N174UA

Part: UNKNOWN — ODOR (CABIN) · airframe 103,026 hrs · 11,303 cycles

DURING ENGINE START, STRONG FUEL ODOR IN FWD CABIN CAUSING PASSENGERS DISCOMFORT. THE NR 3 PACK WAS RUNNING THRUGHOUT THE START SEQUENCE OF ALL ENGINES. RUN UP OF ALL ENGINES PERFORMED. SEPERATION OF BLEED SOURCES IN COMBINATION WITH SINGLE PACK USAGE, NO SINGLE FUEL ODOR SOURCE IDENTIFIED. FUEL ODOR PRESENT DURING COMPLETE RUN UP. ACFT WAC PERFORMED AFTER RUN UP. NO EXTERNAL FUEL LEAKS FOUND. PACK BAY ACCESS PANELS OPENED AND CHECKED. NO FUEL LEAKS FOUND IN PACK AREA.

Part: DOOR FRAME — CRACKED (R4 DOOR) · airframe 85,080 hrs · 9,543 cycles

R4 ENTRY DOOR FRAME CRACKED AT AFT UPPER CORNER. STOP DRILLED. HFEC. MFG & INSTALL REPAIR IAW SRM 52-10-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,993 hrs · 10,998 cycles

UPPER DECK RT DOOR EMER LIGHT INOPERATIVE. R & R EMER LIGHT IAW MM 33-51-04. OPERATIONS CHECKED OK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,993 hrs · 10,998 cycles

FLOORBEAM UPPER CHORD FOUND CORROSION AT STATION 1700, RBL 26. FLOORBEAM UPPER CHORD REPAIRED IAW ECRA 5320-02615.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,993 hrs · 10,998 cycles

MAIN DECK FLOORBEAM CORROSION LEVEL 2 AT BS 520, BETWEEN RBL 11 & 40. REPAIR ACP IAW ECRA 5320-02613.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,993 hrs · 10,998 cycles

FLOORBEAM UPPER CHORD CORROSION, AT STATION 900, BL R18 - R24. REPAIR OF FLOORBEAM ACP IAW SRM 53-20-51 FIG 201 REPAIR 1 CAT A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 99,993 hrs · 10,998 cycles

THREE EACH HOLES WERE FOUND CRACKED, R5 DOOR CUT OUT AFT UPPER CORNER. EA 5331-01798 OP 10 WAS ACCOMPLISHED FOR REPAIR, BUT HAD DEVIATIONS THAT WERE ADDRESSED ON ECRA 5330-05433. NR 5R DOOR AFT UPPER CORNER SKIN REPAIRED IAW ECRA 5330-05433.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 99,993 hrs · 10,998 cycles

FUSELAGE CROWN INTERCOSTAL, BS 320 - 340, BBL0 CRACKED. PERMANENT REPAIR COMPLIED WITH IAW ECRA 5310-06635.

Part: LIGHT — MISSING (CABIN) · airframe 99,993 hrs · 10,998 cycles

SEAT 41 ABC, EMER LIGHT MISSING. REPLACED EMER LIGHT ASSEMBLY & OPERATIONS CHECKED GOOD IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,993 hrs · 10,998 cycles

G1 GALLEY EMER LIGHT INOPERATIVE. REPLACED G1 GALLEY EMER LIGHT & OPERATIONS CHECKED GOOD IAW AMM 33-51-04.

Part: CABLE — DAMAGED (CABIN) · airframe 99,993 hrs · 10,998 cycles

3RT LAVATORY EMER LIGHT CABLE DAMAGED. R & R EMER LIGHT CABLE IAW AMM 33-51-13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,993 hrs · 10,998 cycles

LEFT DOOR 5 EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33- 51-02.

Part: CABLE — DAMAGED (CABIN) · airframe 99,993 hrs · 10,998 cycles

EMERGENCY LIGHT UPPER DECK STAIR INOPERATIVE. REPLACED DAMAGED CABLE IAW MM 33-51-12.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 99,993 hrs · 10,998 cycles

MAIN DECK, RT NR 1 MAIN ENTRY DOOR UPPER SILL, STATION 460 WEB FOUND CRACKED. REPAIRED IAW ECRA 5310-06631.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 99,993 hrs · 10,998 cycles

MAIN DECK LT NR 1 MED UPPER SILL, STATION 460, WEB FOUND CRACK AD 2012-22-03. MAIN DECK LT NR 1 MED UPPER SILL STATION 460 WEB REPAIRED IAW ECRA 5310-06631.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,672 hrs · 10,968 cycles

UPPER DECK STATION 980, FLOORBEAM FAIL SAFE STRAP CORRODED RBL 26 - 34. REPAIRED IAW 747EN -53-0366.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,282 hrs · 10,933 cycles

EMERGENCY LIGHT AT SEAT 54C & 57J INOPERATIVE. REPLACED EMER EXIT LIGHT AT SEAT 57J & IN SEAT HARNESS AT 54C IAW MM33-51-12. OPERATIONS NORMAL.

Part: DOOR FRAME — CRACKED (L4 DOOR) · airframe 85,080 hrs · 9,543 cycles

LEFT NR 4 ENTRY DOOR FRAME CRACKED AT AFT UPPER CORNER. FROM CF DATED 11/10/2011. STOP DRILL, MANUFACTURED & INSTALLED REPAIR IAW SRM 52-10-02.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 97,339 hrs · 10,756 cycles

1 OF 2 FLOOR PROX EMER EXIT LIGHTS OUT AT UPPER DECK STAIRWELL. FOUND LAMP TO HAVE COME UNPLUGGED. REPLUGGED THE LAMP & OPERATIONS CHECKED IAW MM 33-51-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,738 hrs · 10,701 cycles

LEFT NR 1 DOOR GALLEY EMER LIGHT FOUND INOPERATIVE. REPLACED THE EMER LIGHT AT LT NR 1 DOOR GALLEY & TEST PASSED IAW AMM 33-51-12.

Part: CABLE — DAMAGED (CABIN) · airframe 96,738 hrs · 10,701 cycles

LEFT NR 4 DOOR GALLEY EMER LIGHT FOUND INOPERATIVE. REPLACED THE CABLE OF EMER LIGHT AT LT NR 4 DOOR GALLEY & TEST PASSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,738 hrs · 10,701 cycles

EMERGENCY LIGHT AT SEAT NR 25HJK 111 LAVATORY, 112 LAVATORY FOUND INOPERATIVE. REPLACED THE EMER LIGHT AT LT NR 3 DOOR LAVATORY 111 & TEST PASSED. RECONNECTED THE ELEC CONNECTOR OF EMER LT AT SEAT NR 25HJK, LAVATORY 112 & TEST PASSED.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 95,497 hrs · 10,577 cycles

MID LAVATORY MIDDLE & RT OUTER EEL STRIPS ARE INOPERATIVE. FOUND CONNECTOR DISCONNECTED. RECONNECT OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,497 hrs · 10,577 cycles

AFT GALLEY LT OUTER EEL STRIP INOPERATIVE. REPLACED OUTER EEL STRIP. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 95,497 hrs · 10,577 cycles

SEATS 54HJK TO 59HJK, SEAT EEL INOPERATIVE. FOUND TWO BROKEN WIRES CABLE ASSEMBLY PCN 560-4667. STILL NEEDS CABLE ASSEMBLY PCN 560-46 66.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 95,497 hrs · 10,577 cycles

DOOR 2L SLIDE LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM 33-51-06 P40. OPERATIONS CHECKED OK.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 95,497 hrs · 10,577 cycles

AISLE EMER LIGHT BY SEAT 4KH INOPERATIVE. FOUND CONNECTORS AT CEILING PANEL SWAPPED. SWAPPED TO RIGHT CONNECTOR & SECURED CONNECTOR. OPERATIONS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 95,042 hrs · 10,535 cycles

IAW A CHECK, SEAT 60H, SEAT EEL INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT LAMP.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 95,042 hrs · 10,535 cycles

IAW A CHECK, SEAT EEL AT 35A, INOPERATIVE. FOUND ONE PIN PUSHED IN AT CONNECTOR COMING FROM FWD SEAT.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 94,557 hrs · 10,488 cycles

NO LAND 3 STATUS, LT FCC FAIL. IAW MM 22-10-00 ACCOMPLISHED MCP & FCC TESTS ACFT DOWNGRADED TO CAT 1 STATUS IAW SEQ 5576 001. NEED TO ACCOMPLISH GND RECERTIFICATION TO RESTORE ACFT TO FULL CAT 2 - 3 CAPABILITY STATUS.

Part: UNKNOWN — MALFUNCTIONED (WINDOW HEAT) · airframe 94,179 hrs · 10,452 cycles

CAPTAIN`S NR 2 WINDOW HEAT INOPERATIVE. CYCLED CB, OPERATIONS CHECKED OK NO FAULTS FOUND.

Part: MICROPHONE — FAULTY (COCKPIT) · airframe 93,163 hrs · 10,344 cycles

BOOM MICROPHONE OPERATION IS UNSATISFACTORY AT FIRST OBSERVER`S STATION. MINITEL LOCATED BEHIND CAPTAIN'S SEAT. REPLACED BOOM MIC.

Part: SHIELD — DAMAGED (E&E BAY) · airframe 93,053 hrs · 10,333 cycles

MAIN EQUIPMENT DRIP SHIELD REPAIR DISCREPANCIES FOUND WHILE ACCOMPLISHING ROUTINE TASK CARD 295190303. DRIP SHIELD REPAIRED IAW ECRA 2551-01148.

Part: RESERVOIR — DEFECTIVE (R1 DOOR) · airframe 93,053 hrs · 10,333 cycles

DURING ACCOMPLISHMENT OF DOOR 1R EVAC SLIDE DEPLOYMENT & POWER ACTUATION SYS TEST IAW EQ6487, THE DOOR POWER ASSIST BOTTLE FAILED TO OPERATE. REPLACED DOOR POWER ASSIST RESERVOIR, OPERATIONS CHECKED OK IAW AMM 25-69-00.

Part: STRUCTURE — DAMAGED (BS 2590) · airframe 93,053 hrs · 10,333 cycles

RIGHT HORIZONTAL STABILIZER AFT UPPER ANGLE, BS 2590, RBL 43.5 A FASTENER HOLE WAS FOUND DAMAGED. INSTALLED BOLT WITH NUT IAW EVA-72110. REPAIR ACCOMPLISHED IAW ECRA 5510-02362.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 93,053 hrs · 10,333 cycles

BS 2598 RT AFT INNER CHORD & BULKHEAD WEB, CRACKS FOUND IN FASTENER HOLE. REPAIRS ACCOMPLISHED IAW ECRA 5313-01066.

Part: CONNECTOR — BROKEN (CABIN) · airframe 92,997 hrs · 10,328 cycles

IAW A CHECK, STAIRWAY EMERGENCY LUMINESCENT LIGHT INOPERATIVE. BROKEN RIBBON CONNECTOR UPPER DECK 20 INCHES FWD ALONG WALL FROM TOP STEP. REPLACED BROKEN RIBBON IAW AMM, CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,997 hrs · 10,328 cycles

IAW A CHECK, SEAT EMERGENCY EXIT LIGHT AT 35 LT INOPERATIVE. REPLACED SEAT EMERGENCY EXIT LIGHT AT SEAT 35LT, OPERATIONS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,997 hrs · 10,328 cycles

IAW A CHECK SEAT EMERGENCY EXIT LIGHT AT 35 LT INOPERATIVE. REPLACED SEAT EMERGENCY EXIT LIGHT AT SEAT 35 LT, OPERATIONS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 92,997 hrs · 10,328 cycles

AISLE OVERHEAD EMERGENCY EXIT LIGHT SIGN FWD OF 5L MED INOPERATIVE. REPLACED POWER SUPPLY OPERATIONS CHECKED OK. VERIFIED SECURITY OF INSTALLATION & VERIFIED OVERHEAD EMERGENCY EXIT LIGHTS AT DOOR 5L OPERATIONS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,997 hrs · 10,328 cycles

GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE BETWEEN 5L & 5R MED. DEFERRED IAW MEL SUSPECT BAD SOCKET.

Part: BATTERY — OUT OF ADJUST (CABIN) · airframe 92,997 hrs · 10,328 cycles

OVERHEAD EMERGENCY EXIT LIGHT ABOVE UPPER DECK STAIR LIGHT INTENSITY VERY WEAK. BATTERY DISCHARGE RAPIDLY, ADJUSTED & TESTED. OPERATIONS CHECKED OK.

Part: LIGHT — BROKEN (CABIN) · airframe 92,495 hrs · 10,277 cycles

ON CM CHECK FOUND SEAT 19H EMERGENCY EXIT LIGHT BROKEN. REPLACED EMERGENCY EXIT LIGHT & CHECKED OKAY.

Part: LINE — LEAKING (NR 4 BRAKE) · airframe 92,404 hrs · 10,269 cycles

NR 4 FRONT BRAKE BODY GEAR BRAKE LINE LEAKING BEYOND LIMITS. PLUGGED & CAPPED BRAKE LINE BOTH ENDS. NEED BRAKE LINE 180-0265. SEE IPC 32-41-00-010 ITEM 20. INOPERATIVE NR 4 BRAKE IAW METHOD 2. THE BRAKE DEACTIVATED IS NR 6 ACCORDING TO BOEING DIAGRAM. REPLACED BRAKE HOSE, NO LEAK FOUND.

Part: LIGHT — MISSING (CABIN) · airframe 92,360 hrs · 10,264 cycles

SEAT 45H MISSING EMERGENCY EXIT LIGHT STRIP. REPLACED EMERGENCY EXIT LIGHT STRIP IAW MM. VERIFIED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,360 hrs · 10,264 cycles

EMERGENCY EXIT LIGHT DOOR 2 CROSS AISLE FWD WALL MIDDLE LAMP INOPERATIVE. RELAMPED IAW MM. VERIFIED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,360 hrs · 10,264 cycles

DOOR 4R FWD SILL EMERGENCY LIGHT INOPERATIVE. RELAMPED 1317 DOOR 4R FWD SILL EMERGENCY LIGHT. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,360 hrs · 10,264 cycles

DOOR 4R FWD SILL EMERGENCY LIGHT INOPERATIVE. RELAMPED 1317 DOOR 4R FWD SILL EMERGENCY LIGHT. OPERATION CHECKED GOOD.

