N178UA

Part: LIGHT — INOPERATIVE (AFT GALLEY) · airframe 104,298 hrs · 12,302 cycles

DRUING AN 'A' CHECK, AFT GALLEY EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT. OPS CHECKED OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 104,298 hrs · 12,302 cycles

DURING AN 'A' CHECK, SEAT 37 LEFT, EMERGENCY LIGHT FOUND INOPERATIVE. FOUND CONNECTOR LOOSE. SECURED THE CONNECTOR AND WIRES. OPS CHECKED OK.

Part: LIGHT — BROKEN (SEAT 57) · airframe 104,298 hrs · 12,302 cycles

DURING AN 'A' CHECK, SEAT 57 LEFT, EMERGENCY LIGHT FOUND INOPERATIVE. FOUND EMERGENCY LIGHT ON SEAT BROKEN IN HALF. REPLACED THE LIGHT AND OPS CHECKED OK.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 104,298 hrs · 12,302 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 7 JK. FOUND LIGHT ASSY DISCONNECTED AND CONNECTED IT. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (SEAT 39HJK) · airframe 104,298 hrs · 12,302 cycles

DURING AN 'A' CHECK, SEAT EMERGENCY LIGHT AT 39 HJK FOUND INOPERATIVE. REPLACED THE EMERGENCY LIGHT AT SEAT 39HJK. OPS CHECKED OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 104,298 hrs · 12,302 cycles

DURING AN 'A' CHECK, SEAT 8 JK CENTER EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB. OPS CHECKED OK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,115 hrs · 11,292 cycles

RIGHT NR 5 MAIN ENTRY DOOR AFT UPPER CUT OUT SKIN CRACK, STATION 2280, 3" DOWN FROM STRINGER 16R, LENGTH=1". REPAIRED IAW EN -53-0322. REPAIR ACCOMPLISHED IAW EVA 80571 ECRA 5300-05671 REV. REMOVED RIVETS AS SHOWING IN FIGURE 1, PERFORMED OPEN HOLE HFEC INSPECTION OF THIS RIVETS HOLE & NO CRACKS OR OTHER DEFECTS WERE FOUND. INSTALLED NEW RIVETS AT THE AREA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 103,694 hrs · 12,225 cycles

BULK CARGO COMPARTMENT BS 2120 FRAME CHORD LOWER ANGLE PN 65B04343-90 WAS FOUND CRACKED, BETWEEN RBL 40 - 50 APPROX NEAR THE WASTE TANK SUPPORT FITTING. ACCESS DAMAGED ANGLE, CUT & REMOVED DAMAGED PART OF ANGLE. ACCOMPLISHED DVI, HFEC OF SURFACE & OPEN FASTENER HOLES. FABRICATED & INSTALLED FILLER, STRAP & REPAIR ANGLE IAW ECRA 5310-6808.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,694 hrs · 12,225 cycles

AFT CARGO COMPARTMENT, BS 1720 - 1740, STRINGER 50L - 51L, BILGE AREA INTERNAL FUSELAGE SKIN CORRODED. REMOVED CORROSION & FOUND BLEND OUT BEYOND SRM LIMITS. REMOVED DAMAGED SKIN. ACCOMPLISHED DVI, INSPECTION OF SURFACE & FASTENER HOLES IAW ECRA 5330-05676. FABRICATED & INSTALLED FILLER & 2 EACH REPAIR DOUBLERS, TRIPLER, IAW ECRA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 103,694 hrs · 12,225 cycles

FUSELAGE SKIN AT EXTERNAL POWER RECEPTACLE LOCATED BETWEEN BS 400 - 420 & STRINGER 42R - 43R, FOUND CRACKED FROM CUT OUT. TRIMMED OUT DAMAGE & ACCOMPLISHED INSPECTION SURFACE & OPEN HOLE INSPECTION OF REMOVED FASTENERS. FABRICATED & INSTALLED FILLERS, DOUBLER & TRIPLER REPAIR IAW ECRA 5330-05672.

Part: DOUBLER — CRACKED (NR 4 PYLON) · airframe 103,694 hrs · 12,225 cycles

NUMBER 4 PYLON OTBD SKIN EXISTING REPAIR DOUBLER AT FWD UPPER CORNER OF ACCESS PANEL 482ER CRACKED. REMOVED DAMAGED EXISTING DOUBLER & TRIMMED OUT CRACK. ACCOMPLISHED HFEC OF SKIN & OPEN FASTENER HOLES IAW ECRA 5430-02084. FABRICATED & INSTALLED DOUBLER & TRIPLER REPAIR.

Part: SKIN — CRACKED (NR 4 PYLON) · airframe 103,694 hrs · 12,225 cycles

NUMBER 4 PYLON OTBD SKIN HAS CRACK FROM AFT LOWER CORNER OF ACCESS PANEL 482ER CUT OUT. REMOVED DAMAGE & ACCOMPLISHED HFEC OF SURFACE & OPEN FASTENER HOLES IAW ECRA 5430-02084. FABRICATED & INSTALLED REPAIR DOUBLER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 103,694 hrs · 12,225 cycles

EXTERNAL FUSELAGE SKIN AT BS 2658 FOUND CRACKED LOCATED AT BS 2568 AT STRINGER 11L. REMOVED DAMAGE & ACCOMPLISHED NDT FOR CRACKS, NONE FOUND. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 1 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 103,694 hrs · 12,225 cycles

EXTERNAL FUSELAGE SKIN AT BS 1741 - 1760, BETWEEN STRINGER 49R - 51R, HAS EXISTING BLEND OUT & DENT. EVALUATED BLEND & DENT, FOUND BLEND OUT OF SRM LIMITS. REMOVED DAMAGE & ACCOMPLISHED SURFACE & OPEN HOLE NDT FOR CRACKS, NONE FOUND. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-01 REPAIR 15 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 103,694 hrs · 12,225 cycles

EXTERNAL FUSELAGE SKIN AT BS 180 - 190, BETWEEN STRINGER 42L - 42AL, HAS AN EXISTING BLEND OUT REPAIR. EVALUATED BLEND OUT & FOUND OUT OF LIMITS OF SRM 53-00-01 FIG 101. REMOVED DAMAGE & ACCOMPLISHED NDT FOR CRACKS, NONE FOUND. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR IAW SRM 53-00-01 REPAIR 1 FIG 201.

Part: CONNECTOR — LOOSE (CABIN) · airframe 103,529 hrs · 12,207 cycles

UPPER DECK SIDE WALL AFT EMER EXIT LIGHT INOPERATIVE. FOUND LOOSE LIGHT CONNECTOR, CONNECTED & OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,529 hrs · 12,207 cycles

SEAT 37C EMER EXIT LIGHT INOPERATIVE, RELAMPED. OPERATIONS CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 103,529 hrs · 12,207 cycles

AFT CROSS HALLWAY, BETWEEN DOOR 5L & 5R, AFT SIDEWALL RT EMER EXIT LIGHT INOPERATIVE. FOUND LOOSE CONNECTOR. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (STAIRS) · airframe 103,529 hrs · 12,207 cycles

STAIRS EMER EXIT LIGHTS INOPERATIVE. REPLACED LIGHTS. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 101,878 hrs · 12,052 cycles

GALLEY 4 LT SIDE FWD & SIDE EMER EXIT LIGHTS INOPERATIVE. REPLACED GALLEY NR 4 FWD EMER EXIT LIGHTS. OPERATIONS CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 101,878 hrs · 12,052 cycles

SEAT 8K MONITOR STAND EMER EXIT LIGHT INOPERATIVE. SECURED EMER EXIT LIGHT CONNECTOR. OPERATIONS CHECKED OK.

Part: DUCT — DISCONNECTED (BLEED AIR SYS) · airframe 100,858 hrs · 11,953 cycles

DIVERT DUE TO RT BLEED DUCT LEAK EICAS MSG. FOUND AIR DUCT DISCONNECTED AT R2. ADOMG EDGE FLAP PDU. R & R SEAL & SECURED DUCT IAW AMM 27-81-03 201. LE FLAP OPERATIONS CHECKED OK.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 99,575 hrs · 11,839 cycles

DURING ACCESS FOR R1 MIDDLE ENTRY DOOR FWD REVEAL REPAIR FOUND DOOR FRAME FWD UPPER WEB CRACKED. DOOR FRAME UPPER WEB REPAIRED IAW ECRA 5310-06368 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 99,575 hrs · 11,839 cycles

COCKPIT STATION 320 CROWN FRAME LBL 15 CIRCULAR CUT OUT FRAME WEB FOUND CRACK. BS 320 CROWN FRAME WEB REPLACED IAW EA5310-05659 OP3.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 99,575 hrs · 11,839 cycles

L2 DOOR EMER LIGHT INOPERATIVE, PN 9F19948-501. REPLACED L2 DOOR EMER LIGHT. TEST FOUND PASSED IAW AMM 33-51-06 R171.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 99,575 hrs · 11,839 cycles

BS 1780 - 1800 STRINGER 36 - 37R SKIN REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 14 REV 91. THIS IS A CATEGORY B REPAIR & THE CRITICAL ROW OF FASTENERS WERE NOT ZERO TIMED. INSPECTION REQUIREMENTS TO BEGIN AT 15000 PTC SINCE AC DELIVERY, REPEAT INSPECTION TO BE ACCOMPLISHED AT 6000 CYCLE INTERVALS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,575 hrs · 11,839 cycles

DURING TEST FOUND THE LT NR 4 DOOR G5 GALLEY LIGHT, NR 3 DOOR LAVATORY 112 EMER LIGHT INOPERATIVE. REPLACED THE LT NR 4 DOOR G5 GALLEY LIGHT, NR 3 DOOR LAVATORY 112 EMER LIGHT & TEST FOUND PASSED IAW AMM 33-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,608 hrs · 11,747 cycles

FLOOR PROXIMITY LIGHT EEL AT SEAT 19H INOPERATIVE. REPLACED LIGHT ASSEMBLY SEAT MOUNTED EEL CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,608 hrs · 11,747 cycles

FLOOR PROXIMITY LIGHTS, EMER EXIT LIGHT AT SEAT 48H INOPERATIVE. REPLACED LIGHT ASSEMBLY . OPERATIONS CHECKED SEAT MOUNTED EMER EXIT LIGHT OK.

Part: SKIN — WORN (FUSELAGE) · airframe 98,026 hrs · 11,687 cycles

FOUND WEAR AT FUSELAGE SKIN STATION 2614 - 2624 STRINGER 1R - 3R. SKIN WEAR DEPTH MAX 0.025 INCHES EXCEEDS MAX ALLOWABLE LIMITS. REPAIR ACCOMPLISHED IAW ECRA 5331-01902 PART 1. HFEC INSPECT ALL EXISTING HOLES IN REPAIR AREA, NO CRACKS NOTED. NDT INSPECTION ACCOMPLISHED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 98,026 hrs · 11,687 cycles

CORROSION WAS FOUND ON INTERNAL SKIN SURFACE AT FWD CARGO STATION 785 RBL 10 STRINGER 46R TO 47R. REMOVED CORROSION, FABRICATE & INSTALLED REPAIR IAW SRM 53-00-01 REPAIR 6 REV 89.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,662 hrs · 11,651 cycles

2.5 INCH SKIN CRACK, DOOR 5L UPPER AFT CORNER. TRIMMED OUT DAMAGE & INSTALLED DOUBLER-TRIPLER-QUAD REPAIR IAW ECRA 5330-04828, N R 169517.

Part: UNKNOWN — OUT OF ADJUST (FUEL SYSTEM) · airframe 97,575 hrs · 11,643 cycles

WHILE FILLING THE NR 2 RESERVE FUEL TANK TO FULL, 9.2, FUEL STARTED TO MOVE OUT OF THE FWD VENT TUBE IN THE LT SURGE TANK. VENT TUBE LOCATED IN THE CEILING OF THE OTBD ACCESS PANEL FOR THE LT SURGE TANK. THE FWD FUEL VENT DRAIN VLV WAS SUSPECTED BAD. CHECKED OPERATION & VLV INTEGRITY FOUND GOOD IAW 28-13-01. RESERVE NR 2 FILL VLV CHECKED NORMAL IAW 28- 21-02. ADJUSTED VOLUME TOP OFF RES 2 & 3 IAW 28-21-32, CHECKED GOOD.

Part: SOCKET — DAMAGED (CABIN) · airframe 97,204 hrs · 11,606 cycles

ELECTRICAL BURNING SMELL AT ROW 16 UPPER DECK. FOUND MELTED SOCKET AT SIDE WALL LIGHT 15A. REMOVED FLUORESCENT LIGHT BULB TO ISOLATE EVIDENCE OF SMELL, INSPECTED AREA IAW FIM 21-00-810, NO MORE SMELL NOTED. REPLACED BURNED SOCKET & RELAMPED, LIGHTS INOPERATIVE. BURNED SOCKET PROBABLY TOOK OUT THE BALLAST. RELAMPED BOTH SOCKETS, CYCLED CBS L17 & G18 UPPER DECK AUXILIARY & REVEAL LIGHTS, OPERATIONS CHECKED GOOD.

Part: TANK — LEAKING (FUEL SYSTEM) · airframe 97,087 hrs · 11,592 cycles

MAJOR FUEL SPILL 500 USG DURING REFUELING OPERATION. FUEL WAS DRAINING FROM THE SURGE TANK.

Part: UNKNOWN — MALFUNCTIONED (NR 4 ENGINE) · airframe 96,675 hrs · 11,551 cycles

NR 4 ENG WILL NOT ROTATE WHEN START IS ATTEMPTED. CYCLED CB J18 & ATTEMPTED SECOND START, STILL NO ROTATION. AIRCRAFT RETURNED TO GATE.

Part: VALVE — FAULTY (NR 1 ENGINE) · airframe 96,450 hrs · 11,526 cycles

ENG 1 FUEL VLV STATUS MESSAGE. REPLACED FUEL VLV.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,428 hrs · 11,524 cycles

EMERGENCY EXIT LIGHT ON STAIRWAY TO UPPER DECK INOPERATIVE. RPLD EMERGENCY EXIT LIGHT PCN 560-0806 IAW IPC 33-51-12-037 PG1, OPERATIONS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 95,965 hrs · 11,477 cycles

60B EMERGENCY LIGHT STRIP MISSING. REPLACED SEAT 60B EMERGENCY EXIT LIGHT STRIP. OPERATIONS OKAY. INSPECTED & OPERATIONS CHECKS EMERGENCY EXIT LIGHT.

