N175UA

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,982 hrs · 11,198 cycles

EMERGENCY LIGHTS INOPERATIVE, UPPER DECK AFT CEILING AND FLOOR. REPLACED THE LAMPS. REPLACED THE BATTERY AND CHARGER ABOVE SEAT 16AB, REPLACED THE BATTERY IN THE CEILING BETWEEN UPPER DECK DOORS. LIGHTS CHECKED GOOD. ACCOMPLISHED IDT INSPECTION OF ON THE BATTERIES INSTALLATION, VERIFIED OPS CHECKED GOOD. IAW AMM 33-51-04 PB 201.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,668 hrs · 11,076 cycles

UPPER DECK FWD EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED THE EMERGENCY LIGHT

Part: LIGHT — MISSING (CABIN) · airframe 99,668 hrs · 11,076 cycles

PER A CHECK, SEAT 19HJK, EMER EXIT LIGHT STRIP MISSING. REPLACED EMER EXIT LIGHT STRIP AT SEAT 19HJK. OPERATIONS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 99,668 hrs · 11,076 cycles

PER A CHECK, SEAT 49HJK EMER EXIT LIGHT STRIP INOPERATIVE. FOUND CONNECTOR ON EMER EXIT LIGHT STRIP DISCONNECTED UNDER SEAT AT 49HJK, SECURE. OPERATIONS CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 99,668 hrs · 11,076 cycles

PER A CHECK, SEAT 45ABC EMER EXIT LIGHT STRIP INOPERATIVE. FOUND LOOSE CONNECTOR ON EMER EXIT LIGHT STRIP UNDER SEAT 45ABC. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 99,668 hrs · 11,076 cycles

PER A CHECK, DOOR 1L SLIDE LIGHT INOPERATIVE. REPLACED SLIDE LIGHT ASSEMBLY AT DOOR 1L. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,224 hrs · 11,035 cycles

DOOR 2 RT CTR GALLEY FLOOR, SINGLE EMER EXIT LIGHT INOPERATIVE. RELAMPED, OPERATIONS CHECKED OK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 98,879 hrs · 11,004 cycles

EXTERNAL FUSELAGE BELLY SKIN AT BS 770 FOUND CORRODED, BETWEEN STRINGER 46R - 47R. REMOVED DAMAGE, FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR IAW ECRA 5330-05547.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 98,879 hrs · 11,004 cycles

CORROSION ON FWD CARGO STATION 822, STRINGER 47L - 47R, INTERIOR SKIN. REPAIRED IAW ECRA 5330-0554 7.

Part: DOUBLER — CRACKED (NR 1 NACELLE) · airframe 98,879 hrs · 11,004 cycles

NUMBER 1 ENG RT 452ER CUT OUT SURROUND SKIN FOUND REPAIR DOUBLER CRACKED AT NAC 228. REPAIRED IAW ECRA 5430-02069.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 98,879 hrs · 11,004 cycles

PITTING ON FUSELAGE EXTERNAL BELLY SKIN AT BS 740 - 840, STRINGER 44L - 44R. REPAIRED IAW ECRA 5330-05547.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 98,879 hrs · 11,004 cycles

BS 2598, LT FRAME SUPPORT, 65B02508-3 WAS FOUND CRACKED FROM A FASTENER HOLE. CRACK EXISTS IN FRAME SUPPORT ONLY. REMOVE CRACK & FABRICATED & INSTALLED DOUBLERS & FILLER REPAIR IAW ECRA 5310-06753.

Part: WIRE — BROKEN (CABIN) · airframe 98,879 hrs · 11,004 cycles

LEFT NR 3 DOOR LAVATORY, EMER LIGHT CABLE IS BROKEN. WIRE IS PART OF LIGHT ASSEMBLY PN 8054-1. REPLACED LIGHT ASSEMBLY PN 8054-1 IAW AMM 33-31-12.

Part: WIRE — BROKEN (CABIN) · airframe 98,879 hrs · 11,004 cycles

UPPER DECK STAIR EMER LIGHT CABLE BROKEN. INSTALLED NEW WIRE, PN 5919-1, IAW SWPM 20-10-11, AMM 33-51-00 & AMM 33-51-12.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 98,879 hrs · 11,004 cycles

MAIN DECK L1 MED, UPPER SILL WEB STATION 460, FOUND CRACK, AD 2012-22 -03. REPAIRED IAW ECRA 5310-06747.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 98,879 hrs · 11,004 cycles

MAIN DECK RT NR 1 MED, UPPER SILL WEB STATION 460, FOUND CRACK, AD 201 2-22-03. REPAIRED AC IAW ECRA 5310-06747.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 98,412 hrs · 10,962 cycles

SEAT 19H, EMER EXIT LIGHT INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED. CONNECTED & SECURED. OPERATIONS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 98,412 hrs · 10,962 cycles

SEAT 50C EMER EXIT LIGHT INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED. CONNECTED & SECURED. OPERATIONS CHECKED OK.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 97,541 hrs · 10,874 cycles

SEAT 40H EMERGENCY EXIT LIGHT INOPERATIVE. SECURED LIGHT ASSEMBLY CONNECTOR. OPERATIONS CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 96,079 hrs · 10,736 cycles

EMERGENCY PATH LIGHT AT SEAT ROW 25H INOPERATIVE. SECURED LOOSE CONNECTOR AT ROW 25H. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 95,708 hrs · 10,703 cycles

UPPER DECK AFT OVERHEAD EXIT LIGHT INOPERATIVE. REPLACED THE BATTERY & POWER SUPPLY. PERFORMED INSTALLATION TEST IAW AMM 33-51-04 REV 172.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,235 hrs · 10,573 cycles

CABIN DR 5 CREW REST AISLE EMER LIGHT NEAR ENTRY LIGHT FOUND INOPERATIVE. REPLACED & ASSEMBLY TEST CARRIED OUT NORMAL IAW AMM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,235 hrs · 10,573 cycles

UPPER DECK CEILING MOUNTED EMER LIGHTS INOPERATIVE AT TOP OF STAIRWAY & FLIGHT ATTENDANT SEAT. REPLACED LIGHT ASSEMBLIES PN S1356B37 CHANGE IAW AMM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,235 hrs · 10,573 cycles

CABIN MAIN DECK TO UPPER DECK STAIRWAY OVERHEAD EMER LIGHTS INOPERATIVE. REPLACED TWO EACH LIGHT ASSEMBLIES PN S1356B37.

