N171UA

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 95,313 hrs · 11,133 cycles

SEAT NUMBER 45AC EMER LT FOUND INOPERATIVE. RECONNECTED THE CONNECTOR OF THE EMER LIGHT AT SEAT 45AC & TEST FOUND TO PASS IAW AMM 33-51-12 REV 170.

Part: CABLE — DAMAGED (CABIN) · airframe 95,313 hrs · 11,133 cycles

NUMBER 4 DOOR GALLEY SIDEWALL LT EMER LIGHT FOUND INOPERATIVE. REPLACED THE CABLE OF THE EMER LIGHT AT SEAT 45AC. OPERATIONS CHECKED GOOD IAW AMM 33-51-12 REV 170.

Part: WIRE — DAMAGED (CABIN) · airframe 94,134 hrs · 11,019 cycles

ESCAPE PATH LIGHT INOPERATIVE AT ROW 45ABC. REPAIRED WIRING, LIGHTS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 93,641 hrs · 10,971 cycles

UPPER DECK LT DOOR UPPER EMER EXIT LIGHT IS INOPERATIVE. REPLACED BATTERY POWER PACK. OPERATIONS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,641 hrs · 10,971 cycles

STAIRWAY EEL LIGHT IS INOPERATIVE. ORDERED EEL BATTERY, PCN 585-4495.

Part: CRADLE — BROKEN (CABIN) · airframe 92,142 hrs · 10,815 cycles

PHONE CRADLE DOOR 4L IS BROKEN. REPAIRED CRADLE, SYS CHECKED GOOD.

Part: TRIM PANEL — BROKEN (CABIN) · airframe 92,053 hrs · 10,806 cycles

ON CM8401 CHECK FOUND LAVATORY 102 AFT SIDE EMERGENCY EXIT LIGHTS TRIM BROKEN. SIDE TRIM REPLACED & CHECKED NORMAL.

Part: LUG — UNSECURE (CABIN) · airframe 91,953 hrs · 10,795 cycles

IAW STANDBY POWER CHECK, AFT DOME LIGHT INOPERATIVE. WIRES DISCONNECTED FROM LIGHT ASSEMBLY L137. SECURED LUGS TO TERMINALS, OPERATIONS CHECKED OKAY.

Part: SEAT BELT — DEFECTIVE (COCKPIT) · airframe 91,722 hrs · 10,775 cycles

POSITION 1 FLIGHT CREW BELT WILL NOT LOCK. CROTCH STRAP WILL NOT LOCK. REPLACED CROTCH CAPTAIN SEAT BELT, FUNCTION IS BACK TO NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,712 hrs · 10,774 cycles

RT FUSELAGE SKIN HAS EVIDENCE OF DAMAGE AT STATION 1980 NEAR BULK CARGO DOOR FWD EDGE APPROXIMATELY ONE FOOT UPWARD FROM FWD LOWER CORNER. CHECKED DAMAGE AREA NO CRACK FOUND, DAMAGE THAT EXCEEDS THE ALLOWABLE SRM LIMITS WILL BE REPAIRED ON CF, IAW GMM05-30-05 & IS SUBJECT TO APPROVAL BY QC. ACCOMPLISHED HFEC INSP IAW MF8680 NO CRACKS FOUND, HFEC INSP CW NO DEFECTS NOTED OK TO CF9 IAW TOMC. REMOVED DOUBLER. HFEC MFG & INSTALLED REPAIR IAW ECRA 5330-04745.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,712 hrs · 10,774 cycles

ACFT FWD CARGO DOOR AFT SIDE OF FUSELAGE DAMAGED APPROXIMATELY 36 IN FROM BOTTOM OF DOOR WAY, 1 1-2 INCHES WIDE BY 6 INCHES LONG. COMPLIED WITH ECRA 5321-01878. HFEC ACCOMPLISHED NO FAULTS FOUND IAW PTT 6362020, IAW ECRA 5330-04741. REMOVED DAMAGE, HFEC FABRICATED & INSTALLED REPAIR PARTS. IAW ECRA PERMANENT REPAIR TO BE DETERMINED PRIOR TO 20,000 PTC. REPAIRED IAW ECRA 5330-04741.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,712 hrs · 10,774 cycles

CABIN DECK FLOOR BEAM UPPER CORD HAS CORROSION AT STATION 1700, LBL 1". CUTOUT DAMAGE & INSTALLED NEW SECTION IAW SRM 53-60-51 RPR1 NR 0388763.

Part: TRIPLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,712 hrs · 10,774 cycles

RT FUSELAGE AT WASTE SYSTEM OVERBOARD VENT HOLE, TRIPLER HAS EXTERNAL CORROSION STATION 2090, STRINGER 35R TO STRINGER 36R. REMOVED DAMAGE PARTS & INSTALLED NEW TRIPLER IAW SRM53-60-01 RPR 1, REV 87 & ECRA 5330-04755.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,712 hrs · 10,774 cycles

CABIN MAIN DECK FLOOR BEAM HAS CORROSION AT STATION 1660, LBL 11 TO LBL 33 ON UPPER CHORD. CUTOUT DAMAGED UPPER CHORD & INSTALLED NEW SECTION IAW SRM53-60-51, RPR 1, NR 0388315.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,712 hrs · 10,774 cycles

BS 1780 LBL 4 FLOOR BEAM CORROSION, REMOVED DAMAGE. HFEC MANUFACTURED & INSTALLED REPAIR PARTS IAW SRM 53-60-51 REPAIR 1.

Part: WIRE — DAMAGED (STAB TRIM) · airframe 91,679 hrs · 10,771 cycles

"STAB TRIM" STATUS MESSAGE DISPLAYED UPON T TRIMMING STAB NOSE UP WITH "ALTERNATE STAB TRIM SWITCHES" ON PEDESTAL. CMC SHOWS MESSAGE 27147. WITH NR 2 CUTOUT SW ENGAGED ONLY NR 3 IN CUTOUT POS STAB TRIM FAILS TO MOVE TO THE NOSE UP POSITION WITH "ALTERNATE STAB TRIM SWITCHES". SUSPECT RT STAB TRIM CONTROL MODULE B188 AT FAULT. PLACED RT STCM IAW AMM 27-41 -04-201, NO HELP. FOUND DAMAGED WIRE AT S19 6O. REPLACED SWITCH IAW TO MM 27-41-08 PG 401 & SYSTEM CHECKED NORMAL IAW TO MM 27-41-08 PG501.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 91,043 hrs · 10,708 cycles

WEATHER RADAR WILL NOT TEST. FOUND MESSAGE 34010. REPLACED WEATHER RADAR CONTROL PANEL, IAW FIM & AMM. SYSTEM CHECKED GOOD.

Part: SEAL — FAILED · airframe 90,889 hrs · 10,692 cycles

NR 4 ENGINE IDG HAS BAD SEAL TO GEARBOX.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 90,874 hrs · 10,690 cycles

FORWARD CARGO DOOR DENTED AND CRACKED 12" FROM AFT EDGE AND BOTTOM OF CARGO DOOR. IAW ECRA 5230-01927 NEED TO ACP PERMANENT SRM SKIN REPAIR WITHIN 3 A-C CYCLES (PTC 10693 MAX) IAW SRM 52-30-01, REPAIR 2. DVI REPAIR AREA IS TO BE ACP PRIOR TO EACH DEPARTURE CHECKING FOR ADDITIONAL DAMAGE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 90,480 hrs · 10,650 cycles

DURING "A" CHECK, SEAT 56 LEFT, EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN CONNECTOR AT EMERGENCY LIGHT, REPLACED. OPS CHECKED OK. PERFORMED EMERGENCY LIGHT INSPECTION. NO DEFECTS FOUND.

Part: LIGHT — MISSING (SEAT 19RT) · airframe 90,480 hrs · 10,650 cycles

DURING "A" CHECK, SEAT 19 RT, EMERGENCY LIGHT MISSING. REPLACED. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (SEAT 25LH) · airframe 90,480 hrs · 10,650 cycles

DURING "A" CHECK, SEAT 25 LEFT, EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT. OPS CHECKED OK. PERFORMED INSPECTION. NO DEFECTS FOUND.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,480 hrs · 10,650 cycles

SEAT 44 RT TO 53 RT, SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED M6011 BATTERY. OPS CHECKED OK.

Part: LIGHT — UNKNOWN (SEAT 19RT) · airframe 90,480 hrs · 10,650 cycles

REPLACED SEAT EMERGENCY LIGHT AT SEAT 19 RT. PERFORMED INSPECTION, NO DEFECTS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,602 hrs · 10,564 cycles

SEATS 48ABC EEL STRIP INOP. REPLACED EEL STRIP. OP'S CHECKED GOOD. ACCOMPLISHED IDT INSPECTION OF THE EEL STRIP REPLACEMENT, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 89,602 hrs · 10,564 cycles

UPPER DECK EXIT SIGN OVER STAIRS INOP. RELAMPED CHECKED GOOD. ACCOMPLISHED IDT INSP OF THE RELAMPING OF THE EEL LIGHT, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,602 hrs · 10,564 cycles

UPPER DECK SIDEWALL EEL STRIP ACROSS FROM SEATS 12JK INOP.

Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 89,602 hrs · 10,564 cycles

DOOR 4L SLIDE LIGHT INOPERATIVE. REPLACED LIGHT ASSY OP'S CHECKED GOOD. ACCOMPLISHED IDT INSP OF THE EEL LIGHT ASSY, OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,287 hrs · 10,532 cycles

UPPER DECK EMERGENCY DOOR LEFT GROUND MODE INDICATION LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: ANGLE — DAMAGED (RT MLG DOOR) · airframe 89,269 hrs · 10,530 cycles

RIGHT OUTBOARD BODY DOOR SEAL MISSING A PORTION. INSPECTION FOUND 2 INCHES OF FWD SEAL GAP ANGLE BROKEN. VISUAL INSPECTED DAMAGED ANGLE, SEAL AND ADJACENT AREA. NO ADDITIONAL DAMAGE IS PRESENT. GEAR DOOR AND FUSELAGE STRUCTURE NO DAMAGE. REMAINING SECTION OF SEAL IS SECURED AND UNDAMAGED. INSTALLED NEW ANGLE AND BULB SEAL

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 88,674 hrs · 10,465 cycles

L4 GALLEY EMERGENCY LIGHT INOPERATIVE. REPAIRED FEEDER CABLE, OPS CHECKED OK.