Part: CONNECTOR — UNKNOWN (CABIN) · airframe 92,290 hrs · 10,257 cycles

R & R EMERGENCY LIGHTS CONNECTOR ON ROWS 35-37ABC. ACCOMPLISHED EMERGENCY LIGHT CHECK OF ROWS 35-37ABC. OPERATION CHECKED NORMAL

Part: CARBON SEAL — LEAKING (FMU) · airframe 91,919 hrs · 10,219 cycles

NR 4 ENGINE FUEL LEAKING FROM BETWEEN MATING FLANGES OF FMU AND FUEL PUMP. REMOVED PUMP AND FMU IAW AMM 73-11-01-401 AND AMM 73-21-010-401. NEW PUMP AND FMU. NEW CARBON SEAL INSTALLED. REPLACED ENGINE FUEL PUMP IAW MM 73-11-01 AND FMU IAW MM 73-21-01.

Part: WIRE — DAMAGED (GALLEY) · airframe 91,675 hrs · 10,196 cycles

UPPER DECK LT COUNTER HAS GROUND WIRE TORN FROM UNDER-COUNTER TERMINATION POINT. CAPPED AND STOWED DAMAGED GROUND WIRES ON GALLEY IAW SWPM 20-10-11, PAGE 65 TO 73. COLLARED ALL CB TO ALL GALLEY POWERED ITEMS. BROKEN BONDING BRACKET STOWED IN CUTOUT WHERE IT WAS ATTACHED.

Part: WARNING MESSAGE — ILLUMINATED (BLEED OVERHEAT) · airframe 91,589 hrs · 10,188 cycles

CREW REPORTED NR 2 BLEED OVERHEAT PRV EICAS DISPLAYED.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 915,377 hrs · 10,183 cycles

NR 2 ENGINE HAS RUNNING FUEL LEAK FROM FM11 LINE. LINE RUNS BETWEEN FUEL PUMP AND FUEL OIL HEAT EXCHANGER. REMOVED OLD FM11 LINE AND REPLACED WITH NEW FUEL PUMP INLET TUBE IAW MM. ALSO, REINSTALLED HIGH PRESSURE CONTROLLER.

Part: SEAL — BROKEN (LIFE VEST) · airframe 91,371 hrs · 10,167 cycles

LIFE VEST SEAL BROKEN 7G. REPLACED BROKEN SEALS.

Part: RESERVOIR — DISCHARGED (L4 DOOR) · airframe 90,888 hrs · 10,115 cycles

EMERGENCY DOOR ASSIST BOTTLE AT L4 DOOR DISCHARGED. REPLACED IAW 52-11-06.

Part: SLIDER — DAMAGED (THRUST REVERSER) · airframe 90,602 hrs · 10,089 cycles

NR 4 ENGINE RIGHT THRUST REVERSER SLEEVE LOWER AUXILLIARY TRACK SLIDER FOUND WITH LIP MATERIAL MISSING ON ARRIVAL. :TRACK LINER AND SLIDER REPLACED IAW MM.

Part: LIGHT — PULLED (CABIN) · airframe 90,552 hrs · 10,083 cycles

EMERGENCY EXIT LIGHT BY SEAT 56 HJK HAS BEEN PULLED, IS OUT OF SOCKET. REPLACED EMERGENCY LIGHT, OP'S CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 90,489 hrs · 10,077 cycles

EEL LIGHT AT LAV 102 LOWER AFT CORNER DAMAGED BY FOOD CART. SECURED EEL LIGHT ASSY.

Part: WINDOW — DELAMINATED (L3) · airframe 90,489 hrs · 10,077 cycles

DELAMINATION UPPER PART OF CAPTAIN'S AFT SIDE WINDOW. REPLACED L3 WINDOW PER AMM.

Part: RUB STRIP — CRACKED (LT MLG DOOR) · airframe 90,397 hrs · 10,069 cycles

RUB STRIP CRACKED LEFT OUTBOARD GEAR DOOR. REPLACED RUB STRIP LEFT OUTBOARD GEAR DOOR.

Part: CHARGER — FAILED (MAIN BATTERY) · airframe 90,283 hrs · 10,058 cycles

BATTERY CHARGER REQUIRES REPLACING DUE FAILURE OF STBY PWR CHECK DL3387. REPLACED MAIN BATTERY CHARGER, TESTS SATISFACTORY.

Part: TERMINAL — DAMAGED (BATTERY CHARGER) · airframe 90,283 hrs · 10,058 cycles

DURING BATTERY CHARGER REPLACEMENT FOUND DAMAGED LUG ON BATTERY CHARGER TERMINAL LUG W4902-001-06. REPLACED DAMAGED TERMINAL LUG PER SWPM. TESTED PER MM 24-31-02 AND NORMAL.

Part: SKIN — BENT (L5 DOOR) · airframe 90,064 hrs · 10,036 cycles

DOOR 5L, LWR FWD CORNER FOUND BENT. INSP CARRIED OUT CRACKS RUNNING FROM FASTENER HOLE VERTICALLY UP AND DOWN. VISUAL INSP AND HFEC CARRIED OUT TO CONFIRM CRACKS. REPAIR TO BE CARRIED OUT IAW STRUCTURAL REPAIR MANUAL, REPAIR 9, DOOR OUTER SKIN NON FLUSH REPAIR AT 'A' BEAM CH 52.00.01, NEW ITEMS RAISED FOR REPAIR. ACCOMPLISHED RII INSPECTION OF DOOR 5 LEFT SLIDE INSTALLATION, ALL FOUND SATISFACTORY, SLIDE SECURE AND ARMING MECHANISM OPERATIONS SMOOTH AND POSITIVE.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 90,000 hrs · 10,029 cycles

HYDIM 4 REMOVED FOR TROUBLESHOOTING. ACCOMPLISHED WIRING CHECK FOR SHORTS PER WDM 29-32-11 AND FOUND NO DEFECTS. REPLACED HYDIM CARD SYS4 A23 PRECAUTIONARY PER MM.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 90,000 hrs · 10,029 cycles

HYDRAULIC OVERHEAT SYSTEM MESSAGE ILLUMINATED, RETURNED TO FIELD. REMOVED AND REPLACED THE NR 4 HYDRAULIC CASE DRAIN MODULE TEMPERATURE TRANSMITTER PER AM M 29-32-02. REMOVED AND REPLACED THE EDP AND TWO ADP CASE DRAIN FILTERS PER AMM 29-11-18. OPS TESTED NORMAL. LEAK CHECKED ALL THREE COMPONENTS, NO LEAK.

Part: PIN — BACKED OUT (EXIT SIGN) · airframe 89,332 hrs · 9,958 cycles

UPPER DECK RIGHT DOOR AFT EMERGENCY EXIT SIGN INOP. REPAIRED PUSHED BACK PIN IN POWER CONNECTOR PER MM1. LIGHT CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,332 hrs · 9,958 cycles

DOOR 2R DOOR EMERGENCY LIGHT INOP. RELAMPED 2R DOOR SLIDE LIGHT PER MM. LIGHT VERY DIM, NEEDS BATTERY. RELAMPED WITH CORRECT LIGHT BULB 1317, OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 89,170 hrs · 9,940 cycles

FUEL SYSTEM IRREG, FLT DIVERTED. CAPTAIN FELT UNCOMFORTABLE CONTINUING TO HKG DUE TO FUEL SYSTEM IRREGULARITY. UA895 / C4 ORD HKG WE HAVE A 2.5 DIFF BETWEEN TOT AND CALC FUEL 86.2/88.9

Part: IGNITER — FAULTY (NR 1 ENGINE) · airframe 89,157 hrs · 9,939 cycles

PER CREW ENGINE 1 START ATTEMPT, NO START USING IGNITION NR 1, PER FLT MANUAL, SWITCHED TO 'BOTH' START WAS GOOD-NORMAL. OK TO DEFER ENGINE 1, IGNITION SYSTEM NR 1 'INOP' PER MEL 7400A. OK TO DEFER PER MEL7400A TOMC-EMC. REPLACED NR 1 ENGINE SYS 1 IGNITER PLUG PER MM. AUDIBLE TEST OK AMM 74-00-00. ENG RUN PER JRH USES IGN SYS 1 NORMAL.

Part: O-RING — LEAKING (FUEL SYSTEM) · airframe 89,017 hrs · 9,927 cycles

FUEL LEAKING FROM NR 1 MAIN FUEL TANK FILL VALVE CONTROL UNIT. PCN 685-5121 REFUEL VALVE CONTROL UNIT. REPLACED O-RINGS, NO LEAKS.

Part: UNKNOWN — MALFUNCTIONED (CARGO DOOR) · airframe 89,017 hrs · 9,927 cycles

AFT CARGO DOOR. ACCOMPLISHED POWER OPERATION OF THE DOOR, DOOR OPENED FULLY. WHEN DOOR REACHED FULL OPEN POSITION DOOR OPENING ACTUATOR CONTINUED TO RUN WITH SWITCH HELD TO OPEN POSITION. CYCLED DOOR SEVERAL TIMES AND COULD NOT DUPLICATE REPORTED CONDITION. TRIED TO PERFORM CARGO DOOR PWR SHUTOFF SYS INSP-CHECK PER MM AND WDM. COULD NOT LOCATE RELAY R9423 & R9424 TO VERIFY REF COA84205. REF ECRA5235-01001 AMM 52-34-79 SHOULD READ TO SHOW COA 84205 NO LONGER APPLICABLE RE-DIRECTED TO COA 848790. SYSTEM NOW OPERATES AS DIRECTED.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 88,965 hrs · 9,923 cycles

NR 1 MAIN FUEL TANK CONTINUES TO TAKE FUEL AFTER FUELING COMPLETE AND VALVE INDICATING CLOSED. MANUALLY CLOSED NR 1 TANK FUEL VALVE. NR 1 FUEL VALVE INOP IN CLOSED POSITION PER MEL. FUEL TEAM SUSPECTS REFUEL VALVE CONTROL UNIT IS THE FAULT. NEED PCN 643-0005 REF IPC 28-21 -02-002 ITM 120. REPLACED REFUEL VALVE CONTROL UNIT REF AMM, NO HELP -TANK 1 CONTINUES TO TAKE FUEL AFTER VALVE SHOWS CLOSED. OPS CKD VALVE.

Part: PLATE — LOOSE (R1 DOOR) · airframe 88,965 hrs · 9,923 cycles

THE 1R FWD ENTRY DOOR WILL LATCH CLOSED IN THE OPEN POSITION. CONTROL ARM MOUNT ON DOOR ADJUSTABLE PLATE IS LOOSE AND MOVING AROUND, NOT HOLDING CONTROL ADJUSTMENT. SECURED SERRATED PLATE AND ADJUSTED GUIDE ARM PER AMM.

Part: CONNECTOR — FAULTY (FUEL SYSTEM) · airframe 88,456 hrs · 9,873 cycles

MAIN TANK 1 FUEL QTY FLUX. FOUND A3 CARD FOR CENTER WING SNGLE POINT SENSOR CONTROL GREEN LITE ON CARD FOR CHANNEL A ON AND CHANNEL B OUT. ACCOMPLISHED FIM 28-44 TASK 802 FOR CARD Y5BA3 FAIL. REMOVE REAR SPAR CONNECTOR X1011 FOR IN-TANK WIRING TROUBLESHOOTING. CLEANED CLEANED & REASSEMBLED CONNECTOR X1011. SINGLE POINT SYSTEM CHECK NOW TEST GOOD. Y5B SENSOR CARD RETURNED TO ORIGINAL MR LOCATION.

Part: SMOKE DETECTOR — FAILED (E&E BAY) · airframe 88,456 hrs · 9,873 cycles

E AND E SMOKE DETECTOR FAIL MSG 21501. REPLACED COOLING SMOKE DETECTOR, OP CHECKED OKAY.

Part: ACTUATOR — FAULTY (RT AILERON) · airframe 88,401 hrs · 9,867 cycles

AILERON LOCKOUT. REPLACED RIGHT OUTBOARD AILERON LOCKOUT ACTUATOR PER MM AND RE-RACKED LEFT STAB TRIM RR MODULE. TEST OK PER MM 27-11-00, EICAS MSG CLEARED. REPLACE RIGHT OUTBOARD AILERON LOCKOUT ACT PER MM 27-11-16.

Part: LINE — LEAKING (NR 3 ENGINE) · airframe 88,153 hrs · 9,845 cycles

NR 3 ENGINE FUEL LEAK, TRACED FUEL DRAIN SYSTEM AND FOUND AN ACCUMULATION OF FUEL COMING FROM THE TURBINE CASE COOLING ACTUATOR. REPLACED TURBINE CASE COOLING AIR VALVE ACTUATOR PER MM. DURING ENGINE RUN FUEL STILL DRIPPING FROM NR 1 STRUT DRAIN. FOUND FUEL LINE FROM FUEL-OIL COOLER TO FUEL PUMP LEAKING. REPLACED LINE PER MM. RAN ENGINE FOR 5 MINUTES NO LEAKS FOUND.

Part: SENSOR — DIRTY (CABIN TEMP) · airframe 88,109 hrs · 9,841 cycles

UNABLE CONTROL CABIN TEMP ALL ZONES -TOO HOT. CLEANED TEMP SENSORS.

Part: CONTROLLER — FAULTY (CABIN) · airframe 88,109 hrs · 9,841 cycles

C & D ZONE CABIN LIGHTS WILL NOT SHUT OFF. REPLACED LAC2, OPS CHECK GOOD.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHTS) · airframe 88,037 hrs · 9,833 cycles

EMERGENCY LIGHTS INOPERATIVELOWER. FOUND WATER PUDDLING IN GALLEY AREA UNDER GALLEY MAT AT EMERGENCY LIGHT CONNECTOR SHORTING LIGHTS. DRIED AREA, EMERGENCY LIGHTS OPS CHECKED NORMAL AT PRESENT TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,037 hrs · 9,833 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP IAW AMM, OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,037 hrs · 9,833 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FUSE. LIGHTS OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,037 hrs · 9,833 cycles

EMERGENCY EXIT LIGHT INOPERATIV, REPLACED LAMPS, OPS NORMAL.

Part: WIRE — ARCED (AFT GALLEY) · airframe 87,970 hrs · 9,826 cycles

AFT GALLEY PIGTAIL REPORTED TO BE ARCING JUST PRIOR TO DEPARTURE. FOUND P43 PIGTAIL DAMAGED DUE ARCING WHICH WAS CAUSED BY A DEFECTIVE CART. POSITION HAS BEEN ISOLATED CIRCUIT BREAKER PULLED AND COLLARED. CABLE AND RESET CIRCUIT BREAKER, OPS CHECKED WITH TESTER PASSED.

