N860DA

Part: WIRE HARNESS — NOT REPORTED (THRUST REVERSER) · airframe 89,996 hrs · 11,237 cycles

(AIRCRAFT 7001, L/P 1218713) REFERENCE LOG 1218709 WIRE BUNDLE W0800 REQUIRES REPLACEMENT AT NSV. CORRECTIVE ACTION: DEFER TO MONITOR ON LP 1218709. REPLACE AT NSV.

Part: SEAT TRACK — CORRODED (BS 1452-1520) · corrosion level 2 · airframe 86,106 hrs · 10,818 cycles

(AIRCRAFT 7001, L/P 0928363) MTC TASK - CORROSION FOUND ON SEAT TRACK LBL 72 BETWEEN STA 1452 TO STA 1520 WHILE DOING CLOSET 3F-1L INSTALLATION MARKOUT. SEAT TRACK REPAIR CARRIED OUT AS PER B777-200 SRM 53-00-52 , FIG 202 REPAIR 3 WORK ACCOMPLISHED WITH ER/A 574714-14 REV ORIGINAL FOR DISPOSITION.

Part: OXYGEN BOX — BROKEN (SEAT 2BC) · airframe 86,089 hrs · 10,816 cycles

(AIRCRAFT 7001, L/P 0923076) MIDLIFE MOD - PSU OXY BOX ASSY AT SEAT 2BC FOUND BROKEN. WORKCARD RAISED IN ERROR.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 86,089 hrs · 10,816 cycles

(AIRCRAFT 7001, L/P 0920387) MIDLIFE MOD - DOOR L2 EMERGENCY BATTERY M33096 FOUND VOLTAGE LOW. EMER BATT M33096 AT DR2L REMOVED AND REPLACED AS PER B777 AMM 33-51-06 AND OPS TEST CARRIED OUT AS PER B777 AMM 33-51-06 FOUND SATIS.

Part: LIGHT — CRACKED (CABIN) · airframe 86,089 hrs · 10,816 cycles

(AIRCRAFT 7001, L/P 0920396) MIDLIFE MOD - PROX EMER LTS AT AFT GLY AND OFCR FOUND CRACKED. PROXIMITY EMER LTS AT AFT GLY AND OFCR. REMOVED AND REPLACED AS PER B777 AMM 33-51-05. OPS TEST REFR TO WKCARD 2500-01815-08.

Part: FLOOR SUPPORT — DENTED (BS 1916) · airframe 86,089 hrs · 10,816 cycles

(AIRCRAFT 7001, L/P 0915215) AD EM-EO TASK - BULK CARGO AT LBL 25" STA 1916 ATTACHED FLOOR STRINGER SURFACE FOUND DENT. FLOOR STRINGER AT LBL 25", STA 1888 TO STA 1928, REPAIR CARRIED OUT AS PER B777-200 , SRM 53-70-53 , FIG 202, REPAIR 2.

Part: NUT — DAMAGED (FUSELAGE) · airframe 86,089 hrs · 10,816 cycles

(AIRCRAFT 7001, L/P 0908454) AD EM-EO TASK - BULK CARGO FLOOR STRUCTURE AT STRUCTURE AT STA 1916 LBL FOUND 01EA ANCHORNUT DAMAGE. BULK CARGO FLOOR STRUCTURE AT STA 1916 LBL 01EA ANCHORNUT REMOVED AND REPLACED AS PER SRM 51-40-02.

Part: NUT — DAMAGED (FUSELAGE) · airframe 86,089 hrs · 10,816 cycles

(AIRCRAFT 7001, L/P 0908446) AD EM-EO TASK - BULK CARGO FLOOR STRUCTURE AT STA 2050 LBL FOUND 01EA ANCHORNUT DAMAGE. BULK CARGO FLOOR STRUCTURE AT STA 2050 LBL 01EA ANCHORNUT. REMOVED AND REPLACED AS PER SRM 51-40-02.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 85,010 hrs · 10,686 cycles

DAMAGE FOUND ON ARRIVAL. AFT CARGO DOOR OPENING SKIN EDGE DAMAGE 5/32 INCH DEEP. LOWER FWD CORNER 14 INCH ABOVE LOWER EDGE. BLENDED OUT DAMAGE IAW SRM 53-00-01 FIG 102 DETAIL B AND TABLE A. ALODINED BARE METAL AND RESTORED TOPCOAT.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 83,170 hrs · 10,506 cycles

EMERGENCY LIGHTS CIRCUIT BREAKER TRIPPED. REPLACED THE BATTERY AND CHARGER AT THE R2 DOOR IAW AMM 33-51.

