N863DA

Part: CONNECTOR — LOOSE (DOOR LOCK) · airframe 85,121 hrs · 10,074 cycles

DOOR FLIGHT LOCK 1R MESSAGE REOCURRING ISSUE. TIGHTENED DOOR LOCK SWITCH CONNECTOR .

Part: SKIN — DAMAGED (LT NACELLE INLET) · airframe 85,620 hrs · 10,120 cycles

(AIRCRAFT 7004, L/P 1406821) WHILE CLOSING #1 FAN FOUND VISABLE DAMAGE TO LT OUTBD UPPER FAN COWL. CORRECTIVE ACTION: APPLIED PERMANENT REPAIR WITH REFERENCE TO B777 SRM 51-70-04-2R.

Part: WARNING MESSAGE — FALSE ACTIVATION (R1 DOOR LOCK) · airframe 85,121 hrs · 10,074 cycles

DOOR FLIGHT LOCK 1R MESSAGE. ERASED MESSAGE IAW FIM 52-11.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 84,696 hrs · 10,035 cycles

(AIRCRAFT 7004, L/P 1351580) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND COVER BROKEN. REPLACED COVER.

Part: LIGHT — DAMAGED (CABIN) · airframe 84,696 hrs · 10,035 cycles

(AIRCRAFT 7004, L/P 1351575) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: FOUND EMERGENCY FLOOR LIGHT COVER DAMAGED. R/R COVER.

Part: LIGHT — DAMAGED (CABIN) · airframe 84,696 hrs · 10,035 cycles

(AIRCRAFT 7004, L/P 1351579) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND EMERGENCY FLOOR LIGHT COVER DAMAGED R/R COVER.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 84,696 hrs · 10,035 cycles

(AIRCRAFT 7004, L/P 1351578) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: FOUND EMERGENCY FLOOR LIGHT COVER DAMAGED. R&R COVER.

Part: LIGHT — DAMAGED (CABIN) · airframe 84,696 hrs · 10,035 cycles

(AIRCRAFT 7004, L/P 1351577) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND FLOOR LIGHT COVER DAMAGED AT 205 AND R/R COVER.

Part: LIGHT — BROKEN (CABIN) · airframe 84,696 hrs · 10,035 cycles

(AIRCRAFT 7004, L/P 1351585) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND EMERGENCY LIGHT COVER BROKEN. REPLACED COVER.

Part: OVEN — FIRE (GALLEY) · airframe 81,859 hrs · 9,744 cycles

SHIP 7004 -FIRE- FWD GALLEY OVEN FIRE DUE TO MELTED AND SPILLED CHOCOLATE DURING OPERATION. EXTINGUISHER USED (REFERENCE LOGPAGE 5656327) / FIRE EXTINGUISHED /C/B PULLED / FLIGHT CONTINUED. CORRECTIVE ACTION: REMOVED AND REPLACED OVEN LOCATION 401 PER B777 AMM 25-35. OK FOR SERVICE (REFERENCE LOGPAGE 1022470).

Part: LENS — MISSING (CABIN) · airframe 81,499 hrs · 9,708 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING. REPLACED LENS COVER. LP 0972574

Part: SELECTOR SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 81,399 hrs · 9,698 cycles

CHECK PED 4R RIGGING. DUE TO CONFIRMED REPORTS OF EMERGENCY LIGHTS ILLUMINATING AT 4R / PED WITH EMERGENCY LIGHT SW ON P5 ARMED AND 4R DOOR MODE SELECT HANDLE IN DISARMED POSITION AND DOOR HANDLE TO THE FULL OPEN POSITION. CORRECTIVE ACTION: WRANG OUT S52121 PINS 7, 8 REDS M OHMS. REMOVED MODE SELECT SW. PER B777 AMM 52-11-28-000-801 (269944). REINSTALLED NEW S52121 SWITCH IAW B777 AMM 52-11. TEST OK.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 81,161 hrs · 9,671 cycles

(AIRCRAFT 7004, L/P 0919748) WORKING INSPECTION OF EEPLS LENSES, FOUND EMERGENCY LOWER FLOOR PROXIMITY LIGHT ASSY DAMAGED, AFT OF FLIGHT ATTENDANT CREW REST DOOR. REMOVED AND REPLACED LOWER PROXIMITY LIGHT ASSY.

