE MANEUVER WHICH RESULTED IN STRUCTURAL DAMAGE TO BOTH LT AND RT ELEVATORS. (M)SDR G6OA042Bolt · looseNR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON MOUNT BOLTS SHOWS SLIPPAGE ON TORQUE STRIPE INDEX. PERFORMED RE-WORK AS REQUIRED BY REF; DC-10 SB A54-99, REVISION 4 DATED FEB 15, 1995. (M)SDR G6OA041Bolt · looseNR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON MOUNT BOLTS SHOWS SLIPPAGE ON TORQUE STRIPE INDEX. PERFORMED RE-WORK AS REQUIRED BY REF DC-10-SB A54-00, REVISION 4 DATED FEB 15, 1995. (M)SDR G60A017Pawl · wornIN THE PROCESS OF TROUBLESHOOTING, APU STARTING FAULT. THE PAWLS OF THE STARTER ADAPTER WERE FOUND TO BE WORN. PARTS WERE ORDERED IDENTIFIED BY P/N FORM DC-10 IPC 49-44-01 ITEM 80. WHEN THE PARTS WERE RECEIVED THERE WAS ONLY AND ADAPTER WITHOUT THE PAWL. WSDR G6OA010Engine · failedGVA - AT LIFT OFF, CREW REPORTED A LOUD BANG FOLLOWED BY VIBRATION, N1, AND N2 DECAYING, EGT RISE AND LOW FUEL FLOW INDICATIONS FOR NR 1 ENGINE. TOWER REPORTED LARGE FLAME FROM THE TAIL PIPE. NR 1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNEDSDR SCNA96378Engine · failedDURING CLIMB, EXPERIENCED EXTREME VIBRATION AND NUMBER 3 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. RETARDED NUMBER 3 ENGINE THROTTLES AND LIGHT EXTINGUISHED. AFTER SEVERAL MINUTES, OIL PRESSURE DROPPED RAPIDLY, ENGINE FIRE LIGHT ILLUMINATED AND SMOKE ENTERSDR SCNA96320Fire Loop · intermittantFIRE LOOP-B ON ENGINE NUMBER 2 ILLUMINATED INTERMITTANTLY DURING FLIGHT. TROUBLESHOT SYSTEM PER MM 26-11-03 AND FOUND CANNON PLUG P1-8004 PUSHED BACK. RESEATED PIN, CLEANED ALL CONNECTIONS AND OPS CHECKED SYSTEM.SDR SCNA96253Smoke Detector · malfunctionedOBSERVED A MOMENTARY LOWER CARGO FIRE INDICATION. CHECKED FORWARD CARGO SMOKE DETECTOR IN ACCORDANCE WITH TAFI 26-14-00, CLEANED PLUG AND TESTED SEVERAL TIMES ON GROUND.SDR SCNA96203Gear Indication · malfunctionedFOUND ENGINEER'S PANEL LANDING GEAR INDICATOR SHOWING UNSAFE ON RIGHT MAIN. GROUND OPS TESTED NORMAL.SDR SCNA96115Battery Pack · dischargedEMERGENCY LIGHT FAILED TO TEST. REPLACED EMERGENCY BATTERY PACK, OPS TEST NORMAL.