N600GC

Part: DOOR — LOOSE (NLG)

ON GEAR RETRACTION ON DEPARTURE FROM KLAX, FELT SEVERE VIBRATIONIN NOSE GEAR AREA. ON ARRIVAL AT KSAN, FOUND RIGHT NOSE GEAR DOOR OPEN. INSPECTED NOSE GEAR DOORS AND LOCKING MECHANISMS IAW MM 32-21-00. RESECURED NOSE GEAR DOORS AND LOCKING MECHANISMS. NOSE LANDING GEAR DOORS FUNCTION CHECKS GOOD ON TEST FLIGHT. (M)

Part: AUDIO CONTROL — FAILED (F/E'S PANEL)

F/E AUDIO CONTROL PANEL INOPERATIVE AND STARTED SMOKING. DISCONNECTED CONTROL PANEL. REMOVED AND REPLACED AUDIO CONTROL PANEL AND SYSTEM OPS CHECK NORMAL IAW MM 23-44-00. (M)

Part: MOUNT — LOOSE (NR 1 ENGINE)

DURING C-CHECK INSPECTION, NR 1 ENGINE FORWARD MOUNT WAS FOUND SLIGHTLY SEPARATED. FURTHER INVESTIGATION FOUND NUT/BOLT LOOSENED FROM EACH OTHER WHICH ALLOWED THE MOUNTING BRACKET TO SEPARATE. INSPECTED AND RE-WORKED PER EO 99-5415-026. RE-INSTALLED ENGINE, PERFORMED LEAK CHECKS AND POWER ASSURANCE RUN IAW JC105 AND MM 71-06-00. (X)

Part: MOUNT — LOOSE (RT PYLON)

C-CHECK - PYLONS DURING ROUTINE INSPECTION. REF: J/C 0834, FOUND FORWARD ENGINE MOUNT BOLTS WITH LOCKWIRE BROKEN AND CAP BETWEEN FORWARD PYLON ENGINE MOUNT AND FORWARD ENGINE MOUNT, LT SIDE 0.065 INCH. RT SIDE 0.085 INCH.

Part: MOUNT — LOOSE (LT PYLON)

C-CHECK - PYLONS DURING ROUTINE INSPECTION. REF: J/C 0834, FOUND FORWARD ENGINE MOUNT BOLTS WITH LOCKWIRE BROKEN AND CAP BETWEEN FORWARD PYLON ENGINE MOUNT AND FORWARD ENGINE MOUNT, LT SIDE 0.065 INCH. RT SIDE 0.085 INCH.

Part: LATCHES — SHEARED (LT ELEVATOR)

ON TRANSIT WALK AROUND, FOUND INBOARD DETACHABLE ELEVATOR IN DETACHED POSITION. LATCH PINS FOUND SHEARED. REMOVED AND REPLACED LEFT DETACHABLE ELEVATOR LATCHES, TWO P/N H2188-1, AND INSTALLED ALL REQUIRED FASTENERS. RELATCHED ELEVATOR AND CHECKED FOR PROPER MOVEMENT PER MM 27-30-03. REPAIR APPROVED BY MDC, REF FORM 8110-3, 4/5/99, BURCH, DN-DERY-605071-NM. PERMANENT REPAIR REQUIRED WITHIN 4800 FLT HOURS OR NEXT C-CHECK, REF EO 99-2740-007. (M)

Part: LATCHES — FAILED (LT ELEVATOR)

ON TRANSIT WALK AROUND INBOARD DETACHABLE ELEVATOR IN DETACHED POSITION. LATCH PINS FOUND SHEARED. REMOVED AND REPLACED LEFT DETACHABLE ELEVATOR LATCHES, TWO P/N H2188-1, AND INSTALLED ALL REQUIRED FASTENERS. RELATCHED ELEVATOR AND CHECKED FOR PROPER MOVEMENT PER MM 27-30-03. REPAIR APPROVED BY MDC, REF FOR 8110-3, 4/5/99, BURCH, DN-DERY-605071-NM. PERMANENT REPAIR REQUIRED WITHIN 4800 FLT HOURS OR NEXT C-CHECK, REF EO 99-2740-007. (M)

Part: SENSOR — FAILED (SLIDE)

THE L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST SWITCH WAS INOPERATIVE. THIS WAS DEFERRED IAW MEL 25-24. GROUND MAINTENANCE REMOVED AND REPLACED THE PRESSURE SENSE ASSY IAW MM 25-60-03. OPERATIONAL CHECK NORMAL. (M)

Part: ECU — LIGHTNING STRIKE (NR 1 ENGINE)

DURING CLIMB-OUT FROM CDG, THE FLIGHT CREW REPORTED LIGHTNING STRIKE. NR 1 ENGINE PARAMETERS WERE OUTSIDE THE NORMAL PARAMETERS. NR 1 ENGINE WAS SHUT DOWN, FUEL DUMPED IAW AOM VOL 1 AND RETURNED TO CDG. GROUND MAINTENANCE ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW MM 05-53-00. NO DAMAGE NOTED. PERFORMED POWER ASSURANCE CHECK. AS A RESULT, REPLACED THE MEC IAW MM 73-20-01. (X)

Part: FAIRING — CRACKED (LT HORIZ STAB)

GROUND MAINTENANCE FOUND PART OF THE LEFT AFT HORIZONTAL STABILIZER TRAILING EDGE UPPER SIDE MISSING. GROUND MAINTENANCE PERFORMED AN INTERIM REPAIR IAW BOEING TELEX SEQUENCE 9809446. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

GROUND MAINTENANCE WHILE PERFORMING PREVENTIVE MAINTENANCE FOUND THE EMERGENCY LIGHT SYSTEM WOULD NOT TEST. THE SYSTEM WAS INVESTIGATED AND THE BATTERY POWER SUPPLY WAS REPLACED IAW DC-10, MM 33-51-01. (X)

Part: SMOKE IND LIGHT — INOPERATIVE (COCKPIT)

LOWER AFT CARGO SMOKE DETECTOR NR 4 DOES NOT TEST ON ENGINEERS PRE-FLIGHT. RELAMPED LOWER AFT CARGO SMOKE DETECTOR NR 4 IN ACCORDANCE WITH MM 26-14-01. OPS CHECKED GOOD.

Part: SLIDE ASSY — INOPERATIVE (L1 DOOR)

THE L1 DOOR SLIDE REMOTE PRESS-TO-TEST INDICATOR LIGHT STAYS ON. BOTTLE PRESSURE CHECKS OK. REPLACED L1 DOOR SLIDE ASSEMBLY PER MM 52. INSPECTED SLIDE INSTALLATION AND OPS CHECKED REMOTE TEST SYSTEM.

Part: SMOKE DETECTOR — FAILED TEST (CARGO COMPT)

THE NUMBER 2 LOWER AFT CARGO SMOKE DETECTOR FAILED TO TEST. RELAMPED AND CHECKED SMOKE DETECTOR PER DC10 MM 26-14-00 AND DETECTOR CHECKED NORMAL.