Part: LOCK — INOPERATIVE (L4 DOOR) · airframe 81,161 hrs · 9,671 cycles

(AIRCRAFT 7004, L/P 5338782) 4L DOOR FLIGHT LOCK INOP. REMOVED BUSTLE TO MANUALLY UNLOCK FLIGHT LOCK IN ORDER TO OPEN DOOR REPLACED FLIGHT LOCK ACTUATOR PER B777 AMM 52-11-26, OPS CHECK GOOD.

Part: LIGHT — NONE · airframe 81,161 hrs · 9,671 cycles

(AIRCRAFT 7004, L/P 5338771) MTC RECEIVED VERBAC REPORT FROM CLEANING CREW THAT DOOR 4L/R EMERGENCY LTS WERE ON. UPON ENTERING DR4L/R LOCATION FOUND EMERGENCY LTS NOT ILLUMINATED. PERFORMED OPS TEST PER B777 AMM33-51. LTS AT DOOR 4 L/R CHECK OK.

Part: ACTUATOR — MALFUNCTIONED (L2 DOOR FLT LOCK) · airframe 80,364 hrs · 9,590 cycles

(AIRCRAFT 7004, L/P 4683509) DOOR FLIGHT LOCK 2L STATUS MESSAGE IN CRUISE FLIGHT APPROXIMATELY 1 HOUR AFTER DEPARTURE. / REPLACED FLIGHT LOCK ACTUATOR IAW B777 AMM 52-11-26.

Part: BATTERY — DISCHARGED (CABIN) · airframe 80,116 hrs · 9,565 cycles

(AIRCRAFT 7004, L/P 4841186) EMERGENCY SIGN LIGHTS INOP AT DOORS 2R & 2L. REPLACED POWER BASE AT 2L AND BATTERY AT 2R PER AMM 33-51.

Part: COMPRESSOR — LEAKING (ENGINE) · airframe 79,791 hrs · 9,527 cycles

(AIRCRAFT 7004, L/P 4709426) WITH POWER CHANGES CLIMBS AND DESCENT ACRID ORDER THROUGHOUT AIRCRAFT. BOROSCOPE INSPECTION REQUIRED PER FIM TASK 71-05-20-810-822. REMOVED IPC AND HPC BOROSCOPE PLUGS IAW AMM 72-00-00 PERFORMED VISUAL INSPECTION FOR OIL LEAKS WITH BORESCOPE. FOUND LEAKS BETWEEN COMPOSER STAGES IP3 AND IP5. REINSTALLED BOROSCOPE PLUGS IAW AMM 72-00-00 WIP 813089 RAN BOTH ENGINES AND APU NO ODOR DELECTATED WITH PACK FULL HOT OR COLD.

Part: UNKNOWN — ODOR (CABIN) · airframe 79,790 hrs · 9,526 cycles

UNIDENTIFIABLE ODOR OCCURRED THROUGH ENTIRE DESCENT, UNTIL LANDING. HORRIBLY STRONG ODOR. STRONG OIL, ORGANIC, MUSTY ODOR. FOLLOWED AMM 21-00-01-100-801, STEPS 15 TO 19, STEP 15 LT & RT ENGINE RUNNING, BOTH PACKS OFF & ON, NO OIL CONTAMINATION FROM LEFT & RIGHT, GROUND CONDITIONED AIR CONNECTOR, PERFORMED HIGH POWER RUN OF THE ENGINES, NO ODOR OF OIL NOTED. VISUALLY INSPECTED OZONE CONVERTERS AND RECIRCULATION FAN FILTERS, NO OIL CONTAMINATION. INSPECTED APU COMPARTMENT, NO EXTERNAL LEAK NOTED, OIL WAS FULL. REMOVED GROUND PNEUMATIC AIR CONNECTOR CHECK VALVE AND APU BLEED ON, NO CONTAMINATED OIL OR ODOR. INSPECTED BLEED DUCT, DOWN STREAM OF APU, NO OIL CONTAMINATED. OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 79,790 hrs · 9,526 cycles