Part: WIRE — BROKEN (CABIN) · airframe 93,958 hrs · 10,544 cycles

EMERGENCY ESC LIGHTING INOPERATIVE AT SEAT ROWS 23, 24, 25 & 33 ABC. FOUND BROKEN WIRE AT SEAT 24ABC CONNECTOR. REPAIRED IAW SWPM 20-64-17. OPERATIONS TESTED OK IAW AMM 33-51-00-715-004 PG 503 PARAGRAPH D.

Part: LIGHT — UNSECURE (CABIN) · airframe 91,554 hrs · 10,284 cycles

EMERGENCY STRIP LIGHTING AT 1R HANGING OFF THE WALL. SECURED EMERGENCY LIGHT ASSEMBLY AT 1R ALL, OPERATIONS NOW NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,185 hrs · 10,249 cycles

AISLE EMERGENCY EXIT SIGN ATTACHED TO MONITOR INOPERATIVE AT DOOR 3 RT. ORDERED CHARGER 563-1046 & BATTERY PACK 563-1188. OVERHEAD PANEL BY 3 RT IS OPENED UP FOR ACCESS. REPLACED BATTERY PACK M7920 LOCATED AT DOOR 3RT OVER DOOR FAIRING IAW SSM33-51-02 PG 102 SHEET 1. OPERATIONS CHECKED EMERGENCY LIGHT EXIT SIGNS AT DOOR 3 RT OK.

Part: LIGHT — LOOSE (CABIN) · airframe 91,151 hrs · 10,245 cycles

EXIT LIGHT STRIP AT SEAT 58B TORN & LOOSE. SECURED TO SEAT, OPERATIONS CHECKED GOOD.

Part: RELAY — FAILED (CABIN) · airframe 90,953 hrs · 10,225 cycles

LAVATORY GALLEY FANS EICAS STATUS MESSAGE DISPLAYED. BOTH LAVATORY GALLEY VENT FANS FAILED OR INTERFACE FAIL, AFTER TOP OF CLIMB F340. REPLACED RELAY R8671 IAW SSM 21-26-01 PAGE 103.1. OPERATIONS CHECKED SYSTEM IAW AMM 21-26-00-501, ALL OPERATIONS NORMAL, NO CMC OR STATUS MESSAGES.

Part: SATCOM — MALFUNCTIONED (COCKPIT) · airframe 90,943 hrs · 10,224 cycles

'SATCOM HIGH GAIN' EICAS STATUS MESSAGE DISPLAYED. SATCOM HIGH GAIN ANTENNAE SUBSYSTEM FAILURE. DEFERRED IAW SAMC. SATCOM SYSTEM EICAS MESSAGE DISPLAYED, SATCOM SYSTEM IS INOPERATIVE. HF & IRIDIUM OK.

Part: BALLAST — FAULTY (CABIN) · airframe 90,913 hrs · 10,221 cycles

ON CM CHECK FOUND SEAT 6K FWD SIDEWALL LIGHT NOT ILLUMINATED. REPLACED BALLAST AT SEAT 6K, OPERATIONS CHECKED OKAY.

Part: STRUCTURE — TORN (FUSELAGE) · airframe 90,901 hrs · 10,220 cycles

CM CHECKED GALLEY 420 FLOOR EXTRUSION LT TORN. REPLACED EXTRUSION OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,829 hrs · 10,213 cycles

MID GALLEY, RT SMALL INCANDESCENT LAMP INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 90,507 hrs · 10,180 cycles

24H SEAT MOUNTED EMERGENCY EXIT LIGHT MISSING. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT AT 24H IAW MM, OPERATIONS CHECKED OKAY.

Part: ISOLATION VALVE — FAULTY (APU) · airframe 90,135 hrs · 10,142 cycles

APU BLEED VALVE WILL NOT OPEN. REPLACED APU BLEED ISOLATION VALVE PER MM. CHECKED OKAY.

Part: ROLLER — CRACKED (CARGO TRAY) · airframe 89,217 hrs · 10,049 cycles

RAMP REPORTED THAT A CRACK AROUND ROLLER SHAFT ON VERTICAL SECTION OF ROLLER TRAY. LOCATION ZONE V IN AFT CARGO PIT, STA 1800, RBL 5.5. THE CRACK IS 1 SIDE ONLY AND DOES NOT REACH TO BASE. CRACK LENGTH IS .5", POSITION 27 AND 28 IN THE AFT PIT, SHOULD NOT BE LOADED.

Part: AMPLIFIER — FAILED (SATCOM) · airframe 88,695 hrs · 9,999 cycles

CREW REPORTED SATCOM HIGH AND LOW GAIN ARE BOTH INOPERATIVE. NO DATALINK AND NO VOICE AVAILABLE. REPLACED THE HIGH POWER AMPLIFIER PER AMM. ACCOMPLISHED SATCOM SYSTEM GROUND TEST PER AMM. TESTED GOOD.

Part: LINE — LEAKING (NR 1 ENGINE FUEL) · airframe 88,683 hrs · 9,998 cycles

SUSPECT FUEL LEAKING FROM ENG 1. REPLACED FUEL LINE, LEAK CHECKED GOOD.

Part: CONDUIT — DAMAGED (RT BLG) · airframe 88,567 hrs · 9,983 cycles

RT BODY GEAR HAS DAMAGED METAL FLEX CONDUIT. COMES FROM JUNCTION BOX J5,CENTER INBOARD CONDUIT, 2ND FLEX CONDUIT. REPLACED DAMAGED SECTION OF CONDUIT.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 88,343 hrs · 9,959 cycles

EMERGENCY EXIT LIGHTS ON SEATS 15AB AND 16AB WILL NOT TURN OFF, WHEN SWITCH IN FLIGHT DECK IS IN THE OFF POSITION, WILL TURN OFF WITH SWITCH IN ARMED POSITION. REPLACED POWER SUPPLY UNIT. SYSTEM CHECKS NORMAL.

Part: GAUGE — DAMAGED (R3 DOOR BOTTLE) · airframe 88,096 hrs · 9,934 cycles

R3 DOOR ASSIST RESERVOIR BOTTLE PRESSURE GAUGE DAMAGED. PRESSURE INDICATOR NEEDLE COATING ADRIFT. EMERGENCY POWER ASSIST BOTTLE REPLACED IAW AMM.