Part: APU — SHUTDOWN (APU BAY) · airframe 95,767 hrs · 11,456 cycles

APU AUTO SHUTDOWN AT GATE WHEN LOAD WAS APPLIED. CMC MESSAGE WAS 49-11-891 APU RENDERED INOPERATIVE.

Part: COMPUTER — MALFUNCTIONED (RT CMC) · airframe 95,729 hrs · 11,451 cycles

IAW DF0504 CTR CDU INOPERATIVE, NEED TO REPLACE "RIGHT CMC" ON ACCNT "CMC-R FAIL" MESSAGE 45040 COMES UP. REPLACED RT CMC COMPUTER IAW AMM.

Part: LIGHT — UNSECURE (CABIN) · airframe 95,578 hrs · 11,436 cycles

LAVATORY 102 EMERGENCY LIGHTS OUTSIDE DOOR ARE FALLING OFF WALL. SECURED LIGHT ASSEMBLY & PERFORMED, OPERATIONS CHECKED OKAY.

Part: ENGINE — SURGES (NR 4) · airframe 95,424 hrs · 11,420 cycles

NR 4 ENG SURGE, RTFL, NR 4 ENGINE SURGE. ACCESS ENGINE EXCEDANCE (ENG EXCD) EICAS MAINTENANCE PAGE & EICAS PERFORMANCE PAGE IAW AMM 31-61-00 (201).

Part: SCUPPER — CRACKED (NR 1 ENGINE) · airframe 94,830 hrs · 11,361 cycles

NR 1 ENGINE TURBINE OIL SCUPPER DRAIN EXHAUST CRACKED. REPLACED CORE COWL IAW MM 71-11-06 P 401.

Part: PANEL — CRACKED (RT WING LE) · airframe 94,493 hrs · 11,329 cycles

PANEL DEVELOPED A CRACK ACROSS INTERIM REPAIR. REPLACED L/E PANEL.

Part: UNKNOWN — NOISY (COCKPIT) · airframe 94,392 hrs · 11,319 cycles

1ST OBSERVERS AUDIO PANEL HAS HF1 NOISE. UNABLE TO AVOID. REPLACED OTBD PANEL, NO HELP. NEED MORE TIME T/S. HF LEFT C-B PULLED. IF NEEDED HF TRANSCEIVER: (580-9137)

Part: LIGHT — MISSING (CABIN) · airframe 94,338 hrs · 11,313 cycles

40H SEAT MOUNTED EMERGENCY EXIT LIGHT MISSING. REPLACED 40H SEAT MOUNTED EMERGENCY EXIT LIGHT, OPERATIONS CHECKED OKAY.

Part: SKIN — CORRODED (FUSELAGE) · airframe 94,115 hrs · 11,292 cycles

LEFT FUSELAGE SKIN C-T OVERBOARD VENT CUT OUT CRACK CORRODED. REPAIRED IAW EVA81294A.

Part: UNKNOWN — LEAKING (UNKNOWN) · airframe 94,092 hrs · 11,290 cycles

AFT GALLEY HAS CONTINUOUS WATER LEAK FROM CEILING. FOUND WATER CONTAMINATION UNDERNEATH CHILLER C52 SHROUD PAN. OPERATED CHILLER C52 AND FOUND NO LEAKS. ALSO VERIFIED DRAIN PAN & HOSE CONNECTED AND SECURE.

Part: LATCH — CORRODED (DOOR) · airframe 93,708 hrs · 11,252 cycles

BUSINESS CLASS MAIN DECK, COMPARTMENTS 271, 272, 273 AND 274 OUTER DOOR LATCH ASSY CORRODED AND SHEARED AT LOWER PIN POSITION. COMPARTMENT CONTENTS REMOVED AND DOOR SECURED CLOSED. VARIES LATCH COMPONENTS REMOVED AND PLACED IN LOB AT DOOR 2L.

Part: LAMP — INOPERATIVE (CABIN) · airframe 93,636 hrs · 11,243 cycles

UPPER DECK EMERGENCY EXIT LIGHT OUT AND MISSING LENS. REPLACED LAMP AND LENS.

Part: ANGLE — BROKEN (FUSELAGE) · airframe 93,539 hrs · 11,234 cycles

ON ARRIVAL FOUND LEFT OUTBD BODY DOOR THREE INCHES FWD SEAL GAP ANGLE BROKEN. VISUAL INSPECTED DAMAGED ANGLE. SEAL AND ADJOINING AREA. NO ADDITIONAL DAMAGE IS PRESENT. GEAR DOOR AND FUSELAGE STRUCTURE NO DAMAGE. REMAINING SECTION OF SEAL IS SECURED AND UNDAMAGED. REPAIR CARRIED OUT PER EC-RA 3214-01005, REPLACED SEAL GAP ANGLE.

Part: SENSOR — FAULTY (STALL WARNING) · airframe 93,526 hrs · 11,233 cycles

CREW REPORTS: LEFT AOA HEAT FAIL EICAS MSG. MAINTENANCE MSG 30345. LEFT AOA SENSOR AND AOA CURRENT SENSE RELAY R7565. PERFORM OPERATIONAL CHECK REF AMM.

Part: LIGHT — DETACHED (COCKPIT) · airframe 93,343 hrs · 11,214 cycles

LOWER EMERGENCY LIGHT BAR DETACHED AFT OF 1L JUMPSEAT. REFITTED.

Part: LIGHT — UNSECURE (CABIN) · airframe 93,316 hrs · 11,212 cycles

LIGHT DANGLING NEAR FLOOR OUTSIDE LAVATORY. EMERGENCY LIGHT REFITTED.

Part: RELAY — FAILED (STNDBY) · airframe 93,262 hrs · 11,206 cycles

ACFT FAILED STANDBY POWER CHECK (DL3387). REPLACED STBY POWER TX RELAY R7227 IAW MM 24-29-03,B.A. OPS NORMAL.

Part: BATTERY PACK — TORN (EMERGENCY LIGHTS) · airframe 93,272 hrs · 11,207 cycles

EMERGENCY LIGHT LAVATORY 100 BATTERY PACK TORN FROM MOUNT. REPLACED BATTERY PACK , OP CHECKED GOOD.

Part: CHARGER — FAILED (MAIN BATTERY) · airframe 93,262 hrs · 11,206 cycles

MAIN BATTERY NOT CHARGING AFTER TEST. REPLACED MAIN BATTERY CHARGER PER MM. BATTERY NOW CHARGING.

Part: EXTINGUISHER — UNSERVICEABLE (COCKPIT) · airframe 92,927 hrs · 11,170 cycles

COCKPIT FIRE EXTINGUISHER NEEDS SAFETY PIN. SWAPPED FIRE BOTTLE FROM UPPER DECK L JUMPSEAT TO COCKPIT. STOWED INOP BOTTLE IN LOWER STORAGE AT SEAT 14A. REPLACED FIRE EXTINGUISHER.

Part: CONTROL PANEL — DAMAGED (COCKPIT) · airframe 92,885 hrs · 11,165 cycles

CAPT AUDIO PANEL HF 1 LENS BROKEN. MAINT TEXT: PCN 580-9321 RCP. REPLACE AUDIO CONTROL PANEL PCN 580-9129. OPERATIONAL CHECK GOOD.

Part: RELAY — FAULTED (NR 2 FIRE HANDLE) · airframe 92,517 hrs · 11,126 cycles

NUMEROUS STATUS MESSAGES WHEN AC DELIVERED TO GATE. HEAT-L AOA, HEAT P-S L-AUX, HEAT P-S CAPT, HEAT R-AOA, HEAT P-S R AUX, HEAT P-S F-O, ENG 2 EEC C1, FLT RCDR SYS. RESET ALL RELATED CIRCUIT BREAKERS, RESET AC POWER, BUSS POWER SWITCHES, EIU & MAWEA CIRCUIT BREAKERS. THESE STATUS MESSAGES NOT CORRELATED TO EXISTING FAULTS. NO FAULT CODES. RESET CMC CIRCUIT BREAKERS. NO HELP. CONFIRMED ALL AC CB'S ARE PUSHED IN. REPLACED RELAY R7223, NO HELP REF WD 24-33-11. RESET NR 2 ENGINE FIRE HANDLE ON ACCOUNT OF EEC FUEL VALVE MESSAGE, AFTER RESET ALL MESSAGE CLEARED.

Part: WIRE — BURNED (FUEL SYSTEM) · airframe 92,403 hrs · 11,113 cycles

FOUND BURNT WIRING JUST AFT OF THE BOOST PUMP CONNECTOR. CUT WIRES AT DAMAGED AREA AND RETERMINATED NEW CONNECTOR REF WDM28-22-31 PG2. WIRES DAMAGED 3 INCHES FROM CONNECTOR. ENOUGH SLACK TO RE-TERMINATE. REPAIRED DAMAGED WIRE & REPLACED CONNECTOR. REPLACING BOOST PUMP, OPS AND CLOSE.

Part: APU — MALFUNCTIONED · airframe 91,861 hrs · 11,060 cycles

NO APU DUCT PRESSURE. REPLACED APU ASSY, OPS TEST GOOD. NO LEAKS.

Part: SCREEN — MALFUNCTIONED (IFE SYS) · airframe 98,141 hrs · 11,058 cycles

BOTH CT SCREENS ARE DISPLAYING "SMOKE IN SYSTEM". SHUTDOWN THE IFE SYSTEM FOR THE REMAINDER OF THE FLIGHT. REMOVED AND INSTALLED SC. CONFIG CHECKED OK. AFTER RESET, IFE OPS CHECKED GOOD IAW MM. VERIFIED IFE SYS FUNCTIONAL IAW CSM 4.09.

Part: LIGHT — BROKEN (CABIN) · airframe 91,735 hrs · 11,048 cycles

DOOR 1L LOWER EMERGENCY LIGHT ON LAV IS BROKEN OFF. SPLICED ONE WIRE AND EPOXY SMALL EXIT SIGN ON LAV, TRIM PIECE WOULD NOT STAY ON, ADDED SMALL PIECE OF INVISIBLE TAPE TO TRIP PIECE, OP CHECKS GOOD ON GROUND.

Part: LIGHT — LOOSE (CABIN) · airframe 91,735 hrs · 11,048 cycles

EMERGENCY LIGHT ON THE BOTTOM PANEL MAIN DECK BUSINESS CLASS ON THE SIDE OF LAV 102 LOOSE. SECURED BOTTOM EMERGENCY LIGHT AT LAV 102.

Part: LIGHT — LOOSE (CABIN) · airframe 91,735 hrs · 11,048 cycles

EMERGENCY LIGHT ON THE BOTTOM PNL MAIN DECK BUSINESS CLASS ON THE SIDE OF LAV 102 LOOSE. SECURED BOTTOM EMERGENCY LIGHT AT LAV 102.

Part: LIGHT — BROKEN (CABIN) · airframe 91,735 hrs · 11,048 cycles

DOOR 1L LOWER EMERGENCY LIGHT ON LAV IS BROKEN OFF. SPLICED ONE WIRE AND EPOXY SMALL EXIT SIGN ON LAV, TRIM PIECE WOULD NOT STAY ON, ADDED SMALL PIECE OF INVISIBLE TAPE TO TRIP PIECE, OP CHECKS GOOD ON GROUND.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 91,677 hrs · 11,044 cycles

ACTIVE EXISTING FAULT: TANK WIRING HORIZ STAB HI Z LOW RESISTANCE CTR TO SHIELD. MAINT MSG 28083. FOUND REF A-CHECK JIC 800008400 ITEM 3. REMOTE ELEX UNIT CARD A1 HAS BEEN REPLACED, NO HELP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,677 hrs · 11,044 cycles

OVERWING EMERGENCY LIGHT LEFT 2 BOTTOM INOP. REPLACED OVERWING LIGHT ASSY 3L, OVERWING EMERGENCY LIGHTS OPERATIONAL CHECK OKAY.

Part: LIGHT — UNSECURE (CABIN) · airframe 91,677 hrs · 11,044 cycles

EMERGENCY LIGHT LAV 100 WALL NEED TO BE SECURED. RE-SECURED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,677 hrs · 11,044 cycles

EMERGENCY LIGHT ROW 33 THRU 43 INOP. REPLACED BATTERY PACK LIGHTS, OP CHECKED NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 91,677 hrs · 11,044 cycles

EMERGENCY LIGHT LAV 102 NEED TO BE SECURED. RE-SECURED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,677 hrs · 11,044 cycles

EMERGENCY CEILING LIGHT TOP OF THE UPPER DECK STAIRS INOP. RELAMPED, OP CHECK NORMAL.

Part: RELAY — FAILED (COCKPIT) · airframe 91,567 hrs · 11,033 cycles

CREW REPORTS THE FOLLOWING CB'S WERE FOUND OPEN UPON ARRIVAL TO FLT DECK. GRID A11, C10, C12, E11, A6 ALL ON THE OVERHEAD. CREW ALSO NOTED SLIGHT ELECT ODOR IN FLT DECK. ALL OF THE C/B'S ABOVE WERE ON THE 115VAC STBY BUS. FOUND MAIN STATIC INV INOP AND DAMAGED STBY PWR TRANSF RELAY BEHIND COCKPIT P6 PANEL AND FOUND LEFT EFIS CONTROL PANEL INOP. REPLACED ALL, STBY POWER TEST CHECKS NORMAL NOW, ALL C/BS STAY IN, NO SMELL NOTED. OK FOR SERVICE.

Part: B-NUT — LOOSE (RT WLG) · airframe 91,534 hrs · 11,030 cycles

ON ARRIVAL FOUND LARGE HYD LEAK AT RIGHT WING GEAR. FOUND VALVE JUST ABOVE RIGHT WING L GEAR AND FWD WING SPAR, TIGHTEN B-NUT 1 AND HALF TURN VALVE POSSIBLE GEAR DOORS SEQUENCE VALVE. ACP CLN AND LEAK CHECK OF ALL AREA FITTINGS PER MM, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,320 hrs · 11,008 cycles

RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOP, THIRD FROM FORWARD LIGHT ASSY FORWARD BULB. REPLACED LIGHT ASSY, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,320 hrs · 11,008 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 14. RELAMPED UPPER DECK CEILING LIGHT AT ROW 14.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 91,320 hrs · 11,008 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROWS 54 RIGHT THRU 59 RIGHT. SECURED CONNECTOR EEL LIGHTS AT SEAT ROWS 54 RIGHT THRU 59 RIGHT OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,320 hrs · 11,008 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CENTER CEILING AT DOORS FORWARD LIGHT. RELAMPED CEILING AT DOORS FORWARD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 91,320 hrs · 11,008 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 47 RIGHT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,320 hrs · 11,008 cycles

LEFT EXTERIOR OVERWING EMERGENY EXIT LIGHT INOP. THIRD FROM FORWARD LIGHT ASSY AFT BULB. REPLACED LIGHT ASSY PER MM, OPS NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 91,320 hrs · 11,008 cycles

EMERGENCY EXIT LIGHT INOPERATIVE IN FLIGHT DECK. RELAMPED FLIGHT DECK LIGHT.