ACRID ODOR, PERIODICALLY DETECTED IN THE FLT DECK. POSSIBLY OUTPUT FROM LT PACK OR DUCT SYSTEM. REMOVED APU SURGE VALVE, NO CONTAMINATION FOUND IN APU DUCTS. REMOVED LEFT ENG IP CHECK VALVE, NO CONTANMINATION FOUND IN DUCTS. R & R THE LT OZONE CONVERTER, OPS AND LEAK CHECKED GOOD IAW MM 21-73. REPLACED UPPER RECIRCULATION FILTERS IAW IAW AMM 21-25. RAN BOTH ENGINES AND REMOVED APU AIR. RAN PACKS WITH ENGINE BLEED, AIR WENT FULL TEMP RANGE WITH PACKS, NO ODOR DETECTED. REPLACED THE RT SIDE HEPA FILTERS IAW MM 21-25 SYSTEM CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (R3 DOOR FLT LOCK) · airframe 79,766 hrs · 9,524 cycles

R3 DOOR FLIGHT LOCK STATUS MESSAGE. REMOVED AND REPLACED THE R3 DOOR FLIGHT LOCK ACTUATOR IAW AMM 52-11, OPS CHECKED GOOD IAW AMM 52-11-26, LOCK OPERATED OK.

Part: ACTUATOR — MALFUNCTIONED (L3 DOOR) · airframe 79,546 hrs · 9,497 cycles

STATUS MSG: DOOR FLIGHT LOCK 3L. REPLACED 3L FLIGHT LOCK ACTUATOR PER MM 52-11-26, LOCK TEST GOOD.

Part: BRACKET — CORRODED (GALLEY) · airframe 79,218 hrs · 9,467 cycles

DURING PRE-FDA INSPECTION, GALLEY A-2 COMPARTMENT A719 FWD HOLD DOWN BRACKET EXHIBITING CORROSION ON UPPER SURFACE (ACTION ITEM REQUEST ITEM 1). GALLEY A-2 COMPT A719 FWD HOLD DOWN BRACKET REMOVED AND REPAIRED AS PER AMM 25-31-03.

Part: SEAT TRACK — CORRODED (BS 1455-1497) · corrosion level 2 · airframe 79,214 hrs · 9,466 cycles

MAIN CABIN SEAT TRACK, BS 1455 - 1497, RBL 108 FOUND CORRODED. REPAIRED IAW ER/A 566931-14, PRI REV 0, REV 1, AND REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 1520-1640) · corrosion level 2 · airframe 79,214 hrs · 9,466 cycles

CABIN SEAT TRACK, BS 1520 - 1640, RBL 108 FOUND CORRODED. REPAIRD IAW ER/A 566931-14, PRI REV 0, AND REV 1

Part: SEAT TRACK — CORRODED (BS 1455-1505) · corrosion level 2 · airframe 79,214 hrs · 9,466 cycles

CABIN SEAT TRACK AT BS 1455 TO 1505, RBL 74 CORRODED. ER/A 566931-14 PRI REV O AND REV 1 COMPARED WITH FINAL ER/A 566931 REV ORIGINAL AND FOUND COMPLIANCE.

Part: LOCK — FAILED (L3 DOOR) · airframe 79,062 hrs · 9,450 cycles

L3 DOOR FLIGHT LOCK STATUS MESSAGE AFTER TAKE OFF. R & R THE DOOR FLIGHT LOCK IAW MM 52-11-26. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (R4 DOOR) · airframe 78,898 hrs · 9,434 cycles

R4 DOOR FLIGHT LOCK STATUS MESSAGE IN FLIGHT . CARRIED OUT A FLIGHT LOCK GROUND TEST, ALL DOORS LOCKING UNLOCKING NORMAL. STATUS MESSAGE ERASED. OK FOR SERVICE.

Part: VALVE — FAILED (CROSSFEED) · airframe 78,757 hrs · 9,419 cycles

AFT CROSSFEED VALVE IS INTERMITTENT IN OPERATION. THE VALVE FAILED TO OPEN WHEN COMMANDED. AFTER SEVERAL CYCLES OF AFT CROSSFEED VALVE SWITCH, THE AFT VALVE OPENED, EICAS AND STATUS MESSAGES WERE PRESENT, WHEN THE VALVE IS COMMANDED, THE VALVE FAILED TO CLOSED. AFTER SEVERAL CYCLES OF THE AFT CROSSFEED SWITCH, THE VALVE CLOSED. VALVE DISAGREEMENT LIGHT AND DISPLAY OF FUEL SYSTEM SCHEMATIC CONFIRM FAULT. FWD CROSSFEED VALVE OPS NORMAL. R & R THE AFT CROSSFEED VALVE IAW AMM 28-22. ALL CDCCL REQUIREMENTS COMPLIED IAW SFAR 88. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: CIRCUIT CARD — FAILED (RT MLG STEERING) · airframe 78,585 hrs · 9,403 cycles