Part: STRUCTURE — LEAKING (RT WING) · airframe 87,427 hrs · 9,864 cycles

RIGHT WING LOWER SIDE NR 15 BOTTOM SPLICE STRINGER, 30 INCHES OUTBOARD OF NR 3 PYLON HAS FUEL SEEP. REF AMM 28-11-00 IS A FUEL SEEP. RECHECK AT EVERY 3SV. -INF- :MF1554 CREATED TO MONITOR.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 87,427 hrs · 9,864 cycles

EMERGENCY LIGHT INOPERATIVE SEAT ROW 19 LEFT. SECURED CONNECTOR, OPS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 87,427 hrs · 9,864 cycles

EMERGENCY LIGHT INOPERATIVE SEAT ROW 45 LEFT. SECURED CONNECTOR, OPS CHECKED NORMAL.

Part: SEALANT — MISSING (THRESHOLD) · airframe 87,230 hrs · 9,846 cycles

MED 4 RIGHT SQUEAL. FOUND SEALANT MISSING BETWEEN BOTH SIDES OF THRESHOLD, FOR AND AFT. REPLACED SEALANT AND ARE WAITING FOR IT TO DRY AND THEN PRESSURIZE AGAIN. COULD MOVE THRESHOLD EDGES WITH THUMB PRESSURE AND SOUND WOULD CHANGE AS A RESULT. SEALANT NOT DRYING- REMOVING THRESHOLD PLATE IN ORDER TO RESEAL WITH SEALING HAVING BETTER SET-UP TIME. RMV'D THRESHOLD PLATE AND STARTED CLEAN (PARTIAL) CONT OF AMIS ITEM 2302010. CLEANED, RESEALED AND REINSTALLED THRESHOLD PLATE.

Part: LIGHT — FAULTY (CABIN) · airframe 87,219 hrs · 9,845 cycles

SMOKE SMELL AROUND SEATS 23-24 ABC. OVERHEAD LIGHTS TURNED OFF AND SMELL DISSIPATED. SAMC TEXT: NEED TO ACP CHECK PER MM. CONSULTED WITH CREW VERBAL INFORM SMELL DISSIPATED WHEN READING LIGHT TURNED OFF. SURROUND AREA CEILING PANEL DROP DOWN AND INSPECTION PER MM. FOUND NORMAL. OEU AT 24ABC AND READING LIGHT LAMPS ALL REPLACED FOR PRECAUTION. TURN ON ALL LIGHTS FOR 4 HOURS, NO SMELL IN AREA.

Part: ACTUATOR — FAULTY (APU) · airframe 87,203 hrs · 9,843 cycles

CREW REPORT APU WON'T START. APU INOPERATIVE. REPLACED APU DOOR ACTUATOR PER MM.

Part: FUEL TANK — LEAKING (HORIZONTAL STAB) · airframe 87,203 hrs · 9,843 cycles

FUEL LEAKING FROM LEFT HORIZONTAL STAB TANK. SOURCE OF LEAK IS LOCATED APPROX 7 FT OTBD FROM INBD LEFT SIDE OF STAB COMING FROM A WEEP HOLE. SEALED AREA. REPAIR GOOD AFTER SECOND ATTEMPT, LEAK CHECKED GOOD.

Part: COVER — LOOSE (CABIN) · airframe 86,856 hrs · 9,810 cycles

STAIR TO UPPER DECK EEL LIGHT STRIP LOOSE. SECURED PLASTIC EEL COVER ON STAIRWAY. DID NOT AFFECT EEL OPERATION. EEL LIGHT CHECKS GOOD PER MM.

Part: STRUCTURE — CRACKED (BS 2521) · airframe 86,751 hrs · 9,800 cycles

BS 2521 RT UPPER LOBE DOUBLER CRACKED. INSTALLED REPAIR DOUBLER IAW ECRA 5313-01047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,751 hrs · 9,800 cycles

FUSELAGE SKIN ABOVE L1 DOOR CRACKED. INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-10-01 RPR 3.

Part: SKIN — WORN (BS 2552-2628) · airframe 86,751 hrs · 9,800 cycles

FOUND RT FUSELAGE SKIN WORN AT INTERFACE WITH VERTICAL STABILIZER SEAL BETWEEN BS 2552 & 2628. INSTALLED EXTERNAL REPAIR DOUBLER IAW ECRA 5331-01619.

Part: SHEAR TIE — CRACKED (BS 1120 FRAME) · airframe 86,751 hrs · 9,800 cycles

BS 1120 FRAME RT SIDE AT SHEAR TIE CRACKED. REPLACED FRAME.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,751 hrs · 9,800 cycles

FUSELAGE SKIN ABOVE R1 DOOR IS CRACKED. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-10-01 RPR 3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,751 hrs · 9,800 cycles

EMERGENCY LIGHT IS NOT ILLUMINATED IN THE FLIGHT DECK. BATTERY PACK REPLACED.

Part: STRUCTURE — CRACKED (BS 2521) · airframe 86,751 hrs · 9,800 cycles

BS 2521 LT UPPER LOBE DOUBLER CRACKED. INSTALLED REPAIR DOUBLER IAW ECRA 5313-01046.

Part: STRUCTURE — CRACKED (BS 2120) · airframe 86,751 hrs · 9,800 cycles

BS 2120 LOWER LOBE UPPER CAP CRACKED. REPLACED UPPER CAP PER ECRA 5320-02093.

Part: FLOOR SUPPORT — CORRODED (BS 940-980) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

BS 940-980 MAIN DECK FLOOR SUPPORT CORRODED. MANUFACTURED AND INSTALLED NEW FLOOR SUPPORT IAW ECRA 5320-02092.

Part: GATE — CORRODED (R3 DOOR) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

R3 DOOR LOWER GATE CORRODED. REPLACED LWR GATE IAW CMM 52-11-41.

Part: TENSION TIE — DAMAGED (BS 1220) · airframe 86,751 hrs · 9,800 cycles

BS 1220 TENSION TIE CHANNEL TWO 0.375 INCH OVERSIZED HOLES. SUPPLEMENTAL DATA UPDATE, VERIFIED HOLES ARE CRACK FREE BY HFEC. INSTALLED OVER-SIZE FASTENERS PER ECRA 5310-05551.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 86,751 hrs · 9,800 cycles

STA 1140 RT AFT TENSION TIE 1 EACH HOLE CRACKED. REMOVED DAMAGE, INSTALLED REPAIR PARTS PER SRM 53-40-30 RPR 1.