Part: CONTROL PANEL — FAULTED (COCKPIT DOOR) · airframe 91,021 hrs · 10,978 cycles

COCKPIT DOOR DENY HORN DOES NOT SILENCE WHEN DENY IS SELECTED. REPLACED PEDESTAL PANEL P8, OPS CHECKED PER MM AND CHECKED DENY MODE TEST PER MM 52-51-00 PG 505 PASSED. TESTED PER MM 52-51-00 PG 501 PASSED.

Part: LAMP — INOPERATIVE (CABIN LIGHT) · airframe 90,780 hrs · 10,956 cycles

DURING M CHECK, FOUND CEILING LIGHT AT 34K INOP. REPLACED LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,780 hrs · 10,956 cycles

DURING M CHECK, LIGHTING CHECK FOUND CEILING LIGHT LAMP HOLDER ABOVE SEAT 3A WAS INOP AND HAD BURN MARK. REPLACED HOLDER AND LAMP. OPS CHECKED GOOD. CHECKED ALL WIRING TO BALLAST, FOUND NO OTHER DAMAGE.

Part: COVER — INOPERATIVE (SEAT 6 AB) · airframe 90,780 hrs · 10,956 cycles

DURING M-CHECK, FOUND 6AB 23AB IEA CALL LIGHT COVER INOP. REPLACED LIGHT COVER AND TESTED IS OK.

Part: TANK — LEAKING (RT WING) · airframe 90,734 hrs · 10,952 cycles

FUEL DRAINING FROM RIGHT WING SURGE TANK AFTER PUSHBACK, SURGE TANK PREVIOUSLY DRAINED PRIOR TO DEPT FOR SAME SITUATION. DRAINED SURGE TANK AND ACCOMP FIM TASK 28-21 CONFIG 1. VERIFIED NO LEAKS INTO SURGE TANK. TANK EMPTY AFTER REFUELING. OK FOR SVC.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 90,478 hrs · 10,927 cycles

STA 2403-2524 UPPER LOBE DOUBLER REPAIR, ALTERNATE SUPPORT REQUIRED. DEVIATES FROM SB 747-53A2651. ACCOMP REPAIR PER ECRA-5313- 01041. INSTALL SKIN DOUBLER AND SB COMPLIANT SUPPORTS.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 90,479 hrs · 10,927 cycles

BS 2521 UPPER LOBE LEFT DOUBLER P/N 65B92966-1 CRACK REPAIRED IAW ECRA 5313-01043. INSPECTION REQUIRED AT 4,000 FLIGHT CYCLE INTERVAL WITH A THRESHOLD OF 14,927 AIRFRAME TOTAL CYCLES. TEXT IS INCOMPLETE, SEE ECRA 5313-01043. REPAIRED IAW ECRA 5313- 01043. REINSPECTION REQUIRED INCORPORATED INTO MAINT PROGRAM AND EQ6042 WILL BE ACTIVATED AFTER COMP OF COA 851103. TEXT INCOMPLETE, SEE ECRA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 90,479 hrs · 10,927 cycles

BS 2521 UPPER LOBE RIGHT DOUBLER P/N 65B29266-2 CRACK REPAIRED IAW ECRA 5313-01044. INSPECTION REQUIRED AT 4,000 FLIGHT CYCLE INTERVAL WITH A THRESHOLD OF 14,927 AIRFRAME TOTAL CYCLES. TEXT IS INCOMPLETE, SEE ECRA 5313-01044. REPAIRED IAW ECRA 5313- 01044. RE-INSPECTION REQUIRED INCORPORATED INTO MAINT PROGRAM AND EQ6042 WILL BE ACTIVATED AFTER COMP OF COA 851103. TEXT INCOMPLETE-SEE ECRA.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,478 hrs · 10,927 cycles

STA 990-1000 S45R-S46R EXT FUSE SKIN DOUBLER CORROSION AT WATER TANK FILL VALVE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. MFG NEW DOUBLER PER DRAWING 65B09637-1 AND INSTALLED. NON ROUTINE 0290082.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 90,479 hrs · 10,927 cycles

BS 460-480 BETWEEN S14R & S16R, SHORT EDGE MARGIN, SHORT FASTENER SPACING, FASTENER INTERFERENCE, AND FASTENER LAYOUT IS INCORRECT. REF ECRA 5331-01601. REPAIRED IAW ECRA 5331- 01601. RE-INSPECTION REQUIREMENT INCORPORATED IN TO MAINT PROGRAM AND EQ6982 WILL BE ACTIVATED AFTER COMPLETION OF COA 85240. TEXT INCOMPLETE, SEE ECRA. NON ROUTINE 0290219. ALSO NON ROUTINES 0290220 AND 0290223.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,478 hrs · 10,927 cycles

STA 990-1000 S45R-S46R EXT FUSE SKIN DOUBLER CORROSION AT WATER TANK FILL VALVE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. MFG NEW DOUBLER PER DRAWING 65B09637-1 AND INSTALLED. NON ROUTINE 0290082.

Part: WEB — CRACKED (FUSELAGE) · airframe 90,479 hrs · 10,927 cycles

WEB CRACKED BS 140-160 BL 0 TO RBL 50 FLOOR TO SKIN SHEAR TIE INSTALLATION 65B01870-231. BS 140-160 BL 0 TO RBL 50 FLOOR TO SKIN SHEAR TIE INSTALLATION CRACK REPAIRED IAW ECRA 5311-01552. INSPECTION REQUIRED AT 3,000 FLIGHT CYCLE INTERVAL WITH A THRESHOLD OF 25,927 AIRFRAME TOTAL CYCLES. TEXT IS INCOMPLETE, SEE ECRA 5311-01552. ON NON ROUTINE 0287233 AND 0290259. ACCOMPLISH DETAILED VISUAL INSPECTION IAW PART 2 OF ECRA 5311-01552 BEGINNING AT 25,927 AIRFRAME TOTAL CYCLES.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 90,479 hrs · 10,927 cycles

BS 140-160 BL 0 TO RBL 50 FLOOR TO SKIN SHEAR TIE INSTALLATION CRACK REPAIRED. INSPECTION REQUIRED AT 3,000 FLIGHT CYCLE INTERVAL WITH A THRESHOLD OF 25,927 AIRFRAME TOTAL CYCLES. ACCOMPLISH DETAILED VISUAL INSPECTION IAW PART 2 OF ECRA 5311-01552 BEGINNING AT 25,927 AIRFRAME TOTAL CYCLES. **MF1072 CREATED TO MONITOR**

Part: SKIN — CRACKED (R2 DOOR) · airframe 90,479 hrs · 10,927 cycles

RIGHT NR 2 MED EXTERNAL SKIN CRACK AT UPPER HINGE CUTOUT. CATEGORY B REPAIR ACP IAW SRM 52-10-01 REPAIR 3. PER SRM TABLE 2, INSPECTION REQUIRED EVERY 3,000 CYCLES. REMOVABLE STRUCTURAL COMPONENT (RSC) MARKED PER 51-00-80. CF STICKER APPLIED. INSPECTIONS TO START AT 3,000 CYCLES FROM CURRENT PTC 10927.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 90,479 hrs · 10,927 cycles

BS 140-160 BL 0 TO RBL 50 FLOOR TO SKIN SHEAR TIE INSTALLATION CRACK REPAIRED IAW ECRA 5311-01552. INSPECTION REQUIRED AT 3,000 FLIGHT CYCLE INTERVAL WITH A THRESHOLD OF 25,927 AIRFRAME TOTAL CYCLES. ACCOMPLISH DETAILED VISUAL INSPECTION IAW PART 2 OF ECRA 5311-01552 BEGINNING AT 25,927 AIRFRAME TOTAL CYCLES.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 90,478 hrs · 10,927 cycles

BS 1120 LT TENSION TIE FWD CHANNEL CRACKED. REPAIRED TENSION TIE IAW NR-53-033 AND NR-53-021.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 90,478 hrs · 10,927 cycles

BS 1160 RT TENSION TIE DOUBLER CRACKED. INSTALLED NEW DOUBLER PER DRAWING 65B01751-10 AND SRM 51-40-02.

Part: FRAME — CRACKED (BS 1140) · airframe 90,478 hrs · 10,927 cycles

BS 1140 LT SIDE FRAME CRACKED AT TENSION TIE ATTACH. REMOVED AND REPLACED FRAME IAW SRM 51-40-02.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 90,478 hrs · 10,927 cycles

BS 1180 RT TENSION TIE DOUBLER CRACKED. INSTALLED NEW DOUBLER IAW SRM 51-40-02.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 90,478 hrs · 10,927 cycles

BS 1200 RT TENSION TIE FWD CHANNEL CRACKED. REPAIRED TENSION TIE IAW NR-53-032 AND NR-53-013.

Part: FRAME — CRACKED (BS 1140) · airframe 90,478 hrs · 10,927 cycles

BS 1140 RT FRAME CRACK AT TENSION TIE. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: FAILSAFE — CRACKED (BS 1220) · airframe 90,478 hrs · 10,927 cycles

BS 1220 LT TENSION TIE FAILSAFE CRACKED. CUT OUT DAMAGE. INSTALLED REPAIR PARTS IAW SRM 51-70-11.

Part: FRAME — CRACKED (BS 1120) · airframe 90,478 hrs · 10,927 cycles

BS 1120 LT FRAME CRACK AT TENSION TIE. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1200) · airframe 90,478 hrs · 10,927 cycles

BS 1200 RT FRAME CRACK AT TENSION TIE. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: FAILSAFE — CRACKED (BS 1120) · airframe 90,478 hrs · 10,927 cycles

BS 1120 RT TENSION TIE FAIL SAFE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR IAW SRM 51-70-11.

Part: DOUBLER — CRACKED (BS 1200) · airframe 90,478 hrs · 10,927 cycles

STA 1200 RT TENSION TIE DOUBLER CRACKED. INSTALLED NEW DOUBLER IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1120) · airframe 90,478 hrs · 10,927 cycles

BS 1120 LT TENSION TIE DOUBLER CRACKED. REPLACED FRAME IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1220) · airframe 90,478 hrs · 10,927 cycles

BS 1220 RT FRAME CRACK AT TENSION TIE. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 90,478 hrs · 10,927 cycles

BS 1140 RT TENSION TIE FAILSAFE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR IAW SRM 51-70-12.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 90,478 hrs · 10,927 cycles

BS 1180 LT TENSION TIE FWD AND AFT CHANNEL CRACKED. REPAIRED TENSION TIE IAW NR-53-031 AND NR-53-016.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 90,478 hrs · 10,927 cycles

BS 1140 LT TENSION TIE FWD AND AFT CHANNEL CRACKED. REPAIRED TENSION TIE PER NR-53-037 AND NR-53-019.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 90,478 hrs · 10,927 cycles

BS 1160 RT TENSION TIE FWD AND AFT CHANNEL CRACKED. REPAIRED TENSION TIE IAW NR-53-029 AND NR-53-017.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 90,478 hrs · 10,927 cycles

BS 1140 LT TENSION TIE FAIL SAFE CRACKED. REMOVED DAMAGE AND INSTALL REPAIR IAW SRM 51-70-12.

Part: FRAME — CRACKED (BS 1120) · airframe 90,478 hrs · 10,927 cycles

BS 1120 RT FRAME CRACKED AT TENSION TIE. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 90,478 hrs · 10,927 cycles

BS 1120 RT TENSION TIE DOUBLER CRACKED. INSTALLED NEW DOUBLER IAW SRM 51-40-02.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 90,478 hrs · 10,927 cycles

BS 1180 RT TENSION TIE FWD CHANNEL CRACKED. REPAIRED TENSION TIE IAW NR-53-030 AND NR-53-015.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,728 hrs · 10,856 cycles

LOWER FUSELAGE SKIN HAS THE APPEARANCE OF BEING CRACKED JUST FWD OF EQUIPT COOLING EXHAUST VALVE (MARKED). CLEANED AREA AND SMOOTHED MINOR TOOL MARKS IN SKIN. NO MORE CORROSION WAS FOUND. TESTED SKIN THICKNESS WITH ULTRASONIC TESTER. FOUND ONE SMALL AREA WITH IN ONE HALF INCH OF CUTOUT THAT WAS .051. ALL OTHER AREAS WERE .058 OR GREATER. INSP AREA NO CORROSION FOUND. INSTALLED EXTERNAL FUSELAGE SKIN REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,631 hrs · 10,846 cycles

UPPER DECK CEILING AT ROW 12 EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 89,631 hrs · 10,846 cycles

EMERGENCY LIGHT AT SEAT 37 AB INOP. SECURED CONNECTION.

Part: FUEL TANK — LEAKING (RT WING) · airframe 89,172 hrs · 10,800 cycles

FOUND FUEL LEAKING FROM BOTTOM OF RIGHT WING NR 3 MAIN TANK AFT MID SPARE SEAM, 6 INCHES OTBD OF WING ROOT. ACCOMPLISHED PERMANENT REPAIR REF SERVICE TIP MM 57-52-96.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE AT L3 DOOR SLIDE. REPLACED LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE CENTER GALLEY . RELAMPED LIGHT, OPS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE ROW 46 LT. SECURED LOOSE CONNECTOR.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 89,172 hrs · 10,800 cycles

EMERG LT INOP ROW 37 LT. REPLACED CONN AT 37 LT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE SEAT 47 LT. REPAIRED LOOSE CONNECTOR.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE AFT GALLEY LEFT SIDE WALL. REPAIRED FEEDER CABLE FROM SEAT 45, CHECKED OKAY.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE AFT GALLEY FWD WALL. REPAIRED FEEDER CABLE FROM SEAT 45.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,172 hrs · 10,800 cycles

EMERGENCY LIGHT INOPERATIVE L4 DOOR SLIDE. REPLACED LAMP.