Part: WINDOW — FAILED (COCKPIT) · airframe 87,649 hrs · 9,793 cycles

CAPTAIN'S L1 WINDOW DELAMINATED BEYOND LIMITS. CREW REPORT, 1.5 INCH CRACK L1 WINDOW LOWER RIGHT CORNER. MOISTURE INGRESS AND BURN MARK. REMOVED AND REPLACED WINDOW ASSY PER MM. GROUND TEST PASSED.

Part: GIRT BAR — OUT OF ADJUST (L5 DOOR) · airframe 87,369 hrs · 9,766 cycles

L5 DOOR DISARMED BY ITSELF DURING FLIGHT. UNABLE TO REARM. ADJUSTED GIRT BAR POSITION AND CLEANED AND LUBED GIRT BAR LOCK AND BRACKET PER AMM 25-69-03.

Part: LENS — MISSING (CABIN) · airframe 87,247 hrs · 9,753 cycles

EEL LIGHT AT SEAT 4K MISSING LENS. REPLACED LENS COVER AT 4K. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,247 hrs · 9,753 cycles

FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED NORMAL .

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 87,247 hrs · 9,753 cycles

EEL LIGHT INOP RIGHT LOWER TWO WING SLIDE ASSY. REPLACED FUSE IN POWER SUPPLY ABOVE DOOR 3R. LIGHT OPS CHECK NORMAL.

Part: LIGHT — FAILED (CABIN) · airframe 87,247 hrs · 9,753 cycles

EMERGENCY LIGHTS DIM FROM ROW 45 UP TO ROW 53 LEFT SIDE AND GALLEY LOWER WALL INOPERATIVE. REMOVED WATER UNDER CARPET AND REPLACED EMERGENCY LIGHT AT LOWER WALL.

Part: DOOR — MALFUNCTIONED (MLG) · airframe 87,025 hrs · 9,731 cycles

GEAR DOOR INDICATION, ACFT RETURNED TO FIELD WHEN BOTH BODY GEAR DOOR DIDN'T STOW. PER CREW THEY CYCLED GEAR, GEAR DROPPED THEN RETRACTED NORMALLY. BODY GEAR DOOR SHOWED IN TRANSIT WHOLE TIME. WHEN ACFT GOT TO GATE BODY GEAR WERE BOTH HANGING DOWN. ACCOMPLISHED AMM. CONFIRMED ALL CHECKS ARE NORMAL.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 86,832 hrs · 9,711 cycles

UPPER DECK DOOR EMERGENCY LIGHT BATTERY NO TEST. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,323 hrs · 9,663 cycles

EMERGENCY EXIT LIGHT INOP DOOR 4 RIGHT FWD DOOR SILL. RELAMPED, OPS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 86,323 hrs · 9,663 cycles

EMERGENCY EXIT EEL LIGHT INOP DOOR 4 RIGHT GALLEY AREA LOWER WALL CROSSAISLE. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 86,323 hrs · 9,663 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 23 LEFT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,323 hrs · 9,663 cycles

EMERGENCY EXIT LIGHT INOP DOOR 4 LEFT AFT SILL LIGHT. RELAMPED, OPS NORMAL.

Part: BATTERY — DISCHARGED (MAIN) · airframe 85,835 hrs · 9,617 cycles

ACFT BATTERY DEAD. REPLACED SHIPS BATTERY IAW MM.

Part: CHARGER — FAULTY (APU BATTERY) · airframe 85,835 hrs · 9,617 cycles

EICAS MESSAGE, APU BATTERY CHARGER. REPLACED APU BATTERY AND APU BATTERY CHARGER PER AMM. OPS CHECKED OKAY.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 85,548 hrs · 9,589 cycles

EEL LTS KEEP FLICKERING ON & OFF AT DOOR 3L AND FROM 23C THRU 25C. REPLACED BATTERY PACK AT DOOR 3L.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 85,548 hrs · 9,589 cycles

THE 24H EEL HAS COME OFF AISLE SIDE OF SEAT. REPLACED EEL ASSY ON SEAT, SYS CHECKS GOOD.

Part: COUPLING — CRACKED (TRANSMITTER) · airframe 85,475 hrs · 9,582 cycles

FLIGHT CONTROL PROBLEM, RTFL. NO EMERGENCY DECLARED. DUMPED 110,000LBS FUEL. POSITION TRANSMITTER REMOVED AND FOUND COUPLING CRACKED, COUPLING REPLACED AND CHECKED NORMAL. POSITION TRANSMITTER REPLACED AND ADJUSTMENT PERFORMED NORMAL.

Part: SERVO VALVE — NO TEST (LT AILERON) · airframe 85,411 hrs · 9,576 cycles

LEFT AILERON SERVO FAILED OPERATIONAL TEST AND FCC BITE TEST. REMOVED SERVO IAW AMM. INSTALLED LT LCCA SERVO VALVE PER AMM. LEAK CHECKED GOOD, FAILED OPERATIONAL TEST WITH CMCS MESSAGE "AILERON SERVO-L, FCC-L INTERFACE FAIL SERVO POSITION 22055." REPLACED CLCP RT WHEEL WELL PER MM. OPS CHECKED GOOD.

Part: LINE — LEAKING (NR 4 ENGINE OIL) · airframe 85,411 hrs · 9,576 cycles

NR ENGINE OIL LINE FROM ACOC TO FCOC LEAKING BEYOND LIMITS. REMOVED LEAKING OIL LINE FROM ACOC TO FCOC. REPLACED OIL LINE. RAN ENGINE AND LEAK CHECKED. NO LEAKS NOTED. SERVICED ENGINE OIL TO FULL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,411 hrs · 9,576 cycles

RIGHT OVERWING AFT TWO EMERGENCY LIGHT ASSY INOPERATIVE. REPLACED BATTERY CHARGER, OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,411 hrs · 9,576 cycles

SEATS 19-22ABC EMERGENCY LIGHTS IS INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,411 hrs · 9,576 cycles

OVER STAIR FWD EMERGENCY LAMP IS INOPERATIVE. RELAMPED EMERGENCY LIGHT. OPS CHECKED OK.

Part: LIGHT — INTERMITTENT (R3 DOOR) · airframe 85,411 hrs · 9,576 cycles

DOOR 3R FWD SILL EMERGENCY LIGHT IS INOPERATIVE. FWD SILL LIGHT OPS CHECKED NORMAL.

Part: VALVE — LEAKING (FUEL DIST) · airframe 85,411 hrs · 9,576 cycles

NR 3 ENGINE FUEL LEAK FROM INSIDE ENGINE SEEPING FROM BOTTOM OF CASE SEAM FROM BELOW HIGH PRESSURE TURBINE. NOTED AFTER PROLONGED GROUND TIME DURING 'A' CHECK. REPLACED FUEL DISTRIBUTION VALVE PER MM. IDLE RUN AND LEAKS CHECKED OK.

Part: LIGHT — MALFUNCTIONED (R3 DOOR) · airframe 85,400 hrs · 9,575 cycles

EMERGENCY EXIT LIGHTS FLICKERING ON AND OFF AT R3 DOOR. CHECKED EMERGENCY LIGHT OPERATION, OK PER MM.

Part: SMOKE GOGGLES — NONE (1ST OBS) · airframe 85,218 hrs · 9,558 cycles

FOUND 1ST OBSERVER'S SMOKE GOGGLES HEADBAND STRETCHED. ADJUSTED HEADBAND ON SMOKE GOGGLE FOR 1ST OBS SEAT. SMOKE GOOGLE IS ACCEPTABLE IAW GMM 05-30-06.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 85,218 hrs · 9,558 cycles

2ND OBSERVER`S SEAT MISSING SMOKE GOGGLES. REPLACED SMOKE GOGGLES.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 85,141 hrs · 9,550 cycles

EMERGENCY LIGHTS, 21C TO 25C, INTERMITTENT ON AND OFF UNCOMMANDED. SECURED CONNECTOR ON POWER SUPPLY ABOVE DOOR 3L, CHECKED OK.

Part: APU — ODOR (POS A) · airframe 85,095 hrs · 9,546 cycles

OIL ODOR FROM APU. REMOVED AND REPLACED APU IAW 49-11-01.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 85,083 hrs · 9,544 cycles

DURING TEST FLIGHT, BOTH PRESSURE RELIEF VALVES DID NOT OPEN AT 9.5 PSID. REPLACED BOTH PRESSURE RELIEF VALVES, OP CHECKED OK ON GROUND REF AMM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BS 1220 SHORT EDGE MARGIN AT FASTENER HOLE CT FRAME AND TENSION TIE JOINT RBL 68 AND WL 337. AD 2007-23-18. REPAIRED IAW 747EN-53-0369. STAGE 2 INSPECTION REQ AT 2,800 CYCLE INTERVAL WITH INITIAL INSP THRESHOLD AT 12,343 TOTAL AIRFRAME CYCLES. TEXT INCOMPLETE. SEE EVA 81547.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

FUSELAGE DAMAGED 4FT BELOW F/O'S NR 2 WINDOW, INLINE WITH WINDOW AND AOA SENSOR. DENT IS 2.5 INCHES LONG AXIS AND .125" IN DEPTH. CTR HAS CREASE OR GOUGE. DAMAGE IS APPROX STA 297 BETWEEN RT STRINGER 14 & S14-D WITH NO FRAME CONTACT. CUT OUT DAMAGE TO 1 INCH FOR PREPARATION FOR SRM 53-00-01 REPAIR 7. CONT OF AMIS ITEM 2382014 :ACP HFEC FOR DAMAGE REMOVAL. VERIFIED ALL DAMAGE REMOVED. REPAIRED PER SRM 53-00-01 REPAIR 7 TIME LIMITED EXTERNAL REPAIR REQUIRES RECHECK AT 1000 CYCLES AND REPLACEMENT AT 6000 CYCLES REPAIRED IAW 747EN- 53-0367." HFEC, NO CRACK. MFG AND INSTALLED REPAIR.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

STA 1140 RT SIDE FAIL SAFE CHORD 2 EACH HOLES CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. HFEC, NO CRACK. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-40-07 REPAIR 2 (EFS PG 24-32).

Part: FLOORBEAM — PUNCTURED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

FWD PIT BS 580 LBL 7 CARGO FLOORBEAM WEB PUNCTURE. REPAIRED IAW 747EN-53-0363. REPAIR IS TIME LIMITED UNTIL PTC 20,000. FULL COMPLIANCE TO 14CFR HAS NOT BEEN EVALUATED. A NEW FAA APPROVAL MUST BE ISSUED PRIOR TO PTC 20,000 OR AIRWORTHINESS CERTIFICATE IS NO LONGER VALID. TEXT INCOMPLETE. SEE EVA 81552.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

STA 1140 LT SIDE FAILSAFE CHORD 2 EACH HOLES CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. HFEC, NO CRACK. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-40-07 REPAIR 2 (EFS PG 24-32).

Part: BEAM — CRACKED (L4 DOOR) · airframe 85,080 hrs · 9,543 cycles

L4 DOOR UPPER EDGE BEAM WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED IAW 747EN-52-0050.

Part: CHANNEL — CRACKED (BS 1140) · airframe 85,080 hrs · 9,543 cycles

BS 1140 LT TENSION TIE FWD CHANNEL CRACKED AT 2 FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, SPLICED IN NEW SECTIONS OF CHANNEL, REPAIR 1.

Part: BEAM — CRACKED (BS 1120) · airframe 85,080 hrs · 9,543 cycles

BS 1120 LBL 5, CANTED BEAM WEB CRACKED BELOW FLOORLINE. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB.

Part: STRAP — CRACKED (L2 DOOR) · airframe 85,080 hrs · 9,543 cycles

LEFT NR 2 MED COVER CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED REPAIR STRAP REF 747EN-52-0043.

Part: CHANNEL — CRACKED (BS 1140) · airframe 85,080 hrs · 9,543 cycles

BS 1140 RT TENSION TIE FWD CHANNEL CRACKED AT 2 FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTIONS OF CHANNEL REF SRM.

Part: FLOORBEAM — CORRODED (BS 980) · corrosion level 2 · airframe 85,080 hrs · 9,543 cycles

UPPER DECK BS 980 FLOORBEAM FAIL SAFE STRAP CORRODED RBL 26 TO 34. MAJOR REPAIR ACCOMPLISHED. REPAIRED IAW 747EN -53-0366. REPAIR ACCOMPLISHED IAW EVA 81548.

Part: SKIN — CRACKED (APU BATTERY DOOR) · airframe 85,080 hrs · 9,543 cycles

APU BATTERY ACCESS DOOR AFT EDGE EXTERIOR SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER REF AMECO EN 747EN-52-0051 & FAA FORM 8100-9.

Part: PLATE — MISMANUFACTURED (BS 1180) · airframe 85,080 hrs · 9,543 cycles

BS 1180 RT TENSION TIE STEEL PLATE HAS SHORT EDGE MARGIN AT 3 FASTENER HOLES AFTER RPR TO TENSION TIE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED NEW STEEL PLATE.

Part: CHANNEL — CRACKED (BS 1180) · airframe 85,080 hrs · 9,543 cycles

BS 1180 RT TENSION TIE FWD CHANNEL CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED NEW CHANNEL SECTIONS.

Part: SKIN — MISREPAIRED (BS 460 S14-16L) · airframe 85,080 hrs · 9,543 cycles

BS 460 SKIN BETWEEN S14L & S16L MISREPAIRED. MAJOR REPAIR ACCOMPLISHED. REPAIRED IAW 747EN-53-0368.

Part: SKIN — DAMAGED (BS 460 S14-16R) · airframe 85,080 hrs · 9,543 cycles

BS 460 SKIN BETWEEN S14R & S16R HAS SHORT EDGE MARGIN. MAJOR REPAIR ACCOMPLISHED. REPAIRED IAW AMECO 747EN-53-0365.

Part: FRAME — MISREPAIRED (BS 1265) · airframe 85,080 hrs · 9,543 cycles

BS 1265 LT FRAME INNER CHORD AND WEB HAS SHORT EDGE MARGIN 4 LOCATIONS. REPAIRED IAW 747EN- 53-0364.