Part: FLOORBEAM — CORRODED (BS 1100) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

BS 1100 UPPER DECK FLOORBEAM UPPER TEE CORRODED. REMOVED CORRODED TEE ANGLE. MANUFACTURED AND INSTALLED NEW TEE ANGLE AND SPLICES PER ECRA 5320-02090.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 86,751 hrs · 9,800 cycles

BS 1140 RT AFT TENSION TIE HOLE CRACKED. REMOVED DAMAGE, INSTALLED REPAIR PARTS PER SRM 53-40-30 RPR 1. CATEGORY 'B' REPAIR.

Part: FLOORBEAM — CORRODED (BS 1100) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

BS 1100 UPPER DECK FLOORBEAM UPPER TEE CORRODED. REMOVED CORRODED TEE ANGLE. MANUFACTURED AND INSTALLED NEW TEE ANGLE AND SPLICES PER ECRA 5320-02090. CHORD TEE REPLACED FROM RBL 6 TO RT END.

Part: FLOORBEAM — CORRODED (BS 1060 RBL 32) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

STA 1060 RBL 32 UPPER DECK FLOORBEAM UPPER SURFACE CORROSION. REMOVED CORRODED SECTION. MANUFACTURED AND INSTALLED TEE SECTION AND SPLICES PER ECRA 5320-0 2088.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 86,751 hrs · 9,800 cycles

BS 1120 RT FWD TENSION TIE HAD TWO HOLES CRACKED. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 53-40-30 RPR 1.

Part: TENSION TIE — DAMAGED (BS 1220) · airframe 86,751 hrs · 9,800 cycles

BS 1220 TENSION TIE CHANNEL HAS TWO 0.375 INCH OVERSIZED HOLES. VERIFIED HOLES ARE CRACK FREE BY HFEC. INSTALLED OVER-SIZE FASTENERS PER ECRA 5310-05551.

Part: FLOORBEAM — CORRODED (BS 1060 RBL 7) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

UPPER DECK FLOORBEAM CORRODED AT BS 1060 RBL 7. REMOVED CORRODED SECTION. MANUFACTURED AND INSTALLED NEW TEE AND SPLICES PER ECRA 5320-02088.

Part: FLOORBEAM — CORRODED (BS 1660 RBL 30) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

BS 1660 RBL 30, MAIN DECK FLOORBEAM UPPER TEE LOWER SURFACE CORRODED AT SCREW HOLE. REMOVED DAMAGE, INSTALLED FILLERS AND 2 REINFORCING ANGLES PER ECRA 5320-02087. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1660 LBL 25) · corrosion level 2 · airframe 86,751 hrs · 9,800 cycles

BS 1660 LBL 25 MAIN DECK FLOORBEAM UPPER TEE LOWER SURFACE CORRODED AT SCREW HOLE. REMOVED DAMAGE, INSTALLED FILLERS AND 2 REINFORCING ANGLES REF ECRA 5320-02087. MAJOR REPAIR.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 86,751 hrs · 9,800 cycles

BS 1180 RT FWD TENSION TIE 1 HOLE CRACKED. SUPPLEMENTAL DATA, REMOVED DAMAGE, INSTALLED SPLICE AND REINFORCING CHANNEL REF SRM 53-40-30 RPR 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 86,751 hrs · 9,800 cycles

BS 1200 RT FWD TENSION TIE TWO HOLES CRACKED. REMOVED DAMAGE, INSTALLED SPLICE AND REINFORCING CHANNEL REF SRM 53-40-30 RPR 1. THIS A CATEGORY "B" MAJOR REPAIR.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 86,751 hrs · 9,800 cycles

BS 1220 LT FRAME DOUBLER AT TENSION TIE-1 HOLE CRACKED. REMOVED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 51-40-02. MAJOR REPAIR.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 86,751 hrs · 9,800 cycles

BS 1160 RT FWD TENSION TIE TWO HOLES CRACKED. REMOVED DAMAGE, INSTALLED SPLICE AND REINFORCING CHANNEL REF SRM 53-40-30 RPR 1. CATEGORY 'B' MAJOR REPAIR.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 86,751 hrs · 9,800 cycles

BS 1140 RT TENSION TIE FAILSAFE 1 HOLE CRACKED. REMOVED DAMAGE, INSTALLED REPAIR ANGLES REF AMM 53-10-99 AND ECRA 5310-05552. MAJOR REPAIR.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 86,751 hrs · 9,800 cycles

BS 1140 LT TENSION TIE FAILSAFE CHORD 1 HOLE CRACKED. REMOVED DAMAGE, INSTALLED REPAIR ANGLES REF AMM 53-10-99 AND ECRA 5310-05552. MAJOR REPAIR.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 86,751 hrs · 9,800 cycles

STA 1180 RT FWD TENSION TIE 1 HOLE CRACKED. REMOVED DAMAGE, INSTALLED SPLICE AND REINFORCING CHANNEL REF SRM 53-40-30 REPAIR 1. CATEGORY "B' MAJOR REPAIR.

Part: TIRE — FAILED (LT NOSE) · airframe 86,751 hrs · 9,800 cycles

DURING TAKEOFF LT NOSE TIRE FAILED RESULTING IN LWR FUSELAGE DAMAGE.

Part: SKIN — CRACKED (BS 2280) · airframe 86,751 hrs · 9,800 cycles

LT NR 5 MAIN ENTRY DOOR AFT UPPER CUTOUT SKIN CRACK BS 2280, 3 INCHES DOWN FROM S16L, L=1.5 INCH BY- 057806: SKIN AND BEAR STRAP REPAIRED IAW 747EN-53-0329.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,515 hrs · 9,777 cycles

EMERGENCY EEL AT DOOR 2 GALLEY LOWER RIGHT WALL INOP. RELAMPED, OPS NORMAL.

Part: WIRE — SATURATED (CABIN) · airframe 86,515 hrs · 9,777 cycles

EMERGENCY LIGHTS AT AFT GALLEY LEFT SIDE ENTRANCE INOP. FOUND AREA WET ALL AROUND GALLEY 4 WET. DRIED AREA AND DRIED EEL WIRING. NOW OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,515 hrs · 9,777 cycles

EMERGENCY CEILING LIGHT INOP AT SEATS 25 RIGHT, 32 LEFT AND 16 INOP. REPLACED LAMPS AT LOCATIONS.