Part: MONITOR — OVERHEATED (CABIN) · airframe 88,756 hrs · 10,758 cycles

SEAT 2A VIDEO INOP AND APPEARS TO HAVE OVERHEATED, VISIBLE SMOKE FROM MONITOR. CREW SELECTED SEAT POWER OFF AND SMOKE CLEARED. SAMC TEXT: NEED MAINT TO ACP INSPECTION OF SEAT 2A ELECTRICAL COMPONENTS. ISOLATE SOURCE OF SMOKE, ENSURE ADDITIONAL DAMAGE HAS NOT BEEN CAUSED TO THE SEAT-WIRING-IFE COMPONENTS AS A RESULT. REMOVED AND REPLACED 2A MONITOR PER AMM. P/N ON AND OFF RD-FW7854-51, S/N ON D755509, S/N OFF D502369. MONITOR OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 88,756 hrs · 10,758 cycles

EEL LIGHT AT DOOR 4L GALLEY CROSS AISLE BROKEN STRIP WITH A BROKEN WIRE. REPLACED EEL LIGHT ASSY 560-4674. OPS CHECKS OKAY PER MM.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 88,708 hrs · 10,754 cycles

SEAT 3A EMERGENCY LIGHT LENS INCORRECT TYPE. NO RED ARROW. REPLACED LENS.

Part: MONITOR — FAILED (SEAT 13K) · airframe 88,666 hrs · 10,749 cycles

ELECTRICAL ODOR AND SMOKE FROM SEAT 14JK. FLT ATTENDANT REMOVED POWER FROM SYSTEM AND SMOKE ODOR DISSIPATED. FOUND ELECTRICAL ODOR FROM 13K MONITOR. CONFIRMED 13K MONITOR FAILED. NO OTHER DAMAGE FOUND. REPLACED MONITOR AT 13K. CONFIRMED OPERATIONAL CHECK OK AT 13K MONITOR. IFE SYS CHECKED OK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 88,625 hrs · 10,746 cycles

EMERGENCY EXIT SIGN INOP AT DOOR 5L AFT UPPER BULKHEAD. REPLACED FUSELAGE SIGN, OPS CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 88,625 hrs · 10,746 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 21 LEFT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 88,625 hrs · 10,746 cycles

LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP 2 EA. MOST AFT LIGHT ASSY'S. REPLACED POWER SUPPLY, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,625 hrs · 10,746 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 40 RIGHT. REPLACED LIGHT ASSY, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,625 hrs · 10,746 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING JUST AFT OF ROW 17. RELAMPED, OPS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 88,625 hrs · 10,746 cycles

EMERGENCY EXIT LIGHT VERY DIM DOOR 4 LEFT SLIDE LIGHT. RECHECKED AFTER A FEW HOURS TO ALLOW BATTERY TO RECHARGE. LIGHT OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,625 hrs · 10,746 cycles

EMERGENCY EXIT LIGHT INOP. CEILING ROW 60 RIGHT. RELAMPED, OPS CHECK NORMAL.

Part: CONNECTOR — DEFECTIVE (GALLEY) · airframe 88,555 hrs · 10,739 cycles

ECONOMY GALLEY NEW TECH PLUG N44 SPARKED WHEN FLIGHT ATTENDANT TRIED TO PLUG IT IN. INOP CART REPLACED, BEZEL ON CONNECTOR ORIENTATION CORRECTED.

Part: LIFE VEST — MISSING (CABIN) · airframe 88,498 hrs · 10,734 cycles

THE 53A VEST MISSING. REPLACED VEST.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 88,233 hrs · 10,705 cycles

FIRST OFFICER'S PIN ON OXYGEN MASK IS BROKEN. FIRST OFFICER UNABLE TO USE MICROPHONE. REINSTALLED O2 MASK AND OPS CHECKED OKAY.

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 88,101 hrs · 10,690 cycles

UNABLE TO TRANSMIT FROM CAPTS HEADSET. HAND MIC IS OK. REPLACED O2 BOX. OPERATION RETURNED TO NORMAL.

Part: PANEL — CRACKED (TE FLAP) · airframe 88,079 hrs · 10,688 cycles

RIGHT WING INBOARD MID FLAP, LEADING INBOARD EDGE ADJACENT TO ACCORDIAN SEAL FLAP HAS APPROX 2 INCH X 2 INCH. PUNCTURE OR EROSION DAMAGE. STARTED PERMANENT REPAIR REF SERVICE TIP MM. NEED TO COMPLETE REPAIR FROM STEP C8 PAR C AFTER CURE IS COMPLETE. NEED TO COMPLETE REPAIR FROM STEP C8 PAR C AFTER CURE IS COMPLETE. COMPLETED REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,079 hrs · 10,688 cycles

EMERGENCY LIGHT INOPERATIVE IN CEILING, ROW 14. RELAMPED, OPS GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 88,079 hrs · 10,688 cycles

EMERGENCY LIGHTS INOPERATIVE ON STAIRWAY TO UPPER DECK. REPLACED POWER FEEDER CABLE.

Part: LIGHT — UNSECURE (R2 DOOR) · airframe 88,079 hrs · 10,688 cycles

EMERGENCY LIGHT AT 2R, KEEPS FALLING OUT AND HANGS BY WIRES. SECURED LIGHT IN PLACE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,930 hrs · 10,673 cycles

WAC FOUND STA 2090 LHS WASTE SYSTEM OVERBOARD VENT EDGE SKIN CRACKED 0.5 INCH. DAMAGE REPAIRED PER EVA -81294A. FAA APPROVAL FORM 8100-9 RECEIVED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,930 hrs · 10,673 cycles

FUSELAGE SKIN CRACK AT STA 2090-S-36L. PER SRM 53-00-01 ALLOWABLE DMG 2 FIG 101, NEED TO STOP DRILL END OF CRACK WITH .25 INCH DIA HOLE. NOTE, ONLY DRILL THROUGH THE EXTERIOR TOP SKIN, DO NOT DRILL INTO DOUBLER ON INSIDE OF WASTE VENT NOZZLE FLANGE. SAMC TEXT: IF CRACK DOES NOT EXTEND PAST THE FASTENER HOLE, STOP DRILL IS NOT REQUIRED. VISUAL INSPECTION PERFORMED WITH PAINT REMOVAL, THE CRACK DOES NOT EXTEND PAST THE FASTENER HOLE PER SRM. SKIN REPAIR WORK IN PROGRESS IAW EVA 81294 REV 02 ALMOST COMPLETED, WILL START INSTALL WASTE TANK. PAINTED LT LAV EXHAUST REPAIR AREA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,577 hrs · 10,633 cycles

UPPER DECK RT WING DOOR FWD LAMP IS INOPERATIVE. RELAMPED AND RELUGGED, OP CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,577 hrs · 10,633 cycles

DOOR 5R AFT SILL EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,577 hrs · 10,633 cycles

FWD GALLEY CROSS AISLE LOWER WALL EMERGENCY LIGHT IS INOP (2EA). RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,577 hrs · 10,633 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,577 hrs · 10,633 cycles

UPPER DECK CEILING EMERGENCY LIGHT NEAR 13AB IS INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,577 hrs · 10,633 cycles

SEAT EMERGENCY LIGHT AT ROW 58HJK IS INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,577 hrs · 10,633 cycles

SEAT ROW 37ABC EMERGENCY LIGHT IS INOP. RESECURED EMERGENCY LIGHT. OP CHECK NORMAL.

Part: ARM — OUT OF ADJUST (DOOR) · airframe 87,488 hrs · 10,624 cycles

UPPER DECK RT DOOR WAS DIFFICULT TO ARM. ADJUSTED ARM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 87,438 hrs · 10,619 cycles

FOUND UPPER TCAS ANTENNA DOUBLER CORRODED. RMV'D DBLR ORDERED DOUBLER RPR KIT, 141U1125-13 ON M1805, STERLING DEL FROM BACO SEA ETA 1000. CONT ADS-B WIRICOA. *DOR* ARV: 04-1025 PRI-O/CUR-P SPFLT: OSTFS: 1 EST=02 RTG: 863-07 2250 SYD DF/CF: 0/1 EWAS:1800-05 CHG:1602-04

Part: CONNECTOR — UNSECURE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 39 RIGHT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT LIGHT INOP FWD STAIRWELL CEILING FWD LAMP. RELAMPED, CHECKS OKAY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT EEL LIGHT INOP FWD STAIRS EEL. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 37 LEFT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT SIGN INOP DOOR 5 LEFT GALLEY AREA AFT WALL UPPER LEFT EXIT SIGN. REPLACED POWER SUPPLY M6984.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT EEL LIGHT INOP LOWER WALL BETWEEN LAVS 111 AND 112. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING BETWEEN DOORS FWD LIGHT. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 42 RIGHT. SHOULD READ ROW 42 LEFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT LIGHT VERY DIM DOOR 4 LEFT BUSSLE LIGHT. RECHECKED LIGHT AFTER A FEW HOURS AND LIGHT OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,141 hrs · 10,585 cycles

EMERGENCY EXIT EEL LIGHT INOP LOWER WALL ACROSS LAV 100. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,143 hrs · 10,474 cycles

SEAT ROW 55 ABC EMERGENCY LIGHT IS INOP. REPLACED LAMP, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 86,143 hrs · 10,474 cycles

DOOR 4 LEFT SLIDE EMERGENCY LIGHT IS INOP. REPLACED LAMP, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,143 hrs · 10,474 cycles

UPPER DECK CEILING EMERGENCY LIGHT NEAR ROW 13 IS INOP. RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,143 hrs · 10,474 cycles

DOOR 2 RIGHT FWD SILL EMERGENCY LIGHT IS INOP. REPLACED LAMP, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,143 hrs · 10,474 cycles

SEAT ROW 40HJK EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT STRIP, OP CHECKS GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 86,143 hrs · 10,474 cycles

MID LAV LOWER SIDEWALL EMERGENCY LIGHT IS INOP. SECURED CONNECTION.

Part: SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 85,444 hrs · 10,391 cycles

EMERGENCY EXIT LIGHTS FLICKER IN CRUISE. COCKPIT SWITCH LOOSE. SECURED SWITCH.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 85,444 hrs · 10,391 cycles

EMERGENCY EXIT LIGHTS ILLUMINATE IN FLIGHT CONSTANTLY ON LEFT SIDE OF AIRCRAFT FROM DOORS. REPLACED POWER SUPPLY AT L3 DOOR M6009 PER AMM.

Part: LIGHT — FAULTY (CABIN) · airframe 85,412 hrs · 10,387 cycles

EMERGENCY EVACUATION LIGHT ON AFTER TAKEOFF FOR ENTIRE FLT IN ROWS 33C-43C. REPLACED LIGHT ASSY AT SEAT 42A. TESTS OKAY.

Part: VALVE — FAILED (FUEL SYSTEM) · airframe 85,315 hrs · 10,375 cycles

FUEL IMBALANCE CHRONIC. CONFIRMED UNWANTED TRANFER BETWEEN NR 1 MAIN AND NR 2 MAINS. TANK OPENED, PURGED AND VENTED. REMOVED OLD VALVE, & GASKET. FOUND PITTING ON VLV. ORDERED GASKET NON STOCK ON X6778, LC SOURCING NO ETA. NEED TO REPLACE VALVE AND ACTUATOR. PARTS ORDERED. REMOVED TRANSFER VLV BODY. REMOVED CLAMP FROM ACTUATOR SHAFT. PARTS IN TANK. FINISHED REPLACING VALVE BODY. OPS CHECK GOOD.

Part: BEAR STRAP — CORRODED (BS 2280 S24L) · airframe 85,271 hrs · 10,369 cycles

LT NR 5 MAIN ENTRY DOOR CUTOUT AREA AFT LOWER SKIN INBD SURFACE CORROSION. STA 2280 S24L. SIZE = 2.8" X 1.5". REPAIRED IAW 747EN-53-0324. REPAIR ACCOMPLISHED IAW EVA 80572 IS TIME LIMITED UNTIL THE AIRPLANE REACHES 22,000 FLIGHT CYCLES. FULL COMPLIANCE WITH 14 CFR 25.571(B)[25-45] AND 26.43 (D) [26-1] HAS NOT BEEN EVALUATED. A NEW FAA APPROVAL MUST BE ISSUED PRIOR TO INSP THRESHOLD OF 22,000 TOTAL FLIGHT CYCLES. IF NEW APPROVAL IS NOT ISSUED BY THE THRESHOLD, AIRWORTHINESS CERTIFICATE IS NO LONGER CURRENT AS REQUIRED BY 14 CFR 91.203(A). CORRODED AREA APPROX 12.21 X 1.22 INCH LOCATED ON THE BEAR STRAP AT THE AFT LOWER CORNER OF LT NR 5 MED CUTOUT.

Part: SKIN — CRACKED (BS 2280 S16R) · airframe 85,271 hrs · 10,369 cycles

RT NR 5 MAIN ENTRY DOOR AFT UPPER CUTOUT SKIN CRACK. STA 2280, 3" DOWN FROM S16R. LENGTH=1". REPAIRED IAW 747EN -53-0322. REPAIR ACCOMPLISHED IAW EVA 80571 IS TIME LIMITED UNTIL THE AIRPLANE REACHES 22,000 FLIGHT CYCLES. FULL COMPLIANCE WITH 14 CFR 25.571(B)[25-45] AND 26.43 (D)[26-1] HAS NOT BEEN EVALUATED. A NEW FAA APPROVAL MUST BE ISSUED PRIOR TO INSP. THRESHOLD OF 22,000 TOTAL FLIGHT CYCLES. IF NEW APPROVAL IS NOT ISSUED BY THE THRESHOLD, AIRWORTHINESS CERTIFICATE IS NO LONGER CURRENT AS REQUIRED BY 14 CFR 91.203(A). CRACK IS 1.02 INCHES LONG AND EXTENDS FROM THE EDGE OF THE AFT UPPER CORNER OF THE RT NR5 MED CUTOUT, ON THE FUSE BONDED SKIN AND BEAR STRAP (PN 65B38836-4) AROUND STA 2285, S17R.

Part: CIRCUIT CARD — FAULTY (BOOST PUMP) · airframe 85,288 hrs · 10,371 cycles

AFTER CTR TANK WAS EMPTY AND BOOST PUMPS WERE OFF, CREW NOTICED NR 1 AND NR 2 FUEL QTY DECREASING FASTER THAN NR 3 AND NR 4 WITH ALL ENGS BURNING NORMAL GAS. NR 1 AND NR 2 TANKS EA DECREASED 2200 LBS COMPARE WITH NR 3 & NR 4 TANKS. CREW REBALANCED FUEL. NO FUEL TRANSFER WAS NOTICED TO CTR TANK VIA NR 1 AND NR 2 TANKS. NR 3 AND NR 4 TANKS WERE OK. CREW KEEP REBALANCING FUEL AND MONITORING. REPLACED FUEL SYS MANAGEMENT CARD A5.