Part: SKIN — MISREPAIRED (BS 460) · airframe 85,080 hrs · 9,543 cycles

BS 460 SKIN MISREPAIRED, BETWEEN S14R & S16R. HAS SHORT EDGE MARGIN. MAJOR REPAIR ACCOMPLISHED. REPAIRED IAW 747EN-53-0365.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1200 RT TENSION TIE FWD CHANNEL CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE & INSTALLED REINFORCING ANGLE REPAIR.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1160 LT TENSION TIE FWD CHANNEL CRACKED AT 2 FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING REPAIR DOUBLER, RPR 1.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1120 LT TENSION TIE FWD CHANNEL CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING REPAIR ANGLE, RPR 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1265 FRAME WEB CRACKED AT FASTENER HOLE APPROX 6 INCHES ABOVE FLOORLINE AT DOORWAY 3L. MAJOR REPAIR ACCOMPLISHED. REPLACED BS 1265 LT FRAME INNER CHORD, WEB, AND INTERCOSTAL UPPER CHORD & WEB PER COA TASK CARD 897887102.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1180 LT TENSION TIE FRAME CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME SECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1160 RT TENSION TIE FRAME CRACKED AT 4 FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME SECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1200 RT TENSION TIE FRAME CRACKED AT 2 FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME SECTION.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1180 LT TENSION TIE FWD CHANNEL CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE & INSTALLED REINFORCING ANGLE REPAIR.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 1160 RT TENSION TIE FWD CHANNEL CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE & INSTALLED REINFORCING ANGLE REPAIR, RPR 1.

Part: BEAM — DAMAGED (RT WING) · airframe 85,080 hrs · 9,543 cycles

RIGHT WING FIXED T/E BEAM UPPER CHORD LUG BORE DAMAGED AT WBL 235.2. REPAIRED IAW 747 EN-57-0187. REPAIR IS AN INTERIM REPAIR AND DVI FOR BEARING INSTALLATION AT WBL 235.20 MUST BE ACP AT 1C INTERVAL, NOT TO EXCEED 24 MONTHS. THIS CF CAN CLEAR ONCE EC IS CREATED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

FUSELAGE DAMAGED 4 FEET BELOW F/O'S NR 2 WINDOW, INLINE WITH WINDOW AND AOA SENSOR. DENT IS 2.5' LONG AXIS AND .125\ IN DEPTH. CTR HAS CREASE OR GOUGE. DAMAGE IS APPROX STA 297 BETWEEN RT STRINGER 14 & S14-D WITH NO FRAME CONTACT. CUT OUT DAMAGE TO 1\ FOR PREPARATION FOR SRM53-00-01 REPAIR 7. ACP HFEC FOR DAMAGE RMVL. VERIFIED ALL DAMAGE REMOVED. REPAIRED PER SRM 53-00-01 REPAIR 7 TIME LIMITED EXTERNAL REPAIR REQUIRES RECHECK AT 1000 CYCLES AND REPLACEMENT AT 6000 CYCLES. ** MF1596 CREATED TO MONITOR **^08NOV SFO INF- :CURRENT PTC 7803. REPAIRED IAW 747EN- 53-0367.

Part: SKIN — DENTED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

FUSE DENT 4 FEET BELOW F/O'S NR 2 WINDOW, INLINE WITH WINDOW AND AOA SENSOR. APPROX STA 297 BETWEEN S14 & S14D. REF PTT SEQ 0802018. REPAIRED IAW AMECO 747EN-53-0367. PER EVA 81484, INSP SKIN AROUND FIRST ROW OF FASTENERS ALONG EDGE OF DOUBLER AS SHOWN IN SRM 53-00-01 REPAIR 1 DETAIL III AT 6000 FC WITH INT HFEC OR AT 1500 FC WITH EXT LFEC. INSP THRESHOLD 24543 PTC. ONCE EC IS PUBLISHED, CF CAN BE CLEARED. REF: TABLE IV OF SRM.

Part: DOOR FRAME — CRACKED (L4 DOOR) · airframe 85,080 hrs · 9,543 cycles

NR 4 LT MED: UPPER DOOR FORMED FRAME AT GATE HINGE ATTACH HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, HFEC, MFG AND INSTALL REPAIR IAW AMECO EN-52-0050. PER EN PAGE 4 AND MM 51-00-80 PG 204 NOTE 5.B.2 AND NOTE D.2.B, 'UNSURVEYED RSCS MAY ONLY BE INSTALLED ONTO SURVEYED AIRPLANES FOR UP TO 24 MONTHS. PRIOR TO LIMIT, EITHER SURVEY PER AMM 51-00-80 OR REMOVE PART FROM AIRPLANE PRIOR TO 24 MONTH EXPIRATION'.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

BODY STATION 140 BULKHEAD OUTER CHORD CRACKED IN RADIUS AT STR 19L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED NEW ANGLE, BRACKETS & FILLERS REF AMM.

Part: DOOR FRAME — CRACKED (L4 DOOR) · airframe 85,080 hrs · 9,543 cycles

LEFT NR 4 ENTRY DOOR FRAME CRACKED AT AFT UPPER CORNER. STOP DRILL. HFEC MFG AND INSTALL REPAIR IAW SRM. INSP REQ AT 3000 DOOR FLIGHT CYCLES AFTER REPAIR. RII INSP ACP ON NON ROUTINE 0259942.

Part: DOOR FRAME — CRACKED (L4 DOOR) · airframe 85,080 hrs · 9,543 cycles

LEFT NR 4 ENTRY DOOR FRAME CRACKED AT FWD LOWER CORNER. STOP DRILL. MFG & INSTALL REPAIR IAW SRM 52-10-02. PER SRM, PG 206 (EFS PG 33), INSP REQ AT 3000 DOOR FLIGHT CYCLES AFTER REPAIR.

Part: DOOR FRAME — CRACKED (R4 DOOR) · airframe 85,080 hrs · 9,543 cycles

RIGHT NR 4 ENTRY DOOR FRAME CRACKED AT AFT UPPER CORNER. STOP DRILL. HFEC. MFG & INSTALL REPAIR IAW SRM 52-10-02. PER SRM PG 206 (EFS PG 33), INSP REQ AT 3000 DOOR FLIGHT CYCLES AFTER REPAIR. ** MF8309 CREATED TO MONITOR **. ACCOMPLISH RII INSPECTION OF AMIS ITEM 0802009. STOP DRILL. HFEC. MFG & INSTALL REPAIR IAW SRM 52-10-02. PER SRM PG 206 (EFS PG 33), INSP REQ AT 3000 DOOR FLIGHT CYCLES AFTER REPAIR. INSP ACP ON NON ROUTINE 0259943.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

NR 1 RT MED CUTOUT BS 460 CRACK. REPAIR INSTALLED USING ROUTINE JOB CARD 895244020.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 85,080 hrs · 9,543 cycles

NR 1 LT MED CUTOUT BS 460 CRACK. REPAIR INSTALLED USING ROUTINE JOB CARD 895244010.

Part: DOOR FRAME — CRACKED (R4 DOOR) · airframe 85,080 hrs · 9,543 cycles

NR 4 RT MED CRACK ON FRAME AT LOWER AFT CORNER. STOP DRILLED. HFEC MFG AND INSTALL REPAIR IAW SRM 52-10-02 REPAIR 2. PER SRM, INSPECTIONS REQUIRED EVERY 3000 CYCLES (PG 206 - EFS PG 28 & 33). ON NON ROUTINE 0259944. ** MF8291 CREATED TO MONITOR **

Part: DOOR FRAME — CRACKED (L4 DOOR) · airframe 85,080 hrs · 9,543 cycles

NR 4 LT MED CRACK ON FRAME AT UPPER AFT CORNER. STOP DRILLED. HFEC MFG AND INSTALL REPAIR IAW SRM 52-10-02 REPAIR 2. PER SRM, INSPECTIONS REQUIRED EVERY 3000 CYCLES. (PG 206 - EFS PG 28 & 33). ON NON ROUTINE 0259942. ** MF8290 CREATED TO MONITOR **

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 85,080 hrs · 9,543 cycles

NR 4 LT MED CRACK ON FRAME AT LOWER FWD CORNER. STOP DRILLED. HFEC MFG AND INSTALL REPAIR IAW SRM 52-10-02 REPAIR 2. PER SRM, INSPECTIONS REQUIRED EVERY 3000 CYCLES (PG 206 - EFS PG 28 & 33). ** MF8289 CREATED TO MONITOR **

Part: SKIN — DENTED (BS 1830 S35-36L) · airframe 85,080 hrs · 9,543 cycles

SKIN AT BS 1830 S35-36L, DENTED. PERFORMED HFEC, NO CRACK FOUND. DENT MEASURES A=0.58" X 0.0157. A-Y=37. WITHIN LIMITS IAW SRM.

Part: PA SYSTEM — NOISY · airframe 84,976 hrs · 9,531 cycles

CAPT USED EMERGENCY AUTH TO STOP EXCESSIVE NOISE IN 1ST CLASS BY PULLING J9 C/B. CYCLED J9 CB FOR 30 SEC DID NOT FIX THE BUZZING 1ST CLASS SPEAKERS. LEAVING IT OUT FIXED IT. RESET PA AMP, ACCOMPLISHED DATA BASE DOWNLOAD, ALL OPS NOW NORMAL.

Part: FEEDER CABLE — FAULTY (CABIN) · airframe 84,848 hrs · 9,518 cycles

EEL LIGHTS FROM ROW 45C TO 53C INOP. REPLACED FEED IN CABLE.

Part: CABLE — INOPERATIVE (CABIN) · airframe 84,848 hrs · 9,518 cycles

EEL LIGHT AT ROW 42C INOP. REPLACED SEAT CABLE FOR SEAT ROW 42ABC, EEL LIGHTS OPERATE NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,713 hrs · 9,502 cycles

LOCATION 421, BUSINESS AUX GALLEY, LIGHT ABOVE MOVEABLE BIN INOP. BULB REMOVED. FOUND ONE LAMP STILL INSTALLED, SOCKET BURNT AND LAMP WELDED TO SOCKET. REPLACED LIGHT ASSY, OPS CHECKED OKAY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,423 hrs · 9,468 cycles

'C' ZONE ALL CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,423 hrs · 9,468 cycles

DOOR 2 LEFT SLIDE LIGHT INOPERATIVE. RELAMPED DOOR 2LT LIGHT.

Part: CAP — LOOSE (NR 1 SQUIB) · airframe 84,339 hrs · 9,458 cycles

NR 1 ENG NR 1 SQUIB WILL NOT TEST. SECURED NR 1 ENG SQUIB TEST BULB CAP.

Part: SEAL — DAMAGED (LT WLG DOOR) · airframe 84,312 hrs · 9,456 cycles

BULB SEAL DAMAGED WHERE WLG DOOR SEALS ON WHEEL WELL NOT DOOR. INSTALLED NEW PIECE OF BULB SEAL AT LT WLG DOOR FRAME CUTOUT.

Part: LIGHT — MISSING (CABIN) · airframe 84,118 hrs · 9,432 cycles

THE 36C SEAT MOUNTED EEL LIGHT MISSING. REPLACED SEAT MOUNTED EEL LIGHT.

Part: OXYGEN SYSTEM — LOW (CREW O2) · airframe 83,928 hrs · 9,410 cycles

OXYGEN PSI DROP. SERVICED CREW O2.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 83,843 hrs · 9,402 cycles

OVERWING RT 2 BOTTOM EMERGENCY LIGHT INOP. REPLACED FUSE ON BATTERY CHARGER. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,843 hrs · 9,402 cycles

AFT WALL LT EMERGENCY LIGHT ALONG DOOR 5C INOP. REPLACED EMERGENCY LIGHT RIBBON. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,843 hrs · 9,402 cycles

EMERGENCY LIGHT ROW 39 LIGHT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 83,524 hrs · 9,365 cycles

EMERGENCY FLOOR LIGHTING ROWS 19-22C ON DURING FLIGHT. CHECKED ALL EMERGENCY LIGHTS AFTER RESETTING THE GUARD AT L1. ALL OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 83,291 hrs · 9,342 cycles

DOOR 2 LEFT SLIDE LIGHT INOP. RELAMPED DOOR 2L SLIDE.

Part: FEEDER CABLE — FAULTY (CABIN) · airframe 83,291 hrs · 9,342 cycles

EMERGENCY EXIT EEL LIGHTS INOP FWD STAIRWELL LOWER EEL LIGHTS AND TOP OF STAIRS LOWER AISLE EEL LIGHTS. REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (R3 DOOR) · airframe 83,291 hrs · 9,342 cycles

DOOR 3 RIGHT SLIDE LIGHT INOP. RELAMPED DOOR 3R SLIDE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,067 hrs · 9,318 cycles

LT UPPER DECK DOOR SLIDE ILLUMINATION LIGHTS INOP. INOPED DOOR PER MEL. REF WD & RELAMPED L2927 AND L2930, NO HELP. SUSPECT M7027 NEEDS NEW BATTERY. REPLACED LEFT BATTERY PACK M7027 REF WD, TEST OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 83,016 hrs · 9,312 cycles

EEL STRIP IS MISSING AT 36C. REPLACED LIGHT STRIP PER MM, OPS CHECKS OKAY.

Part: SENSOR — DEFECTIVE (COCKPIT WINDOW) · airframe 82,836 hrs · 9,294 cycles

REPEAT WINDOW 2R HEAT FAULTS, MANEUVER WIRING AT S761 & S1028 ENSURE VOLTAGE READING DOES NOT FLUCT AND GND REMAINS STEADY. IF 115VAC NOT AT "B" CHK S1028 & S761 FOR OPEN. IF GND NOT AVAIL AT "A" SUSPECT R7338 DEFECTIVE. IF PWR & GND OK OPEN CB C69, DISC WIRING AT "A&B" ON WDO & CHK RESISTANCE OF WDO 2R PER FIM 30-40 FAULT TREE BOX 5. IF NO FAULT FOUND. REPLACE S761 & S1028. SEE HIST FOR PREV ACTIONS. COMPLETED ALL CHECKS AND MEASURMENTS ALL OK, REPLACED S761 AND S1028 OF WINDOW 2R.