Part: PROXIMITY SENSOR — OUT OF ADJUST (L3 DOOR) · airframe 82,495 hrs · 10,433 cycles

SHIP STATUS MESSAGE IN CRUISE "DOOR FLIGHT LOCK 3L". ADJUSTED GAP ON FLIGHT LOCK PROX SENSORS IAW AMM 52-71 AND 52-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,472 hrs · 10,332 cycles

LEFT OVERHEAD EMERGENCY LIGHTS AT ROWS 35, 38, 40, 43 & THE L3 DOOR FWD EMERGENCY LIGHTED SIGN INOPERATIVE. REPLACED THE SIGN ASSEMBLY AT THE L3 DOOR. REPLACED THE BATTERY AT THE L3 DOOR. OPS CHECKED GOOD.

Part: LOCK — FAILED (L3 DOOR) · airframe 80,969 hrs · 10,280 cycles

L3 DOOR LOCK STATUS MESSAGE. TESTED THE L3 DOOR FLT LOCK IAW MM 52-11, OPS NORMAL, NO HISTORY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 80,035 hrs · 10,180 cycles

EMERGENCY LIGHT LENS MISSING AFT GALLEY ARE BETWEEN F/A SEAT. REPLACED LENS ASSY. CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,900 hrs · 10,165 cycles

EMERGENCY LIGHTS AT SEAT ROWS 10-12 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK M33098.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 79,805 hrs · 10,155 cycles

EXIT SIGN AT THE L2 DOOR FELL OFF. SECURED THE EXIT SIGN LENS.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 78,869 hrs · 10,048 cycles

NR 2 ENGINE OTBD THRUST REVERSER INNER LINER HAS AREA OF THERMAL DAMAGE.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 78,869 hrs · 10,048 cycles

NR 2 ENGINE INBD THRUST REVERSER HAS AREA OF THERMAL DAMAGE ON THE INNER LINER.

Part: SKIN — DAMAGED (BS 2022) · airframe 78,869 hrs · 10,048 cycles

DAMAGE ON FUSELAGE SKIN AT BS 2022 BETWEEN STRINGERS 43 AND 44L. REPAIRED IAW SRM 53-00-01, REPAIR 7.

Part: SKIN — CORRODED (BS 1874-2033.5) · airframe 78,869 hrs · 10,048 cycles

CORROSION ON FUSELAGE SKIN FROM BS 1874 TO 2033.5 BETWEEN STRINGERS 43 AND 44L. REPAIRED IAW ERA 558381-14, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 1916-2200) · airframe 78,869 hrs · 10,048 cycles

CORROSION ON STRINGER 44L FROM BS 1916 TO 2200. REPAIRED IAW ERA 558298-14, REV ORIGINAL.

Part: SUPPORT FRAME — CRACKED (NR 1 NACELLE) · airframe 78,869 hrs · 10,048 cycles

NR 1 PYLON INNER DOOR SUPPORT IS CRACKED 10 INCHES AFT OF HYD CONNECTION. REPLACED THE SUPPORT FRAME IAW DWG 313W3550.