Part: BOTTLE — DISCHARGED (L2 DOOR) · airframe 86,515 hrs · 9,777 cycles

MED 2L - DURING MAINTENANCE ASSIST BOTTLE DISCHARGED, DOOR DID NOT FULLY OPEN AND SLIDE DID NOT DEPLOY. REMOVED 2L DOOR EMERGENCY POWER RESERVOIR. NEW RESERVOIR ON HAND AT DOOR. CONT OF AMIS ITEM 5152009. SUSPECT LOOSE OR BROKEN CONNECTION AT PWR ACTUATOR. NO ACCESS. FOUND PRESSURE LINE DISCONNECTED AT PWR ACTUATOR. REPLACED BOTTLE ASSY.

Part: LIGHT — SATURATED (CABIN) · airframe 86,515 hrs · 9,777 cycles

EMERGENCY AT LEFT SEAT ROWS 45-53 INOP. FOUND WHOLE AREA AT GALLE Y 4 WET. DRIED AREA. DRIED EEL STRIPS. NOW OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,515 hrs · 9,777 cycles

EEL K SEAT LIGHT ROW 25 RIGHT INOP. REPLACED LIGHT ASSY.

Part: RECEPTACLE — LOOSE (EMERGENCY LIGHT) · airframe 86,263 hrs · 9,753 cycles

A-CHECK JOB, SEAT 38H EMERGENCY LIGHT INOPERATIVE. FOUND RECEPTACLE LOOSE. RECONNECTED AND OP CHECKED NORMAL.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHTS) · airframe 86,263 hrs · 9,753 cycles

DURING A-CHECK, SEAT 45C-53C EMERGENCY LIGHTS INOPERATIVE. AFT GALLEY FLOOR WET SHORTING OUT SEAT EMERGENCY LIGHTS 45C-53C. PULLED CARPET UP TO LET FEEDER CABLE DRY. RECONNECTED. EMERGENCY LIGHTS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,263 hrs · 9,753 cycles

DURING A-CHECK, L2 DOOR LOWER MID CLOSET EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 86,263 hrs · 9,753 cycles

DURING AN A-CHECK, SEAT 25H EMERGENCY LIGHT INOPERATIVE. FOUND DISCONNECTED AND OP RECONNECTED AND OP CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,796 hrs · 9,711 cycles

EMERGENCY LIGHT LOWER WALL FWD GALLEY NEAR DOOR 2 RT AND DOOR 2 LEFT, INOP. RELAMPED, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 85,796 hrs · 9,711 cycles

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

Part: CONNECTOR — UNSECURE (CABIN) · airframe 85,796 hrs · 9,711 cycles

EMERGENCY LIGHT AT SEAT 20A INOP. SECURED CONNECTION AT LIGHT. SECURED OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,796 hrs · 9,711 cycles

EMERGENCY LIGHT LOWER WALL FWD GALLEY NEAR DOOR 2 RT AND DOOR 2 LEFT INOP. RELAMPED, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 85,796 hrs · 9,711 cycles

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

Part: CONNECTOR — UNSECURE (CABIN) · airframe 85,796 hrs · 9,711 cycles

EMERGENCY LIGHT AT SEAT 38A INOPERATIVE. SECURED CONNECTION UNDER SEAT, OPS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 85,796 hrs · 9,711 cycles

EMERGENCY LIGHT AT SEAT 20A INOP. SECURED CONNECTION AT LIGHT. SECURED OPS NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 85,109 hrs · 9,638 cycles

THE 41H SEAT MOUNTED EMERGENCY LIGHT IS MISSING. REPLACED SEAT MOUNTED EMERGENCY LIGHT PER MM, OPS CHECKED OKAY.

Part: WIRE — CORRODED (CABIN) · airframe 84,832 hrs · 9,612 cycles

MAIN GALLEY DOOR 4 LT FWD AND SIDE EMERGENCY LIGHT INOP. REPAIRED WET AND CORRODED WIRING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,832 hrs · 9,612 cycles

EMERGENCY LIGHT ROW 52 RT INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 84,832 hrs · 9,612 cycles

EMERGENCY LIGHT ROW 45 THROUGH 52 INOP. REPAIRED WET AND CORRODED EEL POWER STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,832 hrs · 9,612 cycles

EMERGENCY LIGHT ROW 41 RT INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,832 hrs · 9,612 cycles

EMERGENCY LIGHT ALONG AISLE DOOR 2R INOP. RELAMPED, OP CK NORMAL.

Part: ACTUATOR — MALFUNCTIONED (CARGO DOOR) · airframe 84,312 hrs · 9,562 cycles

AFT CARGO DOOR INTERMITENTLY FAILS TO CLOSE LAST 2 INCHES. SUPPLEMENTAL DATA UPDATE LIFT ACTUATOR STOPS BUT HOOK SYTEM FAILS TO ACTIVATE AND PULL DOOR CLOSED. DOOR RIG IS GOOD REF JOB 8-830 OF A CHECK. PROBLEM APPEARS TO NOT BE RIG RELATED. REPLACED HOOK POSITION YABS05 IAW AMM, NO HELP. AFTER SWITCH RPL, HOOK ACTUATOR INTERMITTENTLY OPERATES BEFORE DOOR CLOSES. REF 52-53 FAULT TREE, HOOK POS (PARTIAL) CONT OF AMIS ITEM 3122102. REPLACED AFT CARGO PIT HOOK ACTUATOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,312 hrs · 9,562 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 22ABC. RELAMPED, OP CHECKED NORMAL.

Part: INDICATOR — DAMAGED (L1 DOOR SLIDE) · airframe 84,312 hrs · 9,562 cycles

L1 DOOR DISARM WINDOW CRACKED, BUT READABLE & SECURE. REPLACED COVER.

Part: KEYPAD — WORN (COCKPIT) · airframe 84,052 hrs · 9,538 cycles

COCKPIT ENTRY PAD BUTTON 1 NUMBER WORN OFF. :BUTTON WORKS NORMAL. JUST NUMBER ON THE SW WAS WORN OUT. NEXT STA PLZ CHECK KEYPAD, USE PERMANENT MARKER TO ID KEY AS NR 1. REPLACED KEYPAD PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 83,654 hrs · 9,493 cycles

THERE ARE SOME LOOSE WIRES ON FLOOR BY JUMPSEAT AT DOOR 3L. SEAT ESCAPE PATH LT LOOSE, SECURED SAME. OPS CHECKED OKAY.

Part: SKIN — DELAMINATED (LT WING) · airframe 83,565 hrs · 9,484 cycles

NOTICED A BLISTER ON TOP OF LEFT WING BETWEEN AILERON AND WINGLET. REPAIRED AREA.