Part: WINDOW — FAULTY (COCKPIT) · airframe 82,836 hrs · 9,294 cycles

WINDOW 3R HEATER WIRE CONNECTION B MOUNTING STUD BURNT AND PULLED OUT OF WINDOW. UPPER FWD CORNER. COMPLETED 3 RIGHT WINDOW CHANGE THROUGH END OF TASK. REPLACED 3R WINDOW IAW MM AND TESTED. OPERATES NORMAL.

Part: BRACE — DAMAGED (NR 2 COWLING) · airframe 82,801 hrs · 9,290 cycles

NR 2 ENG CORE COWL STRUCTURAL BRACE IS CONTACTING OIL TUBE SUPPORT BRACKET ON BOTH LEFT AND RIGHT SIDES. AREA OF DAMAGE IS BELOW AFT HOLD OPEN ROD MOUNT BRACKET. REMOVED DOUBLER AT COWL HOLD OPEN ROD AT I/B AND O/B COWLS AND DUPLICATED PER BOEING DRAWING. NEEDS MORE WORK AND PRIMING. TRIMMED, DRILLED, PRIMED, ALODINED AND INSTALLED MFG 2 PIECE DOUBLER. WAITING FOR EVA FROM O (PARTIAL). REPAIRED PER UA-EVA-80715 AND UA-EVA-80717 RT AND LT CORE COWLS RESPECTFULLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,713 hrs · 9,280 cycles

SEAT 54HJK EMERGENCY LIGHT INOP. REPLACED SEAT 54HJK EMERGENCY LIGHT. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,713 hrs · 9,280 cycles

UPPER DECK CEILING EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,713 hrs · 9,280 cycles

DOOR 2L SLIDE EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,166 hrs · 9,216 cycles

ZONE 'D' RIGHT SIDE CEILING EMERGENCY LIGHT INOP. RELAMPED. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 37ABC) · airframe 82,166 hrs · 9,216 cycles

SEAT 37ABC EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY SEAT LIGHT AT 37ABC, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,166 hrs · 9,216 cycles

UPPER DECK CEILING EMERGENCY LIGHT NEAR STAIRS IS INOP. RELAMPED BULBS, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (5R DOOR SLIDE) · airframe 82,166 hrs · 9,216 cycles

DOOR 5R SLIDE EMERGENCY LIGHT INOP. REPLACED DOOR 5R EMERGENCY LIGHT ASSY, OPS CHECKED NORMAL.

Part: RESERVOIR — OUT OF TOLERANCE (EMERGENCY EXIT) · airframe 82,166 hrs · 9,216 cycles

LEFT UPPER DECK DOOR EMERGENCY BOTTLE SQUIB IS OUT OF DATE. INSTALLED EMERGENCY POWER RESERVOIR AS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,166 hrs · 9,216 cycles

DOOR 2R SILL EMERGENCY LIGHT IS INOP. RELAMPED. CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,069 hrs · 9,088 cycles

OVERWING RT AFT 2 INOP. REPLACED BATTERY CHARGER. OP CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,069 hrs · 9,088 cycles

EMERGENCY LIGHT ROW 52 LT INOPERATIVE. RELAMPED. OPS CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,069 hrs · 9,088 cycles

CEILING EMERGENCY LIGHT ABOVE ROW 60 RT INOP. RELAMPED. OP CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,026 hrs · 8,973 cycles

ROW 22 SEAT HJK EMERGENCY LIGHT INOPERATIVE. RELAMPED.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 80,026 hrs · 8,973 cycles

RT SIDE BOTTOM (2) DOOR SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. OPS ARE NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 80,026 hrs · 8,973 cycles

ROW 19 SEAT HJK EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTION.

Part: NOSE COWL — DAMAGED (NR 4 ENGINE) · airframe 79,837 hrs · 8,950 cycles

NR 4 ENG NOSE COWL DAMAGED AT 0430 POS.

Part: PIN — INSTALLED (MLG DOOR) · airframe 79,447 hrs · 8,906 cycles

UPON T/O, GEAR DISAGREE MSG, GEAR DOOR. HM FAULTS BOTH PRIM AND ALT L BODY GEAR DOOR. F/A REPORTED AIR NOISE BY WHEEL WELL AREA. FOUND LT BODY GEAR PIN INSTALLED NEED TO REMOVE BEFORE FLT. REMOVED LT BODY GEAR SAFETY PIN. ACCOMPLISHED SUCCESSFUL GROUND TEST OF THE PSEU. STATUS MESSAGES CLEARED.

Part: LIGHT — INOPERATIVE (SEAT 20L) · airframe 79,445 hrs · 8,905 cycles

SEAT 20L EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY STRIP LIGHT, OP CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,445 hrs · 8,905 cycles

DOORS 2L 2R CROSS AISLE LT EMERGENCY LIGHT INOPERATIVE. RELAMPED.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 79,445 hrs · 8,905 cycles

RT OVERWING AFT LOWER EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,445 hrs · 8,905 cycles

AFT GALLEY LIGHT, SEATS 45-53, DOOR 4L FWD, DOOR 5R AFT EMERGENCY LIGHTS INOP COMMON PROBLEM. RELAMPED, CHECKS OK.

Part: LIGHT — DAMAGED (CABIN) · airframe 78,897 hrs · 8,844 cycles

EMERGENCY EXIT LIGHT 2R BELOW LAV 102 HAS DAMAGE. LIGHT WORKS OKAY. NEEDS TO BE REMOUNTED. TAPED IN PLACE. NOT ENOUGH TIME TO REPAIR LIGHT, FELL OUT RETAPED IN PLACE. SECURED LIGHT FIXTURE.

Part: GIRT BAR — LOOSE (EVAC SLIDE) · airframe 78,734 hrs · 8,826 cycles

DOOR 5L GIRT BAR FOUND HANGING LOOSE ON 3SVC DOOR CHECK. FOUND GIRT BARE SLIDER LOOSE, REPOSITIONED SLIDE AND OPS CHECK OF DOOR ARMING AND DISARMING OK.

Part: SLIDE — UNSERVICEABLE (R5 DOOR) · airframe 78,734 hrs · 8,826 cycles

DOOR 5R GIRT BAR AND MATERIAL HANGING OUTSIDE WHEN DOOR CLOSED. REPLACED SLIDE. INSPECTED SLIDE INSTALLATION. WITNESSED SLIDE PIN REMOVED & BOTTLE PIN REMOVED.

Part: WINDOW — LEAKING (COCKPIT) · airframe 78,696 hrs · 8,818 cycles

WINDOW AIR LEAK AND POPPING NOISE. REPLACED L2 WINDOW. PERFORMED PRESSURIZATION GROUND CK. NO AIR LEAK NOTED.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 78,669 hrs · 8,814 cycles

EEL LIGHTS FLASH AT ROWS 33HJK TO 43HJK. REPLACED M6009 PWR SUPPLY. SYSTEM OP'S CHECKED GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 78,478 hrs · 8,789 cycles

UPPER DECK CEILING AT EMERG EXIT DOORS, EMERGENCY EXIT SIGN WILL NOT STAY ILLUMINATED. REPLACED BATTERY PACK, OPS CHECK OK REF AMM.

Part: DOUBLER — CRACKED (BS 2491-2521) · airframe 78,478 hrs · 8,789 cycles

FOUND RT UPPER LOBE DOUBLER CRACKED FROM BS 2491 TO 2521, COMMON TO VERT STABILIZER. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLERS, SHEAR TIES, & STIFFENERS ON LT & RT SIDES OF ACFT.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 78,478 hrs · 8,789 cycles

'C' ZONE CEILING EMERGENCY EXIT LIGHTS WILL NOT STAY ILLUMINATED. REPLACED BATTERY PACK ABOVE SEAT ROW 21 CTR. LIGHTS OPS CHECK OK.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 78,478 hrs · 8,789 cycles

MID-LAV EMERGENCY EXIT LIGHTS WILL NOT STAY ILLUMINATED. REPLACED BATTERY PACK, LIGHTS OP CHECK OK.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 78,478 hrs · 8,789 cycles

DOOR 3R UPPER SILL, EMERGGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,478 hrs · 8,789 cycles

EMERGENCY LIGHTS INOP 'D' ZONE RT SIDE. REPLACED BATTERY PACK. OP CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,478 hrs · 8,789 cycles

EMERGENCY LIGHT INOP ON LAV 111 FRONT WALL. RELAMPED, OP CHECK OKAY.

Part: WIRE — FAULTY (EMERGENCY LIGHT) · airframe 78,478 hrs · 8,789 cycles

EMERGENCY LIGHT CABLES AND CONNECTOR BROKEN AT SEAT ROW 25R TO LAV 112 SIDE WALL. REPLACED EMERGENCY LIGHT WIRING AND CONNECTOR, OP CHECK OKAY.

Part: SKIN — CRACKED (BS 237.2 S15L) · airframe 78,478 hrs · 8,789 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT FASTENER HOLE, BS 237 2 STR 15L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, INSTALLED EXTERNAL DOUBLER.

Part: CONNECTOR — FAULTY (EMERGENCY LIGHT) · airframe 78,478 hrs · 8,789 cycles

EMERGENCY LIGHT INOP AT SEAT 36C. REPLACED CONNECTOR & CONTACTS UNDER EMERGENCY LIGHT CABLE, OP CHECK OKAY.

Part: FEEDER CABLE — SHORTED (EMERGENCY LIGHTS) · airframe 78,478 hrs · 8,789 cycles

GREEN EMERGENCY STRIP LIGHT ON SIDE WALL FWD OF DOOR 4L. FOUND SHORT IN EMERGENCY LIGHT WIRING, REPLACED EEL CABLES FROM SEAT 45L TO G5 GALLEY. OP CHECK OKAY.

Part: PANEL — DAMAGED (RT WING) · airframe 78,326 hrs · 8,771 cycles

RT WING LE SECOND PANEL INBD OF NR 4 ENG HAS 1 RIVET MISSING FROM INBD EDGE OF PANEL. REPLACED 3 DAMAGED RIVETS ON LE PANEL NR14 AT RT 822 ILES, IAW UA-EVA-72940 A.

Part: PANEL — DAMAGED (LT WING) · airframe 78,326 hrs · 8,771 cycles

LT WING L/E PANEL JUST INBD OF NR 2 ENGINE HAS 3 MISSING RIVETS ON INBD EDGE OF PANEL. REPLACED 3 DAMAGED RIVETS ON L/E PNL NR 5 LT 630 ILES, IAW UA-EVA-72940A.

Part: PANEL — DAMAGED (RT WING) · airframe 78,326 hrs · 8,771 cycles

RT WING L/E: SECOND PANEL INBD OF NR 3 ENGINE HAS 1 RIVET MISSING ON INBD EDGE OF PANEL. REPLACED 1 DAMAGED RIVET ON L/E PNL NR 10, RT 302 ILES, IAW UA-EVA-72940 A.

Part: INSERT — UNSECURE (EMERGENCY LIGHT) · airframe 78,251 hrs · 8,761 cycles

LAV 101 OUTSIDE LWR EMERGENCY LIGHT HSG HAS COME AWAY. MOUNTING INSERTS PULLED AWAY. EPOXY REPAIR CARRIED OUT AND EMERGENCY LIGHT HOUSING RESECURED.

Part: BOLT — IMPROPER PART (DOOR SILL) · airframe 77,776 hrs · 8,712 cycles

UPPER DECK LT SLIDE SILL HINGE BOLTS ARE WRONG PARTS. ENGINEERING HAS UPDATED THE ONLINE IPC 26-68-01-001 TO INCLUDE NAS6706D-28 INSTALLED 2(EA) ON LT UPPER DECK SLIDE SILL HINGE. ACCOMPLISHED INSP OF CORRECT HARDWARE INSTALLED.

Part: LIGHT — LOOSE (CABIN) · airframe 77,476 hrs · 8,678 cycles

LOWER EEL LIGHT, ON LAV CORNER, JUST FWD OF DOOR 2R, IS BROKEN FREE OF IT'S MOUNT. ACP INTERIM REPAIR, USING TAPE, SO AS TO NOT BLOCK THE LIGHT. THE EEL LIGHT. FUNCTIONS NORMALLY. FOUND LWR CORNER EEL LT TRIM SECURED IN PLACE.

Part: STRUCTURE — DAMAGED (NR 16 KRUEGER) · airframe 77,388 hrs · 8,668 cycles

NUMBER 16 LE KRUEGER FLAP DAMAGED AND MISSING CORNER DUE TO BIRD STRIKE. (INBD OF NR 3 ENGINE). SUPPLEMENTAL DATA UPDATE REMOVED NR 16 KRUEGER FLAP. INSTALLED ROBBED FLAP & TORQUED. COULD NOT RIG DUE TO FLAP OUTBOARD EDGE INTERFERRING WITH PYLON, WILL NEED TRIMMING. FLAP TORQUE TUBE DISCONNECTED. RPLC'D BULL NOSE ON KRUEGER FLAP. CONNECTED AND SECURED ALL CONNECTIONS AND RIGGED, OPS CK OK. ACP'D RII INSP.

Part: SKIN — DAMAGED (KRUEGER FLAP) · airframe 77,388 hrs · 8,668 cycles

NR 15 L/E KRUEGER FLAP HAS SURFACE DAMAGE, APPROX 4 SQ INCHES DUE TO BIRD STRIKE (2ND I/B OF NR 3 ENG). REMOVED NR 15 KRUEGER FLAP. INSTALLED ROBBED FLAP, BOLTS ARE NOT TORQUED AND BONDING STRAPS ARE NOT CONNECTED. COMPLETED TORQUE OF NR 15 KRUEGER FLAP. RIGGED FLAP TO DIMENSIONS. WILL NEED FINAL FIT CHECK AFTER OPERATING FLAPS. FLAP ON P/N 65B3 9250-10, S/N 000133. SECURED ALL CONNECTIONS. OPS CHECKED FLAPS CHECKED OKAY.

Part: STRUCTURE — DAMAGED (RT HORIZ STAB) · airframe 73,069 hrs · 8,191 cycles

RT HORIZONTAL STABILIZER AFT UPPER CHORD, STATION 2590, RBL 43.5 A FASTENER HOLE WAS FOUND DAMAGED DURING COA 850111. OVER-SIZED HOLE TO APPROXIMATELY 0.469 INCHES & INSTALLED BOLT WITH NUT IAW UA-EVA-72110 & FAA FORM 8100-9. (DIFFICULTY DATE SUBMITTED AS 11/10/2008)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,958 hrs · 8,618 cycles

EEL LIGHTS ARE INOP FROM DOOR 4L TO ROW 45 AND GALLEY WALL ALSO EXIT LIGHTS AT DOOR 4L AND 4R. ORDERED LIGHT ASSYS. REMOVED AISLE LIGHT & DISCONNECTED FEEDER ALL OTHER LIGHTS NOW OKAY. REPLACED EEL LIGHTS L9025, 3 EA.