Part: BATTERY PACK — SEPARATED (EMERGENCY LIGHT) · airframe 78,661 hrs · 10,026 cycles

EMERGENCY LIGHTS INOPERATIVE SEAT 10-17 CENTER ROW BOTH SIDES. FOUND BATTERY PACK HAD SEPARATED FROM POWER SUPPLY. REINSTALLED, AND OPS CHECKED GOOD IAW AMM 33-51.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 78,558 hrs · 10,014 cycles

UPON ARRIVAL FROM HND, FOUND AFT CARGO DOOR AFT LOWER CORNER DAMAGED/BENT AND RIVET HEAD SHEARED. ACCOMPLISHED REWORK OF DAMAGE ON LOWER AFT CORNER OF AFT CARGO DOOR. REF SRM 52-30-01 FIG 102 SHT 1. DAMAGE DESCRIPTION (BEND AT AN EDGE) REWORK PER FLAG NOTE 5. C/W HFEC NDT PT-651-00-01. NO DISCREPANCIES NOTED. DAMAGED AREA FALLS INTO AREA A OF DAMAGE PERCENTAGE. REINSTALLED RIVETS AND SEAL RETAINER INSTALLED NEW SEAL AND NEW DRAIN PLUG. RESTORED SURFACE FINISH. OKAY FOR SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 78,438 hrs · 10,003 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. REPLACE MISSING LIGHT LENS COVER.

Part: LIGHT — UNKNOWN (CABIN) · airframe 78,438 hrs · 10,003 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 406. REPLACED MISSING LIGHT LENS COVER.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 77,814 hrs · 9,949 cycles

WHITE EMERGENCY LIGHT AT SEAT 10B, BULBS AND COVER ARE MISSING. REPLACED THE BULBS AND COVER AT SEAT 10B.

Part: FUSE — BLOWN (CABIN) · airframe 77,677 hrs · 9,937 cycles

DURING SVC FOUND EMERGENCY LIGHTS IN SEATS 10-12 AB INOP. REPLACED BLOWN FUSE ON EMERGENCY POWER SUPPLY M33098 IAW AMM 33-51.

Part: LIGHT — UNKNOWN (CABIN) · airframe 77,677 hrs · 9,937 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHTING LENS PER AMM 33-51.

Part: LIGHT — UNKNOWN (CABIN) · airframe 77,677 hrs · 9,937 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT LENS PER AMM 33-51.

Part: OVEN — SMOKE (GALLEY) · airframe 74,405 hrs · 9,614 cycles

CREW REPORTS OVEN 814 SMOKING. RAN OVEN; SMOKES. NOT ELECTRICAL. CLEANED OVEN, NO HELP. R & R OVEN IAW AMM 25-34, OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,912 hrs · 9,474 cycles

EMERGENCY LIGHTS IN CEILING ON LT SIDE FROM SEAT ROW 32, FWD INOPERATIVE BATTERY PACK AT L1 AND L2. REPLACED BATTERY PACK AND CHARGER AT L1 AND L2 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,073 hrs · 9,391 cycles

LIGHTS FIRST CLASS LT SIDE INOPERATIVE. R & R BATTERY PACK IAW MM 33-51-06. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,692 hrs · 9,154 cycles

EMERGENCY LIGHTS INOPERATIVE ON SEATS, FROM ROW 29 TO ROW 43. REPLACED NR 4 FUSE IN POWER SUPPLY M33404 AND EMERGENCY LIGHTS TEST OK AMM 33-51-06/201. 1923682.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 69,156 hrs · 9,059 cycles

EMERGENCY LIGHT INOPERATIVE ON SEAT ROWS 10-12 BOTH SIDES. REPLACED FUSE IN POWER SUPPLY.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 65,464 hrs · 8,651 cycles

AT GEAR DOWN AMS RECEIVED A GEAR DISAGREE EICAS. BOTH MAINS INDICATED UP AND NOSE GEAR INDICATED DOWN. DISCONTINUED APPROACH WENT AROUND AND FOLLOWED CHECK LIST. ALT GEAR DOWN EXTENSION SUCCESSFUL - 3 GEAR DOWN INDICATIONS AND CONTINUED TO UNEVENTFUL LANDING. RII: N ENTR 371145 W TROUBLESHOT IAW FIM 32-30-00 AND FOUND SYS 1 & SYS 2 FAULTS. R & R LANDING GEAR CONTROL LEVER MODULE IAW AMM 32-31-01-401. PERFORMED RQD TESTS AND FOUND SYS 1 OPS NORMAL. FAULT IS SYS 2 SOLENOID ON LANDING GEAR SELECTOR VALVE. LANDING GEAR CONTROL LEVER MODULE IS A BORROWED PART IN LT R, MPN D724-03-001, SN 707/05-2001.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,472 hrs · 8,436 cycles