Part: LIGHT — FAILED (R2 DOOR) · airframe 88,674 hrs · 10,465 cycles

R2 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LIGHT ASSY AND OP CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT ROW 33ABC) · airframe 88,674 hrs · 10,465 cycles

ROW 33ABC SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT AND ACCOMPLISHED OPS TEST PER MM, TESTED GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 88,509 hrs · 10,447 cycles

FLIGHT LOST ALL NR 1 HYDRAULICS ABOUT 30 MINUTES OUT. FLIGHT RETURNED. EMERGENCY DECLARED. NR 1 HYD EDP FOUND HEAVY LEAKAGE. NR 1 ENG EDP REPLACED. TUBE REPAIRED PER GNMM 1-0-13-020. SWAGE UNION INSTALLED AT HYD TUBE IN BS 1200 LT FUSELAGE. NO LEAK FOUND.

Part: SPOILER — DEPARTED (LT WING) · airframe 88,264 hrs · 10,418 cycles

LEFT INBOARD SPOILER FELL OFF WHEN FLAPS EXTENDED. REMOVED AND REPLACED LEFT I/B SPOILER REF MM 27-62-01. PERFORMED GENERAL VISUAL INSPECTION OF LEFT AND RIGHT WINGS FUSELAGE AFT OF WINGS AND TAIL SECTION. REF PTT2642031 FOUND SMALL DENT ON LEFT SIDE OF VERT STAB. NO OTHER DAMAGE NOTED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 88,116 hrs · 10,404 cycles

EMERGENCY EXIT LIGHT FLOOR STRIP FLASHING INTERMIT BY SEATS 19, 20, 21 AND 22C. REPLACED EEL LIGHT ASSY AT SEAT 19C AND PWR SUPPLY M6003 ABOVE DOOR 2L. REF SSM 33-51-03 WD 33-51-33 AND IPC 33-51-04. OPS CHECK OK.

Part: ROD — WORN (RT WLG DOOR) · airframe 88,061 hrs · 10,398 cycles

VIBRATION FROM MAIN GEAR RETRACTION REPORTED ON TAKEOFF. FLIGHT CREW WILL FILL OUT VIBRATION REPORT EVEN THOUGH EVERYTHING NORMAL IN FLT DECK CABIN ATTENDANT REPORTED VIBRATION FROM 4R MODERATE TO HEAVY VIBRATION DURING GEAR RETRACTION AND STOPPED WITH GEAR FULL UP. FLT CREW DID NOT FEEL VIBRATION. ONLY FELT BY FLT ATTENDANT AT DOOR 4 RIGHT. SUSPECT GEAR DOORS HAVE PLAY, HAVE DOOR BUSHINGS ON AOG. REPLACED LINKAGE ROD.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 87,877 hrs · 10,379 cycles

ELECTRICAL ODOR UPPER DECK STAIRWAY LIGHT. CHECKED FOUND THE ODOR IS FROM THE LIGHT L2976, REMOVED THE LIGHT L2976 AND DEACTIVATED BALLAST M7564, SO THE LIGHT L2977 IS INOP. FOUND ONE OF THE LAMP SOCKETS BURNT AND CRACKED.

Part: BALLAST — FAULTY (CABIN) · airframe 87,877 hrs · 10,379 cycles

ELECTRICAL ODOR UPPER DECK STAIRWAY LIGHT. CHECKED FOUND THE ODOR IS FROM THE LIGHT L2976, REMOVED THE LIGHT L2976 AND DEACTIVATED BALLAST M7564, SO THE LIGHT L2977 IS INOP ALSO. PLZ REF TO WDM 33-29-21. DF DUE TIME. FOUND ONE OF THE LAMP SOCKETS BURNT AND CRACKED. REPLACED BALLAST AND LAMP HOLDERS, CKS OK.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 87,865 hrs · 10,378 cycles

EMERGENCY LIGHT STRIP AT 1L IS INOPERATIVE. UNABLE TO DUPLICATE PROBLEM, RESEAT CONNECTION, EEL SYSTEM TESTED NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 87,865 hrs · 10,378 cycles

EEL DOOR 2L FLICKERS UNABLE TO DUPLICATE PROBLEM. RESEAT CONNECTION, ALL CHECKS NORMAL.

Part: CABLE — UNSECURE (GALLEY) · airframe 87,480 hrs · 10,341 cycles

BEFORE PUSHBACK FLT ATTENDANT REPORT AFT GALLEY ONE PIGTAIL CABLE INOP. RE-SECURED CABLE OKAY.

Part: TRIM PANEL — DAMAGED (CABIN) · airframe 87,262 hrs · 10,322 cycles

ON CM CHECK FOUND LAV 101 LEFT DOOR SIDE EEL PLASTIC TRIM LOWER DAMAGE. SIDE TRIM REPLACED.

Part: SEALANT — DISPLACED (NR 2 PYLON) · airframe 87,248 hrs · 10,321 cycles

FUEL LEAKING UNDER WING JUST OUTBOARD OF NR 2 ENGINE FWD PYLON, FUEL LEAK UNDER WING RUNNING TO FUSELAGE. FOUND FUEL LEAKING FROM UPPER OR 2ND FROM TOP BOLT ON PYLON LINK BRACKET, ABOVE PANEL 521AB. ARROW POINTS TO LEAKING BOLT, SEALANT PARTIALLY REMOVED FROM BOLT. AREA IS DIRECTLY OVER ENGINE 2. CLEANED SEALANT OFF OF BOLTS APPLIED SEALANT TO BOLTS INSIDE AND OUTSIDE OF TANK AT 240 0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,248 hrs · 10,321 cycles

DOOR 5L THRESHOLD EEL LIGHT INOP. RELAMPED, OP CHECKED OK.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 87,248 hrs · 10,321 cycles

ROW 19ABC EEL LIGHTS INOPERATIVE. SECURED UNDERSEAT PLUG, OP CHECKED OK.

Part: BATTERY — FAULTY (CABIN) · airframe 87,198 hrs · 10,317 cycles

1L EEL STRIP FLICKERS ON THE WALL. REPLACED BATTERY, SYSTEM CHECKS GOOD.

Part: REVEAL — CRACKED (WINDOW) · airframe 87,187 hrs · 10,316 cycles

WINDOW 7J INNER PANE SEAL WEAK. FOUND WINDOW ASSY INNER BOTTOM CRACKED. ASSY CANNOT KEEP IN POSITION. INTERIM REPAIR WITH TAPE. MAKE CF ITEM. REMOVED AND REPLACED 7J WINDOW REVEAL AS REQUIRED. SHADE OPS CHECKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 86,824 hrs · 10,281 cycles

EMERGENCY LIGHT SEAT 42H BROKEN IN HALF. REPLACED EMERGENCY LIGHT SEAT 42H, OPERATIONAL CHECK OKAY.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT) · airframe 86,824 hrs · 10,281 cycles

CAPT'S WINDSHIELD AIR FAILED. CREW COMMENTS: AT FL330. FOUND BOTH CAPT & F/O WINDSHIELD DEFOG VALVES FAILED CLOSED. MANUALLY OPENED BOTH VALVES PER MEL REQUIREMENTS, AIRFLOW NOTED ON BOTH CAPTS & F/O'S WINDOWS. REPLACED CIRCUIT BREAKER C10291 ON THE P180 PANEL, OPS CHECK GOOD PER AMM.

Part: COVER — UNSECURE (ESCAPE HATCH) · airframe 86,482 hrs · 10,248 cycles

COCKPIT ESCAPE HATCH NEEDS TO BE RETAPED. SECURED ESCAPE HATCH COVER.

Part: ACTUATOR — FAILED (APU DOORS) · airframe 86,459 hrs · 10,246 cycles

ON PUSHBACK, APU INLET DOOR ADVISORY AND STATUS MESSAGE. FOUND APU DOOR IS PARTIALLY OPENED. INSTALLED NEW ACTUATOR.

Part: SOCKET — FAULTY (CABIN LIGHT) · airframe 86,380 hrs · 10,238 cycles

UPPER DECK CEILING LIGHT AT SEAT 17 IS INOPERATIVE. REPLACED LIGHT SOCKETS. CHECKS NORMAL.

Part: CONTROLLER — FAULTY (REFUEL VALVE) · airframe 86,033 hrs · 10,205 cycles

AIRCRAFT HAVING TROUBLE ACCEPTING FUEL. MANIFOLD NOT OPENING. REPLACED NR 3 REFUEL VALVE CONTROLLER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,004 hrs · 10,203 cycles

EMERGENCY CEILING LIGHT AT ROW 50. RELAMPED, OPS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 86,004 hrs · 10,203 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 51 ABC. SECURED CONNECTOR, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,004 hrs · 10,203 cycles

EMERGENCY LIGHT UPPER DECK CEILING AT ROW 13 INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,552 hrs · 10,159 cycles

UPPER DECK CEILING EMERGENCY LIGHTS 2EA IS INOPERTIVE. RELAMPED CEILING LIGHTS IN UPPER DECK CEILING. CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,552 hrs · 10,159 cycles

SEAT 53 HJK EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, OPS CHECKED NORMAL

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,552 hrs · 10,159 cycles

R2 DOOR GALLEY AREA LOWER SIDEWALL EMERGENCY LIGHT IS INOPERATIVE. RELAMPED. CHECKED NORMAL PER MM 33-51-12.

Part: LAMP — INOPERATIVE (CABIN) · airframe 85,416 hrs · 10,145 cycles

SEAT BELT AND NO SMOKE SIGN INOPERATIVE. REPLACED LAMPS, OPS CHECKED OKAY.

Part: DRAIN VALVE — LEAKING (HORIZ STAB) · airframe 85,119 hrs · 10,114 cycles

FOUND LEFT HST SUMP DRAIN SOLENOID LEAKING EXTERNALLY. RE-ACTIVATED HST ISO VALVES DV439 AND DV440 AS REQUIRED. ON ARRIVAL CHECK FOUND FUEL SEEPAGE FROM RT HORIZONTAL STABILIZER DRAIN HOLE NEAR STA 285. MUST EMPTY TANK AND CONFIRM NO LEAKS BEFORE DEPT. HST IS TO REMAIN EMPTY. STABILIZER TANK EMPTIED AND NO LEAK AND LOCK OUT NOT TO USE PER MEL 2817E BY BOTH FWD IS O VLV ACT CONNECTORS DV439 DV440 DISCONNECTED AND VLV MANUAL OVERRIDE LEVERS SECURED CLOSED BY WIRE. REPLACED LT HST TANK SUMP DRAIN VALVE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,983 hrs · 10,100 cycles

DOOR 2 GALLEY AISLE EMERGENCY LIGHT FWD WALL INOPERATIVE. RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,983 hrs · 10,100 cycles

UPPER DECK DOOR RT EMERGENCY LIGHT INOP. RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,983 hrs · 10,100 cycles

DOOR 4 LT FWD EMERGENCY SILL LIGHT INOP. RELAMPED, CHECKS NORMAL.