Part: UNKNOWN — LEAKING (NR 3 ENGINE) · airframe 83,209 hrs · 9,441 cycles

LEAK CHECK NR 3 ENGINE FUEL & OIL COOLER DUE TO OIL LEAK. ACP LEAK CHECK NO LEAKS. CLOSED REVERSER AND COWLS PER AMM. FOUND FUEL LEAKING FROM WHERE COMBUSTION & EXHAUST CASE JOIN TOGETHER. APPEARS TO BE INTERNAL. NR 4 ENGINE REMOVED AND STARTED INSTALLATION. FINISH BY STARTING AT PARG H STEP 4 (PG 409) TO END. NEEDED TO REMOVE AND THEN REINSTALLED FUEL DISTRIBUTION VLV UP TO ITEM 3 PARA I STEP 7 PER AMM. ENGINE RUN AND LEAK CHECK NEEDED. MRDATA INPUT NEEDED. MR73139 -39O (PARTIAL). ACP ENG RUN AND LEAK CHECK. NO LEAKS NOTED. CLOSED REVERSERS & COWLS PER AMM.

Part: PANEL — CRACKED (RT WING) · airframe 83,209 hrs · 9,441 cycles

RT WING UPPER SURFACE L/E PNL IS CRACKED ON UPPER SURFACE, LOCATED BETWEEN L/E FLAPS 16 & 17. REF (A) CHECK JOB 8-8031. ACCOMPLISHED OVERLAY REPAIR PER SRM, NEEDS PRIMED & PAINTED. APPLIED CONDUCTIVE PAINT AND FR PRIMER. STILL NEEDS GRAY TOP COAT PAINT.

Part: PANEL — CRACKED (RT WING) · airframe 83,209 hrs · 9,441 cycles

RT WING UPPER SURFACE L/E PNL IS CRACKED ON UPPER SURFACE, LOCATED BETWEEN L/E FLAPS 21 & 22. REF [A] CHECK JOB 8-8031. ACCOMPLISHED OVERLAY REPAIR PER SRM, NEEDS PRIMED & PAINTED. APPLIED CONDUCTIVE PAINT & PRIME, STILL REQUIRES GRAY TOPCOAT.

Part: UNKNOWN — LEAKING (NR 4 ENGINE) · airframe 83,209 hrs · 9,441 cycles

FOUND FUEL LEAKING FROM WHERE COMBUSTION & EXHAUST CASE JOIN TOGETHER. APPEARS TO BE INTERNAL. NR 4 ENGINE REMOVED & STARTED INSTALLATION. FINISH BY STARTING AT PARAGRAPH STEP 4 (PG 409) TO END. NEEDED TO REMOVE & THEN RE-INSTALLED FUEL DISTRIBUTION VALVE UP TO ITEM 3 PARAG I STEP 7 PER AMM. ENGINE RUN AND LEAK CHECK NEEDED. MRDATA INPUT NEEDED. MR73139 -39 (PARTIAL) CONT OF AMIS ITEM 2092070 ACP ENG RUN AND LEAK CHECK. NO LEAKS NOTED. CLOSED REVERSERS AND COWLS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,209 hrs · 9,441 cycles

UPPER DECK LT DOOR FWD EMERGENCY LIGHT INOPERATIVE. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 83,209 hrs · 9,441 cycles

DOOR 4 LT GALLEY SIDEWALL EMERGENCY LIGHT INOP. RE-SECURED LIGHT, OP CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 83,209 hrs · 9,441 cycles

EMERGENCY LIGHT ROW 25 RT INOP. RE-SECURED EMERGENCY LIGHT CONNECTOR, OP CHECK NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 83,209 hrs · 9,441 cycles

EMERGENCY EXIT SIGN DOOR 4 RT AFT INOP. SECURED LAMP, OP CHECK NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 83,209 hrs · 9,441 cycles

DOOR 4 GALLEY WALL FWD LT EMERGENCY LIGHT INOPERATIVE. RE-SECURED LIGHT, OP CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 83,209 hrs · 9,441 cycles

EMERGENCY LIGHT ROW 45 THROUGH 53 LT INOP. RE-SECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,209 hrs · 9,441 cycles

EMERGENCY CEILING LIGHT ROW 60 RT INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,209 hrs · 9,441 cycles

DOOR 1 RT EMERGENCY SLIDE LIGHT INOP. RELAMPED, OP CHECK NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 83,209 hrs · 9,441 cycles

EMERGENCY EXIT SIGN DOOR 4LT FWD INOP. RE-SECURED LIGHT. OP CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 82,731 hrs · 9,387 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. FWD STAIRS LOWER STAIRWELL LIGHT. SECURED CONNECTOR, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,731 hrs · 9,387 cycles

EMERGENCY EXIT LIGHT INOP. DOOR 2 GALLEY AREA LOWER RIGHT WALL LIGHT. RELAMPED, OP CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,731 hrs · 9,387 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. SEAT ROW 25 RIGHT. REPLACED LIGHT, OPS CHECKED OK.

Part: CHARGER — FAULTY (CABIN) · airframe 82,731 hrs · 9,387 cycles

UPPER DECK EXIT EMERGENCY LIGHTS 2 EACH NEAR WING DOORS STAYS ON WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. REPLACED BATTERY CHARGER ABOVE AT WING DOORS. OP CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,731 hrs · 9,387 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 22 LEFT. REPLACED EEL LIGHT, OP CHECK OK.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 82,731 hrs · 9,387 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. SEAT ROWS 45 THRU 54 LEFT, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL LIGHT ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL LIGHT. REMOVE WATER UNDER CARPET.

Part: LIGHT — UNSECURE (CABIN) · airframe 82,731 hrs · 9,387 cycles

EMERGENCY LIGHT ON STAIRWELL FALLING OFF. REMOVED OLD TAPE AND RETAPED LIGHT AND CARPET AROUND LIGHT STRIP. OPS NORMAL.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 82,365 hrs · 9,347 cycles

WHITE WIRE HANGING BELOW SEAT. REPLACED SEAT MOUNTED EMERGENCY LIGHT STRIP.

Part: TRANSMITTER — FAULTY (AILERON) · airframe 82,188 hrs · 9,328 cycles

LEFT INBD AILERON NOT RESPONDING NORMALLY DURING PRE TAKEOFF CHECK. AILERON POSITION INDICATING SYS INOP. VISUAL CONFIRMATION REQUIRED BEFORE EACH FLIGHT. REPLACED LEFT INBD AILERON POSITION TRANSMITTER PER MM.