EMERGENCY LIGHTS INOPERATIVE AT R1 DOOR INTERIOR AND EXTERIOR AND RT AISLE OF F/C CABIN. R & R BATTERY PACK M33094 IAW MM 33-51-06. OPS CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (L3 DOOR SLIDE) · airframe 63,028 hrs · 8,386 cycles

DURING L3 DOOR SLIDE DEPLOYMENT EPAS SYS FAILED TO OPERATE. SYS TESTED IAW AMM 52-11-20. OPS CHECKED GOOD. REMOVED AND INSTALLED SERVICABLE EPAS RESERVIOR IAW AMM 52-11-22. OPS CHECKED GOOD. REPLACED EPAS RESERVOIR IAW AMM 52-11-22, PB 401 SYS TEST NORMAL. FOUND EPAS BATTERY PACK FAILED, REPLACED EPAS BATTERY PACK IAW 52-11-20. SYS OPS NORMAL. OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,345 hrs · 7,897 cycles

EMERGENCY LIGHT ARE INOPERATIVE AT ROWS 10 THRU 14. REPLACED POWER SUPPLY FUSES PER AMM 33-51-06-960. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 330) · airframe 69,074 hrs · 9,051 cycles

DURING WALK AROUND, HOLES IN FUSELAGE IN BS 330, STRINGER 25.

Part: BATTERY — INOPERATIVE (L3 DOOR SLIDE) · airframe 56,435 hrs · 7,821 cycles

DURING MAINTENANCE VISIT, THE 3L EPAS BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY WAS REPLACED.

Part: FUSE — OPEN (EMERGENCY LIGHTS) · airframe 56,035 hrs · 7,777 cycles

DURING CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT ROWS 31 TO 42 LEFT AND RIGHT INOPERATIVE. MAINTENANCE REPLACED A POWER SUPPLY FUSE. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,183 hrs · 7,691 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR EXIT LIGHT BATTERY AT DOOR 4L WAS FOUND TO BE WEAK. MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,183 hrs · 7,691 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR EXIT LIGHT BATTERY AT DOOR 3R WAS FOUND TO BE WEAK. MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,483 hrs · 7,512 cycles

CREW REPORTED EMERGENCY LIGHTS OUT FROM SEAT 44-57 ON LEFT AND RIGHT SIDES. REPLACED BATTERY PACK (M33401) AND POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,660 hrs · 7,345 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY LIGHTS AT SEATS FORWARD MOST SECTION OF TOURIST CLASS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY M33404. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: LIGHT — BROKEN (DOOR 1R) · airframe 50,554 hrs · 7,229 cycles

DURING EMERGENCY LIGHT TEST FOUND DOOR 1R EXIT LIGHT BROKEN, REPLACED LIGHT AND CHECKS OK.

Part: STRUCTURE — DAMAGED (L4 DOOR) · airframe 50,367 hrs · 7,208 cycles

LOWER AFT CORNER OF L4 DOOR DAMAGED REPAIRED IAW ERA 486782-14, REV ORG.

Part: PLUG — MISSING (NR 1 ENGINE) · airframe 47,061 hrs · 6,873 cycles

FOUND DURING WALK AROUND ON ARRIVAL - NR 1 ENGINE AFT EXHAUST PLUG MISSING. SCREWS STILL ATTACHED TO FWD PLUG SECTION. NO DAMAGE FOUND TO AIRCRAFT. REPLACING FWD AND AFT EXHAUST PLUGS. FOUND INSULATION BLANKET ENG COVER DAMAGED. REMOVED AND REPLACED INSULATION BLANKET END COVER. ALSO INSTALLED A TURBINE EXH PLUG AS PER AMM. TIGHTENING ALL BOLT/SCREWS WITH SPECIFIC TORQUE IAW AMM. CHECKS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: IGNITER — FAILED (APU ENGINE) · airframe 45,031 hrs · 6,692 cycles