Part: FIRESHIELD — WORN (NR 4 COWLING) · airframe 84,983 hrs · 10,100 cycles

NR 4 ENG OUTBOARD CORE COWL TRAILING EDGE IS WORN. NR 4 ENGINE, RT CORE COWL FIRESHIELD WORN. REPLACED CORE COWL.

Part: LINE — LEAKING (CARGO BAY) · airframe 84,601 hrs · 10,061 cycles

WATER LEAKING FROM THE BELLY OF FUSELAGE UNDER THE AFT CARGO PIT. COMPLIED WITH MEL 3810W, ONLY TO REVERSE MEL PROCEDURE AFTER LINE REPLACED. NEW LINE INSTALLED AND LEAK CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,409 hrs · 10,042 cycles

SEAT ROW 54HJK TO 60 HJK EMERGENCY LIGHTS IS INOP. REPLACE BATTERY PACK FOR EMERGENCY LIGHTS SEAT ROWS 54-60 HJK. CHECKS NORMAL.

Part: CIRCUIT CARD — FAILED · airframe 84,300 hrs · 10,034 cycles

"HUMID FLT DK" EICAS ADVISORY MESSAGE DISPLAYED. FLIGHT DECK HUMIDIFICATION SYSTEM FAILURE. REPLACED ECS CARD. YMLA13 CARD. OPS CHECKED COVERED ON DF444. REPLACED & REINSTALLED FLIGHT DECK HUMIDIFIER, OPS TESTED GOOD.

Part: BALLAST — FAULTY (CABIN LIGHTS) · airframe 83,970 hrs · 10,000 cycles

G1 GALLEY LIGHT REPORTED FLASHING. AREA INSPECTED. NO ODOR OR EVIDENCE OF ARCING. INSPECTED BEHIND CIRCUIT BREAKER PANEL. NO ODOR OR EVIDENCE OF ARCING. RELAMPED LIGHT ASSY. NO HELP. CIRCUIT BREAKER PULLED AND COLLARED. ALL OTHER COMPONENTS OPS NORMAL. . REPLACED BALLAST M002, OPS CHECKED OKAY.

Part: TRIM PANEL — MISINSTALLED (RUDDER) · airframe 83,970 hrs · 10,000 cycles

RUDDER AND AILERON TRIM PANEL IS INSTALLED THE WRONG WAY AND USE OF TRIM IS OPPOSITE OF WHA FOUND AIL, RUD TRM CTL PANEL MOUNTED UP SIDE DOWN AND TRIM INDICATOR IN WRONG POSITION AS STATED. REMOVED AIL, RUD TRIM CTL PANEL TO CORRECT CONFIGURATION AND RELOCATED TRIM INDICATOR TO PROPER POSITIONS PER AMM. SYSTEMS OP CK OK. ITEM SHOULD READ REMOVED AND REPLACED AILERON & RUDDER TRIM CONTROL MODULE PER AMM AND REMOVED AND REPLACED RUDDER TRIM INDICATOR PER AMM. SYSTEMS OP CK OK.

Part: FRAME — CRACKED (BS 2120) · airframe 83,896 hrs · 9,991 cycles

BS 2120 FRAME UPPER STRUCTURE CRACKED BETWEEN RBL 40 & RBL 45.3. MAJOR REPAIR ACCOMPLISHED, MANUFACTURED & INSTALLED NEW FRAME SECTION REF ECRA 5300-01382, EN 747EN-53-038 5.

Part: INTERCOSTAL — CRACKED (BS 1220) · airframe 83,896 hrs · 9,991 cycles

LEFT OVERWING INTERCOSTAL WEB CRACKED BS 1220. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB SECTION PER SB 747-53A2750.

Part: INTERCOSTAL — CRACKED (BS 1220) · airframe 83,896 hrs · 9,991 cycles

RIGHT OVERWING INTERCOSTAL WEB CRACKED BS 1220. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB SECTION PER SB 747-53A2750.

Part: INTERCOSTAL — CRACKED (BS 1200) · airframe 83,896 hrs · 9,991 cycles

RIGHT OVERWING INTERCOSTAL WEB CRACKED BS 1200. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB SECTION REF SB 747-53A2750.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,880 hrs · 9,990 cycles

FOUND BULGES IN FUSELAGE SKIN AT AND BETWEEN RIVETS IN STR 51R AND 51L APPROX BODY STA 1940-1950. PERFORMED VISUAL INTERNAL INSPECTION, CORROSION APPEARS TO BE LOCALIZED TO AREA BETWEEN STRINGERS AND SKIN AT TWO LOCATIONS STR 51L&R STA 1945 LUMP APPEARANCE LATER FOUND TO HAVE EXTENSIVE CORROSION ON THOSE STRINGERS. CORROSION FOUND ON LWR SURFACE OF STR 51L & 51R. MATERIAL LOSS BEYOND LIMITS AFTER CLEAN UP. CUT OUT DAMAGED SECTIONS OF BOTH STRINGERS. ACPD EXTRUDED STRINGER REPAIRS AT BOTH STRINGERS BY INSTALLING 094372U-CHANNEL AND REINFORCING SIDE ANGLES. CUT OUT DAMAGED SECTION OF SKIN, INSTALLED REINFORCING EXTERNAL DOUBLER & TRIPLER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,829 hrs · 9,986 cycles

TWO EMERGENCY AISLE CROSSOVER LIGHTS INOP AT BOTTOM OF STAIRWAY. RELAMPED, OPS CHECK OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 83,729 hrs · 9,976 cycles

SEAT MOUNTED EMERGENCY LIGHT MISSING. REPLACED MISSING EMERGENCY LIGHT.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 83,459 hrs · 9,948 cycles

CAPTAIN'S OXYGEN MASK WILL NOT TEST. REPLACED OXYGEN MASK PER 35-11-18-0401, 35-11-00 PG 506.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,388 hrs · 9,942 cycles

EMERGENCY LIGHT AT SEAT 25 ABC INOPERATIVE. RELAMPED, OP CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,388 hrs · 9,942 cycles

EMERGENCY LIGHT AT SEAT 56 ABC INOPERATIVE. RELAMPED, OP CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,388 hrs · 9,942 cycles

AFT FLOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.

Part: COWLING — DAMAGED (NR 4 ENGINE) · airframe 83,077 hrs · 9,908 cycles

UNDERSIDE OF NR 4 ENGINE NACELLE IS DAMAGED. REPLACED INLET COWL NR 4 ENGINE REF MM & CHECKS REF JRH 2-86-1, ALL SATISFACTORY, NO FURTHER DEFECTS.

Part: NOSE COWL — DAMAGED (NR 4 ENGINE) · airframe 83,077 hrs · 9,908 cycles

NOSE COWL DAMAGED BY GROUND EQUIP. UNDERSIDE OF NUMBER 4ENGINE NACELLE IS DAMAGED. CARRIED OUT INSPECTION. WILL REQ RPL OF NOSE COWL. PCN 185-9199 COWL AND SLING 056-0097 ON ORDER. RPLC'D INLET COWL NR 4 ENGINE AND CHECKS ALL SATISFACTORY, NO FURTHER DEFECTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,835 hrs · 9,879 cycles

DOOR 3R FWD SILL EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL.

Part: SKIN — CORRODED (RT WING) · airframe 82,835 hrs · 9,879 cycles

RT UPPER WING SURFACE HAS CORROSION JUST FWD OF DOOR 3R APPROX 2FT OUT FROM WING ROOT. BLENDED AREA, PERFORMED ULTRA SOUND INSP FOUND .310" MATERIAL REMAINING AT DEEPEST BLENDED AREA. ACP-HFEC SURFACE EDDY CURRENT CHECK FOR CRACKS AT WING SURFACE INDICATED BLEND AREA =REF 747 NDT PT 1 51-06-00, NO CRACKS DETECTED AT THIS TIME. ACCOMPLISHED ROTOPEENING, ALODINE, PRIME AND PAINT. REF EVA-81238 ACCOMPLISHED, CLASSIFIED AS MINOR REPAIR. NO FURTHER ACTION REQUIRED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,835 hrs · 9,879 cycles

UPPER DECK RIGHT WING DOOR 2 EA EMERGENCY LIGHTS IS INOP. REPLACED RT UPPER DECK EMERGENCY BATTERY PACK, ALL LAMPS CHECK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,835 hrs · 9,879 cycles

LEFT OVERWING SECOND LIGHT ASSY FWD LAMP IS INOP. RELAMPED, OP CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,835 hrs · 9,879 cycles

UPPER DECK EMERGENCY LIGHT ABOVE STAIRWAY IS INOP. REPLACED EEL BAT PACK, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,835 hrs · 9,879 cycles

SEAT 53HJK EMERGENCY LIGHT IS INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 82,835 hrs · 9,879 cycles

SEAT 25 HJK EMERGENCY LIGHT IS INOP. RESECURED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: HOUSING — LEAKING (PCU) · airframe 82,340 hrs · 9,824 cycles

FUEL LEAKING FROM RT HST INBD PCU HOUSING DRAIN HOLE. BOROSCOPED RT INBD HST PCU ACT HOUSING. FOUND SEVERAL LEAKS AT INBD SIDE FASTENERS MID SECTION.BLOWN BACK TO CLEAN AND VERIFIED SOURCE OF LEAK. DEFUELED HST AND SUMPED. BLOW BACK SUSPECTED AREA, NO LEAK DETECTED, SCRAPED SEALANT APPROX 2 IN LONG AT LOWER AFT CORNER OF PCU HOUSING. APPLIED SEALANT.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 82,195 hrs · 9,808 cycles

ON TAXI OUT AT SFO FUEL WAS COMING OUT THE RT SIDE VENT. WILL NEED TO CHECK FUEL FILL VALVES PER MM. IF GOOD WILL NEED TO CHECK FUEL VENT VALVES. ALL TANK FUEL VALVES OPERATE NORMAL AND ARE CLOSING. FILLED WING TANKS TO FULL TAXIED AIRCRAFT 15 MINUTES NO FUEL LEAKAGE FROM WINGS, DID OBSERVE WATER CONDENSATION RUNNING OFF AFT EDGE OF WING IN WING VENT AREA DURING TAXI. FUEL LEVELS STAYED EQUAL NO TRANSFER PROBLEM.