TROUBLESHOT IAW FIM 32-53-00-810-810. COMPLETED MLG STEERING TEST, NO FDE'S PRESENT. R & R THE RT MLG STEERING PCA IAW AMM 32-53-03-000-801. PERFORMED MLG STEERING FAULT ISOLATION PROCEDURES 32-53-00-810-810. NO FAULTS PRESENT. OK FOR SERVICE.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 78,937 hrs · 9,438 cycles

DURING SVC CHK FOUND 2 CRACKS IN LT WING TO BODY FAIRING PN 191DL. REPAIRED MPN 149W1212-5 PANEL PER ERA 561376-14 PER SRM 53-00-70.

Part: PANEL — DAMAGED (LT WING) · airframe 78,198 hrs · 9,361 cycles

DURING WALK AROUND CHECK, FOUND THE LEFT WING PANEL 511AB DAMAGED. REMOVED AND REPLACED THE PANEL IAW SRM 57-41-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,093 hrs · 9,348 cycles

EMERGENCY LIGHT AT SEATS 1D TO 7D INOPERATIVE. R & R THE BATTERY AND CHARGER ASSY IAW AMM 33-51. OPS CHECKED GOOD.

Part: SEAL — LEAKING (L4 DOOR) · airframe 77,382 hrs · 9,271 cycles

L4 DOOR EXTREMELY LOUD NOISE COMING FROM LOWER HALF FRONT AND BACK OF DOOR SEALS. NEVER DISSIPATES THROUGHOUT FLIGHT. TROUBLESHOT IAW TSM 52-09-01. PERFORMED A FLASHLIGHT CHECK OF DOOR SEAL AND OPS CHECKED WITH NO DAMAGE FOUND. CLEANED THE SEAL AND VERIFIED SEAL IN GOOD CONDITION.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 77,313 hrs · 9,264 cycles

EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED OK.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 77,313 hrs · 9,264 cycles

EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED OK.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 77,313 hrs · 9,264 cycles

EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED OK.

Part: LIGHT — SHORTED (CREW REST) · airframe 76,591 hrs · 9,181 cycles

FLUORESCENT BULB SHORTED CAUSING FUMES IN F/A CREW REST AREA. REPLACED CREW REST NR 2 BUNK LIGHT ASSEMBLY.

Part: LIGHT — MISSING (SEAT 34D) · airframe 76,193 hrs · 9,137 cycles

EMERGENCY EXIT LIGHT AT SEAT 34D MISSING. REPLACED LIGHT ASSEMBLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,151 hrs · 9,133 cycles

L3 DOOR, LEFT OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.

Part: LIGHT — DAMAGED (CABIN) · airframe 76,043 hrs · 9,121 cycles

EMERGENCY FLOOR LIGHTING DAMAGED AT POSITION 405. REPLACED EMERGENCY LIGHTING LENS COVER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,969 hrs · 9,114 cycles

FOUND EMERGENCY FLOOR LIGHT LENS MISSING NEAR THE SEAT 57. INSTALLED A NEW LENS. LIGHT CHECKED GOOD.

Part: COVER — LOOSE (EXIT SIGN) · airframe 75,220 hrs · 9,035 cycles

EMERGENCY EXIT SIGN COVER LOOSE LOCATIONS:01R. EMERGENCY EXIT COVER FIXED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 75,205 hrs · 9,033 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:407. ADJUSTED LIGHT OPS CHECK GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 75,205 hrs · 9,033 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:405. ADJUSTED LIGHT OPS CHECK AND LENS OPS CHECK GOOD.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 74,030 hrs · 8,925 cycles

DURING PDC CHECK, L1 DOOR, AFT SIDE EMERGENCY EXIT SIGN MISSING LENS. INSTALLED MISSING EMERGENCY EXIT SIGN DOOR 1 LEFT.