ATTEMPTED 5X APU STARTS IN CRUISE AS REQUESTED BY MX. APU WOULD NOT START. PEAK RPM 29 PERCENT. CA-NO LATCHED FAULTS APU OPERATES NORM. REMOVED AND REPLACED APU IGNITORS IAW MM FIM 49-40-00-810-814. OPS CK GOOD ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: OVEN — DEFECTIVE (MID GALLEY) · airframe 39,706 hrs · 6,285 cycles

ELEC SMELL IN MID GALLEY NR 1 OVEN SHUTDOWN TURNED OFF SMELL DISSIPATED. REMOVED NR 1 OVEN AND INSP WIRING BEHIND OVEN AND OVEN ELEC CONNECTOR. NO TROUBLE FOUND. REMOVED AND STOWED OVEN ELEC CONNECTOR. PULLED AND COLLARD OVEN NR 1 C/BS FWD TO NEF USING FRC 253.30. REPLACED OVEN, CKS GOOD, REMOVED MCO. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: ENGINE — VIBRATION (NR 1) · airframe 38,584 hrs · 6,189 cycles

NR 1 ENGINE REPLACED DUE TO HOC AND N3 VIBS.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 36,381 hrs · 5,986 cycles

NR 1 ENG CHANGE DUE TO STAGGER. REPLACED ENGINE ON TRANS 11T003.

Part: MICROPHONE — UNSERVICEABLE (COCKPIT) · airframe 36,022 hrs · 5,951 cycles

FROM OBSERVERS POSITION HOT MIC ON PUSHBACK. REMOVED AND REPLACED MIC. OPS CK GOOD.

Part: ENGINE — SURGES (NR 2) · airframe 34,087 hrs · 5,761 cycles

DURING ROTATION AND CLIMB, NR 2 ENGINE SURGED 4 TO 6 TIMES ENGINE CONTINED TO OPERATE AND SAFETY RETURNED TO NRT. FOUND EGT EXCEEDENCE.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 34,087 hrs · 5,761 cycles

ON TAKE OFF OUT OF NRT THE RIGHT EXPERIENCED 4 TO 6 STALLS WITH FLAMES FROM TAILPIPE. A/C RTB TO NRT. ENGINE WAS NOT SHUTDOWN. FURTHER INSPECTION REVEALED METAL ON THE MCD AND IN THE TAILPIPE. MAX TGT OF 946 AND 940 FOR 8 SECONDS. PER AMM ENGINE CHANGE REQUIRED. PERFORMED BORO INSP PER AMM. FOUND SEVERAL BLADES BENT/DAMAGED HPC BORO PLUG HP5S. PERFORMED POWERPLANT AFTER SURGE INSP PER AMM. REPLACED NR 2 E PER TRANS 11T003. ETOPS CATEGORY 'C': UNCOMMANDED PWR CHANGES, SURGES, OR STALLS

Part: CONNECTOR — NOT SEATED (ELECTRICAL) · airframe 29,665 hrs · 5,280 cycles

ELEC STBY SYS STATUS MSG RE-OCCURRED AT CRUISE ALT. AFTER LANDING ELEC STBY SYS EICAS MSG APPEARED W/NUMEROUS STATUS MSGS FOUND LOW INSULATION VALUE ON CABLE BETWEEN ELMS 310 31016 PIN 13. STBY PWR SW 5671 PIN 9 DISCONNECTED D4753 FAULT WAS ON ELMS UNIT SIDE. RECONNECTED 4753. DISCONNECTED D4828. FOUND PINS PUSHED BACK. RESEATED SAME. REFITTED PLUG. CABLE INSULATION NOW GOOD. RAN ENGINES CARRIED OUT TAXI TEST. NO FAULTS ON STBY ELEC SYS OK FOR SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 29,561 hrs · 5,269 cycles