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 76,958 hrs · 8,618 cycles

EEL INOP AT DOOR 4R, AISLE WALL NEXT TO GALLEY. REPLACED LIGHT L9025.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 76,759 hrs · 8,596 cycles

EMERGENCY LIGHT DOOR 4R AFT LWR WALL INOPERATIVE. REPLACED AFT FEED CABLE.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 76,759 hrs · 8,596 cycles

RIGHT WING BODY FAIRING AFT 2 EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE CHECKS OKAY.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 76,759 hrs · 8,596 cycles

EMERGENCY COCKPIT OVERHEAD LIGHT INOPERATIVE, OPS NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 76,759 hrs · 8,596 cycles

EMERGENCY EXIT LIGHTS INOP SEAT ROWS 45 TO 53 LEFT DOOR 4L FWD EXIT SIGN DOOR 4R AFT EXIT SIGN, LWR WALL EEL ACROSS DOOR 4L AND DOOR 4 GALLEY AREA LWR WALL EMERGENCY LIGHT. THIS IS REPETITIVE PROBLEM IN THIS AREA FOR ACFT 84XX ACFT OUT OF INTERIOR MODIFICATION. RE-SECURED LOOSE CONNECTOR IN GALLEY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,759 hrs · 8,596 cycles

EMERGENCY LIGHT MISSING ON SEAT 57 RT. RELAMPED, CHECKS OKAY.

Part: WIRE — SEVERED (CABIN) · airframe 76,629 hrs · 8,582 cycles

EEL LIGHT ON 39C HAS SEVERED WIRES. REPLACED CABLE. TESTS OKAY.

Part: O-RING — DAMAGED (APU) · airframe 76,407 hrs · 8,558 cycles

HEAVY OIL SMELL IN CABIN WITH APU RUNNING. FOUND OIL FILTER HOUSING LEAKING, REPLACED O-RING, NO LEAKS NOTED. SERVICED APU TO FULL, REPLACED COALESCER BAGS AND RAN APU. OIL QUANTITY DROPPED TO 50 PERCENT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,257 hrs · 8,541 cycles

EMERGENCY LIGHT LIGHT INOP AT SEAT 34 ABC. RELAMPED EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (SEAT 36 ABC) · airframe 76,257 hrs · 8,541 cycles

EMERGENCY LIGHTS INOP AT 36 ABC. RELAMPED EMERGENCY LIGHTS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,257 hrs · 8,541 cycles

RIGHT SIDE EMERGENCY BOTTOM 2 SLIDE LIGHTS INOPERATIVE. RELAMPED EMERGENCY LIGHTS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,257 hrs · 8,541 cycles

UPPER DECK TOP OF STAIRS TWO EMERGENCY LIGHTS INOP. RELAMPED EMERGENCY LIGHTS.

Part: SLIDE — UNSERVICEABLE (DOOR) · airframe 75,768 hrs · 8,489 cycles

DOOR MOUNTED SLIDE INFLATION PRESSURE IS BELOW GREEN TEMPERATURE COMPENSATOR INDICATOR AT MED NR 5 LT. REPLACED SLIDE-RAFT. VERIFIED TRIGGER SAFETY PIN REMOVED, INFLATION BOTTLE SAFETY PIN REMOVED AND ASSIST BOTTLE SAFETY PIN REMOVED. OPERATED ARM-DISARM LEVER, NO BINDING.

Part: TRACK — CRACKED (FUSELAGE) · airframe 75,700 hrs · 8,480 cycles

STA 1840 RT FLOOR TRACK IN AFT PIT 4 FT INBOARD HAS CRACKED RADIUS AT ATTACH POINT OVER THE TORQUE BOX. THE SECOND INBOARD TRACK LOCK RAIL HAS A SIX IN CRACK IN THE BASE OF THE RAIL LOCATED IN DOOR AREA. FOUND ADDITIONAL CRACK APPX 12 INCH FWD BEGAN REMOVING FASTENERS IN AREA. REMOVED RAIL & DRILLED UP BLIND FASTENERS IN TORQUE BOX AREA. PICKED UP CROSS BEAM SCREW HOLES. REPLACED RAIL. CLEANED DEBRIS FROM FLOOR STRINGER AREA UPON COMPLETION OF WORK BETWEEN STATION 1800 AND 1900 IN AFT CARGO PIT.

Part: FUSE — FAILED (CABIN) · airframe 75,700 hrs · 8,480 cycles

RT OVERWING SLIDE 2 AFT MOST EMERGENCY LIGHTS INOP. REPLACED FUSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,700 hrs · 8,480 cycles

EEL LIGHT INOP AT SEAT 39ABC. REPLACED LIGHT ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,187 hrs · 8,429 cycles

EMERGENCY EXIT LIGHT INOP. FLIGHT DECK CEILING. RELAMPED. OPS CKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,187 hrs · 8,429 cycles

EMERGENCY EXIT SIGN ILLUMINATES FOR A FEW SECONDS THEN EXTINGUISHES UPPER DECK TOP OF STAIRS. REPLACED BATTERY PACK. OPS NORMAL.

Part: LIGHT — FAULTY (CABIN) · airframe 75,187 hrs · 8,429 cycles

EMERGENCY EXIT LIGHTS INOP. SEAT ROWS 45 THRU 53 LEFT, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL EEL. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON 84XX AIRCRAFT COMING OUT OF INTERIOR MODIFICATION. REPLACED WATER SOAKED FEEDER CABLE AND TWO EMERGENCY WALL LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,638 hrs · 8,367 cycles

SEAT EEL LIGHT 57KJH INOP. RELAMPED EMERGENCY LIGHT, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,638 hrs · 8,367 cycles

SEAT EEL LIGHT 23 ABC INOP. RELAMPED EMERGENCY LIGHT, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,638 hrs · 8,367 cycles

MIDDLE COACH CLASS LAV LEFT FLOOR EEL INOP. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,076 hrs · 8,305 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT ROW 20 LEFT. REPLACED LIGHT STRIP, CHECKS NORMAL.

Part: CABLE — SHORTED (GALLEY) · airframe 74,076 hrs · 8,305 cycles

EMERGENCY EXIT EEL LIGHTS INOP SEAT ROWS 45 THRU 53, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL EEL ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL EEL. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON 84XX AIRCRAFT COMING OUT OF INTERIOR MODIFICATION. T/S AND FOUND WATER UNDER GALLEY MAT SHORTING POWER FEEDER CABLE. DRIED AREA OF WATER AND REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,076 hrs · 8,305 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 4 LEFT FWD SILL LIGHT. RELAMPED EMERGENCY LIGHT, OPS NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 74,076 hrs · 8,305 cycles

EMERGENCY EXIT EEL LIGHTS INOP AT SEAT ROWS 45 THRU 53 RIGHT, AND LOWER WALL EEL ACROSS DOOR 4 RIGHT. REPAIRED WIRING AT SEAT 48.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 74,076 hrs · 8,305 cycles

EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3 LEFT LOWER WALL. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 73,508 hrs · 8,243 cycles

THE 21H EMERGENCY LIGHT ON SIDE OF SEAT IS DAMAGED. EMERGENCY LIGHT ASSY REPLACED. CHECKED OKAY.

Part: FEEDER CABLE — DEFECTIVE (EMERGENCY LIGHTS) · airframe 73,487 hrs · 8,240 cycles

LT SEAT EEL LIGHTS INOP 45ABC TO 53ABC. REPLACED FEEDER CABLE, CHECKS OK.

Part: FEEDER CABLE — DEFECTIVE (EMERGENCY LIGHTS) · airframe 73,487 hrs · 8,240 cycles

FWD EXIT SIGN LIGHT INOP DOOR 4L. REPLACED FEEDER CABLE, CHECKS OK.

Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 73,487 hrs · 8,240 cycles

AFT EXIT LIGHT INOP DOOR 4R. REPLACED FEEDER CABLE. CHECKS OK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 73,487 hrs · 8,240 cycles

RT OVERWING EMERGENCY LIGHTS FWD AND AFT INOP. REPLACED BATTERY, CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,487 hrs · 8,240 cycles

LT B-ZONE EMERGENCY CEILING LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,487 hrs · 8,240 cycles

FWD GALLEY EMERGENCY CEILING LIGHT INOP. RELAMP EMERGENCY LIGHT, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,487 hrs · 8,240 cycles

SEAT EMERGENCY LIGHT 21ABC INOP. REPLACED EMERGENCY LIGHT INOP AT SEAT 21ABC. OPS CHECKED OKAY.

Part: EXTINGUISHER — LOW PRESSURE (CARGO BAY) · airframe 73,470 hrs · 8,237 cycles

PRIOR TO DEPT CREW REPORTED BTL LOW CARGO A DISPLAYED. FIRE EXTINGUISHER REPLACED. CMC GRD FIRE TEST PASS.

Part: LIGHT — DAMAGED (CABIN) · airframe 73,379 hrs · 8,227 cycles

THE 24C EMERGENCY LIGHT STRIP DAMAGED, REPLACED SEAT 24C EMERGENCY LIGHT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,069 hrs · 8,191 cycles

FWD CARGO COMPT BILGE AREA SKIN HAS SMALL AREA OF CORROSION, BS 740 BETWEEN STR 44R - 45R. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SKIN, INSTALLED SKIN DOUBLER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,069 hrs · 8,191 cycles

LT OVERWING EMERGENCY EXIT LIGHTS INOP, FWD & AFT POSITIONS. RELAMPED EMERGENCY LIGHT, OP CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

UPPER DECK, BS 945 CENTER, EMERGENCY EXIT LIGHT BATTERY PACK WEAK. REPLACED BATTERY PACK. OP CHECKS OKAY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

EMERGENCY EXIT LIGHTS INOP UPPER DECK CEILING BS 360, 570, & 670. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

EMERGENCY EXIT LIGHTS INOP UPPER DECK CEILING BS 660 CL & BS 690 RT. REPLACED BATTERY PACKS, OP CHECK OKAY.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,069 hrs · 8,191 cycles

CORROSION ON CANTED DECK SKIN BS 1265-1480, LBL 33.99-R BL 11.33. AFTER CORROSION REMOVAL FOUND EXCESSIVE MATERIAL LOSS AT BS 1265-1308 BL 0 TO LBL 33.99, AND BS 1377-1398 LBL 11.33 - LBL 33.99. MAJOR REPAIR ACCOMPLISHED. BS 1265-1308, CUT OUT DAMAGED WEB. SPLICED IN NEW WEB SECTION WITH LONG DOUBLER FROM BS 1265-1313, OUTBOARD OF LBL 11.33 AND TRANSVERSE DOUBLER AT BS 1310 BL 0- OUTBOARD OF LBL 11.33. FOR BS 1377-1398, CUT OUT DAMAGED WEB, SPLICED IN NEW WEB SECTION WITH 1 LONG DOUBLER INBOARD 094372 OF LBL 11.33 BEAM, 1 LONG DOUBLER INBOARD OF THE LBL 33.99 BEAM, 1 TRANSVERSE DOUBLER AT BS 137.5, AND 1 TRAN DOUBLER AT APPROX BS 1410.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

UPPER DECK BS 900 LT, EMERGENCY EXIT LIGHT BATTERY PACK WEAK. REPLACED BATTERY PACK. OP CHECKS OKAY.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 73,069 hrs · 8,191 cycles

UPPER DECK CEILING EMERGENCY EXIT LIGHT DIM, BS 945 BL 0. RELAMPED, OP CHECK OKAY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

EMERGENCY EXIT LIGHT INOP ABOVE DOOR 5L. REPLACED BATTERY PACK, OP CHECK OKAY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

DOOR MOUNTED EMERGENCY EXIT LIGHTS INOP AT 3L & 5L. REPLACED BATTERY PACK FOR DOOR 3L. REPLACED LIGHT FOR DOOR 5L. OP CHECKS OK.

Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 73,069 hrs · 8,191 cycles

RT HORIZONTAL STABILIZER AFT UPPER CHORD, STA 2590, RBL 43.5 A FASTENER HOLE WAS FOUND DAMAGED DURING COA 850111. OVER-SIZED HOLE TO APPROX 0.469 INCHES & INSTALLED BOLT WITH NUT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,069 hrs · 8,191 cycles

EELS INOP ROW 54 TO 60, LT & RT AISLES. REPLACED BATTERY PACK, OP CHECK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,955 hrs · 8,180 cycles

EMERGENCY LIGHT FWD GALLEY CEILING INOP. LIGHT FOUND INOPERATIVE. REPLACED LAMP, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,955 hrs · 8,180 cycles

SEAT 4F AFT EMERGENCY LIGHT INOP. LIGHT IS INOPERABLE. REPLACED LAMP. OP CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,955 hrs · 8,180 cycles

SEAT 4E AFT EMERGENCY LIGHT INOP. LIGHT IS DEFECTIVE. REPLACED LAMP. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,955 hrs · 8,180 cycles

SEAT 5A AFT EMERGENCY LIGHT INOP. LAMP IS UNSERVICEABLE. REPLACED LAMP. ALL CHECKS GOOD.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 72,955 hrs · 8,180 cycles

LEFT BOTTOM 2 OVERWING EMERGENCY LIGHT INOP. LIGHT FOUND INOP. REPLACED FUSE ON POWER SUPPLY. OP CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,955 hrs · 8,180 cycles

AFT GALLEY AISLE EMERGENCY LIGHT INOP. LIGHT FOUND DEFECTIVE. REPLACED LAMP, OP CHECK OKAY.