Part: LIGHT — UNSECURE (CABIN) · airframe 82,195 hrs · 9,808 cycles

LOWER EXIT PATH LIGHTING AT 2R IS HANGING OFF. SECURED LIGHT, OP'S CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 82,138 hrs · 9,801 cycles

LAV 102 LOWER CORNER EMERGENCY LIGHT BROKEN. SECURED EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,730 hrs · 9,756 cycles

TWO EA EMERGENCY LIGHTS NEAR FLOOR BETWEEN DOOR TWO LEFT AND TWO RIGHT LIGHTS INOPERATIVE. RELAMPED, OPS CHECKED GOOD.

Part: COVER — DAMAGED (COCKPIT) · airframe 81,319 hrs · 9,712 cycles

COCKPIT EVAC HORN COVER SMASHED IN. EVAC HORN COVER DAMAGED. NO PART AVAIL. HORN TEST - OK. REPLACED DAMAGED EVAC PANEL.

Part: CONTROL UNIT — FAULTED (FUEL SYSTEM) · airframe 81,212 hrs · 9,698 cycles

FUEL IMBALANCE BETWEEN NR 2 AND NR 3 TANKS. CONFIRMED UNWANTED FUEL TRANSFER TO NR 3 MAIN TANK. WITH CENTER PUMPS ON TRANSFER RATE 1000LB IN 10 MIN. WILL REQUIRE TANK ENTRY FOR INSP OF NR 3 MAIN TANK PLUMBING. FOUND NR 2 MAIN JETTINSON TRX VLV INOP AND NR 3 MAIN FUEL VALVE LEAKING FUEL. REPLACED NR 2 MAIN JETTISON VLV PER MM. NEEDS OPS CHECK PER MM. REPLACED NR 3 MAIN OTBD REFUEL VALVE CONTROL UNIT, OPS AND LEAK CHECKED GOOD.

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 81,212 hrs · 9,698 cycles

REPAIR HAS DEPARTED AIRCRAFT FROM NR 4 ENGINE ACOUSTIC LINER ON RT REVERSER SLEEVE BETWEEN 3 AND 4 O'CLOCK. DAMAGED AREA IS 5.0" LONG X 1.25" WIDE X 0.5" DEEP. INSTALLED NEW SLEEVE PER MM, OPS CHECKED GOOD.

Part: ACOUSTIC PANEL — DAMAGED (NACELLE) · airframe 81,199 hrs · 9,697 cycles

ON ARRIVAL INNER ACOUSTIC PANEL DAMAGED BETWEEN 3 AND 4 O'CLOCK POSITION 4"X 2"X .25" DENT-PUNCTURE. AREA REPAIRED PER MM 54-00-01 REPAIR 2 AND AREA TAPED.

Part: PANEL — MISSING (NR 4 STRUT) · airframe 80,802 hrs · 9,650 cycles

NR 4 ENGINE INTERMEDIATE CASE STRUT FAIRING AT APPROX 7 O'CLOCK POSITION, INNER PANEL MISSING. INSTALLED AND SECURED PANEL TO NR 4 ENG STRUT FAIRING.

Part: SLEEVE — GOUGED (THRUST REVERSER) · airframe 80,802 hrs · 9,650 cycles

6 INCH GOUGE IN NR 4 INBD REVERSER SLEEVE AT BOTTOM APROX 06:30. INSIDE SLEEVE. REMOVED NR 4 ENG INBD THRUST REVERSER SLEEVE PER MM. INSTALLED NR 4 THRUST REVERSER SLEEVE INBOARD SIDE. MANUALLY RETRACTED REVERSER HALF. UNABLE TO CHECK OPERATION DUE TO REVERSER SLEEVE NOT LOCKING AND NO GREEN INDICATIONS. MANUALLY RETRACTED REVERSER HALF. UNABLE TO CHECK OPERATION DUE TO REVERSER (PARTIAL). REPLACED REVERSER SLEEVE, ALL CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,746 hrs · 9,644 cycles

EMERGENCY EXIT LIGHT SIGN INOPERATIVE. UPPER DECK LT DOOR UPPER EXIT SIGN. REPLACED BATTERY. OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,746 hrs · 9,644 cycles

EMERGENCY EXIT LIGHT SIGN INOPERATIVE. UPPER DECK CEILING JUST AFT OF DOORS. REPLACED BATTERY. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,746 hrs · 9,644 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. UPPER DECK LT DOOR INTEGRAL LIGHTS. REPLACED BATTERY POWER SUPPLY AND BATTERY. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ROW 17) · airframe 80,746 hrs · 9,644 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE UPPER DECK CEILING JUST AFT OF ROW 17. REPLACED LIGHT ASSY. OPS CHECKED NORMAL.

Part: LIGHT — MISSING (SEAT 37C) · airframe 80,570 hrs · 9,624 cycles

LOW TECH REPORTS EMERGENCY PATH LIGHT MISSING AT SEAT 37C. REPLACED MISSING EMERGENCY PATH LIGHT ASSY, CHECKED OK IAW MM.

Part: START VALVE — FAULTY (NR 2 ENGINE) · airframe 80,508 hrs · 9,618 cycles

ON PRE-FLT CHK FOUND NR 2 ENG START VALVE STATUS MESSAGE. FAULTED ASCTU FAIL OR BLEED -2 ELECTRICAL FAIL MESSAGE 36312, OK TO DEFER IAW MEL. ALSO FAULTED ENGINE NR2 START VALVE MESSAGE 72085.

Part: FEEDER CABLE — MISROUTED (EMERGENCY LIGHT) · airframe 80,490 hrs · 9,616 cycles

FOUND FEEDER WIRE ROUTED ON GALLEY WALL UNDER KICK STRIP AND UNDER CORNER BUMPER. ROUTED IAW REF IPC.

Part: LIGHT — UNSECURE (LAVATORY) · airframe 80,373 hrs · 9,602 cycles

EMERGENCY LIGHT ON LAV WALL BY JUMPSEAT AT 2R IS FALLING OFF THE WALL, TAPED TO HOLD UP. SECURED LIGHT WITH CLEAR TAPE. SECURED LIGHT.

Part: SCAVENGE PUMP — FAULTY (CENTER TANK) · airframe 80,303 hrs · 9,593 cycles

CTR TANK DID NOT SCAVANGE COMPLETELY, .8 USEABLE FUEL AFTER PUMP OFF. AIR MODE SCAVENGE SYST TEST FAILED. SCAVANGE PUMP WAS REPLACED AND LEAKED CHECKED. SCAV PUMP CB PULLED & COLLARED IN P414 PANEL. THIS SCAVG TEST WILL TAKE APPPOX 3-4 HRS. ADJUSTED TO REFLECT TIME REMAINING ON DF155 ORIGINALLY. DEFERRED ON 04JAN11. REPLACED SINGLE POINT SENSOR CONTROL CARD A2. OPS CHECKED GOOD. DID CTR WING TANK SCAVENGE SYS TEST. RANG OUT WIRES FROM P.180 TO RELAY R296. ALSO FROM RELAY R296 TO DM810 PUMP CONNECTOR REF WD, ALL CHECKED NORMAL. RAN CTR WING TANK SCAVENGE SYS TEST IN AIR MODE. TEST PASSED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,153 hrs · 9,576 cycles

EMERGENCY LIGHT ON WALL DOOR 2R 1 INOP. RELAMPED. OP CHECKED NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 80,153 hrs · 9,576 cycles

SEAT 2A EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE UNDER FOOT CUSHION, OPS CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 79,667 hrs · 9,513 cycles

RT WINDSHIELD OUTER PANE CRACKED. WINDOW HEAT WAS WORKING PRIOR TO CRACKING. EICAS MSG AFTER CRACKED. R1 WINDSHIELD REPLACED IAW AMM AND CHECKS SATISFACTORY.

Part: FAIRING — CRACKED (RT WING) · airframe 79,667 hrs · 9,513 cycles

ON ARRIVAL FOUND RT WING INBD STRUT DOOR INBD FAIRING WITH CRACK APPROX 6 INCHES LONG AT THE T/E. FAIRING REPLACED IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,625 hrs · 9,508 cycles

EMERGENCY EXIT LIGHT INOP. SEAT ROW 19 LT. RELAMPED, CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,625 hrs · 9,508 cycles

EMERGENCY EXIT LIGHT INOP, UPPER DECK CEILING JUST AFT OF ROW 17. RELAMPED, CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,625 hrs · 9,508 cycles

EMERGENCY EXIT LIGHT INOP, SEAT ROW 56 LT. RELAMPED, CHECKS OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 79,077 hrs · 9,445 cycles

EMERGENCY EXIT LIGHT INOP, LOWER WALL ACROSS DOOR 4 RT. SECURED CONNECTOR, OPS CHECKED NORMAL.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,077 hrs · 9,445 cycles

EMERGENCY EXIT LIGHT INOP, LOWER WALL ACROSS L3 DOOR. REPLACED POWER FEEDER CABLE. OPS CKS NORMAL.

Part: RESERVOIR — OUT OF TOLERANCE (RT PAX DOOR) · airframe 79,077 hrs · 9,445 cycles

PRESSURE CARTRIDGE ON UPPER DECK EMERGENCY POWER RESEVOIR FOR RT DOOR OUT OF TOLERANCE. REPLACED UPPER DECK DOOR EMERGENCY POWER RESERVOIR AND SQUIB ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,077 hrs · 9,445 cycles

EMERGENCY EXIT LIGHTS INOP. DOOR 2 GALLEY AREA 2 EA. OUTBD LOWER WALL. RELAMPED. OPS CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 79,077 hrs · 9,445 cycles

EMERGENCY EXIT LIGHT INOPERATIVE, SEAT ROW 56 LT, SECURED CONNECTOR. OPS CHECKED NORMAL.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 78,797 hrs · 9,416 cycles

CEILING PANEL AT SEAT 14AB PARTIALLY INSTALLED. CEILING LIGHT NEEDS BALLAST TO BE REPLACED. WAITING FOR ACFT TO RETURN FROM HIGH POWER RUN. PERSONAL TOOLS ARE ONBOARD. FINISHED INSTALLING CEILING PANELS CTR STRIPS AT 14AB.