OVERHEAD LIGHT BALLAST IN FLT ATTENDANT CREW REST AREA MADE BURNING ODOR WHEN TURNED ON. MIDDLE COMPARTMENT AFT ON CAPT SIDE. FLT ATTENDANT REPORTS NO SMOKE OR FIRE. RAN LIGHT ON GRD AND NO TROUBLE FOUND. DISCONNECT AND STOW BALLAST CONNECTOR AS PRECAUTIONARY. AFT ZONE MIDDLE BUNK CAPT SIDE FLUORESCENT LIGHT FWD TO MCO AND PLAC PER MEL 33-21-01. REPLACED BALLAST M33132, LIGHT OPS NORM MFG P/N 8184-1. REMOVED MCO AND PLACARD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 28,646 hrs · 5,164 cycles

FWD CARGO DOOR EICAS MSG ON CLIMBOUT AT APPROX 24000 FT LIGHT EXTINGUISHED AT 8000 FT ON DESCENT BUT RE-ILLUMINATED ON TOUCHDOWN. VISUAL INSPECTION BY FMS AFTER LANDING SHOWED FWD DOOR CLOSED. UNABLE TO DUPLICATE.

Part: PCU — LEAKING (NR 7 SPOILER) · airframe 28,226 hrs · 5,116 cycles

DURING WALK AROUND FOUND HYDRAULIC LEAK AROUND THE LEFT WW FOUND LEAK TO BE FROM THE NR 7 SPOILER ACT HOUSING. REPLACED NR 7 SPOILER PCU.

Part: WARNING HORN — ACTIVATED (WINDSHEAR) · airframe 28,167 hrs · 5,110 cycles

RTO AT 100 KNOTS WINDSHEAR WARNING. A/C RETURNED TO GATE. UNABLE TO DUPLICATE OR FIND FAULT.

Part: WARNING LIGHT — ILLUMINATED (SPOILERS) · airframe 27,994 hrs · 5,090 cycles

DURING TAXI OUT SPOILERS ECIAS MSG APPEARED. RAN CHECKLIST, NO HELP. FLT CONTROL STATUS MSG FAULTED NR 7 SPOILER PCA. RAN MAT TEST FAULT CLEARED. ALL FLT CONTROLS OPS NORMAL. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,962 hrs · 5,087 cycles

FOUND ROWS 30 THROUGH 41 SEAT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: SPRING — FAILED (RT MLG UPLOCK) · airframe 26,505 hrs · 4,886 cycles

DURING PDC FOUND RT MLG UPLOCK SPRING MISSING. REPLACED SAME.

Part: FUSE — UNSERVICEABLE (CABIN) · airframe 26,354 hrs · 4,867 cycles

SEATS 30 DEF TO 41 DEF EMERGENCY LIGHTS INOP. REPLACED FUSE IN POWER SUPPLY.

Part: HEADSET — ARCED (CABIN) · airframe 25,285 hrs · 4,722 cycles

LOG BOOK WRITE UP STATED THAT THERE WAS ARCING AT SEAT 38E. CREW CONFIRMED TO MTC HEADSET WAS PROBLEM NOT A/C EQUIPMENT. DISCARDED HEADSET.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,665 hrs · 4,634 cycles

JUMP SEAT 4L FWD FLASHING LIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY.

Part: LINE — CHAFED (NR 2 ENGINE) · airframe 22,508 hrs · 4,365 cycles

FUEL LEAK FROM ENG AFTER START, FOUND FUEL LEAKING FROM LINE BETWEEN FMU AND DRAIN CANISTER. REMOVED AND CLEANED FMU DUMP FILTER REF 73-21-13-100-801. REMOVED DRAIN LINE DUE DAMAGE AT CLAMP AREA INSTALLED NEW LI PURCHASED FROM AA P/N FK21039, AA P/N 4066928 PERF ENG RUN, L CHK ALL NORMAL. OK FOR SERVICE. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: FAN — BURNED (LWR) · airframe 21,137 hrs · 4,218 cycles

FOUR HRS INTO FLT F/A SMELLED ELEC ODOR IN CABIN MID GALLEY AREA SMELL DISSIPATED, 30 MIN LATER SMELL RETURNED AND THERE WAS A RECIRC FAN STATUS MSG IN COCKPIT. TURNED BOTH RECIRC FANS OFF AND ODOR DISSIPATED. MTC MSG 21-24700 RECORDED FOUND RT LWR REC FAN INOP. NOTED BURNING ODOR UPON REMOVAL. INSTALLED NEW FAN PER M/M, OPS NORMAL MAT SYS TEST PASS OK FOR SERVICE.