Part: MOUNT — BROKEN (CABIN) · airframe 73,817 hrs · 8,906 cycles

ROW 43D EMERGENCY LIGHT MOUNT BROKEN. SECURED EMERGENCY LIGHT MOUNT IAW CMM 25-27-89.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 73,276 hrs · 8,842 cycles

FOUND EMERGENCY LIGHT AT R1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: SEAT TRACK — CORRODED (BS 1444-1557) · airframe 71,464 hrs · 8,631 cycles

PASSENGER CABIN, BS 1444-1557, RBL 74 SEAT TRACK FOUND CORROSION AT MULTIPLE LOCATIONS. SEAT TRACK REPAIRED SRM 53-00-52, REPAIR 4, SRM 51-40-02 AND ER/A 543546-14, PRI REV 0.

Part: SEAT TRACK — CORRODED (BS 1444-1480) · airframe 71,464 hrs · 8,631 cycles

PASSENGER CABIN BS 1444-1480, RBL 108 SEAT TRACK FOUND CORROSION AT MULTIPLE LOCATIONS. SEAT TRACK REPAIRED IAW SRM 53-00-52, REPAIR 4, SRM 51-40-02 AND ER/A 543546-14 PRI REV 0.

Part: SEAT TRACK — CORRODED (BS 976) · airframe 71,464 hrs · 8,631 cycles

PASSENGER CABIN BS 976, RBL 74, SEAT TRACK FOUND CHAFING. SEAT TRACK REPAIRED IAW SRM 53-00-52, REPAIR 3, SRM 51-40-02 AND ER/A 543546-14, PRI REV 0.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,265 hrs · 8,213 cycles

PASSENGER SEATS 10-12 LT AND RT FLOOR EMERGENCY LIGHTS INOPERATIVE. POWER SUPPLY M33098 FAILING. REMOVED IAW AMM 33-51-06. CEILING PANEL OPEN AT DOOR 2R. WIP 588392. REPLACED FUSE IAW AMM 33-51-06. OPS NORMAL, CLOSED ACCESS. OK FOR SERVICE. 1888895.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,173 hrs · 6,888 cycles

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

Part: LIGHT — MISSING (CABIN) · airframe 53,769 hrs · 6,846 cycles

SEAT 5B EMERGENCY LIGHT MISSING LENS AND BULB. SEATS 10BC-1414BC EMERGENCY AISLE LIGHTS INOPERATIVE. RELAMPED SEAT 5B. REPLACED CHARGER AND BATTERY M33098. SEATS 10BC-14BC CK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,603 hrs · 6,828 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 12B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE PROXIMITY LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,372 hrs · 6,410 cycles

DURING EMERGENCY LIGHT TEST FOUND LIGHTS INOPERATIVE, ROW 10 THROUGH 13. REPLACED POWER SUPPLY ABOVE DOOR 2R AND TESTS OK.

Part: FAN — FAILED (CABIN) · airframe 46,019 hrs · 6,064 cycles

ODOR IN AFT CABIN FOUND RT LWR RECIRCULATION FAN FAILED. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: FAN — OVERHEATED (CABIN) · airframe 46,019 hrs · 6,064 cycles

F/A REPORTED BURNING RUBBER ODOR IN AFT GALLEY AREA. SHUTOFF OVENS, LIGHTS, IFE, RECIRC FANS. ODOR DISSAPATED. TURNED LIGHTS BACK ON AND STILL NO SMELL. T/S SYS. CHECKED LIGHTS OVENS IFE AND RECIRC FANS. FOUND LATCHED MSG FOR LOWER RT RECIRC FAN OVERHEATED. MX MSG 21-24700. DEACTIVATED LWR RT RECIRC FAN AND FWD TO MCO AND PLAC IAW MEL 21-25-01. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: CONNECTOR — BURNED (BOOST PUMP) · airframe 42,175 hrs · 5,723 cycles

LEFT AFT BOOST PUMP LIGHT ON PUSHBACK RETURNED TO GATE. FOUND LEFT AFT FUEL BOOST PUMP AND ELECTRIC CONNECTOR PINS BURNED. REPLACED LEFT FUEL BOOST PUMP AND CONNECTOR DM28102 OPS CKS NORMAL.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 42,175 hrs · 5,723 cycles

LEFT AFT FUEL BOOST PUMP LIGHT ON PUSHBACK, RETURNED TO GATE. FOUND LEFT AFT FUEL BOOST PUMP AND ELECTRIC CONNECTOR PINS BURNED. REPLACED LEFT FUEL BOOST PUMP AND CONNECTOR DM28102. OPS CKS NORMAL.