Part: LIGHT — BROKEN (CABIN) · airframe 78,685 hrs · 9,402 cycles

BUSINESS CLASS GALLEY LT CROSS AISLE EMERGENCY LIGHT BROKEN. REPLACED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 78,488 hrs · 9,380 cycles

DOOR 4R AFT EXIT SIGN IS INOPERATIVE. REPLACED EXIT SIGN AND SECURED. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,488 hrs · 9,380 cycles

AFT GALLEY SIDEWALL EMERGENCY LIGHTS IS INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,488 hrs · 9,380 cycles

UPPER DECK RIGHT DOOR FWD EMERGENCY LAMP IS INOP. RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,488 hrs · 9,380 cycles

B-ZONE RIGHT CEILING EMERGENCY LIGHT IS INOP. RELAMPED LIGHT ASSY, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,488 hrs · 9,380 cycles

SEAT ROW 51 HJK EMERGENCY LIGHT IS INOPERATIVE. REPLACED EMERGENCY LAMP STRIP. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,488 hrs · 9,380 cycles

DOOR 5 RIGHT SLIDE EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, CHECKS NORMAL.

Part: DENSITOMETER — MALFUNCTIONED (FUEL SYSTEM) · airframe 78,249 hrs · 9,353 cycles

INTERMITTENT BLANKING OF THE NR 4 MAIN FUEL QTY IND AND TOTALIZER. NO TOTAL FUEL. NO CMC FUEL DISPLAY. NO KNOWLEDGE OF FUEL QTY MAIN TANK NR 4 QTY INDICATION INOP. ACP'D MEL 2841AC. REPLACED FUEL QUANTITY DENSITOMETER IN REF TO MM. GROUND - BITE CHECK PASSED.

Part: FIRE LOOP — FAILED (APU BAY) · airframe 78,167 hrs · 9,344 cycles

DET FIRE APU' EICAS ADVISORY MESSAGE DISPLAYED. APU FIRE LOOP A AND B FAILURE. CKD APU COMPART AREA, NO EVIDENCE OF FIRE. PERFORMED GROUND TEST, FOUND APU FIRE LOOP B FAIL , MSG 26037. LOOP A OPERATION NORMAL ALSO SQUIB TEST NORMAL. REF FIM 26-15-00-812-TASK 807, NOTE (A21) CARD HAD BEEN PREVIOUSLY REPLACED ON 11JUN10. PERFORMED CHECKED RESISTANCE BETWEEN PIN 19 AND PIN 20 AS REQUIRED PER FIM, RESISTANCE READ 24.95 K OHMS AND MEASURED PIN 19 AND 230640PIN20 TO GROUND, FOUND OPEN CIRCUIT. SUSPECT DETECTOR AT FAULT. APU FIRE TEST, PASSED. NO MSG FOUND. REPLACED FIRE LOOP DETECTOR. OPERATIONS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT ROW 56L) · airframe 77,975 hrs · 9,324 cycles

EMERGENCY EXIT EMERGENCY LIGHT INOP. SEAT ROW 56 LT. REPLACED LIGHT ASSY OPS CKS. NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,975 hrs · 9,324 cycles

EMERGENCY EXIT LIGHT INOP. DOOR 2 GALLEY AREA RT LOWER WALL. RELAMPED. OPS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 77,975 hrs · 9,324 cycles

EMERGENCY EXIT LIGHTS INOP. FIRST CLASS AREA SEAT ROWS 2 THRU 4 INBD SEATS. SECURED CONNECTOR. OPS CKS NORMAL.

Part: FEEDER CABLE — SATURATED (EMERGENCY LIGHTS) · airframe 77,975 hrs · 9,324 cycles

EMERGENCY EXIT LIGHTS INOP. SEAT ROWS 45 THRU 53 LT, DOOR 4 LT FWD EXIT SIGN, DOOR 4 RT AFT EXIT SIGN, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LT AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON ACFT. FOUND WATER PUDDLING IN GALLEY AREA UNDER GALLEY MAT AT EMERGENCY LIGHT CONNECTOR SHORTING EMERGENCY LIGHTS. DRIED AREA OF WATER, EMERGENCY LIGHTS CK NORMAL AT THIS TIME.

Part: LIGHT — DAMAGED (SEAT 19C) · airframe 77,324 hrs · 9,248 cycles

SEAT 19C EMERGENCY LIGHT DAMAGE. REPLACED EMERGENCY LIGHT ASSY. CK OK.

Part: FIRE LOOP — FAULTY (CARGO BAY) · airframe 77,287 hrs · 9,236 cycles

FWD CARGO LOOP 1 EICAS MESSAGE. LAST MINUTE CALL IN, NO TIME TO T/S. ORDERED PART PCN 585-4855. OSTF:S1481. FOUND PRESENT LEG FAULT MSG 26160 NOT ACTIVE, NO EXISTING FAULTS, FIRE SYS TEST OK, NO FURTHER ACTION IS REQUIRED.

Part: FIRE LOOP — SHORTED (NR 4 NACELLE) · airframe 77,282 hrs · 9,235 cycles

'ENG 4 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 4 FIRE LOOP B FIRE OR FAULT OUTPUT. CREW COMMENTS: REPEAT ENG 4 FIRE LOOP B STATUS MSG. REPLACED R7223 RELAY IAW FIM. PCN 585-1052 PER MM 24-31-03, NO HELP. REPLACED TS682 & TS683 FIRE DETECTION LOOPS ENG 4, NO HELP. "ENG 4 FIRE LP B" STATUS MSG SHOWS ON EICAS. AFTER REPLACEMENT OF WIRING, SYS STILLS FAILS TEST. FOUND UPPER AFT LOOP HAD INTERMITTENT RESISTANCE TO THE CASE OF DETECTOR TS681, REPLACED UPPER AFT LOOP AGAIN, GROUND TEST PASSED, NO EXISTING FAULT. NO STATUS.

Part: LIGHT — MISSING (CABIN) · airframe 77,287 hrs · 9,236 cycles

THE 18 ABC EEL STRIP MISSING. REPAIRED EEL STRIP WITH ORIGINAL. CHECKS OK ON GROUND.

Part: LIGHT — BROKEN (SEAT 19C) · airframe 77,159 hrs · 9,215 cycles

SEAT 19C HAS BROKEN AISLE EMERGENCY LIGHT. REPLACED SEAT EMERGENCY LIGHT. OPS CK GOOD.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 76,709 hrs · 9,155 cycles

NEED 2 PAIR SMOKE GOGGLES F-COCKPIT. REPLACED GOGGLES AS NEEDED.

Part: STRUCTURE — CRACKED (BS 450 S10R) · airframe 76,508 hrs · 9,128 cycles

FOUND FWD FASTENER HOLE CRACKED AT STR 10R BS 450. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: STRUCTURE — CRACKED (BS 500 S10R) · airframe 76,508 hrs · 9,128 cycles

FOUND FWD AND AFT FASTENER HOLES CRACKED AT STR 10R BS 500. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: FITTING — CRACKED (R3 DOOR) · airframe 76,508 hrs · 9,128 cycles

DOOR 3R LWR FWD CORNER REVEAL FITTING CRACKED AT BS 1265. MAJOR REPAIR ACCOMPLISHED: MFG AND INSTALLED NEW 2 PIECE FITTING.

Part: WEB — CRACKED (R4 DOOR) · airframe 76,508 hrs · 9,128 cycles

DOOR 4R, FWD AND AFT LWR CORNER WEBS CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLERS.

Part: STRINGER — CRACKED (BS 480 S10L) · airframe 76,508 hrs · 9,128 cycles

FOUND FWD FASTENER HOLE CRACKED AT STR 10L BS 480. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: STRUCTURE — CRACKED (BS 460 S10L) · airframe 76,508 hrs · 9,128 cycles

FOUND FWD FASTENER HOLE CRACKED AT STR 10L BS 460. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: FITTING — CRACKED (L3 DOOR) · airframe 76,508 hrs · 9,128 cycles

DOOR 3L LWR FWD CORNER REVEAL FITTING CRACKED AT BS 1265. MAJOR REPAIR ACCOMPLISHED: MFG AND INSTALLED NEW 2 PIECE FITTING.

Part: STRUCTURE — CRACKED (BS 480 S8L) · airframe 76,508 hrs · 9,128 cycles

FOUND FWD FASTENER HOLE CRACKED AT STR 8L BS 480. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: DOOR FRAME — CRACKED (5R DOOR) · airframe 76,508 hrs · 9,128 cycles

DOOR 5R UPPER FRAME CRACKED AT 2 EACH GATE ATTACH FASTENER HOLES, 9TH AND 11TH HOLES FROM FWD END. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: STRUCTURE — CRACKED (BS 500 S10L) · airframe 76,508 hrs · 9,128 cycles

FOUND FASTENER HOLE CRACKED AT STR 10L BS500. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: DOOR FRAME — CRACKED (L4 DOORWAY) · airframe 76,508 hrs · 9,128 cycles

DOOR 4L UPPER FRAME CRACKED AT 3 EACH GATE ATTACH FASTE NER HOLES, 7TH, 8TH, & 9TH HOLES FROM FWD END. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: STRUCTURE — CRACKED (BS 480 S8R) · airframe 76,508 hrs · 9,128 cycles

FOUND FWD FASTENER HOLE CRACKED AT STR 8R BS 480. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: LAMP — INOPERATIVE (INDICATOR LIGHT) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK RT EMERGENCY EXIT BATTERY INDICATOR LIGHT INOPERATIVE. RELAMPED, OP CHECK OK.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 76,508 hrs · 9,128 cycles

DOOR 2L UPPER FRAME CRACKED AT GATE ATTACH HOLE, 9TH HOLE FROM FWD END. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE.

Part: FLOORBEAM — MISREPAIRED (BS 1265) · airframe 76,508 hrs · 9,128 cycles

DURING REPAIR OF MAIN DECK FLOORBEAMS AT BS 1265 LT AND RT FOUND REPAIR ANGLES WITH SHORT EDGE MARGIN. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED NEW REPAIR ANGLES AT BS 1265 LT AND RT.

Part: FRAME — CRACKED (BS 1180) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK BS 1180 RT FRAME, TENSION TIE CRACKED AT 8 HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED CHANNEL AND REPAIR ANGLES.

Part: FRAME — CRACKED (BS 1120) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK BS 1120 LT FRAME AND TENSION TIE CRACKED. FRAME CRACKED AT 4 HOLES, TENSION TIE CRACKED AT 8 HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CHANNEL SECTION AND REPAIR ANGLES.

Part: FRAME — CRACKED (BS 1200) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK BS 1200 LT FRAME AND TENSION TIE CRACKED. FRAME CRACKED AT 2 HOLES, TENSION TIE CRACKED AT 6 HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CHANNEL SECTION AND REPAIR ANGLES.

Part: FRAME — CRACKED (BS 1265) · airframe 76,508 hrs · 9,128 cycles

MAIN DECK BS 1265 RT FRAME WEB CRACKED AT THE NR 1 HOLE. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME WEB, INTERCOSTAL UPPER CHORD AND WEB.