Part: CONNECTOR — SHORTED (NR 1 ENGINE) · airframe 82,149 hrs · 9,323 cycles

NR 1 ENGINE CONNECTOR D8450P REQUIRES REPLACEMENT AS THERE IS A INTERNAL PIN SHORT. (CONFIRMED ORD ON SHORT) NEW CONNECTOR ON AOG Y0640, WD 26-11-13. REPLACED CONNECTOR D8450P NEEDS TO BE SECURED AND SAFTIED. T-FITTING ADJACENT TO FLEX CONDUIT ALSO REMOVED FOR ACCESS TO REPLACE CONNECTOR. SECURED CONNECTOR & INSTALLED T-FITTING. OP-CHECK ACP ON SMC 83.

Part: CONNECTOR — FAULTY (NR 1 ENGINE) · airframe 82,149 hrs · 9,323 cycles

ENG 1 FIRE LOOP A FAILS CMC TEST, ACTIVE EXISTING FAULT AND STATUS MSG PRESENT. MAINT MSG 26020. NR 1 ENGINE CONNECTOR D8450P REQUIRES REPLACEMENT AS THERE IS A INTERNAL PIN SHORT (CONFIRMED ORD ON SHORT) NEW CONNECTOR ON AOG Y0640, WD 26-11-13. REPLACED CONNECTOR D8450P NEEDS TO BE SECURED AND SAFTIED. T-FITTING ADJACENT TO FLEX CONDUIT ALSO REMOVED FOR ACCESS TO REPLACE CONNECTOR. SECURED CONNECTOR AND INSTALLED T-FITTING. FIRE TEST PASSED AFTER ACP OF SEQ 1492132. OP-CHECK ACP ON SMC 83.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,149 hrs · 9,323 cycles

EMERGENCY EXIT LIGHT INOP DOOR 2 GALLEY AREA LOWER RIGHT WALL. RELAMPED, OPS. CHECKED NORMAL

Part: CONNECTOR — CONTAMINATED (EMERGENCY LIGHT) · airframe 82,149 hrs · 9,323 cycles

EMERGENCY EXIT LIGHTS INOP SEAT ROWS 45 THRU 53 LEFT, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON 84XX AIRCRAFT.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 82,149 hrs · 9,323 cycles

EMERGENCY EXIT LIGHT INOP LOWER WALL BETWEEN LAVS 111 AND 112. REPLACED FEEDER CABLE. OPS CHECKED NORMAL.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 82,149 hrs · 9,323 cycles

EMERGENCY EXIT LIGHT INOP LOWER WALL ACROSS DOOR 3 RIGHT. REPLACED FEEDER CABLE. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,149 hrs · 9,323 cycles

EMERGENCY EXIT LIGHT INOPERATIVE SEAT ROW 37 RIGHT.

Part: CLOSEOUT PANEL — CRACKED (BS 1241 LBL 76) · airframe 81,144 hrs · 9,205 cycles

CANTED PRESSURE DECK CLOSE OUT PANEL CRACKED, STA 1241 LBL 76. SUPPLEMENTAL DATA UPDATE, PANEL REPAIRED IAW EN53-0330.

Part: HYDRAULIC LINE — LEAKING (HNYDRAULIC SYS) · airframe 81,993 hrs · 9,305 cycles

EVIDENCE OF HYD LEAK FROM NR 4 SYS FLUID DRIPPING FROM SAIL TAIL UPON ARRIVAL. LINE REMOVED AND ROUTED TO SHOP ON SMC16.

Part: COVER — LOOSE (CABIN) · airframe 81,913 hrs · 9,294 cycles

EEL LIGHT FLOOR LEVEL AT DOOR 1R LAV DAMAGED. FOUND ONLY EEL LIGHT COVER LOOSE, SECURED COVER AND EEL LIGHT. OPERATION CHECKED NORMAL.

Part: SMOKE GOGGLES — UNSERVICEABLE (COCKPIT) · airframe 81,701 hrs · 9,269 cycles

SMOKE GOGGLES STRAP TOO LOOSE FOR USE. CHECK FOUND SECOND OBSERVER SEAT SMOKE GOGGLE NEEDS TO BE REPLACED, NIL PARTS IN PEKJT. DF PER MEL. NOTIFIED SAMC. REPLACED 2ND OBSERVER'S SEAT SMOKE GOGGLE.

Part: ENGINE — VIBRATION (NR 3) · airframe 81,555 hrs · 9,254 cycles

F/A REPORTED BIG VIBRATION NEAR 2R ON TAKEOFF AND DURING CLIMB. ENG 3 VIB MSG IN CMC. SAMC TEXT: FOUND FOD DAMAGE TO NR 3 ENGINE FAN BLADES, INLET ACCOUSTIC PANELS, 10TH & 15TH HPC BLADES ALL BEYOND LIMITS. ENGINE TO BE REPLACED BEFORE ACFT RETURNS TO REVENUE SERVICE. REPLACED ENG, SEE HISTORY.

Part: SKIN — CRACKED (BS 2280 S16L) · airframe 81,144 hrs · 9,205 cycles

LT NR 5 MED AFT UPPER CUTOUT SKIN CRACK STA 2280, 3 INCHES DOWN FROM S16L. L=1.5 INCH. MAJOR REPAIR ACCOMPLISHED: SKIN AND BEARSTRAP REPAIRED IAW EN-53-0329.

Part: PANEL — CRACKED (FUSELAGE) · airframe 81,144 hrs · 9,205 cycles

CANTED PRESSURE DECK CLOSE OUT PANEL CRACKED. LENGTH = 1". STA 1241 LBL 76. PANEL REPAIRED IAW 747EN53-0330. REPAIR IS TIME LIMITED FOR 24 MONTHS FROM MAR, 2011 AND PANEL MUST BE REPLACED AT NEXT C-CK, NTE 24 MONTHS. REPAIR ALSO REQ REPETITIVE INSP AT 1000 FLIGHT HOUR INTERVAL. IF DAMAGE IS FOUND, PANEL MUST BE REPLACED PRIOR TO FURTHER FLIGHT. MF7305 CREATED TO MONITOR, PANEL TO BE RPL AT C-CK, TIME LIMITED FOR 24 MONTHS. REF EVA80680 REPETITIVE 1000HR INSPECTION REQUIREMENTS REF SB747-53-2329 PG 27 FOR ACCESS & INSPECTION.