Part: WEB — DAMAGED (FUSELAGE) · airframe 72,628 hrs · 8,147 cycles

UPPER DECK FLOORBEAM WEB IS DAMAGED, AS VIEWED FROM GALLEY AT DOOR 2 IN ELEVATOR COMPARTMENT AT TOP FWD SIDE OF COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STIFFENER. REMANUFACTURED NEW STIFFENER FROM LIKE MATERIAL. BLENDED ALL DAMAGE, FOUND WITHIN LIMITS EXCEPT SMALL GOUGE WHICH WAS REPAIRED PER 53-00-51 NOTE "C". ALL AREAS AND PARTS TREATED, PRIMED, INSTALLED WITH SEALANT AND PAINTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,421 hrs · 8,129 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 32 RT INOP. *S/D* RELAMPED, OP CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,421 hrs · 8,129 cycles

EMERGENCY LIGHT ROW 4A INOP. *S/D* REPLACED LAMP, OP CHECKS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,421 hrs · 8,129 cycles

EMERGENCY LIGHT ROW 4F INOP. *S/D* RELAMPED, OP CHECK NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 72,150 hrs · 8,104 cycles

UPPER LT WING L/E SURFACE, JUST OUTBOARD OF NR 2 ENG, HAS CRACK APPROX 4 FEET IN LENGTH, ORIENTATED IN A FORE TO AFT DIRECTION. DOUBLER MANUFACTURED. LAID UP & DRILLING FASTENER HOLES. DOUBLER REPAIR INSTALLED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 58 LEFT. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

EMERGENCY EXIT CEILING LIGHT INOP AT DOOR 4 FWD SIDE OF GALLEY AREA. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5 LEFT LOWER WALL CROSSAISLE. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP, TWO MOST AFT LIGHT ASSY'S. FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3 LEFT LOWER WALL. FOUND BROKEN FEEDER WIRE. REPAIRED FEEDER WIRE, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5F AFT LIGHT ASSY. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,903 hrs · 8,082 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: FUSE — INOPERATIVE (OVERWING LIGHT) · airframe 71,376 hrs · 8,030 cycles

LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP, TWO MOST FWD LIGHT ASSY'S. FOUND OPEN FUSE. REPLACED FUSE OP CHECKED GOOD. AC OK FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4J FWD LIGHT ASSY. FOUND LOOSE CONNECTION. SECURED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT EEL LIGHT INOP AT ROW 48 LEFT. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 42 RIGHT CEILING. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT EEL LIGHT INOP AT ROW 56 LEFT. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,376 hrs · 8,030 cycles

RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP, TWO MOST AFT LIGHT ASSY'S. FOUND OPEN FUSE. REPLACED FUSE OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 44 RIGHT CEILING. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5E FWD LIGHT ASSY. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,376 hrs · 8,030 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 2J AFT LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL.

Part: MOTOR — FAULTY (GALLEY) · airframe 71,342 hrs · 8,026 cycles

CART LIFT INOP WITH ACRID ELECTRICAL ODOR. NOTE CHRONIC HISTORY. MOTOR AND LIMIT SWITCH TO BE FAULTY. REPLACED SWITCH S10 OPS NORMAL PER MM 25-38-00. REPLACED MOTOR PER 25-38-02 OPS NORMAL. ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (SEAT 32HJK) · airframe 70,897 hrs · 7,978 cycles

SEAT 32 HJK EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 2J AFT) · airframe 70,897 hrs · 7,978 cycles

SEAT 2J AFT EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,897 hrs · 7,978 cycles

UPPER DECK CEILING 2 EMERGENCY LIGHTS IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NO.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,897 hrs · 7,978 cycles

DOOR 5R SILL EMERGENCY LIGHT IS INOP. REPLACED LAMP. CHECKS NORMAL. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 4F AFT) · airframe 70,897 hrs · 7,978 cycles

SEAT 4F AFT EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 4A AFT) · airframe 70,897 hrs · 7,978 cycles

SEAT 4A AFT EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL.

Part: OXYGEN BOTTLE — READS LOW (L3 DOOR SLIDE) · airframe 70,742 hrs · 7,960 cycles

FOUND DOOR 3L O2 BOTTLE PRESSURE LOW. SUSPECT FAULTY SEAL. REPLACED OXYGEN BOTTLE. AC OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EEL POWER SUPPLY) · airframe 70,416 hrs · 7,926 cycles

EMERGENCY ESCAPE LIGHTS INOP: RT OVERWING 2 AFT ASSY'S. REPLACED FUSE ON POWER SUPPLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,416 hrs · 7,926 cycles

EMERGENCY LIGHTS INOP: DOOR 2L FWD SILL ILLUM. RELAMPED

Part: LIGHT — INOPERATIVE (R3 DOOR) · airframe 70,416 hrs · 7,926 cycles

EMERGENCY EXIT LIGHT INOP: DOOR 3R AFT DOOR SIGN. REPLACED LIGHT ASSY

Part: LIGHT — INOPERATIVE (ROW 32 RT) · airframe 70,416 hrs · 7,926 cycles

EEL LIGHT INOP: ROW 32RT. REPLACED LIGHT ASSY

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

EMERGENCY LIGHT INOP: DOOR 2L CEILING. RELAMPED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

WALL EEL INOP: RIGHT SIDE WALL AFT GALLEY. SECURED CONNECTOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

SEAT EEL INOP AT 32 HJK. RELAMPED.

Part: LAMP — INOPERATIVE (AFT CREW REST) · airframe 69,992 hrs · 7,883 cycles

EMERGENCY LIGHT INOP: AFT CREW REST STAIRS ILLUM O/B LAMP. RELAMPED

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

EMERGENCY LIGHTS INOP: RIGHT OVERWING 2 AFT ASSEMBLIES. REPLACED FUSE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

SEAT EEL INOP AT 3A AFT SECT. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

WALL EEL INOP, UPPER DK STAIR WALL FWD SECT. RELAMPED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 69,992 hrs · 7,883 cycles

SEAT EELS INOP: 4E & 5E BOTH SECTIONS. SECURED CONNECTOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,518 hrs · 7,831 cycles

DOOR 1 LEFT FWD SILL & DOOR 5R SILL 2EA EMERGENCY LIGHTS ARE INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,518 hrs · 7,831 cycles

SEAT 32 HJK EMERGENCY LIGHT IS INOP. REPLACED LIGHT STRIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,518 hrs · 7,831 cycles

SEAT 4J AFT EMERGENCY LIGHT IS INOP. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,518 hrs · 7,831 cycles

UPPER DECK CEILING EMERGENCY LIGHT IS INOP NEAR CENTER WING DOORS (1 EA). RELAMPED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,238 hrs · 7,803 cycles

FUSELAGE DAMAGED 4 FEET BELOW F/O'S NR 2 WINDOW, INLINE WITH WINDOW AND AOA SENSOR. DENT IS 2.5" LONG AXIS AN D .125" IN DEPTH. CTR HAS CREASE OR GOUGE. DAMAGE IS APPROX STA 297 BETWEEN RT STRINGER 14 & S14-D WITH NO FRAME CONTACT. REPAIRED PER SRM 53-00-01 REPAIR 7 TIME LIMITED EXTERNAL REPAIR. MF1596 CREATED TO MONITOR. AC OK FOR SERVICE.

Part: GIRT BAR — OUT OF ADJUST (L4 DOOR) · airframe 68,977 hrs · 7,773 cycles

DOOR 4L WILL NOT ARM. DOOR 4L GIRT BAR READJUSTED. OP CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,099 hrs · 7,683 cycles

ZONE-C LEFT CEILING EMERGENCY LIGHTS 2EA ARE INOP. *S/D* RELAMPED IN TWO POSITIONS. BOTH OP CHECK NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,099 hrs · 7,683 cycles

DOOR 5 RIGHT FWD SILL EMERGENCY LIGHT IS INOP. *S/D* RELAMPED DOOR 5L EEL. OP CHECKS NORMALLY.

Part: LAMP — INOPERATIVE (SEATS 1J AFT, 4A) · airframe 68,099 hrs · 7,683 cycles

SEATS 1J AFT, 4A FWD, 55HJK & 8ABC EMERGENCY LIGHTS ARE INOPERATIVE. *S/D* RELAMPED SEAT EEL LIGHTS AT EACH SEAT POSITION. ALL OP CHECK NORMALLY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,099 hrs · 7,683 cycles

RIGHT OVERWING AFT TWO EMERGENCY LIGHTS ARE INOP. *S/D* REPLACED BATTERY CHARGER. OP CHECKS NORMALLY.

Part: LIGHT — DAMAGED (SEAT 1A) · airframe 67,713 hrs · 7,642 cycles

SEAT 1A EMERGENCY LIGHT STRIP DAMAGED.

Part: LIGHT — FIRE (CABIN) · airframe 67,652 hrs · 7,636 cycles

SMOKE ODOR DOWNSTAIRS AND THEN FIRE FORWARD OF UPPER DECK GALLEY IN THE CEILING. ONE HALON EXTINGUISHER FIRED. [08-08-07] FOUND FLUORESCENT LITE SOCKETS WITH HEAT DAMAGE. REPLACED UPPER DECK CEILING FLUORESCENT LIGHT SOCKETS. ALSO REPLACED BALLAST. ALL CKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,624 hrs · 7,633 cycles

EMERGENCY LIGHT ROW 1J AFT INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 67,624 hrs · 7,633 cycles

EMERGENCY LIGHT ROW 4J AFT INOP. RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 67,432 hrs · 7,611 cycles

AFT GALLEY CEILING FLICKER ON AND OFF. RELAMPED AS REQUIRED.

Part: SKIN — CRACKED (T/E FOREFLAP) · airframe 67,181 hrs · 7,585 cycles

RIGHT WING INBOARD TRAILING EDGE FOREFLAP LOWER SURFACE CRACKED. LENGTH OF CRACK IS APPROX 7.5 FEET SPANWISE, APPROX 6 INCHES FROM LEADING EDGE. [07-27-07] REPLACED RIGHT HAND INBOARD FOREFLAP IN ACCORDANCE WITH MM 27-51-02 PAGE 401. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,136 hrs · 7,579 cycles

FWD CARGO COMPT FLOORBEAM UPPER CHORD CRACKED, BS 560 RBL 30. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. INSTALLED FILLER & ANGLE DOUBLER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,136 hrs · 7,579 cycles

FWD CARGO COMPT FLOORBEAM UPPER CHORD CRACKED AT BS 780 RBL 70. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED FILLER & ANGLE REPAIR.

Part: SKIN — CRACKED (RT FOREFLAP) · airframe 67,136 hrs · 7,579 cycles

RIGHT WING INBOARD TRAILING EDGE FOREFLAP LOWER SURFACE CRACKED. REPAIRED WITH WET LAYUP AND BMS8-301 RESIN PER UA-EVA-70288 AND BOEING TELEX 8100-9. SUSPECT INSTALATION & RIG CAUSED UNUSUAL DYNAMIC LOADING DURING FLIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,136 hrs · 7,579 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP, 2ND FROM FWD POSITION. LAMP INOPERATIVE. [SUP 06-06-07] RELAMPED, OP CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,136 hrs · 7,579 cycles

DOORWAY 2L UPPER SILL, AFT EMERGENCY EXIT LIGHT INOP. REPLACED LAMP. OP CHECKED OK RE F MM 33-51-05. ACPD ON.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,136 hrs · 7,579 cycles

DOOR 4R EMERGENCY EVAC PANEL "EVAC" BUTTON LIGHT INOP. REPLACED LAMP. OP CHECKED OK RE F MM 25-63-01. ACPD ON.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE)

LOW BOTTLE PRESSURE. [SUP 05-16-07] SMALL PIN HOLE LEAK AROUND FILLER VALVE AND BAD O-RING. REPLACED O-RING AND FITTING CHARGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,778 hrs · 7,537 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 61 RT. REPLACED LIGHT ASSY AND CHECKED OK.

Part: CABLE — DEFECTIVE (CABIN) · airframe 66,778 hrs · 7,537 cycles

EMERGENCY LIGHT LEFT FWD GALLEY ACROSS DOOR 1 LEFT. REPLACED EEL CABLE. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,778 hrs · 7,537 cycles

EMERGENCY LIGHT ROW 5A AFT & SEATS 32 HJK ARE INOP. REPLACED LAMP, OP CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,778 hrs · 7,537 cycles

OVERWING EMERGENCY LIGHT 2 TOP LIGHT INOP. REPLACED BATTERY CHARGER ASSY. OP CHECK NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 65,861 hrs · 7,446 cycles

EEL AT 2A AFT AND 55 HJK ARE INOPERATIVE. CONNECTOR LOOSE AT ASSY JUNCTION. RETIGHTENED. OP CHECKS OK.

Part: LIGHT — INOPERATIVE (L2 DOOR SLIDE) · airframe 65,861 hrs · 7,446 cycles

FOUND EMERGENCY LIGHT AT DR 2L SLIDE ILLUMINATED INOPERATIVE. EMERGENCY LT AT DR 2L SLIDE ILLUM INOP. BATTERY PACK LOST CHARGE. AFTER CHARGING EEL CKS OK.

Part: LAMP — FAULTY (EMERGENCY LIGHTS) · airframe 65,861 hrs · 7,446 cycles

EMERGENCY LIGHT AT ROW 4 RT IS INOPERATIVE AND EMERG EXIT SIGN AT AFT CREW REST AREA LAMP IS DIM. RELAMPED ROW 4 RT EEL & EMERGENCY EXIT SIGN IN AFT CREW REST AREA. BOTH POSITIONS OP CHECKED OK.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 65,861 hrs · 7,446 cycles

FOUND EMERGENCY LIGHTS AT DOOR 1L SLIDE ILLUM, ROW 34 ABC AND ROW 46 HJK ARE INOPERATIVE. REPLACED LT ASSY AT EACH POSITION. ALL OP CHECKED OK FOR SERVICE.