Part: FRAME — CRACKED (BS 1160) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK BS 1160 RT FRAME, TENSION TIE CRACKED AT 3 HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CHANNEL SECTION AND REPAIR ANGLES.

Part: FRAME — CRACKED (BS 1265) · airframe 76,508 hrs · 9,128 cycles

MAIN DECK BS 1265 LT FRAME WEB CRACKED AT NR 1 HOLE. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME WEB, INTERCOSTAL UPPER CHORD AND WEB.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 76,508 hrs · 9,128 cycles

LT AFT WING TO BODY FAIRING, OVERWING EMERGENCY EXIT LIGHT INOP. FOUND LIGHT GROUND TERMINAL BROKEN. REPLACED TERMINAL. LIGHT OP CHECK OK.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 76,508 hrs · 9,128 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP, 3RD FROM FWD. REPLACED LIGHT ASSY, OP CHECK OKAY.

Part: SKIN — MISREPAIRED (BS 760-780 S24R) · airframe 76,508 hrs · 9,128 cycles

AN EXTERNAL DOUBLER IS INSTALLED WITH BLIND FASTENERS AT BS 760-780 STR 24R-25R. MAJOR REPAIR ACCOMPLISHED: REPLACED BLIND FASTENERS WITH SOLID FASTENERS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,508 hrs · 9,128 cycles

LT OVERWING FWD EMERGENCY EXIT LIGHT INOP. RELAMPED, OP CHECK OK.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK FRAME FAIL-SAFE CHORD CRACKED AT BS 1140 RT. MAJOR REPAIR ACCOMPLISHED: SPLICED IN NEW SECTION OF FAIL-SAFE CHORD.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK FRAME FAIL-SAFE CHORD CRACKED AT BS 1140 LT. MAJOR REPAIR ACCOMPLISHED: SPLICED IN NEW SECTION OF FAIL-SAFE CHORD.

Part: FRAME — CRACKED (BS 1220) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK FRAME FLANGE CRACKED AT BS 1220 LT AT TENSION TIE. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER.

Part: FRAME — CRACKED (BS 1160) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK BS 1160 RT FRAME CRACKED AT 4 HOLES COMMON TO TENSION TIE. MAJOR REPAIR ACCOMPLISHED: SPLICED IN NEW FRAME SECTION.

Part: FLOORBEAM — CORRODED (BS 900 LBL 20-40) · airframe 76,508 hrs · 9,128 cycles

MAIN DECK FLOORBEAM UPPER CHORD HAS CORROSION, BS 900, LBL 20 - LBL 40. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR.

Part: FRAME — CRACKED (BS 1160) · airframe 76,508 hrs · 9,128 cycles

UPPER DECK BS 1160 LT FRAME AND TENSION TIE CRACKED. FRAME CRACKED AT 4 HOLES, TENSION TIE CRACKED AT 6 HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR AT FWD TENSION TIE.

Part: SKIN — CRACKED (CARGO DOORWAY) · airframe 76,508 hrs · 9,128 cycles

AFT CARGO DOOR CUTOUT UPPER FWD CORNER SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL REPAIR.

Part: STRINGER — CRACKED (BS 1910 S8L) · airframe 76,508 hrs · 9,128 cycles

MAIN DECK, FUSELAGE STRINGER CRACKED AT ST 1910 STR 8L. MAJOR REPAIR ACCOMPLISHED: INSTALLED HAT SECTION REPAIR.

Part: SKIN — GOUGED (BS 2380 S19-20R) · airframe 76,508 hrs · 9,128 cycles

MAIN DECK AFT PRESSURE BULKHEAD FWD FACE SKIN GOUGED, BS 2380 STR 19R-20R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. INSTALLED REPAIR REF SRM 53-80-08 REPAIR 3 DETAIL 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,415 hrs · 9,120 cycles

EMERGENCY EXIT LIGHT INOP AFT CREW REST AREA STAIR ILLUMINATION LIGHT. REPLACED LAMPS AND OP CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 76,415 hrs · 9,120 cycles

EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5 RIGHT AFT LOWER WALL EEL. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,415 hrs · 9,120 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 17 LEFT AFT LIGHT. REPLACED LIGHT ASSY OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,415 hrs · 9,120 cycles

EMERGENCY EXIT LIGHT INOP, DOOR 2 LEFT CEILING ENTRY. RELAMPED, OPS CHECKS NORMAL.

Part: FEEDER CABLE — FAULTY (CABIN) · airframe 76,415 hrs · 9,120 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT 5E FWD AND AFT LIGHT ASSY'S. REPLACED POWER FEEDER CABLE, OPS CHECKS NORMAL.

Part: BLOWOUT PANEL — MISSING (LT WING) · airframe 76,063 hrs · 9,089 cycles

ON WALK AROUND, FOUND BLOWOUT PANEL MISSING ON BOTTOM OF LEFT WING, LEADING EDGE WING ROOT. CHECKED AREA IN LEADING EDGE AND FOUND NO DEFECTS. LOGISTIC PURCHASED PANEL PER SAMC PLNR. INSTALLED PANEL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 75,934 hrs · 9,078 cycles

EEL LIGHT AT SEAT 61H INOPERATIVE. SECURED CONNECTOR.

Part: TRANSFER VALVE — FAILED (NR 3) · airframe 75,020 hrs · 8,991 cycles

FUEL IMBALANCE MAIN 2-3. REPLACED NR 3 FUEL JETTISON TRANSFER VALVE BODY AND ACTUATOR. ACCOMPLISHED JETT TRANSFER VALVE GROUND TEST AND JETT TRANSFER VALVE-FUEL TRANSFER OPERATIONAL TEST. OPS CHECKED OKAY.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 74,850 hrs · 8,972 cycles

FUEL LEAK UNDER LEFT WING. FLIGHT DIVERTED. UNWANTED FUEL TRANSFER CONFIRMED. FUEL TRANSFER FROM CENTER TO NR 2 MAIN, 500LB IN 10 MIN. OPENING NR 2 FOR TROUBLESHOOTING, FOUND NR 2 MAIN OVERRIDE JETTISON PUMP DISCHARGE CHECK VALVE BAD. REPLACED JETTISON PUMP. NEEDS OPS CHECK. OP CHECKS GOOD. NO UNWANTED TRANSFER NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,371 hrs · 8,922 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,371 hrs · 8,922 cycles

EMERGENCY EXIT EMERGENCY LIGHT INOP AT SEAT 4J AFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 74,371 hrs · 8,922 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT 52 RIGHT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 74,240 hrs · 8,907 cycles

FUSELAGE SKIN DENTED BEYOND LIMITS OF SRM, BS 720-740, STR 25L-26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER WITH BLIND FASTENERS.

Part: LAMP — INOPERATIVE (DOOR 3L) · airframe 73,822 hrs · 8,856 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR 3 LT FWD. SILL LIGHT. RELAMPED, CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,822 hrs · 8,856 cycles

EMERGENCY EXIT LIGHT INOP. AT DOOR 3 LT FWD. SILL LIGHT. RELAMPED, CHECKS OK.

Part: BATTERY — ACTIVATED (CABIN) · airframe 73,822 hrs · 8,856 cycles

EMERGENCY EXIT EMERGENCY LIGHTS VERY DIM FROM SEATS 35 LT THRU 43 LT AND DOOR 3 LT FWD. EMERGENCY LIGHT EXIT SIGN ALSO VERY DIM. REPLACED BATTERY. OP CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,822 hrs · 8,856 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT 44 LT. RELAMPED, CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,822 hrs · 8,856 cycles

EMERGENCY EXIT LIGHT AT SEAT 44 RT INOP. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,822 hrs · 8,856 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT 46 LT. RELAMPED, OP CHECKS OK.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 72,527 hrs · 8,717 cycles

AFT GALLEY SMOKE APPEARING. OCCURRED JUST PRIOR TO LANDING AND ELECTRICAL POWER REMOVED FROM GALLEY AS A PRECAUTION. PER FLIGHT ATTENDENTS, THEY SAW A SMALL AMOUNT OF SMOKE COMING FROM AREA NEAR AFT LEFT COFFEE WARMER. OPERATED ALL AFT GALLEY EQUIPMENT. CHECKED AREA. NO SMOKE DETECTED. CLEANED COFFEE WARMER AS PRECAUTION. NO REPEAT OF REPORTED SMOKE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 72,527 hrs · 8,717 cycles

SMOKE APPEARED IN AFT GALLEY.

Part: UNKNOWN — SMOKE (AFT GALLEY) · airframe 72,527 hrs · 8,717 cycles

SMOKE APPEARED IN AFT GALLEY. PER FLIGHT ATTENDANT, SAW A SLIGHT AMOUNT OF SMOKE COMING FROM AREA NEAR AFT LEFT COFFEE WARMER. OPERATED ALL AFT GALLEY EQUIPMENT. CHECKED AREA. NO SMOKE DETECTED. GALLEY 428 NR 181 GETS TOO HOT. OPS OK. NO OTHERS DEFECTS NOTED.

Part: FIRE BOTTLE — MALFUNCTIONED (CARGO BAY) · airframe 72,467 hrs · 8,711 cycles

BTL LOW CARGO B MSG DISPLAYED AND DISCHARGE LIGHT ON OVERHEAD PANEL ILLUMINATED, NO FWD OR AFT LIGHT ON. REPLACED FIRE "B" BOTTLE.

Part: BOTTLE — LOW

LOW BOTTLE.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP JUST AFT OF SEAT 8 LEFT BELOW COAT CLOSET. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP FROM SEATS 6L THRU 8L. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP ACROSS LAV 104 LOWER WALL EEL. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED POWER FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP ACROSS LAV 100 LOWER WALL EEL. *S/D* FOUND FAULTY POWER FEED CABLE. REPLACED POWER FEEDER CABLE, OP CHECK NORMAL. AC OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP JUST AFT OF DOOR 1L LOWER WALL EEL. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP JUST TO THE RIGHT OF LAV 100 LOWER WALL EEL. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 54 HJK. *S/D* FOUND FAULTY LIGHT. REPLACED LIGHT, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 4A) · airframe 72,091 hrs · 8,673 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. *S/D* EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. AC OK FOR SERVICE.