Part: BATTERY — OVERHEATED (APU) · airframe 41,608 hrs · 5,681 cycles

NOTICED ELEC BURNED ODOR AND SMOKE IN AFT CABIN AREA, FOUND APU BATTERY THERMAL DISCHARGED. REPLACED APU BATTERY AND CHARGER. FOUND APU BATTERY WITH BURN SPOT ON BACK AND IN CONTACT WITH INSULATION REPLACED APU BATTERY AND CHARGER PER MM. REMOVED BUR INSULATION. POSITIONED INSULATION CORRECTLY

Part: GUIDE VANE — DAMAGED (NR 1 ENGINE) · airframe 40,950 hrs · 5,629 cycles

BORO NR 1 ENG HPC DUE TO PARAMETER SHIFT ON TRENDS AMM 72-00-00-200-802-R00. FOUND DAMAGE TO IPT NOZZLE GUIDE VANES BEYOND LIMITS REF M/M 72-000-00-200-810-R00-00 CHANGED ENGINE NR 1 PER TRANSMITTAL 11T00.

Part: OVEN — ODOR (GALLEY) · airframe 40,612 hrs · 5,603 cycles

GALLEY 401 OVEN 2 AFTER COOKING 8 MINS MADE HIGH PITCH BUZZ THEN QUIT W/ASSOCIATED BURNT WIRE ODOR NO FAULT LIGHT.

Part: WHEEL — MISSING (NR 8) · airframe 32,381 hrs · 4,877 cycles

NR 8 WHEEL ASSY MISSING ON ARRIVAL ATL. NOTIFIED BY TLV A WHEEL HUBCAP FOUND ON RUNWAY. C/W BURST TIRE INSPECTION ON LOG ITEM 030 INSTALLED TIRE ASS PER M/M. INSTALLED NEW NR BRAKE AND SLEEVE IAW 32-45-07. INSTALLED TRANSDUCER PER AMM 32-42-05, ALL CHECKS GOOD. REMOVED AND REPLACED CENTER AXLE RT MLG PER MM 32-11-26-400-802 AND 32-11-26-000-802.

Part: BRAKE ASSY — CONTAMINATED (MLG) · airframe 31,804 hrs · 4,817 cycles

TOWER REPORTED SMOKE COMING FROM AIRCRAFT MAIN GEAR AFTER VERY SMOOTH LANDING. FOUND RESIDUAL DEICING FLUID ON WHEELS AND BRAKES. CLEANED BRAKES. OK FOR SERVICE. NO DEFECTS NOTED.

Part: VALVE — FAILED (ANTI ICE SYSTEM) · airframe 30,858 hrs · 4,715 cycles

ANTI-ICE ENG L EICAS MSG ON ENG SHUTDOWN. MTC MSG 30-10101 VLV FAILED IN CLOSED POSITION. NO ICE NOT AVIAL TRIED TO MEL PER 30-21-01B. MTC UNABLE TO C/W MEL ENG RUN. DEFERRED TO CREW PROCEDURE WHICH FAILED AFTER PUSH BACK. MTC REPLACED L ENG ANTI ICE VALVE AND REMOVED MCO.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 29,833 hrs · 4,605 cycles

NR 1 ENG SHOWED TREND SHIFT. C/W BORO OF HPC COMPRESSOR. FOUND 6TH STAGE PC COMPLETELY FO OUT. OUT OF LIMITS IAW MM. NR 1 ENG S/N 51177 ENG CHANGE REQUIRED. C/W ENG CHANGE IAW TRANS 11T003.

Part: FAN — ODOR (CABIN) · airframe 29,288 hrs · 4,548 cycles

ELECTRICAL SMELL IN CABIN UPPER AFT FAN FWD TO MCO CB COLLARED REMOVED AND REPLACED FAN IAW MM OPS CK GOOD MCO AND PLACARD REMOVED ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: VIDEO UNIT — BURNED (SEAT 48 GHJ) · airframe 22,397 hrs · 3,676 cycles

VIDEO SYSTEM IN CNTR SECTION 45-49 DID NOT WORK PROPERLY. FLICKERING ON AND OFF RESET NO HELP. UNFAMILIAR ODOR ASSOCIATED WITH THE FLICKERING. INSPECTED FOUND AVU UNDER SEAT 48 GHJ OVERHEATING CAUSING BURNING ODOR. REPLACED AVU LOADED SOFTWARE, CHECKS OK, ODOR GONE.