Part: COVER — UNSECURE (SEAT 54H) · airframe 19,874 hrs · 4,065 cycles

SEAT 54H GETS AN ELECTRICAL SHOCK ON FOOT FROM ENTERTAINMENT UNIT UNDER SEAT 53H. CAUSED PROBLEM TO OTHER DISPLAYS IN AREA. FOUND PLASTIC COVER ON AVU UNDER SEAT 53H AND 1 EA CONNECTOR ON AVU UNSECURE. SECURED SAME. VIDEO / AUDIO, NOW OPS NORMAL. PERFORMED INSPECTION VISUAL OF OTHER IFE WIRING UNDER 53H. NO OTHER TROUBLE FOUND.

Part: FAN — FAILED (RECIRCULATION) · airframe 17,850 hrs · 3,796 cycles

RECIRC FAN STATUS MESSAGE IN FLIGHT WITH ELEC ODOR IN FWD BUSINESS SECTION AND SLIGHT VISUAL. NO ODOR IN COCKPIT. DISSIPATED IN 1-2 MINUTES. REPLACE RECIRC FAN. SYSTEM OPS CK NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: ACM — ODOR (LT PACK BAY) · airframe 15,463 hrs · 3,392 cycles

FUMES IN COCKPIT ON CLIMB AND DESCENT WENT AWAY WHEN LT PACK SWITCHED OFF. SNAPSHOTS SHOWED LT PACK O/P TEMP HIGH WITH TBV IN SAME POSITION AS RT DISCONNECTED AND OPENED LT TBV ODOR DISAPPEARED. SUSPECT LT ACM FWD TO MCO AND PLACED PER MEL 21-52-01. UPDATE: REACTIVATED TURBINE BYPASS VALVE AND RAN LT PACK F HOURS AT DIFFERENT TEMP SETTINGS, NO FUMES OR ODORS. PACK INDICATIONS NORMAL, C/W LT PACK TEMP CONTROL PASS MCO AND PLACARD REMOVED.

Part: VALVE — INOPERATIVE (LEFT ENG) · airframe 15,114 hrs · 3,313 cycles

LEFT ENG BLEED INOP. R/R LEFT ENG PRSOV PER M/M AND RAN ENG CHECK GOOD PER M/M 36-10-00-5 ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,508 hrs · 3,058 cycles

STATUS MSG LEFT EQUIP COOLING FAN. PULLED AND SECURED EQUIP COOLING SUPPLY C/B P110 PANEL. DISCONNECTED AND STOWED CONNECTOR DB21581.

Part: ODOR — DETECTED (CABIN) · airframe 11,956 hrs · 2,789 cycles

CREW REPORTS FOUL SMELL IN THE AIR CONDITIONING SYSTEM AT LOW ALTITUDES. REMOVED WATER SEPARATOR ON LEFT PACK, SEPARATOR CLEAN. CLEANED RESIDUE IN OUTLET OF COMPRESSOR REHEATER, RAN PACKS WITH APU AIR AND WITH ENGINES AT PWR. NO ODOR NOTED AT THIS TIME.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 9,883 hrs · 2,420 cycles

REPLACED FLASHLIGHT BATTERY AT 4L DOOR FOUND BY CREW DURING EMERGENCY EQUIPMENT CHECK.

Part: BATTERY — FAILED (E/E BAY) · airframe 9,827 hrs · 2,412 cycles

MAIN BATT FAILED PRIOR TO DEPT MTC MSG24-13054. REPLACED MAIN BATT AND BATT CHARGER PRECAUTIONARY PER MM. BATT P/N 263BA101-2 S/N 1484 OFF.