Part: SKIN — CRACKED (PAX DOOR) · airframe 85,271 hrs · 10,369 cycles

LT NR 5 MAIN ENTRY DOOR SKIN CRACK. 8" FWD FROM STA 2240, S18L. LENGTH 1". MAJOR REPAIR ACCOMPLISHED: TRIMMED SKIN AND INSTALLED DOUBLER IAW EVA 80568. CRACK IS ON EXT DOOR SKIN, LONGITUDINALLY FROM THE FWD EDGE OF THE DOOR, JUST ABOVE DOOR HORZ BEAM 13, REPORTED AS 0.75 INCHES LONG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,184 hrs · 10,360 cycles

SEAT 45R EMERGENCY LIGHT INOPERATIVE. RELAMPED, CHECKS OKAY.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,184 hrs · 10,360 cycles

LEFT OVERWING 2 AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, CHECKS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,184 hrs · 10,360 cycles

SEAT 43L EMERGENCY LIGHT INOPERATIVE. RELAMPED CKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,184 hrs · 10,360 cycles

RT EMERGENCY CEILING LIGHT INOP ACROSS FROM FIRST CLASS GALLEY. RELAMPED, CHECKS OKAY.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 84,591 hrs · 10,299 cycles

LT INBD ELEVATOR UPPER SURFACE HAS 1 HAIL DAMAGE PENETRATION AT 29 INCH FROM INBOARD END AND 5 INCH FROM TRAILING EDGE, .25 INCH DIAMETER. MADE INTERIM REPAIR REF SRM. MF6666 CREATED TO MONITOR. REPAIRED ELEV ON OV WU B8519W.

Part: SKIN — DAMAGED (LT WING) · airframe 84,591 hrs · 10,299 cycles

SKIN HAS IMPACTED AREAS WITH DELAMINATION OF APPROX 1 INCH DIAMETER, WITHOUT PENETRATION. LEFT WING TRAILING EDGE BETWEEN WING TIP AND AILERON: 25 SPOTS IN 11 AREAS. AREAS WITH PERMANENT DEFLECTION AVG DEPTH APPROX .010 INCH AND NO EXPOSED FIBERS NOTED AT THIS TIME. MADE REPAIRS TO DELAMINATED AREAS PER SRM.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 84,591 hrs · 10,299 cycles

LT WING NR 2 SPOILER HAS 50 SMALL DENTS NO HOLES PENETRATION AT IMPACT, ONLY 1 DELAMINATION AT RT AFT CORNER . AVERAGE .008 IN DEPTH AND 1 INCH IN DIAMETER. REPAIRED ON DOCK WU B8477W.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 84,591 hrs · 10,299 cycles

RT OTBD ELEVATOR HAS 1 HAIL DAMAGE PENETRATION UPPER SURFACE AT 50 INCHES FROM INBD END OF ELEV AND 12 INCHES FROM TRAILING EDGE, .25 INCH DIA. SUPPLEMENTAL DATA UPDATE, ACCOMPLISHED REPAIR REF REMOVED AND REPLACED R28166 AND 8130 TRACKING NR 016-A00392817.

Part: SKIN — DAMAGED (NR 4 SPOILER) · airframe 84,591 hrs · 10,299 cycles

THE LEFT WING NR 4 FLT SPOILER UPPER SURFACE HAS SUSTAINED HAIL DAMAGE. THERE ARE A TOTAL OF 81 HITS WITH AN AVERAGE DEPTH OF .018, 1 INCH IN DIAMETER AND NO PENETRATION. REPAIRED ON DOCK WU B8479W.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 84,591 hrs · 10,299 cycles

LT WING NR 1 SPOILER HAS 85 SMALL DENTS NO HOLES AVERAGE .008 IN DEPTH 1 INCH IN DIAMETER NO DELAMINATION. REPAIRED ON DOCK WU B8475W.

Part: SKIN — DAMAGED (LT WING) · airframe 84,591 hrs · 10,299 cycles

UPPER LEFT WING PANEL JUST FWD OF THE INBD AILERON HAS SUSTAINED HAIL DAMAGE, PANEL HAS BEEN IMPACTED WITH 6 HITS AND AN AVERAGE OF .005 DEEP WITH A DIAMETER OF 1 INCH ALL WITH NO PENETRATION. ACCOMPLISHED REPAIR PER SRM 57-51-01, REPAIR 1 ON OV WU B8476W.

Part: SKIN — DAMAGED (LT WING) · airframe 84,591 hrs · 10,299 cycles

LEFT WING UPPER SURFACE PANEL JUST OUTBOARD OF INBD AILERON. WS834.50 AND WS862.00 HAVE SUSTAINED HAIL DAMAGE, THERE HAS BEEN A TOTAL OF 11 HITS, AVERAGE DEPTH IS .003, 1 INCH IN DIAMETER AND NONE HAVE PENETRATED ACCOMPLISHED REPAIR PER SRM, REPAIR 1 ON OV WU B8478W.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHT) · airframe 84,587 hrs · 10,298 cycles

WASH LIGHT UNDER OTTOMAN AT SEAT 15B INOP. LAMP ASSY CONNECTOR CORRODED, REPLACED LAMP ASSY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,587 hrs · 10,298 cycles

OVER STAIRWAY FWD EMERGENCY LIGHT INOPERATIVE. RELAMPED, CHECKS OK.

Part: FEEDER CABLE — CONTAMINATED (EMERGENCY LIGHTS) · airframe 84,587 hrs · 10,298 cycles

EMERGENCY LIGHTS INOP AFT GALLEY FWD AND LT, DOOR 4L FWD EXIT, DOOR 5R AFT EXIT, LT SEATS 45-54. CLEANED WATER FROM FEEDER CABLE CKS OK.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 84,587 hrs · 10,298 cycles

HAIL DAMAGE INSP FOUND ON THE LT O/B AILERON ABOUT 132 SPOT DELAMINATION ON THE UPPER SURFACE NO HOLES. AREA INVOLVED IS THAT OF THE OTBD AILERON UPPER SURFACE ONLY BETWEEN WS 1224.00 AND 1551.25 SPECIFICALLY. IMPACTED AREAS ARE OF AN AVERAGE OF .008 IN DEPTH AND 1 INCH IN DIAMETER. THERE IS DELAMINATION AT THE IMPACT AREA OF EACH SPOT WITH NO PENETRATION AT ANY IMPACT. ACCOMPLISHED REPAIR PER SRM ON OV WU B8478W.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,587 hrs · 10,298 cycles

CENTER AISLE BETWEEN DOORS 2L AND 2R THE CENTER AND RT EMERGENCY LIGHTS INOPERATIVE. RELAMPED, CHECKS OK.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHT) · airframe 84,587 hrs · 10,298 cycles

WASH LIGHT UNDER OTTOMAN AT SEAT 14A INOP. WIRE CONNECTOR FOR LAMP ASSY CORRODED, REPLACED LAMP ASSY.

Part: FEEDER CABLE — BURNED (APU GEN) · airframe 84,206 hrs · 10,256 cycles

FOUND APU GEN-1 FEEDER CABLES BURNED IN THE BULK CARGO COMPARTMENT LOCATION STA 2060 INNER FRAME NEAR FWD LEFT WASTE TANK. ALSO HAVE CMC EXISTING FAULT MESSAGES: APU GENERATOR-FEEDER-1 FAIL 24049 & APU GENETATOR-1 FAIL 24048. FOUND WIRE W944-113 OUTER SKIN WORN AT STA 2060 NEAR BRACKET. TAPE FEEDER CABLE. APU GEN 1 UNABLE TO BE USED UNTIL FEEDER CABLE REPLACED. PICTURES ON RVI SITE. CHK WITH LINE EG FOR POSSIBLE EVA UNTIL C-CK OR REPAIR AS NECESSARY. SFOLE IS TO MEET AC & EVAL REPAIR TO CABLES. SUGGEST REPLACING SECTION BETWEEN SP430 AND SM3 ONLY. SEE WIRE LIST PAGE 744. REPAIRED REF EVA 80190. IDG OPS CHECKED NORMAL.

Part: SEAL — DETERIORATED (NR 1 WINDOW) · airframe 84,045 hrs · 10,235 cycles

LEFT NR 1 WINDSHEILD MOISTURE SEAL SHOWS SIGN OF DETERIORATION ALONG TOP EDGE. INSTALLED MOISTURE SEALANT AT NR 1 LT WINDOW IAW MM. WINDOW TO BE REPLACED WITHIN 150 HRS OR LESS. WINDOW REPLACED.

Part: LIGHT — UNSECURE (CABIN) · airframe 84,080 hrs · 10,238 cycles

EMERGENCY LIGHTS AFT OF DOOR 1L IS HANGING FROM WIRES. SECURED WIRES.

Part: PAN — CRACKED (GALLEY DRAIN) · airframe 83,929 hrs · 10,223 cycles

WATER POURING OUT OF CEILING ON T/O ROWS 20-25 ON LT SIDE CABIN TO RT OF THE LIGHTS. CONFIRMED U-D GALLEY SINK DRAIN AND CHILLER DRAIN PAN LINES ARE CLEAR, POUR SEVERAL GAL H2O DOWN EACH AND CONFIRM NO LEAKS INTO CABIN. CK U-D GALLEY CHILLER DRAIN PAN IS NOT DAMAGED, CK U-D GAL FOR H2O LEAK ONTO FLOORING, U-D GALLEY SINK TO BE DEFERRED IF SOURCE IS NOT DETERMINED. AFTER POURING H20 DOWN GALLEY DRAIN, INSPECTED CEILING & STOWBINS IN AREA OF ROWS 19-25. ALL AREAS WERE DRY. UPPER DECK GALLEY DRAIN DEACTIVATED PRECAUTIONARY UNTIL FURTHER TROUBLESHOOTING ACCOMPLISHED. FOUND CRACK IN GALLEY PAN DRIP SHIELD. SEALED PER MM. DRAIN REACTIVATED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 83,519 hrs · 10,175 cycles

EMERGENCY CEILING LIGHT DOOR 3L THROUGH DOOR 4L ARE INOP. REPLACED BATTERY ABOVE SEAT 36. OP CHECK NORMAL.

Part: LAMP — INOPERATIVE (DOOR 2R GALLEY) · airframe 83,519 hrs · 10,175 cycles

DOOR 2R GALLEY LOWER EMERGENCY LIGHT INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,519 hrs · 10,175 cycles

EMERGENCY LIGHT ON SEAT 54 THROUGH 60 RT INOP. REPAIRED EEL STRIP ON FLOOR NEAR AFT GALLEY, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,519 hrs · 10,175 cycles

EMERGENCY LIGHT SEAT 50ABC INOP. RELAMPED, OP CHECK NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,519 hrs · 10,175 cycles

EMERGENCY CEILING LIGHT ABOVE SEAT 35, 38, 40, 43 AND 45 INOPERATIVE. FOUND DEFECTIVE BATTERY. REPLACED BATTERY ABOVE SEAT 36. OP CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,519 hrs · 10,175 cycles

EMERGENCY LIGHT SEAT 57ABC INOPERATIVE. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 83,519 hrs · 10,175 cycles

EMERGENCY LIGHT AT AFT GALLEY RT LOWER WALL INOP. REPAIRED EEL STRIP NEAR FLOOR BY AFT GALLEY, OPS NORMAL.

Part: TOILET — LEAKING (LAVATORY) · airframe 83,368 hrs · 10,159 cycles

WATER LEAK AT MID CABIN LAV, RTFL. LEAK FROM COMMODE ASSY. REPLACED LEAKING TOILET ASSEMBLY. OPS ARE NORMAL.

Part: FIRE BOTTLE — UNDERSERVICED (CARGO BAY) · airframe 83,021 hrs · 10,120 cycles

FWD PIT FIRE BOTTLE 'A' IS UNDERSERVICED. REPLACED "A" BOTTLE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 82,945 hrs · 10,108 cycles

SEAT ROWS 45ABC THROUGH 53ABC EMERGENCY LIGHTS INOP, GALLEY EMERGENCY LIGHT STRIP BY DOOR 4L INOP, DOOR 4L & 4R EXIT LIGHTS INOPERATIVE. REPLACED GALLEY EMERGENCY LIGHT STRIP LIGHT, CLEANED CONNECTORS, OP CHECKS GOOD.

Part: FEEDER CABLE — DISCONNECTED (EMEGENCY LIGHT) · airframe 82,945 hrs · 10,108 cycles

SEAT ROW 37HJK SEAT BOTTOM EMERGENCY LIGHT STRIP INOPERATIVE. CONNECTED UNDER SEAT CABLE, OP CHECKS GOOD.

Part: WIRE HARNESS — CHAFED · airframe 82,945 hrs · 10,108 cycles

FOUND WIRE BUNDLE STARTING TO CHAFE ON OEU ABOVE AFT LT INBD LAV. DAMAGE LIMITED TO INSULATION ONLY. REPAIRED WITH TEFLON WRAP AND SECURED. PROVIDED CLEARANCE.

Part: ADC — FAILED (NR 2) · airframe 82,732 hrs · 10,085 cycles

AIRCRAFT HAS PITCH OSCILLATION (PORPOISES) WITH ANY AUTOPILOT IN COMMAND AND (V-S, ALT HOLD, VNAV, FLCH) MODE SELECTED. REPLACED LOWER RT ADC. PERFORMED THE FOLLOWING: HOOKED UP AIR DATA TESTER TO LT & RT ADC'S. APPLIED PRESSURE FOR 5000 FT & 250 KTS, THEN 15000 FT & 250 KTS. CAPT & FO'S AIR DATA INSTRUMENTS AGREE. RECONNECTED HOSES TO ADC'S THEN CONNECTED TO PITOT PROBES. PERFORMED 5000 FT LEAK CHECK & FOUND LOWER RT PITOT (AUX 2 PITOT) LEAKING. REPLACED LOWER RT PITOT PROBE IAW MM, PITOT LEAK CHECK OK, ACCURACY CHECK OK.

Part: LIGHT — INOPERATIVE (SEAT 56) · airframe 82,671 hrs · 10,080 cycles

SEAT 56H FLOOR PROX EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,415 hrs · 10,050 cycles

DOOR 5L GALLEY WALL EMERGENCY LIGHT INOP. REPLACED EMERGENCY LAMP, OP CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,415 hrs · 10,050 cycles

EMERGENCY CEILING LIGHT FROM ROW 35 THROUGH 45 LT INOP. REPLACED BATTERY PACK. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 82,415 hrs · 10,050 cycles

DR2 LT EMERGENCY BUSSEL LIGHT INOPERATIVE. REPLACED LIGHT ASSY, CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,415 hrs · 10,050 cycles

EMERGENCY LIGHT ROW 45 THROUGH 53 LT INOP. REPLACED BATTERY PACK ABOVE DR 4LT . CLEANED AND RESECURED EMERGENCY LIGHT CONNECTOR. OPS CK NORMAL.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 82,415 hrs · 10,050 cycles

MAIN GALLEY WALL EMERGENCY LIGHT FWD AND S SIDE WALL INOP. REPLACED BATTERY PACK. CLEANED AND RESECURED CONNECTOR. OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,415 hrs · 10,050 cycles

EMERGENCY CEILING LIGHT ROW 35 THROUGH 45 RT INOP. REPLACED BATTERY PACK. OP CK NORMAL.