Part: LIGHT — BURNED (CREW REST AREA) · airframe 21,135 hrs · 3,484 cycles

CREW REST SIDE LIGHT HAS BURNED END. REPLACED SAME.

Part: ENGINE — LEAKING (NR 1) · airframe 16,375 hrs · 2,833 cycles

EXCESSIVE OIL CONSUMPTION LEFT ENGINE DUE TO REPORT OF LEFT ENGINE HOC AND AT ROLLS ROYCE RECOMMENDATION, REPLACE THE LEFT ENGINE.

Part: MONITOR — FAILED (CABIN) · airframe 16,314 hrs · 2,824 cycles

SMOKE COMING FROM VIDEO SCREEN OVERHEAD AT SEAT ROW 33G/32G ATL AMT'S. REMOVED AND REPLACED OVERHEAD MONITOR 32H AND VDU 5. OPS CHECK NORMAL.

Part: RECEPTACLE — ARCED (EXTERNAL POWER) · airframe 14,549 hrs · 2,569 cycles

AFTER HOOKING UP EXTERNAL POWER, NOTICED ARCING COMING FROM RECEPTICLE. DISCONNECTED CORD FROM A/C. RECEPTACLE HAD BURNED. REPLACED EXTERNAL POWER RECEPTACLE IAW M/M. OPS CHECK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: OVEN — UNSERVICEABLE (MID GALLEY) · airframe 8,372 hrs · 1,494 cycles

GALLEY FWD 2 DOOR CENTER OVEN OVERHEATS WHEN TURNED ON STRONG ELECT SMELL NOTICED BY FLT ATTEND. REPLACED OVEN IN MID GALLEY POS 1 OPS CHECK GOOD MCO AND PLACARD REMOVED ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: ACTUATOR — FAILED (STEERING SYS) · airframe 7,796 hrs · 1,391 cycles

ABORTED T/O DUE TO MAIN GEAR STEERING AND T/O WARN HORN. MTC MSGS 32-63010 AND 32-63020 ACTIVE. AUTO EVENT RT ACTUATOR FAILED. FWD TO MCO AND PLC. LT ACTUATOR WILL NOT LOCK. PERFORMED MDM BLOCK PROCEDURE TO ZE OUT AND LOCK.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 4,956 hrs · 923 cycles

CAPTS O2 MASK CAME APART WHEN TAKING FROM STOWAGE. CAPTS O2 MASK REPLACED LEAK CK CARRIED OUT

Part: UNKNOWN — ODOR (CABIN) · airframe 3,321 hrs · 618 cycles

STRONG BURNING ODOR COMING FROM APPROXIMATE LOCATION OF ROW 44 FG FLOOR LEVEL. INSPECTED AREA AROUND 44 FG SUSPECT ROCKWELL COLLINS ENTERTAINMENT SYSTEM SEAT BOX CHECK ROCKWELL AVU - UPCUS AND WIRING. NO HEATING OR BURN SMELL ON COMPONENTSSYSTEM WORKS FINE. PERFORMED ROCKWELLCOLLINS CONFIDENCE CHECK. ALL NORMAL. UNABLE TO DUPLICATE PROBLEM. CONTINUE TO MONITOR SYSTEM.

Part: HARNESS — CHAFED (NR 1 ENGINE) · airframe 2,148 hrs · 427 cycles

LEFT ENG EEC C1 MAINT MSG 73-70211 - FMU. FOUND WIRE HARNESS W0816 CHAFING ON 1 OIL LINE APPROX 10 INCHES FROM CONNECTOR PM76001A ON FMU EVIDENCE OF ARCING EXIST. REPLACED WIRE W816-2001 R/R FROM DM73003A TO DM76001A PER WDM. CKS GOOD PER FIM 73-21-20-2 AND ENG RUN.

Part: LINK — BROKEN (RAM AIR DOOR) · airframe 2,132 hrs · 425 cycles

AIRCRAFT BEGAN A LOUD VIBRATION PASSING 15000 FT/305KNTS. LOUDEST ON LEFT SIDE OF AIRCRAFT AT ROW 12, OVERWING AREA. FOUND LEFT RAM AIR DOOR ACTUATOR CONTROL LINKS HAD SHEARED AND SEPARATED. REPLACED LT PACK RAM AIR DOOR AND MECHANISMS. RAN OPERATION CHECK, DOOR OPS NORMAL.