Part: DOOR — OUT OF ADJUST (CARGO DOOR) · airframe 70,823 hrs · 8,547 cycles

FOUND AFT LOWER CORNER OF FWD CARGO DOOR NOT FLUSH WITH FUSELAGE GAP OF 5-32 OF INCH BETWEEN INNER DOOR SKIN AND OUTER FUSELAGE SKIN. PERMANENT REPAIR ACCOMPLISHED PER SRM 52-30-01. CONDITION IS ACCEPTABLE PER MM52-34-00. NO FURTHER ACTION REQUIRED. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,823 hrs · 8,547 cycles

EMERGENCY DOOR MOUNT LIGHT INOP AT DOOR 5R. REPLACED EMERGENCY DOOR MOUNT LIGHT OP CHECKED GOOD PER AMM 33-51-00 PB 500. AC OK FOR SERVICE.

Part: DOOR — OUT OF TOLERANCE (FWD CARGO) · airframe 70,823 hrs · 8,547 cycles

FWD CARGO DOOR AFT LOWER CORNER FAIR TOLERANCE OUT OF LIMIT. MAJOR REPAIR ACCOMPLISHED IAW SRM52-30-01 FIG 201. FAIR TOLERANCE CHECKED GOOD ACTUAL:0.020" PER MM52-34-00. NO FURTHER ACTION REQUIRED.AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,823 hrs · 8,547 cycles

EMERGENCY DOOR MOUNT LIGHT INOP AT 4R DOOR. REPLACED EMERGENCY DOOR MOUNT LIGHT OP CHECKS GOOD PER AMM 33-51-00 PB500. AC OK FOR SERVICE.

Part: SKIN — CRACKED (RT PYLON) · airframe 70,823 hrs · 8,547 cycles

RT WING TO NR 4 PYLON ATTACH AREA "D" L/E NOSE INTERNAL SKIN CRACKED (5") AND UPPER AND LOWER CHORD CRACKED.

Part: LIGHT — BROKEN (CABIN) · airframe 70,823 hrs · 8,547 cycles

SEAT EEL ASSY BROKEN AT SEAT 59BC. REPLACED EEL ASSY. OP CK'D NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 70,823 hrs · 8,547 cycles

LAV 111 SIDEWALL EEL LIGHT PIN BROKEN. FOUND CONNECTOR PIN BROKEN. REPLACED PIN OPS CHECKED OK. AC OK FOR SERVICE.

Part: PANEL — FAULTY (EMER EVAC SYS) · airframe 70,823 hrs · 8,547 cycles

EMERGENCY EVACUATION SYSTEM INTERMITTENT AT L3. FOUND EMERGENCY EVACUATION PANEL FAULTY. REPLACED EMERGENCY EVACUATION PANEL OP CHECK NORMAL PER MM25-63-01 PB400 PARA 2. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,823 hrs · 8,547 cycles

G5 GALLEY AREA EEL LIGHT INOP. REPLACED CABLE ASSY AND COVER OP CHECK NORMAL PER MM 33-51-12 PB 200 CONFIGURE 2 PARA 2. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,823 hrs · 8,547 cycles

EEL LIGHT INOP AT SEAT 3A AFT. REPLACED EEL LIGHT. OP CHK'D NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 70,591 hrs · 8,522 cycles

FLOOR EMERGENCY LIGHT FWD OF LAV 102 INOP. SECURED CONNECTOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,591 hrs · 8,522 cycles

FOUND CEILING EMERGENCY LIGHT ABOVE LAV 100 INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 70,591 hrs · 8,522 cycles

FOUND FLOOR EEL ACROSS DR 4R INOP. REPLACED LIGHT ASSEMBLY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 70,591 hrs · 8,522 cycles

FLOOR EEL INOP, SECURED CONNECTOR.

Part: LIGHT — INOPERATIVE (SEAT 47) · airframe 70,591 hrs · 8,522 cycles

FOUND EMERGENCY LIGHT SEAT 47 HJK INOP. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (ROW 5J AFT) · airframe 70,591 hrs · 8,522 cycles

EMERGENCY LIGHT ROW 5J AFT INOP. REPLACED LIGHT ASSEMBLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 70,591 hrs · 8,522 cycles

EMERGENCY LIGHT INOPERATIVE, RELAMPED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,672 hrs · 8,425 cycles

UPPER DECK EMERGENCY EXIT SIGN INOP BETWEEN DOORS CEILING AFT SIGN. REPLACED BATTERY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,672 hrs · 8,425 cycles

UPPER DECK EMERGENCY EXIT SIGN INOP AT LEFT CEILING DOOR SIGN. REPLACED BATTERY.

Part: VALVE — FAULTY (CREW REST O2) · airframe 69,465 hrs · 8,406 cycles

UPPER AFT CREW REST FWD LWR BUNK, O2 MASK DOOR WILL NOT OPEN, WITH OPS CK OF THE FLOW CONTROL UNITS. SUSPECT FAULTY VALVE ASSEMBLY. REPLACED UNITIZED VALVE ASSEMBLY. REF MM 35-21-36. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,190 hrs · 8,377 cycles

EEL 5A AFT INOPERATIVE. RELAMPED LIGHT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 69,190 hrs · 8,377 cycles

EEL 61 HJ INOPERATIVE. SECURED CONNECTOR.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 69,190 hrs · 8,377 cycles

FIRST OFFICERS O2 MASK, WHILE IN EMERGENCY MODE O2 FLOW "CHOO CHOO'S". SUSPECT FAULTY FLOW VALVE. REPLACED MASK PER MM 35-11 -18 OPS CHECKS NORMAL. AC OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,190 hrs · 8,377 cycles

EMERGENCY LIGHT AT DOOR 2L BUSTLE INOP. REPLACED POWER SUPPLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,787 hrs · 8,333 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 35 INOP. *S/D* RELAMPED EEL CEILING LIGHT. OP CHECKS NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,787 hrs · 8,333 cycles

DOOR SILL EEL LIGHT, DOOR 2R INOPERATIVE. *S/D* RELAMPED LIGHT. OP CHECKED NORMALLY.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,787 hrs · 8,333 cycles

EMERGENCY LIGHT AFT GALLEY WALL LEFT INOP. *S/D* REPLACED EEL LIGHT FEEDER CABLE, AFT GALLEY WALL, LEFT SIDE. OP CHECKS OK FOR SERVICE.

Part: COMPENSATOR — MALFUNCTIONED (NR 4 FUEL TANK) · airframe 68,698 hrs · 8,322 cycles

AIRCRAFT EXPERIENCING FUEL QUANTITY/FUEL TRANSFER PROBLEMS. 10-16-07 AFTER TROUBLESHOOTING ISOLATED PROBLEM TO FUEL COMPENSATOR IN NR 4 TANK. REPLACED NR 4 FUEL MAIN TANK COMPENSATOR WITH NEW UNIT PER MM 28-41-02-4 01. SYSTEM CHECKED OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 68,461 hrs · 8,297 cycles

EEL LIGHT AISLE STRIPS AT ROWS 6-8 TURN OFF AND ON AT RANDOM. SECURED STRIPS CONNECTOR & CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,333 hrs · 8,284 cycles

EMERGENCY EXIT CEILING LIGHTS INOP ROWS 48 THRU 61 RIGHT AND ROW 46 THRU 61 LEFT. 08-31-07 REPLACED BATTERY AT POWER SUPPLY M7928. LIGHTS OP CHECKS NORMALLY.

Part: A/C PACK — INOPERATIVE (CABIN) · airframe 68,333 hrs · 8,284 cycles

EMERGENCY EXIT CEILING LIGHT INOP AT ROW 6 RIGHT. REPLACED LAMP.

Part: GIRT BAR — DIRTY (R5 DOOR) · airframe 68,060 hrs · 8,257 cycles

DOOR 5R WILL NOT STAY IN ARMED POSITION. HANDLE POPS UP TO DISARMED POSITION AFTER ARM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 67,839 hrs · 8,232 cycles

EMERGENCY LIGHTS FWD GALLEY BOTTOM OF LT WALL & FWD OF LAV 100 LT BOTTOM OF WALL AFT DOOR 1 ARE INOPERATIVE. RESECURED EMERGENCY LIGHT CONNECTOR. OP CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,839 hrs · 8,232 cycles

EMERGENCY SILL LIGHT AFT ON DOOR 1L INOPERATIVE. RELAMPED SILL LIGHT. OP CK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,839 hrs · 8,232 cycles

EMERGENCY LIGHT ROW 3A AFT INOP. REPLACED EMERGENCY LIGHT. OP CHECKS NORMAL.

Part: A/C PACK — INOPERATIVE (CABIN) · airframe 67,839 hrs · 8,232 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 44 LT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,378 hrs · 8,188 cycles

EMERGENCY LIGHT INOP AT 34ABC & DOOR 3 CROSSAISLE. [06-22-07] RESECURED POWER CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,378 hrs · 8,188 cycles

CEILING EMERGENCY LIGHTS INOP AT ROW 26R, AFT CREW REST AREA, ROW 46L & DOOR 3R. [06-22-07] RELAMPED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 67,378 hrs · 8,188 cycles

EMERGENCY LIGHT INOPERATIVE AT 17AB LOWER. [06-22-07] RESEATED PWR CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,378 hrs · 8,188 cycles

EMERGENCY LIGHT INOP AT 22GH FWD, 28ABC, 44HJK & SEAT 51HJK. [06-22-07] REPLACED LIGHT ASSEMBLY.

Part: LIGHT — FAULTY (CABIN) · airframe 67,378 hrs · 8,188 cycles

BUSSLE EMERGENCY LIGHTS FAULTY AT 5L & 2R. [06-22-07] RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,935 hrs · 8,144 cycles

EMERGENCY LIGHT INOP AT DOOR 2L AFT SILL LIGHT. [SUP 05-08-07] RELAMPED. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,935 hrs · 8,144 cycles

EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5A AFT EEL LIGHT. [SUP 05-08-07] RELAMPED. OPS CHECKED GOOD. [SUP 05-16-07] RELAMPED. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,442 hrs · 8,094 cycles

EMERGENCY EXIT CEILING LIGHT INOP AT ROW 4 RIGHT & JUST AFT OF ROW 8 RIGHT. [SUP 4-17-07] RELAMPED BOTH POSITION. OP CHECKS NORMALLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 65,573 hrs · 8,003 cycles

EMERGENCY LIGHT INOP AT DR4L SLIDE ILLUM. REPLACED EEL ASSY. OP CHECKS OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 65,573 hrs · 8,003 cycles

EMERGENCY LEFT INOP AT CEILING ROW 61 LEFT. REPLACED LAMP, OP CHECKS OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,573 hrs · 8,003 cycles

EEL LIGHT INOP AT EXIT SIGN AT AFT SIDE DR2L AND LEFT SIDE B-ZONE. *S/D* REPLACED EEL BATTERY. OP CHECKS OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 65,573 hrs · 8,003 cycles

EEL INOP AT SEAT 5E AFT SECTION AND ROW 46L. REPLACED EEL LIGHT ASSY. OP CHECKS NORMALLY.