Part: VIDEO UNIT — MALFUNCTIONED (CABIN) · airframe 8,961 hrs · 2,245 cycles

ABOUT 2.5 HOURS AFTER TAKEOFF AN ODOR APPEARED IN THE FORWARD CABIN IN THE VICINITY OF ROWS 4-5. A SOURCE WAS NOT FOUND. THE SMELL MOVED AS FAR AS ROW 2 THEN DISSIPATED WITHIN 15 MINS. THE SMELL WAS CHEMICAL NOT STRONG. THE VIDEO CONTROLS FOR SEATS 5C AND 5G WERE LOST. FOUND BURNT SMELL FROM SEAT 5 C/G AVU. REMOVED AND REPLACED SEAT AVU, OPS GOOD RAN FOR 2.5 HOURS.

Part: HARNESS — FAULTY (CABIN) · airframe 8,879 hrs · 2,232 cycles

EMERGENCY LIGHTS 1-6 LEFT AND RIGHT IN WILL NOT TEST. FOUND FUSE IN EMERGENCY LIGHT PACK BAD. TROUBLESHOT TO 4G AFT LIGHT ASSY. TRIED NEW ONE, NO HELP. REPLACED SEAT HARNESS.

Part: COFFEEMAKER — SHORTED (AFT GALLEY) · airframe 8,068 hrs · 2,081 cycles

REAR COFFEE MAKER SHORTED OUT REPLACED DISPENSER.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 7,835 hrs · 2,036 cycles

ON DECENT, MAX SPEED AUTOPILOT EICAS LT ILLUMINATED. AS WENT ABOUT 2 KNOTS HIGH INTO RED-OVERSPEED WARNING TRIED TO SOUND BUT WAS MUFFLED SOUNDING. AN ELECTRICAL SMELL ON LEFT SIDE OF COCKPIT WAS NOTICED SUSPECT OVERSPEED SHAKER FAILURE. T/S AP MTC MSG PER FIM SUGGESTED SEQUENCE ERROR NO ACTION NEEDED FOR FAULT. ALSO PERFORMED WEU SYSTEM TEST ON MAT TO VERIFY SPEAKER OPN. TEST PASSED PERFORMED STALL WARNING TEST OF STICK SHAKER MOTORS ALL OK. NO ELECTRIC OR BURNING SMELL NOTED OK FOR SERVICE

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 5,262 hrs · 1,569 cycles

FLASHLIGHT AT R-3 DOOR INOP. REPLACED FLASHLIGHT.

Part: HARNESS — CHAFED (NR 2 ENGINE) · airframe 5,114 hrs · 1,538 cycles

DURING THE PERFORMANCE OF THE SERVICE CHECK, FOUND WIRE BUNDLE FROM EEC SUITCASE TO BE CHAFED ON SEVERAL WIRES. ENGINE CHANGED TO FACILITATE MAINTENANCE.

Part: UNKNOWN — ODOR (CABIN) · airframe 4,515 hrs · 1,430 cycles

PASSENGERS IN THE AREA NEAR SEAT 49J EXPERIENCED A BURNING RUBBER SMELL FOR APPROX 5 SECONDS. NO CHANGES IMMEDIATELY PRIOR TO THE SMELL IN ANY OF THE AUDIO/VIDEO EQUIP SEAT POSITION OR AIR VENTS. DELTA MTC PERSONNEL INSPECTED AREA AND EQUIPMENT FOR HEAT DAMAGE AND ABNORMAL CONDITIONS, NONE FOUND. OK FOR SERVICE.

Part: COFFEE MAKER — FAILED (GALLEY)

LEFT COFFEEMAKER POPPED. RESETTING CENTER C/B CAUSES ARCING IN AFT COFFEEMAKER. ISOLATED PROBLEM TO NR 2 C/M IN LEFT AFT GALLEY. PULLED AND COLLARED POWER C/B FOR NR 2 C/M. FWD TO MCO AND PLACARD. C/M NASI LGW.

Part: COFFEE MAKER — FAILED (CABIN)

COFFEEMAKERS INOP AFT CO-PILOTS SIDE, COFFEEMAKERS 108, 109, 110. ELECTRICAL SMELL NOTICED IN AREA AND CIRCUIT BREAKERS PULLED. REPLACED COFFEEMAKERS.