Part: EXTINGUISHER — DEFECTIVE (APU BAY) · airframe 82,145 hrs · 10,019 cycles

PRIOR TO DEPARTURE STATUS MESSAGE 26043 - APU BOTTLE LOW PRESSURE DISPLAYED. DEFERRED IAW MEL. APU NOT TO BE USED. BASED ON AHM, THIS IS 1ST HIT. MAY NEED BOTTLE PCN 635 -1090. REPLACED BOTTLE.

Part: UNKNOWN — SPARKS · airframe 81,979 hrs · 9,999 cycles

E WITH A SINGLE SPARK OCCURRED WHILE LEVELING AT FL330 NO BURN MARKS OR OTHER SAMC TEXT: OR OTHER ANOMALIES NOTED. NO POPPED CB. PER FLT CREW.. NO RECURRANCE OF THE SPARK. MAY HAVE BEEN STATIC OF SOME SORT. ALL IS WELL. OPENED OVHD CIRCUIT BREAKER PANELS TO CHECK FOR EVIDENCE OF SUSPECTED PROBLEM. ALL AREAS SHOWED NO SIGNS OF ARCING OR OTHER ELECTRICAL ANOMALIES. ALL GLARESHIELD AND CKPT PANEL LIGHTING WORKING NORMALLY.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 81,916 hrs · 9,991 cycles

EMERGENCY EXIT LIGHT INOP DOOR 5, LT GALLEY AREA, LOWER AFT WALL. REPAIRED WIRING.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,916 hrs · 9,991 cycles

LEFT WING EXTERIOR EMERGENCY EXIT LIGHTS INOP. 2 EA. AFT LIGHT ASSY'S. REPLACED FUSE. LIGHTS OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,916 hrs · 9,991 cycles

EMERGENCY EXIT LIGHTS INOP, DOOR 2 GALLEY AREA LOWER WALL LT AND RT. RELAMPED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 81,916 hrs · 9,991 cycles

EMERGENCY EXIT EMERGENCY LIGHTS INOP. DOOR 4 GALLEY AREA LOWER WALL, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LT, AND SEAT ROW 45 LT. REPAIRED WIRING.

Part: MODULE — FAULTY (UPPER DECK DOOR) · airframe 81,787 hrs · 9,977 cycles

RIGHT UPPER DECK DOOR BATTERY TEST INOP. REPAIRED SWITCH MODULE ASSY, CHECKS OK.

Part: CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,345 hrs · 9,918 cycles

EMERGENCY LIGHT ROW 38 RT INOPERATIVE. REPLACED EMERGENCY LIGHT CABLE. OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,345 hrs · 9,918 cycles

EMERGENCY LIGHT AT BOTTOM OF WALL, AFT GALLEY AT DR5 RT, INOP. RESECURED EMERGENCY LIGHT CONNECTOR. OPS CK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,345 hrs · 9,918 cycles

EMERGENCY LIGHT ROW 54 TO ROW 59 RT INOPERATIVE. RESECURED EMERGENCY LIGHT CONNECTOR. OPS CK NORMAL.

Part: LAMP — INOPERATIVE (DOOR 4L) · airframe 81,345 hrs · 9,918 cycles

DOOR 4L SILL EMERGENCY LIGHT INOP. RELAMPED. OPS CHECKS NORMAL.

Part: O-RING — UNSERVICEABLE (ESCAPE SLIDE)

LOW BOTTLE PRESSURE. LEAKING AT ACTUATOR ASSY. REPLACED O-RING BETWEEN VALVE BODY AND ACTUATOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,060 hrs · 9,884 cycles

EMERGENCY LIGHT FROM ROW 45 TO 53 LEFT SIDE INOP, NOTICED WHILE OP CHECKING SEAT 33C. REPLACED EMERGENCY LIGHT LAMP STRIP. EMERGENCY LIGHTS OPS CHECKS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 39 LT INOPERATIVE. RELAMPED. OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 33R INOP. RELAMPED. OP CK NORMAL.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHT) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 25 LT INOP. FOUND FEEDER DISCONNECTED, CKS OK.

Part: CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY FLOOR LIGHT ON MAIN GALLEY FWD AND SIDE LT INOP. REPLACED EMERGENCY LIGHT CABLE. OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 38R INOP. RELAMPED. OP CK NORMAL.

Part: PANEL — CRACKED (RT WING) · airframe 80,811 hrs · 9,856 cycles

RT WING UPPER PANEL HAS APPROX 3FT LONG CRACK. ACCOMPLISHED INTERIM REPAIR, REF UA-EVA-73177. ACCOMPLISHED INTERIM REPAIR, REF UA-EVA-73177. WILL NEED PERMANENT REPAIR BY C CHECK. WILL REQUIRE AUTOCLAVE REPAIR OF EXISTING PANEL OR A NEW PANEL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT, SEAT 6 LT INOP. RELAMPED, CHECKS OK.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 45 TO 53 INOP747422. REPLACED EMERGENCY LIGHT CABLE. OP CK NORMAL.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHT) · airframe 80,811 hrs · 9,856 cycles

ON DR3 CROSS AISLE EMERGENCY LIGHT INOP. FOUND FEEDER CABLE DISCONNECTED. CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 40R INOP. RELAMPED. OPS CK NORMAL.

Part: CONNECTOR — DISCONNECTED (BATTERY PACK) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY CEILING LIGHT FROM SEAT 37 TO SEAT 45 RT INOPERATIVE. RESECURED BATTERY CONNECTION. OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 21 LT INOPERATIVE. RELAMPED. OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,811 hrs · 9,856 cycles

EMERGENCY LIGHT SEAT 54R INOP. RELAMPED. OPS CK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT LIGHTS INOP LEFT OVERWING EXTERIOR AFT 2 LIGHT ASSY'S. REPLACED M7919 POWER SUPPLY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT SIGN INOP UPPER DECK CEILING JUST AFT OF ROW 17. REPLACED BATTERY, OPS CHECKS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT LIGHT INOP FWD STAIRS ILLUMINATION. REPLACED BATTERY, OPS CHECKS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT SIGN INOP AT STAIRS FWD SIGN. REPLACED BATTERY, OPS CHECKS NORMAL.

Part: CONNECTOR — INOPERATIVE (SEAT ROW 42 R) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT LIGHT INOP SEAT ROW 42 RIGHT. SECURED CONNECTOR.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING JUST AFT OF ROW 17. REPLACED BATTERY, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT ROW 38R) · airframe 79,809 hrs · 9,747 cycles

EMERGENCY EXIT LIGHT INOP SEAT ROW 38 RIGHT. INSTALLED NEW LIGHT AT SEAT 33J. OPS CHECKS GOOD.

Part: HINGE FITTING — DAMAGED (L1 DOOR) · airframe 79,619 hrs · 9,725 cycles

DOOR 1L REPLACE THE UPPER TORQUE TUBE HINGE FITTING. MAJOR REPAIR ACCOMPLISHED. UPPER TORQUE TUBE FITTING HOLES PICKED UP, LOCATED TORQUE TUBE BEARING STARTED PARTIAL INSTALLATION. COMPLETED INSTALLATION OF FITTING NR 145.

Part: TORQUE BOX — DAMAGED (FUSELAGE) · airframe 79,619 hrs · 9,725 cycles

REMOVED UPPER CASTING OF DOOR 1L FUSELAGE HINGE TORQUE BOX ACCOUNT OF DAMAGED. MAJOR REPAIR ACCOMPLISHED. BEGAN INSTALLATION OF FITTING. COMPLETED INSTALLATION OF UPPER TORQUE BOX CASTING.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 79,619 hrs · 9,725 cycles

DOOR 1L REPLACE UPPER STOP FITTING. MAJOR REPAIR ACCOMPLISHED. PICKED UP HOLES IN STOP FITTING, STARTED PARTIAL INSTALLATION. REPLACED DOOR 1L FITTING NR 650.

Part: REVEAL — DAMAGED (L1 DOOR FRAME) · airframe 79,619 hrs · 9,725 cycles

REMOVED UPPER FRAME REVEAL AT STA 434 DOOR 1L CUTOUT. MAJOR REPAIR ACCOMPLISHED. DRILLED AND FIT REVEAL. NEEDS TO BE PRIMED AND FINAL INSTALLATION. PICKED UP HOLES STARTED PARTIAL INSTALLATION NEED SKIN FOR FINAL HOLE LOCATION AND INSTALLATION. COMPLETED INSTALLATION OF DOOR 1L REVEAL.

Part: SKIN PANEL — DAMAGED (L1 DOOR) · airframe 79,619 hrs · 9,725 cycles

DOOR 1 LEFT LOWER FWD SKIN PANEL DAMAGED DUE TO DOOR CONTACT WITH JETWAY. MAJOR REPAIR ACCOMPLISHED. MFG'D AND INSTALLED NEW LOWER FWD SKIN SECTION OF DOOR 1L. INSPECTED INSTALLATION OF LOWER SKIN SECTION OF DOOR 1L.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 78,728 hrs · 9,627 cycles

EMERGENCY LIGHTS INOP ON STAIRS INOP. REPAIRED WIRING.

Part: WEB — MISREPAIRED (FUSELAGE) · airframe 78,521 hrs · 9,602 cycles

FOUND SHORT EDGE MARGIN AT 2 FASTENER HOLES FOR WEB P/N 146U1321-7 AT BS 2292-2300, RBL 60-80. MAJOR REPAIR ACCOMPLISHED MANUFACTURED & INSTALLED NEW WEB & INTERCOSTAL.

Part: STRUCTURE — CRACKED (HORIZ STAB) · airframe 78,521 hrs · 9,602 cycles

FOUND FASTENER HOLE CRACKED COMMON TO RT SIDE OF HORIZONTAL STAB. CENTER SECTION & LOWER SPLICE PLATE. OVERSIZED FASTENER HOLE & REPLACED RT LOWER SPLICE PLATE.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,521 hrs · 9,602 cycles

FUSELAGE SKIN DENTED AT BS 2320-2340 STR 21R-22R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED EXTERNAL DOUBLER & REPLACED STRINGER 21 HAT SECTION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,521 hrs · 9,602 cycles

EEL DOES NOT REMAIN ON AT UPPER DECK CEILING FWD END. REPLACED BATTERY PACK AT LOCATION 675C, OP CHECK OKAY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 78,521 hrs · 9,602 cycles

EEL INOP AT SEAT 6B. SECURED CONNECTOR, OP CHECK OKAY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 78,521 hrs · 9,602 cycles

EEL INOP AT G1 GALLEY LT WALL. SECURED CONNECTOR, OP CHECK OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,521 hrs · 9,602 cycles

LT OVERWING EMERGENCY EXIT LIGHTS INOP, 3RD & 4TH FROM FWD END. REPLACED FUSE & LAMPS, OP CHECK OKAY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 78,521 hrs · 9,602 cycles

EEL INOP AT LAV 111 LT OUTER WALL. RE-SECURED CONNECTOR, OP CHECK OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 78,521 hrs · 9,602 cycles

EEL'S INOP FROM SEAT 1K TO 4K. FOUND CONNECTOR P1 LOOSE AT SEAT 4K. RE-SECURED, OP CHECK OKAY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 78,521 hrs · 9,602 cycles

EMERGENCY EXIT GREEN STRIP LIGHTS INOP ROWS 45 ABC THRU 53 ABC. SECURED EEL CONNECTOR AT BS 1745 LT SIDEWALL, OP CHECK OKAY.

Part: CABLE — FAULTY (CABIN) · airframe 78,521 hrs · 9,602 cycles

EEL'S INOP AT LAV 111 FWD WALL & LAV 112 SIDEWALL. REPLACED EEL CABLE ASSY, OP CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,521 hrs · 9,602 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP, 3RD FROM FWD END. RELAMPED, OPS CHECK OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 78,521 hrs · 9,602 cycles

EMERGENCY EXIT GREEN STRIP LIGHT SEAT 42KJH INOP. EEL LIGHT PLUG LOOSE SO RECONNECTED THE PLUG AND THEN OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,153 hrs · 9,558 cycles

EMERGENCY EXIT EEL INOP ACROSS DOOR 3 RIGHT LOWER WALL. REPLACED EEL AT RIGHT LOWER WALL AT 3R, OPS NORMAL.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHTS) · airframe 78,153 hrs · 9,558 cycles

EMERGENCY EXIT LIGHTS VERY DIM SEAT ROWS 54 RIGHT THRU 60 RIGHT, DOOR 5 RIGHT FWD EXIT SIGN, AND DOOR 5 RIGHT AFT LOWER WALL EMERGENCY LIGHT. FOUND WET UNDER FLOOR MAT. REPAIRED SHORT UNDER FLOOR MAT.

Part: CONNECTOR — SHORTED (CABIN) · airframe 78,153 hrs · 9,558 cycles

EMERGENCY EXIT SIGN IS INOP AT DOOR 4 RIGHT AFT EXIT SIGN, EMERGENCY LIGHTS AT SEAT ROWS 45 THRU 53 LEFT, EMERGENCY LIGHT SIGN AT DOOR 4 LEFT FWD SIGN, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LEFT, AND LOWER WALL EMERGENCY LIGHT IN GALLEY AREA. REPAIRED SHORT UNDER RUBBER MAT, FOUND WET.

Part: CONNECTOR — LOOSE (CABIN) · airframe 78,153 hrs · 9,558 cycles

EMERGENCY EXIT EEL INOP BETWEEN LAVS 111 AND 112 LOWER WALL. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,153 hrs · 9,558 cycles

EMERGENCY EXIT LIGHT INOP DOOR 5 RIGHT FWD SILL. RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 78,153 hrs · 9,558 cycles

EMERGENCY EXIT EELS INOP SEATS 33 RIGHT THRU 43 RIGHT. SECURED CONNECTOR. OPS CHECKS NORMAL.