Part: SKIN — DAMAGED (BS 2080 S35R) · airframe 65,133 hrs · 7,953 cycles

BS 2080 STR 35R EXTERNAL SKIN CORRODED AND .5" CRACK AT WASTE VENT OUTLET. INSTALLED REPAIR DOUBLER & TRIPLER PER SRM. OK FOR SERVICE. SUSPECT CORROSION RELATED TO VENT EMISSION & PRESSURIZATION CYCLES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,720 hrs · 7,902 cycles

EMERGENCY LIGHT INOP AT SEATS 22H AND 43RH. REPLACED LIGHT ASSY.

Part: SOCKET — BURNED (EMERGNECY LIGHT) · airframe 64,252 hrs · 7,839 cycles

BURNING ODOR REPORTED FROM CREW AT SEAT AB. PULLED CB'S FOR UPPER DECK CEILING LT S ON P414 H22. SIDE WALL LIGHT AND READING LIGHT WORKED NORMALLY. UPPER DECK CELING LIGHT INOP. CONTACTED SAMC FOR CIRCUIT I.D. FURTHER TROUBLESHOOTING FOUND BURNED MARKS ON FLUORESCENT LIGHT SOCKET. REPLACED FLUORESCENT LAMP. CHECKS OK

Part: LIGHT — WEAK (EMERGENCY LIGHT) · airframe 61,985 hrs · 7,583 cycles

FOUND DOOR 1 RIGHT EMERGENCY LIGHT ON DOOR BUSTLE DIM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 61,985 hrs · 7,583 cycles

FOUND EMERGENCY LIGHT INOP AT SEATS 17AB AFT, 5F, AND 1A FWD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 61,985 hrs · 7,583 cycles

FOUND EMERGENCY LIGHT AT SEAT 4A BOTH INOP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 61,985 hrs · 7,583 cycles

EMERGENCY CEILING LIGHT INOP AT AFT OF ROW 8 LEFT AND AFT CREW REST.

Part: LIGHT — INOPERATIVE (VIEWPORT) · airframe 61,539 hrs · 7,534 cycles

EMERGENCY LIGHT AT RIGHT UPPER DECK DOOR VIEWPORT INSPECTION INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,539 hrs · 7,534 cycles

EEL AT SEAT 44HJK AND 17AB FWD INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,539 hrs · 7,534 cycles

EEL AT SEAT 4J AFT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,539 hrs · 7,534 cycles

EMERGENCY LIGHT AT DOOR 1L CEILING INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,666 hrs · 7,429 cycles

EMERGENCY LIGHTS OUT IN ROWS 55, 56, 57 & 58 SEATS ABC. REPAIRED FEEDER CABLE.

Part: DOOR — BROKEN (NR 2 A/C PACK) · airframe 57,099 hrs · 7,006 cycles

CHRONIC WRITE UP BANGING IN FLOOR BEHIND DOOR 2L, 5 ROWS BACK ALSO STOP WITH NR 2 PACK OFF. THE NR 2 AIR CONDITIONING PACK INLET DOOR WAS FOUND BROKEN. THE DOOR WAS REPLACED AND THE AIRCRAFT HAS HAD NO FURTHER PROBLEMS.

Part: DOOR — UNSECURE (CARGO) · airframe 53,279 hrs · 6,510 cycles

AFTER TAKEOFF UNABLE TO PRESSURIZE A/C. EICAS CAUTION DOOR AFT CARGO ILLUMINATED. FOUND LATCH CAM MANUAL LOCK HITTING CAM ON AFT CARGO DOOR. RERIGGED LATCH CAM TO ALLOW FOR 0.06 INCH CLEARANCE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,918 hrs · 6,455 cycles

STATION 100 LWR CHORD CRACKED JUST I/B OF STR 47L. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER MM 53-10-89.

Part: SKIN — DAMAGED (LT WING) · airframe 52,918 hrs · 6,455 cycles

LEFT WING INBOARD L/E HAS 4 EACH INTERIM REPAIR DOUBLERS INSTALLED AT L/E STATIONS 330, 415, & 543. MAJOR REPAIR ACCOMPLISHED. PERMANENT FLUSH REPAIRS WERE ACP PER SRM 57-41-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,918 hrs · 6,455 cycles

STRINGER 43AR CRACKED AT FUSELAGE STATION 240. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER SPLICE REPAIR.

Part: SUPPORT BEAM — DAMAGED (T/E FLAP) · airframe 52,918 hrs · 6,455 cycles

FIXED T/E SUPPORT BEAM WBL 235.20 FINAL REAM EXCEEDED THE MAX BORE SIZE ALLOWED. MAJOR REPAIR. REPLACED DAMAGED SECTION PER UAL EVA IMC-30172 AND MOBILE AEROSPACE ENGINEERING EA 47-5751-13-A1059.

Part: GROUND WIRE — BROKEN (CABIN) · airframe 52,556 hrs · 6,339 cycles

DURING FLIGHT, THERE WAS A BURNING SMELL NEAR UPPER DECK ROW 12. OVERHEAD CEILING LIGHT SOCKET MELTED AND SPARKED FORWARD AND AFT OF ROW 12. BOTH FLORESCENT LIGHT BALLASTS WERE DISCONNECTED. SUPPLEMENTAL DATA UPDATE FOUND BROKEN GROUND CONNECTION ON LIGHT ASSEMBLY. REPAIRED GROUND CONNECTION. REPLACED SOCKET AND BALLAST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,623 hrs · 6,001 cycles

EEL LIGHT INOP AT AFT GALLEY LEFT HAND NEXT TO LAV 117. REPLACED EEL STRIP NEXT TO LAV 117.

Part: SLIDE — DEPLOYED (R4 DOOR) · airframe 48,156 hrs · 5,803 cycles

MAIN ENTRY DOOR NR 4 RIGHT SLIDE IRREGULAR DEPLOYED DOOR CYLINDER DISCHARGED. DOOR NOT FULLY DISARMED PRIOR OPENING. REPLACED SLIDE.

Part: FITTING — DAMAGED (CARGO DOOR) · airframe 47,720 hrs · 5,743 cycles

MAJOR REPAIR REPORTING THE 65B38230-3 AFT CARGO DOOR FORWARD ACTUATOR SUPPORT FITTING AND BRACKET WERE DAMAGED. REPAIR ACCOMPLISHED PER EVAG-7736 REV A REPAIR HAS BOEING APPROVAL AND DER APPROVAL.

Part: INTERCOSTAL — CRACKED (BS 322)

AT APPROXIMATELY BODY STATION 322, THERE EXISTS A CRACK IN THE 141U8007-502 INTERCOSTAL. THE CRACK EXISTS IN THE LOWER HORIZONTAL FLANGE AND EXTENDS TO THE SECOND FASTENER HOLE COMMON TO THE 141U8007-501 SPLICE. *S/D* 141U8007-502 TRIMMED OUT AROUND CRACKED AREA. 141U8007-501 SPLICE STRAP EXTENDED TO PICK UP ADDITIONAL FASTENERS BEYOND CRACKED AREA. PART ROUTED TO BAC FOR ANALYSIS.

Part: LIGHT — BROKEN (GALLEY)

EEL LIGHT BROKEN AT RIGHT-HAND MIDDLE GALLEY AREA. REPLACED EEL LIGHT AT RIGHT-HAND GALLEY AND REPLACED FEEDER WITH COVER.

Part: LIGHT — INOP (DOOR 2R)

EEL STRIP AT DOOR 2R IS TORN AND THE CONNECTOR IS RIPPED OFF. ALSO, THE COVER IS MISSING. *S/D* REPAIRED AND CHECKS OK.

Part: SILL — CRACKED (BS 338)

VERY LOUD WHISTLE OUT OF NR 3 COCKPIT WINDOW, RIGHT REAR WINDOW ON FO SIDE WAS NOTICED ON DEPT AND ARRIVAL WITH CAB DIFF PRESS AT 5.O. *S/D* DUE TO SQUEALING, THE WINDOW WAS REMOVED AND CORROSION DAMAGE WAS FOUND AT THE LOWER AFT CORNER STA 338. THE DAMAGE WAS CONTAINED IN THE UPPER OUTBOARD FLANGE OF THE LOWER SILL. THE CORROSION REMOVAL RESULTED IN A 3 INCH SECTION OF THE FLANGE BEING TRIMMED OFF REVEALING A 3 INCH LONG CRACK. THE SILL WAS REPLACED.

Part: MECHANISM — BENT (3L DOOR)

DOOR 3L WARNING LIGHT ON DURING TAXI. *S/D* RELATCHED AND CLOSED DOOR CHECKED OK.

Part: SEAL — MISSING (NR 3 GEARBOX)

AIRCRAFT DIVERTED TO SEA DUE TO A NR 3 ENGINE OIL QUANTITY PROBLEM. *S/D* FUEL PUMP DRIVE PAD ON ENGINE ACCESSORY GEARBOX LEAKING OIL. REPLACED GEARBOX DRIVE PAD CARBON SEAL, OPERATION CHECKS NORMAL.

Part: SWITCH — WATER DAMAGE (PAX DOOR)

RETURNED TO FIELD DUE TO DOOR 1L WARNING LIGHT. *S/D* DOOR INDICATION SWITCH WAS REPLACED WITH REDESIGNED SWITCH, OPERATION CHECKS NORMAL.

Part: COMPRESSOR — FAILED (NR 4 ENGINE)

WHEN TAKEOFF THRUST WAS SET HEARD LOUD BANG FROM RIGHT SIDE OF AIRCRAFT. SMOKE SEEN IN NR 4 ENGINE. FIRED BOTH BOTTLES TO ENGINE. *S/D* HIGH COMPRESSOR STG 5 BLADE FAILURE, NO EVIDENCE OF FIRE. REPLACED ENGINE.

Part: ACTUATOR — FAILED (LT MLG DOOR)

LANDING GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF. AIRCRAFT LOST NR 4 HYDRAULIC SYSTEM AND RETURNED TO FIELD. LANDING GEAR LOWERED MANUALLY. REPLACED LEFT WING GEAR INBOARD DOOR ACTUATOR.

Part: BULKHEAD — FAILED (SLIDE)

SLIDE RAMP FAILED DURING FLAT FIRE IN SHOP. INTERNAL BULKHEAD FAILURE THE ENTIRE LENGTH OF SLIDE RAMP. SCRAPPED SLIDE RAMP.