Part: SHAFT — BROKEN (NR 3 GEARBOX) · airframe 65,116 hrs · 7,362 cycles

NR 3 ENG FLAMEOUT. WHEN THE AGB COVER WAS REMOVED, THE TOWERSHAFT & TOWERSHAFT RETAINING RING FELL OUT. IT WAS CONCLUDED THAT THE TOWERSHAFT RETAINING RING WAS ONLY PARTIALLY ENGAGED IN THE TOWERSHAFT'S MATING GROOVE AT INSTALLATION. IN TIME, THIS ALLOWED THE TOWERSHAFT TO SLIP DOWNWARD. THIS RESULTED IN ITS LOWER TEETH DISENGAGING FROM THE AGB GEARS. THEREFORE, ALTHOUGH THE TOWERSHAFT WAS STILL SPINNING, NO TORQUE WAS BEING TRANSMITTED TO THE MGB. JICS HAVE BEEN REVISED TO ALERT MECHANICS & LEADS TO THIS POSSIBILITY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 64,919 hrs · 7,340 cycles

AFT REST CREW EXIT EMERGENCY LIGHT INOP. RELAMPED, OKAY.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,919 hrs · 7,340 cycles

RT SIDE LOWER TWO EMERGENCY LIGHTS INOP. REPLACED FUSE ON BATTERY CHARGER. OP CK'D LIGHTS, OP CK'D NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 64,470 hrs · 7,292 cycles

SEAT 1J AFT EMERGENCY LIGHT IS INOP. SEAT 1J AFT EMERGENCY LIGHT IS INOP.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 64,024 hrs · 7,245 cycles

WALL EEL INOP AT CLOSET FLOOR FWD OF LAV 102. WALL EEL INOP: CLOSET FLOOR FWD OF LAV 102. SPLICED FEEDER WIRE, OP CHKS OK

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,024 hrs · 7,245 cycles

EMERGENCY LIGHT INOP AT DOOR 2R AND 4L SLIDE ILLUM. RELAMPED LIGHT. OP CHECKS OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,024 hrs · 7,245 cycles

EMERGENCY LIGHTS INOP AT EXIT SIGN DOOR 1R AFT SIDE AND CEILING ROW 26 RT. RELAMPED LIGHTS. OP CHECKS OK.

Part: O-RING — FAILED (R2 DOOR SLIDE) · airframe 63,804 hrs · 7,223 cycles

FOUND DOOR 2R SLIDE BOTTLE PRESSURE IS LOW. SLIDE REPLACED. A/C OK FOR SERVICE. SLIDE PROBLEM ROOT CAUSE IS SLIDE BOTTLE PRESSURE LOW. O-RINGS ON CONNECTIONS TO BOTTLE HARDEN WITH TIME & LEAKED.

Part: FRAME — DAMAGED (BS 840) · airframe 62,628 hrs · 7,087 cycles

FOUND FRAME CHORD DAMAGED AT STA 840, JUST FWD OF CENTER CARGO GUIDE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,161 hrs · 6,918 cycles

AFT CARGO DOOR CUTOUT UPPER FWD CORNER HOLE HAS CRACK (IN BODY SKIN). CRACK FOUND BY COA TO ADDRESS CRACKS IN THIS AREA, AS MANDATED BY AD. REPAIRED PER BOEING SERVICE BULLETIN 747-53A2448.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,158 hrs · 6,917 cycles

M-D FLOOR STA 1283-1335 SEAT TRACK BEAM TO W-W SKIN ATTACH AREA HAS CORROSION (PRESSURE DECK AND LWR CORD). CORROSION REPAIRED PER OSV ENGINEERING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,158 hrs · 6,917 cycles

BULBS FOR EMERGENCY LIGHTS INOPERATIVE AT AISLE EMERGENCY EXIT SIGN ROW 22AB AND 62BD. REPLACED EEL LIGHT.

Part: SPAR — CRACKED (BS 1000) · airframe 61,158 hrs · 6,917 cycles

FWD PIT STA 1000 SPAR CHORD CRACK, STR 46-47L, 1.42 INCH AND 46-47R, 0.87 IN. STATION 1000 CHORD CRACK FOUND UNDER EXISTING MAINTENANCE PLAN WRITTEN FOR THIS TYPE OF DAMAGE. REPAIRED PER AMM & FAA-APPROVED SERVICE BULLETIN.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,176 hrs · 6,677 cycles

EMERGENCY EXIT LIGHTS ON IN BUSINESS CLASS RIGHT SIDE ROW 6-8 AND DOOR 2R. REPLACED EMERGENCY LIGHT BATTERY AT DOOR 2R, OPS CHECKED OK.

Part: OIL COOLER — LEAKING (NR 4 ENGINE) · airframe 59,164 hrs · 6,675 cycles

FUEL LEAK NR 4 ENGINE. DIVERTED TO NARITA. CP07 AIR/OIL COOLER TUBE CRACKED. TUBE & CLAMPS WERE REPLACED. AGB REMOVED. SUSPECT AGB VIBRATION CAUSED TUBE CRACK. AGB TEARDOWN REVEALED NO DISCREPANCIES. ENGINE SUBSEQUENTLY REMOVED AS PRECAUTIONARY. SHOP INPUT POSTPONED INDEFINITELY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,624 hrs · 6,612 cycles

EMERGENCY EXIT LIGHT ON AT 4L AND 4R. LOW BATTERY. REPLACED BATTERY.

Part: ODOR — DETECTED (COCKPIT) · airframe 58,571 hrs · 6,606 cycles

WINDOW HEAT 2L EICAS MSG DISPLAYED. A WEIRD ODOR WAS APPARENT IN THE COCKPIT THEN C/B TRIPPED FOR 2L. NO RESET ATTEMPTED. INVESTIGATED & FOUND LOOSE WINDOW HEAT CONTROL THERMOSTAT WIRING & "WINDOW HEAT 2L" MESSAGE ON EICAS. LOOSE WIRING MAY HAVE CAUSED ARCING & ODOR. THE LOOSE WIRE WAS REATTACHED TO COCKPIT WINDOW. "WINDOW HEAT 2L" MESSAGE WAS GONE, AND A/C RETURNED TO REVENUE SERVICE WITHOUT FURTHER ODOR OR WINDOW HEAT PROBLEM.

Part: DOOR — NOISY (4L) · airframe 57,910 hrs · 6,522 cycles

AFTER TAKEOFF, LOUD NOISE FROM DOOR 4L. ALSO, EICAS MESSAGE FOR DOOR. EXAMINATION OF THE DOOR DID NOT REVEAL ANY DISCREPANCIES. THE DOOR WAS OPERATED SEVERAL TIMES EACH TIME SATISFACTORILY.

Part: BLADES — FAILED (NR 4 ENGINE) · airframe 56,783 hrs · 6,386 cycles

NR 4 ENGINE SHUT DOWN DUE TO HIGH EXHAUST GAS TEMPERATURE & LOSS OF POWER. ENGINE EXPERIENCED SURGE AFTER TAKEOFF. UPON INVESTIGATION FOUND MASSIVE HPC DAMAGE. ROOT CAUSE OF THE FAILURE WAS THE 6TH STAGE BLADE DETACHMENT THIS IS AN INDUSTRY ISSUE WITH THE FRONT END DURABILITY BEING WORKED BY THE OEM.

Part: RECEPTACLE — BURNED (GALLEY) · airframe 56,620 hrs · 6,368 cycles

FLAME CAME OUT OF SERVICE OUTLET AFTER SWITCHING TO EXTERNAL POWER BY DOOR 1L. ELECTRICAL OUTLET AT DOOR 1 LEFT WAS FOUND MELTED. OUTLET WAS REPLACED AND OP CHECKED GOOD. ENGINEERING WILL EVALUATE THE ELECTRICAL OUTLET TO LOOK FOR POSSIBLE DEFECTS. ENGINEERING ALSO CREATED CALLOUT EG3435 TO CHECK DOOR 1 LEFT SERVICE OUTLET WIRING TO LOOK FOR ANY POSSIBLE CAUSES.

Part: DRIVE UNIT — INOPERATIVE (TE FLAPS) · airframe 55,112 hrs · 6,175 cycles

FLIGHT RETURNED TO NARITA DUE TO FLAP PROBLEM.CREW HAD EICAS MESSAGE FLAPS PRIMARY, AND RT MIDSPAN INDICATION WENT TO RED, EACH SPEED INCREASE. THE CREW SENSED NO CONTROL PROBLEMS. NRTMM REPLACED THE NR 3 RT LE SLAT DRIVE UNIT. NO FURTHER HITS HAVE BEEN REPORTED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,537 hrs · 6,065 cycles

FWD PIT STA 760 RBL 56 FLOORBEAM CRACKED AND DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. FABRICATED AND REPLACED SECTION.

Part: SLIDE — FAILED (NR 2 DOOR) · airframe 53,790 hrs · 5,997 cycles

DOOR 2 RIGHT SLIDE FAILED OVER PRESSURE TEST AT 3.80 PSI DURING OVERHAUL. SLIDE OEM ANALYSIS OF FAILURE WAS INCONCLUSIVE. INFLATABLE PORTION OF SLIDE SCRAPPED.

Part: LINE — LEAKING (NR 1 HYD SYSTEM) · airframe 52,597 hrs · 5,843 cycles

NR 1 HYDRAULIC QUANTITY SYSTEM READ ZERO WITH NO PRESSURE. FOUND LT LCCA HYDRAULIC LINE LEAKING. REPLACED LINE WITH NEW MANUFACTURED LINE. RESERVICED NR 1 SYSTEM. LEAK CHECKED NEW INSTALLED LINE, CHECKED OK.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 52,537 hrs · 5,832 cycles

FLIGHT DECK 3L WINDOW FRAME HAS CORROSION ON LWR SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED WINDOW SILL.

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 52,537 hrs · 5,832 cycles

FWD PIT STA 720 FLOORBEAM T-CHORD AT RBL 10 APPROX IS DENTED ON THE HORIZONTAL FLANGE & EXTENDS INTO THE RADIUS OF THE FLANGE. MAJOR REPAIR ACCOMPLISHED. THE FLANGE WAS TRIMMED OUT AS MUCH AS POSSIBLE. ACP HFEC NDT INSP OF AREA FOR CRACKS, NONE FOUND. THIS REPAIR APPROVED BY BOEING-FAA 8110-3 ON MOBILE AEROSPACE ENGINEERING AUTHORIZATION 47-5325-13-A1038.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,537 hrs · 5,832 cycles

FORWARD PIT FRAME STA 740 APPROX. RBL 51 HAS DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,472 hrs · 5,434 cycles

UPPERDECK LEFT EMERGENCY DOOR BATTERY PACK INOP. REPLACED BATTERY - CHECKED OK.

Part: COMPRESSOR — STALLED (NR 4 ENGINE) · airframe 48,333 hrs · 5,292 cycles

COMPRESSOR STALL ON NR 4 ENGINE. SUPPLEMENTAL DATA UPDATE THIS IS A GROUP 3 (TAKEOFF ) SURGE DUE TO EXCESSIVE HPC REAR STAGE BLADE TIP CLEARANCE. ENGINE WAS REPLACED AT TERMINATION OF THE FERRY FLIGHT FOR COMPRESSOR REFURBISHMENT. PW4000 ENGINE TAKE-OFF SURGES ARE BEING MANAGED PER AD 2001-25-11

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 44,647 hrs · 4,833 cycles

MAJOR REPAIR ACCOMPLISHED TO FLOORBEAM WEB PER SRM 51-70-13-001 DOUBLER INSTALLED AFT SIDE OF CABIN FLOORBEAM BS 880 RBL 9 WL 199 HEIGHT OF BEAM APPROX 7 INCHES WIDE. *S/D* DAMAGE CAUSED AT CURRENT MAINTENANCE CHECK BY ACCIDENT WHEN PERFORMING WORK IN VICINITY. REPAIRED PER SRM 51-70-13-001.

Part: HEATER — FAILED (COCKPIT) · airframe 42,061 hrs · 4,537 cycles

ELECTRIC BURN SMELL IN COCKPIT. TURNED OFF LOWER RECIRCULATING FAN PER MEL. SMELL WENT AWAY. *S/D* REPLACED PILOTS SHOULDER HEATER (P/N: 2831-2). NO PROBLEMS AFTER, PROBABLE CAUSE WAS INTERNAL FAILURE.

Part: TUBE — CRACKED (BEARING OIL) · airframe 41,572 hrs · 4,466 cycles

ENGINE NUMBER TWO OIL QUANT ZERO, OIL PRESSURE DECREASING. SHUT DOWN NR 2WITH 73 PSI. WINDMILL OIL PRESS 15-16 PSI. NR 2 ENGINE IN FLIGHT SHUT DOWN DUE TO LOSS OF OIL PRESSURE AND OIL QTY. ENGINE WILL REQUIRE REMOVAL. OIL LOSS WAS CAUSED BY A CRACKED NUMBER 4 BEARING OIL TUBE. SUBSEQUENT BORESCOPE REVEALED 1 HPT T2 BLADE FAILED AT MID SPAN. RESULTANT VIBRATION CAUSED THE OIL LINE FRACTURE.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT SIDE UPPER DECK DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND WORKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INTERMITTENT ROWS 51 TO 59 LEFT HAND SIDE E-ZONE. *S/D* DEFECTIVE BATTERY PACK WAS REMOVED AND REPLACED.

Part: FAN — FAILED (CABIN)

ELECTRICAL SMELL AND SMOKE IN CABIN CONCENTRATED BETWEEN GALLEY 402 AND LAV 111-112. LEFT AND RIGHT UTILITY BUSES TRIPPED. SMOKE REMOVAL PROCEDURE, CLEARED CABIN. *S/D* UPPER NR 2 RECIRCULATION FAN BEARING FAILURE. REPLACED FAN.

Part: VALVE BODY — BROKEN (CTR FUEL TANK)

UNWANTED FUEL TRANSFER. *S/D* THE SHAFTS TO BOTH JETTISON TRANSFER VALVES IN THE CENTER TANK WERE BROKEN. DUE TO PRESSURE IN THE MANIFOLD, THE VALVE BODY WAS FREE TO FLOP OPEN AND CAUSED THE FUEL IMBALANCE PROBLEM. REPLACED TRANSFER VALVES, OPERATION CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLOOR EMERGENCY EXIT LIGHTS INOP IN RIGHT HAND FORWARD E-ZONE IN ADDITION TO CEILING LIGHT AND FLOOR LIGHTS IN D-ZONE. BATTERY PACKS LOW, REPLACED BATTERY PACKS.

Part: SWITCH ASSY — MALFUNCTIONED (LE FLAPS)

AIRCRAFT EXPERIENCED INTERMITTENT -FLAPS PRIMARY+ AND -FLAPS DRIVE+ MESSAGES IN-FLIGHT SOON AFTER TAKE-OFF. FLIGHT CREW ELECTED TO DUMP FUEL AND RETURN TO FIELD. THE L1 LEADING EDGE FLAP DRIVE UNIT POSITION SWITCH ASSEMBLY WAS REPLACED WITH AN IMPROVED P/N SWITCH. THE OLD SWITCH HAS BEEN KNOWN TO CAUSE NUISANCE EICAS MESSAGES.

Part: EEL JUMPER — BROKEN (CABIN)

FLOOR EEL INOP IN E-ZONE RT AISLE AT ROWS 46 TO 52. REPLACED BROKEN JUMPER AT ROW 52.