Part: WIRE — PULLED (CONNECTOR) · airframe 78,037 hrs · 9,546 cycles

FOUND EMERGENCY LIGHT ON SEAT 35H TORN OFF. REPLACED SEAT LIGHT, NO HELP. FOUND WIRE PULLED OUT AT CONNECTOR OF SEAT HARNESS. REPLACED CABLE. CHECKS GOOD.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 77,594 hrs · 9,497 cycles

EMERGENCY EXIT EEL LIGHTS INOP AT DOOR 4 RT AFT. EXIT EEL SIGN, DOOR 4 LT FWD EXIT EEL SIGN, SEATS 45 THRU 53 LT, LOWER WALL EEL LIGHT ACROSS DOOR 4 LT, AND LOWER WALL EEL LIGHT AT DOOR 4 GALLEY AREA. REPLACED POWER FEEDER. ALL EEL LIGHTS OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,594 hrs · 9,497 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT ROW 46 LT. RELAMPED. CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,594 hrs · 9,497 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 5 RT BUSTLE LIGHT. REPLACED LIGHT ASSY. OPS CKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,594 hrs · 9,497 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 5 LT FWD SILL LIGHT. REPLACED LAMP. OPS CKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,594 hrs · 9,497 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT 57 RT. RELAMPED, CHECKS OKAY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT LIGHT INOP DOOR 3 RIGHT CEILING ENTRY LIGHT. REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT LIGHT INOP DOOR 3 RIGHT BUSTLE LIGHT. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT EEL LIGHT INOP DOOR 2 LEFT AFT EXIT SIGN. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT LIGHT INOP DOOR 2 LEFT CEILING ENTRY LIGHT. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT LIGHT INOP SEAT ROW 10 RIGHT FWD LIGHT ASSY. REPLACED LAMP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT SIGN INOP AT DOOR 3 RIGHT UPPER SIGN. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,044 hrs · 9,436 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 39 LEFT. REPLACED LIGHT ASSY.

Part: LIGHT — BROKEN (CABIN) · airframe 76,978 hrs · 9,428 cycles

EEL LIGHT BROKEN AT 45C, 35H, 38H. REPLACED EEL AT 45C, CHECKS OKAY. REPLACED EEL STRIP AT SEAT 35H & 38H. OPS OKAY.

Part: CONNECTOR — CONTAMINATED (CABIN) · airframe 76,978 hrs · 9,428 cycles

SEAT EEL INOP FROM SEAT 45ABC TO 53ABC. REPLACED BATTERY PACK (M6011) ABOVE DOOR 4L, NO HELP. FOUND EEL CONNECTOR UNDER GALLEY MAT SOAKING WET, DRIED OUT WIRING AND SECURED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,697 hrs · 9,398 cycles

EEL LIGHT SEAT 42 ABC INOP. LIGHT INOPERATIVE. REPLACED LAMP, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,697 hrs · 9,398 cycles

EMERGENCY CEILING LIGHT AFT OF DOOR 1 LEFT INOP. LAMPED FOUND INOPERATIVE. REPLACED LAMP, OPS NORMAL.

Part: CONNECTOR — CONTAMINATED (EMERGENCY LIGHT) · airframe 76,697 hrs · 9,398 cycles

FLOOR EEL LIGHTS INOP SEAT 54 TO 60 HJK. FOUND CONNECTION AT DOOR 5 CROSSAISLE FOR EMERGENCY LIGHT, WET AND SHORTING CONNECTION. DRIED AREA & CONNECTION. ALL OPS NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 76,697 hrs · 9,398 cycles

FLOOR EEL LIGHTS INOP SEAT 33 TO 43 HJK. FOUND SHORTED EMERGENCY LIGHT AT 36 HJK. REPLACED LIGHT. ALL OPS NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 76,697 hrs · 9,398 cycles

FLOOR EEL LIGHTS INOP SEAT 45 TO 53 ABC. REPLACED BAD AND WET SUPPLY WIRE FOR EEL LIGHT SYS. OPS CHECK OK.

Part: LIGHT — MISSING (CABIN) · airframe 76,697 hrs · 9,398 cycles

FLOOR EEL LIGHT MISSING SEAT 56HJK. REPLACED EEL LAMP SEAT. OPS CHECK OK.

Part: WIRE — DAMAGED (CABIN) · airframe 76,697 hrs · 9,398 cycles

AFT GALLEY LWR LEFT TWO EEL LIGHTS INOP. REPLACED DAMAGED SUPPLY WIRE DUE. OPS CHECK OK.

Part: LIGHT — MISSING (CABIN) · airframe 76,697 hrs · 9,398 cycles

FLOOR EEL LIGHT MISSING SEAT 54 HJK. LIGHT DISCOVERED MISSING. REPLACED SEAT EEL LAMP. OPS CHECK OK.

Part: SLIDE — FAULTY · airframe 76,494 hrs · 9,376 cycles

RT UPPER DECK SLIDE ARM-DISARM LEVER HARD TO MOVE. REPLACED UPPER DECK SLIDE ASSY. FUNCTION OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (ROW 56) · airframe 76,153 hrs · 9,336 cycles

EMERGENCY LIGHT ROW 56 RT INOP. *S/D* RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,153 hrs · 9,336 cycles

EMERGENCY LIGHT AFT GALLEY LOWER WALL LT INOP. *S/D* REPLACED EEL CABLE. OP CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 76,153 hrs · 9,336 cycles

DOOR 4 RT AFT EXIT LIGHT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECK GOOD. ACFT OK FOR SERVICE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 76,153 hrs · 9,336 cycles

EMERGENCY LIGHT LT FROM ROW 45 TO 53 INOP. *S/D* REPLACED EEL CABLE. OP CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,733 hrs · 9,286 cycles

EEL'S INOP AT DOOR R3 & L3 AISLEWAYS. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK OK REF MM 33-51-04. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,733 hrs · 9,286 cycles

DOOR 1L OVERHEAD EMERGENCY EXIT LIGHT INOP. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK OK REF MM 33-51-04. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP, LEFT SIDE LOWER WALL BY LAV 111. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD.AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 43L) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 43 LEFT. SUPPLEMENTAL, REPLACED LIGHT ASSY. OP CKS NORMAL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 39 RIGHT. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT LIGHT INOP, JUST AFT OF ROW 18 CEILING LIGHT. SUPPLEMENTAL, RELAMPED. OPS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 55R) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 55 RIGHT. SUPPLEMENTAL, REPLACED LIGHT ASSY. OPS CHKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP, ACROSS DOOR 4 RIGHT LOWER WALL EEL. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT LIGHT INOP, AT DOOR 4 RIGHT BUSTLE LIGHT. REPLACED BUSTLE LIGHT ASSEMBLY. OP CHECKS OK. ACFT OK FOR SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 40 RIGHT. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 33R) · airframe 75,002 hrs · 9,208 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 33 RIGHT. SUPPLEMENTAL, REPLACED LIGHT ASSY. OP CKS NORMAL.

Part: LAMP — MISSING (CABIN) · airframe 74,537 hrs · 9,158 cycles

SEAT 4HJK EMERGENCY LIGHT IS MISSING. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,100 hrs · 9,112 cycles

EMERGENCY EXIT LIGHT INOP AT UPPER DECK DOORS FWD CEILING LIGHT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,100 hrs · 9,112 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 5 LEFT BUSTLE. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,100 hrs · 9,112 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 2 RIGHT BUSTLE. REPLACED LIGHT ASSEMBLY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 74,100 hrs · 9,112 cycles

EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3 LEFT LOWER AISLE WALL. SECURED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,100 hrs · 9,112 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT 55 RIGHT. REPLACED LIGHT ASSEMBLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,621 hrs · 9,066 cycles

EMERGENCY CEILING LIGHT AT ROW 23 ABC INOPERATIVE. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,621 hrs · 9,066 cycles

EMERGENCY LIGHT AT ROW 34 SEAT HJK INOP. RELAMPED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 73,126 hrs · 9,012 cycles

EMERGENCY EXIT EEL LIGHTS INOP FROM ROWS 32 THRU 34 LEFT AND AT ROW 49 LEFT. RESECURED CONNECTOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,126 hrs · 9,012 cycles

EMERGENCY EXIT CEILING LIGHTS INOP. ALL IN FIRST CLASS AND FROM ROW 6 THRU 8 LEFT AND RIGHT. REPLACED BATTERY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,126 hrs · 9,012 cycles

UPPER DECK EMERGENCY EXIT CEILING LIGHT AT ROW 13 AND EMERGENCY EXIT STAIRS CEILING LIGHT LEADING TO UPPER DECK ARE INOPERATIVE. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,683 hrs · 8,966 cycles

D-ZONE LEFT COLUMN EEL NOT ON. 11-01-07 REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,683 hrs · 8,966 cycles

D-ZONE LEFT EMERGENCY PATH LIGHT OUT. 11-01-07 REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: CABLE — CUT (CABIN) · airframe 72,683 hrs · 8,966 cycles

ZONE-C RIGHT EEL CABLE CUT. 11-01-07 REPLACED WITH NEW CABLE. OPS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,683 hrs · 8,966 cycles

STATION 400-420 S41-42R, EXTERNAL FUSELAGE SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: CYLINDER — LOW PRESSURE (EVAC SLIDE) · airframe 72,683 hrs · 8,966 cycles

NR 5R MED ESCAPE SLIDE CYLINDER PRESSURE LOW. SUSPECT FAULTY RELEASE VALVE SEAL. REPLACED SLIDE RAFT ASSEMBLY. AC OK FOR SERVICE.

Part: SEAL — LEAKING (EVAC SLIDE) · airframe 72,683 hrs · 8,966 cycles

ESCAPE SLIDE PRESSURE LOW, UPPER DECK RT AFT. SUSPECT FAULTY RELEASE VALVE SEAL. REPLACED WITH SERVICEABLE RESERVOIR AT UPPER DECK RT AFT PER AMM 25-68-02. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,611 hrs · 8,959 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 13 INOP. 10-19-07 RELAMPED. OP CHECKS NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,611 hrs · 8,959 cycles

EMERGENCY LIGHTS AT ROWS 1A, 2A AFT & 35ABC ARE INOPERATIVE. 10-19-07 RELAMPED ALL SEAT POSITIONS. ALL OP CHECKED OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,181 hrs · 8,913 cycles

FOUND SEAT 2A AFT EMERGENCY LIGHT AND ROW 47 HJK EMERGENCY LIGHTS INOPERATIVE. 08-31-07 RELAMPED EMERGENCY LIGHTS, BOTH POSITIONS. OP CHECKS NORMALLY.

Part: CONNECTOR — UNSECURE (ROW 42 ABC) · airframe 72,181 hrs · 8,913 cycles

FOUND ROW 42 ABC EMERGENCY LIGHT INOPERATIVE. 08-31-07 RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (ROW 53 ABC) · airframe 72,181 hrs · 8,913 cycles

FOUND ROW 53 ABC EMERGENCY LIGHT INOP. 08-31-07 RESECURED EMERGENCY LIGHT. OP CHECKS NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,181 hrs · 8,913 cycles

FOUND ROW 24 EMERGENCY LIGHTS INOP. 08-31-07 RELAMPED EMERGENCY CEILING LIGHT . OP CK NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,692 hrs · 8,863 cycles

UPPER DECK CEILING 2 EA EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,692 hrs · 8,863 cycles

SEAT 2A FWD EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,692 hrs · 8,863 cycles

DOOR 3R FWD SILL EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 71,692 hrs · 8,863 cycles

FWD ASSY FWD EMERGENCY LIGHT IS INOP. [07-27-07] RELAMPED LEFT OVERWING EMERGENCY LIGHT ASSY. CHECKS NORMAL.

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHTS) · airframe 71,692 hrs · 8,863 cycles

DOOR 5R SLIDE EMERGENCY LIGHT FLICKERS ON WHEN DOOR IS CLOSED AND LOCKED. FOUND WIRE HARNESS FAULTY. [08-08-07] FOUND WIRES W2088-004-20 & W2088-005-20 BROKEN IN FLEX CONDUIT BETWEEN CONNECTOR DX323 & TB214, REF WDM 33-51-61 PG.1 SH.1. REPLACED HARNESS AND GRD CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (FWD CARGO BAY) · airframe 71,562 hrs · 8,852 cycles

MAINTENANCE MSG -CARGO FWD-1 LOOP-A- ON ARRIVAL. [07-27-07] CONDUCTED TROUBLE-SHOOTING BASED ON MAINT MSG "CARGO FWD-1 LOOP-A" ON ARRIVAL. PERFORMED GND TEST & SYSTEM FAILED. REPLACED FWD CARGO NR 1 LOOP A DETECTOR.

Part: COVER — BROKEN (CABIN) · airframe 71,591 hrs · 8,855 cycles

EEL COVER BROKEN ZONE 614 BEHIND SEAT 47H. [07-24-07] REPLACED EEL LIGHT AT SEAT 47H. LIGHT OPERATES NORMALLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,237 hrs · 8,818 cycles

WALL EEL INOP, DOOR 4R AISLE. [06-22-07] REPLACED POWER SUPPLY FOR EEL. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,237 hrs · 8,818 cycles

EMERG LT INOP, CEILING ROW 12. [06-22-07] RELAMPED,OPS CHECK GOOD RE FMM 33-51-00.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 71,237 hrs · 8,818 cycles

EEL INOP, SEAT 4F BOTH SECTIONS. [06-22-07] REPLACED AFT EEL AT 4F AND SECURED LOOSE CONNECTOR UNDER SEAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,237 hrs · 8,818 cycles

EEL INOP: ROW 55 HJK AND ROW 57 HJ. [06-22-07] REPLACED SEAT EEL LAMP,OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,237 hrs · 8,818 cycles

EMERGENCY LT INOP:RT OVERWING FWD ASSY. [06-22-07] REPLACED LAMPS OP CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,237 hrs · 8,818 cycles

WALL EEL INOP BETWEEN MID LAVS. [06-22-07] SECURED CONNECTOR. OPS. CKS. NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,237 hrs · 8,818 cycles

EEL INOP: ROWS 35 & 46 ABC. [06-22-07] SECURED CONNECTOR. OPS CKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,237 hrs · 8,818 cycles

EMERGENCY LIGHT INOP DOOR 5L SLIDE ILLUMINATED. [06-22-07] RELAMPED. OPS. NORMAL.

Part: LUG — CORRODED (NR 1 PYLON) · airframe 70,710 hrs · 8,761 cycles

BORE CORRODED AND SCRATCHED - NR 1 PYLON STRUT FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 1 PYLON STRUT FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2750" OUTBTD=2.2450". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION.

Part: LUG — CORRODED (NR 4 PYLON) · airframe 70,710 hrs · 8,761 cycles

BORE CORRODED AND SCRATCHED - NR 4 PYLON DUAL SIDE BRACE FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 4 PYLON DUAL SIDE BRACE FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2450" OUTBTD=2.2452". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION.

Part: LUG — CORRODED (NR 1 PYLON) · airframe 70,710 hrs · 8,761 cycles

BORE CORRODED AND SCRATCHED - NR 1 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 1 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2446" OUTBTD=2.2447". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION.

Part: LUG — CORRODED (NR 4 PYLON) · airframe 70,710 hrs · 8,761 cycles

BORE CORRODED AND SCRATCHED - NR 4 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 4 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA AFTER HONE: INBD=2.2446" OUTBTD=2.2448". CORROSION & VIBRATION AGGRAVATED BY HIGH TEMP CAUSED DUAL SIDE BRACE HOLE SURFACE DETERIORATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,864 hrs · 8,671 cycles

EMERGENCY EEL LIGHT INOPERATIVE AT DOOR 4 GALLEY RIGHT AFT AISLE. FOUND LOOSE CONNECTOR. SECURED CONNECTOR. OPS. CKS. NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,864 hrs · 8,671 cycles

EMERGENCY EXIT EEL LIGHTS INOPERATIVE AT SEATS 33 RT & 39 RT. REPLACED LAMP ASSY AT BOTH SEATS. ALL EEL LIGHTS OP. CHECK NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,864 hrs · 8,671 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 2 RIGHT CEILING ENTRY. RELAMPED. OP CHECKS NORMALLY.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 69,864 hrs · 8,671 cycles

P5 EMERGENCY STANDBY LIGHTING FAILS TO ILLUM MODULES BACKLIGHTING. REPLACED DIMMING MODULE FUSE, CHKS OK

Part: HINGE — CORRODED (AFT CARGO DOOR) · airframe 69,864 hrs · 8,671 cycles

AFT CARGO DOOR UPPER PIANO HINGE HAS PEELING PAINT AND SURFACE CORROSION (RUST) ON SEVERAL OF THE HINGE SEGMENTS. CLEANED UP SURFACE CORROSION (RUST) ON AFT CARGO DOOR UPPER PIANO HINGE. APPLIED CIC. A/C RETURNED TO SERVICE.

Part: O-RING — UNSERVICEABLE (ESCAPE SLIDE) · airframe 69,260 hrs · 8,611 cycles

LOW BOTTLE, LEAKING AROUND GAUGE O-RING. REPLACED O-RING. REPLACED SLIDE. A/C RETURNED TO SERVICE. ROOT CAUSE SUSPECTED TO BE GAUGE OVER TORQUED DURING INSTALLATION WITH RESULTING DAMAGE TO O-RING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,959 hrs · 8,577 cycles

EEL INOP AT ROW 5F BOTH SECTIONS. REPLACED CONNECTOR . OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,959 hrs · 8,577 cycles

EEL INOP AT ROW 25 RIGHT. REPLACED LAMP, OP CHECKS OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,959 hrs · 8,577 cycles

EEL INOP AT ROW 55-61, EXIT SIGN FWD OF DOOR 5R, AND DOOR 5R AFT CROSS AISLE. *S/D* REPLACED BATTERIES. CHECKS NORMALLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 68,959 hrs · 8,577 cycles

EMERGENCY LIGHTS INOP AT DOOR 4R, DOOR 5L AND DOOR 1L SLIDE ILLUM. *S/D* REPLACED LAMPS IN EACH POSITION. OP CHECKS OK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 68,012 hrs · 8,473 cycles

EEL INOP AT 3A AFT AND 39 HJK. RELAMPED, OP CHECK OKAY.

Part: BOTTLE — LOW (EVAC SLIDE) · airframe 56,148 hrs · 5,451 cycles

LOW BOTTLE PRESSURE.

Part: STRINGER — CORRODED (BS 1930-1960) · airframe 66,603 hrs · 8,315 cycles

FOUND BULK CARGO COMPT BILGE AREA, STRINGER 51L CORRODED BS 1930-1960.

Part: FRAME — CRACKED (BS 1140 S10R) · airframe 66,603 hrs · 8,315 cycles

FOUND BS 1140 STR 10R FRAME AND FWD AND AFT TENSION TIES CRACKED.

Part: STRINGER — CRACKED (BS 460 S10L) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 10L AT BS 460 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 10L AT BS 460 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN 747-53A2484. WORK ACPD ON JOCR 250278.

Part: STRINGER — CRACKED (BS 480 S8R) · airframe 66,603 hrs · 8,315 cycles

FOUND STRINGER 8R AT BS 480 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 8R AT BS 480 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 & SERVICE BULLETIN 747-53A2482 REV. 0.

Part: STRINGER — CRACKED (BS 500 S8L) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 8L AT BS 500 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 8L AT BS 500 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 7 SERVICE BULLETIN 747-53A2484 REV 0. WORK ACPD ON JOCR 250288.

Part: STRINGER — CRACKED (BS 500 S10L) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 10L AT BS 500 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 10L AT BS 500 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN 747-53A2484.

Part: STRINGER — CRACKED (BS 480 S8L) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 8L AT BS 480 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR. 8L AT BS 480 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN 747-53A2482 REV 0.

Part: STRINGER — CRACKED (BS 500 S10R) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 10R AT BS 500 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 10R AT BS 500 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN 747-53A2484. WORK ACCOMPLISHED ON JOB CARD 250287.

Part: STRINGER — CRACKED (BS 480 S10R) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 10R AT BS 480 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 10R AT BS 480 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN 747-53A2484. WORK ACCOMPLISHED ON JOB CARD 250285.

Part: STRINGER — CRACKED (BS 480 S10L) · airframe 66,603 hrs · 8,315 cycles

FOUND STR 10L AT BS 480 CRACKED AT FASTENER HOLE. MAJOR REPAIR, DURING ACCOMPLISHMENT OF COA 849781 FOUND STR 10L AT BS 480 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN 747-53A2482 REV 0.

Part: STRINGER — CRACKED (BS 460 S10R) · airframe 66,603 hrs · 8,315 cycles

FOUND STRINGER 10R AT BS 460 CRACKED AT FASTENER HOLE. DURING ACCOMPLISHMENT OF COA 849781, FOUND STRINGER 10R AT BS 460 CRACKED AT FASTENER HOLE. INSTALLED REPAIR ANGLE REF COA 849781 AND SERVICE BULLETIN SB 747-53A2484 REV 0 WORK ACPD ON JOBCARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,277 hrs · 8,165 cycles

EEL INOP SEAT 48 LT AND 55 LT. *S/D* REPLACED EEL LIGHT.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 65,277 hrs · 8,165 cycles

EEL INOPERATIVE AFT GALLEY CROSS AISLE AT DR 3L AND INOPERATIVE AT RT SIDE AFT GALLEY AT DR 3RT. REPLACED EEL.

Part: SKIN — DAMAGED (STR 28L STA 490) · airframe 63,816 hrs · 7,998 cycles

CRACK FOUND ADJACENT TO FASTENER HOLE STR 28L STA 490. OUTER SKIN CRACKED AT FASTENER HOLE AND TRIMMED AWAY. SKIN'S INNER BONDED DOUBLER ALSO CRACKED AND TRIMMED AWAY. ALSO, FOUND INTERCOSTAL BRACKET ATTACHED TO SKIN AND INTERCOSTAL WEB BUT NOT ATTACHED TO FRAME WEB. SUSPECT THIS PRODUCTION ERROR TO BE RESPONSIBLE FOR SKIN AND BONDED DOUBLER CRACKS.

Part: WIRE — DAMAGED (LAV 110) · airframe 63,462 hrs · 7,956 cycles

EEL INOP AFT SIDE LAV 110. DAMAGED FEEDER CABLE WAS REPAIRED OK.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 63,462 hrs · 7,956 cycles

EEL INOP, ALL LT C ZONE ROWS 22-26. BATTERY PACK NOT HOLDING CHARGE, REPLACED OK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 63,462 hrs · 7,956 cycles

EEL LIGHTS INOP AT ROW 58 LT, ROW 35 LT, LT MID GALLEY, ROW 56 RT, ROW 4A AFT SECTION, ROW 5F AFT SECTION. EEL LIGHTS BURNED OUT, REPLACED OK.

Part: WARNING LIGHT — FALSE INDICATION (CARGO FIRE) · airframe 61,550 hrs · 7,730 cycles

FIRE CARGO FWD MSG ON UPPER EICAS ON FINAL APPROACH. FWD CARGO FIRE BOTTLES WERE DISCHARGED ON ARRIVAL. A CHECK OF THE FORWARD CARGO PIT AFTER LANDING REVEALED NO EVIDENCE OF A FIRE. THE SMOKE DETECTORS WERE COVERED WITH MOISTURE. THIS IS CONSISTENT WITH SIMILAR EVENT ON UNITED 747-400 AIRCRAFT IN THE PAST. IT SUGGESTS THE CARGO WAS PROBABLY SOME SORT OF PRODUCE THAT HAD NOT BEEN PROPERLY WRAPPED TO CONTAIN ITS MOISTURE. FALSE FIRE WARNINGS DUE TO MOISTURE IN THE CARGO PIT ARE A LIMITATION OF BOEING'S SMOKE DETECTION SYSTEM DESIGN.

Part: FRAME — DENTED (FUSELAGE) · airframe 61,081 hrs · 7,674 cycles

DENT WAS FOUND ON THE UPPER I/B T-CHORD ON FRAME AT STA 900 APPROX LBL 20 IN THE FWD HORIZONTAL FLANGE OF THE CHORD. REPAIR ACCOMPLISHED.

Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 61,081 hrs · 7,674 cycles

UPPER T-CHORD FWD FLANGE OF AFT CARGO COMPARTMENT FLOORBEAM AT STA 1760, LBL 51 WAS FOUND DENTED. REPAIR ACCOMPLISHED.

Part: BATTERY — MALFUNCTIONED (ESCAPE SLIDE) · airframe 57,633 hrs · 7,209 cycles

UPPER DECK RIGHT DOOR SLIDE BATTERY LIGHT PRESS TO TEST FUNCTION INOP. CHANGED BATTERIES.

Part: SKIN — DAMAGED (EMPENNAGE) · airframe 57,337 hrs · 7,165 cycles

TAIL STRIKE ON TAKEOFF. AT BEGINNING OF FLIGHT, AT LIFTOFF, EMPENNAGE WAS SCRAPPED ON RUNWAY BETWEEN STATIONS 2635-2734. APU BATT ACCESS DOOR AND APU CLAMSHELL DOORS WERE REPLACED. ALL OTHER FRAME/SKIN DAMAGE BETWEEN NOTED STATIONS REPAIRED. AREA STRUCTURAL INSPECTIONS ACCOMPLISHED WITH NO FURTHER FINDINGS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,210 hrs · 7,023 cycles

RT UPPER DECK EMERGENCY BATTERY PACK NO TEST. REPLACED BATTERY PACK.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,208 hrs · 7,023 cycles

CORROSION IN CENTER OF STRINGER 5L AT STA 1924, LBL 4, WL 92. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: TRANSDUCER — FAILED (MLG) · airframe 53,947 hrs · 6,706 cycles

AIRCRAFT RECEIVED ANTI SKID EICAS MSG ON TAKEOFF ROLL. REPLACED NR 5 ANTI-SKID TRANSDUCER. OP CHECK NORMAL.

Part: ODOR — DETECTED (CABIN) · airframe 53,067 hrs · 6,565 cycles

ONE TO TWO HOURS AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE-ELECTRICAL ODOR IN CABIN. FLIGHT ATTENDANT INDICATED SMOKE-ODOR EMANATED FROM CART LIFT AREA.

Part: HUMIDIFIER — SMOKING (COCKPIT)

SMOKE IN COCKPIT SUDDENLY OCCURRED DURING CRUISE FLIGHT. SELECTED HUMIDIFIER OFF AND SMOKE DISSIPATED.

Part: HUMIDIFIER — DIRTY (COCKPIT)

SMOKE IN COCKPIT SUDDENLY OCCURRED DURING CRUISE FLIGHT. SELECTED HUMIDIFIER OFF AND SMOKE DISSIPATED. *S/D* HEAVY CALCIUM DEPOSITS IN UNIT. SUSPECT SMOKE WAS ACTUALLY CALCIUM IN DUCTS. SHOP CLEANED AND CHECKED UNIT SERVICEABLE.

Part: WIRE — FAILED (CABIN)

UPPER DECK WINDOW LIGHTS AT SEATS 12AB AND 14GH PREVIOUSLY DEFERRED INOP. ON TAXI TO INBOUND GATE CIRCUIT BREAKERS TRIPPED ON P180 AND P414 PANELS. FOUND SEVERAL BURNT AND OVERHEATED WIRES COMMON TO WIRE BUNDLE W7510. *S/D* FOUND EVIDENCE OF ARCING ON AIR DISTRIBUTION DUCT AND SIDE WALL PANEL END CAP LIGHT ASSY UPPER EDGE (P/N 417U7572-1 ASSY 417U7514-1 DETAIL). REPAIRED FIBERGLASS WIRE/WOUND AIR DISTRIBUTION DUCT AND INSULATION. REMOVED DAMAGED WIRE SECTIONS AND SPLICED IN NEW WIRE SECTIONS AND SECURED CLEARANCE BETWEEN SIDE WALL PANEL END CAP UPPER EDGE. TESTED ALL EFFECTED SYSTEMS.

Part: BEARING — FAILED (NR 2 ENGINE GB)

NR 2 ENGINE FLAME-OUT. *S/D* ANGLE GEARBOX AB-1 BEARING FAILED. ENGINE REPLACED.

Part: HUMIDIFIER — FAILED (COCKPIT)

SHORTLY AFTER LEVEL OFF AT CRUISE ALTITUDE, SMOKE APPEARED IN COCKPIT. SMOKE CEASED AFTER LOWER RECIRCULATION FAN SWITCHED OFF. CAUSE UNKNOWN. COULD NOT DUPLICATE CONDITION ON GROUND. HUMIDIFIER WAS REPLACED AS A PRECAUTION.

Part: OVEN — DIRTY (GALLEY)

AIRCRAFT RETURNED TO GATE WITH AN OVEN FIRE. REPLACED OVEN. REMOVED OVEN WAS DISASSEMBLED AND A SMALL DEPOSIT OF SOLIDIFIED PLASTIC WAS FOUND ADHERING TO UPPER SURFACE OF OVEN UPPER INTERNAL BAFFLE PLATE CLOSEST TO FAN MOTOR AND BURNER ELEMENTS. IDENTIFICATION OF SOURCE OF PLASTIC IS UNKNOWN. NO DEFECTS IN OVEN PROPER.