Part: SLIDE — LOW PRESSURE (R5 DOOR) · airframe 81,144 hrs · 9,205 cycles

NR 5 RT MED SLIDE RESERVOIR BOTTLE PRESS LOW. REPLACED SLIDE IAW AMM.

Part: PACKING — LEAKING (WATER SYSTEM) · airframe 80,964 hrs · 9,182 cycles

RAN OUT OF WATER 9 HRS INTO FLIGHT. QTY WAS FULL BEFORE DEPARTURE. SERVICED WATER TO 95 PERCENT FULL THEN CHECK. NO LEAK FOUND ON GROUND. WATER SOV SWITCH OFF AND M41, 42 COFFEEMAKER DEACTIVATED. DEFER IAW MEL. REPLACED PACKING. OPS CHECKED OK. NO LEAK FOUND. REACTIVATED CMS AND WATER SHUTOFF VALVE OPENED.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 80,964 hrs · 9,182 cycles

UPPER DECK ROW 13 EMERGENCY LIGHT COVER FELL OFF. SECURED COVER OK.

Part: FEEDER CABLE — MISROUTED (EMERGENCY LIGHTS) · airframe 80,819 hrs · 9,167 cycles

EMERGENCY LIGHT FEEDER CABLE AFT GALLEY MISROUTED. REROUTED EMERGENCY CABLE, CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,606 hrs · 9,144 cycles

EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 55 RIGHT. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,606 hrs · 9,144 cycles

EMERGENCY EXIT LIGHT INOP DOOR 3 RIGHT BUSSLE. SUPPLEMENTAL DATA UPDATE RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,606 hrs · 9,144 cycles

EMERGENCY EXIT LIGHT INOP CEILING ROW 20 RIGHT. RELAMPED, CHECKS OKAY.

Part: FEEDER CABLE — OUT OF TOLERANCE (CABIN) · airframe 80,606 hrs · 9,144 cycles

EMERGENCY EXIT EEL LIGHTS INOP SEAT ROWS 45 THRU 54 LEFT, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL EEL ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL EEL. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON 84XX AIRCRAFT. SUPPLEMENTAL DATA UPDATE, REPLACED FEEDER, CKS OKAY.

Part: LIGHT — LOW (COCKPIT) · airframe 80,606 hrs · 9,144 cycles

EMERGENCY EXIT LIGHT VERY DIM IN FLIGHT DECK. RELAMPED WITH 1317 BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,606 hrs · 9,144 cycles

EMERGENCY EXIT LIGHT AT DOOR 2 GALLEY AREA FWD LOWER WALL AT RIGHT SIDE INOP AND CENTER LIGHT LENS MISSING. SUPPLEMENTAL DATA UPDATE, REPLACED LENS AND RELAMPED.

Part: LAVATORY — UNDERSERVICED · airframe 80,550 hrs · 9,137 cycles

LAVS INOP, FLIGHT DIVERTED. APPEARS FWD TANKS (LT AND RT) ARE SHUTDOWN. NO AHM DATA SHOWING ANY FAILURES. SENSOR "INOP" LIGHTS ARE ILLUMINATED ON ACCESS PANEL (R2 DOOR) FOR LAV BOTH FWD LAV TANKS. LAVATORY TANKS SERVICED PROPERLY AND ALL LIGHTS WENT OUT WITH ALL LAVS WORKING. WORK ACCOMPLISHED PER MM. OK FOR SERVICE.

Part: LIGHT — UNSECURE (SEAT 21HJK) · airframe 80,541 hrs · 9,136 cycles

21HJK SEAT MOUNTED EMERGENCY LIGHT STRIP ADRIFT. SECURED EMERGENCY LIGHT. OPS NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 80,241 hrs · 9,106 cycles

EMERGENCY LIGHT ON STAIRWAY TO UPPER DECK IS LOOSE. SECURED EMERGENCY LIGHT. OPS NORMAL.

Part: ESCAPE REEL — NONE (COCKPIT) · airframe 80,158 hrs · 9,099 cycles

FLIGHT CREW REPORTED EMERGENCY INERTIAL ESCAPE REELS ONE NO EXPIRE DATE. REPLACED EMERGENCY DESCENT REEL PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,035 hrs · 9,087 cycles

EMERGENCY EXIT LIGHTS INOP RT UPPER DECK DOOR PORT HOLES 2 EA LIGHTS INOP. REPLACED BATTERY PACK AT UPPER DECK DOOR. CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 80,035 hrs · 9,087 cycles

EMERGENCY EXIT LIGHTS INOP. LT AND RT CEILING BETWEEN DOORS 3 AND 4. EMERGENCY BATTERY REGAIN FULL CHARGE. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,035 hrs · 9,087 cycles

EMERGENCY EXIT LIGHTS INOP. SEAT ROWS 45 THRU 53 LT, DOOR 4 LT FWD EXIT SIGN, DOOR 4 RT AFT EXIT SIGN, LOWER WALL EMERGENCY ACROSS DOOR 4 LT, AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON 84XX ACFT. REPLACED AISLE LOWER SIDE WALL EMERGENCY LAMP. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,035 hrs · 9,087 cycles

EMERGENCY EXIT LIGHT INOP. LT UPPER DECK DOOR PORT HOLE. (1) EA LIGHT INOP. REPLACED LAMP. CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,035 hrs · 9,087 cycles

EMERGENCY EXIT LIGHT INOP, DOOR 2, GALLEY AREA LOWER RT WALL. REPLACED EMERGENCY LIGHT ASSY. CHECKS NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 80,014 hrs · 9,085 cycles

NOTICEABLE ODOR EMANATING FROM CARPETED AREA NEAR SEATS JUST IN FRONT OF DOOR 3R. ACFT JUST OUT OF MAJOR MAINT CHECK. MIGHT BE CAUSED BY SOLVENT SPILL. ODOR RESEMBLES AN AEROSOL INSECTICIDE. DOES NOT SMELL LIKE FUEL OR CLEANING SOLVENT. CLEANERS CLEANED AREA WHICH REDUCED THE ODOR SUBSTANTIALLY.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 80,004 hrs · 9,084 cycles

NR 3 RT MED CUTOUT CRACK LOWER FWD CORNER BEAR STRAP. REPAIR ACCOMPLISHED PER EVA 80355 IS TIME LIMITED UNTIL 15,000 PTC. FULL COMPLIANCE TO CFR HAS NOT BEEN EVALUATED. A NEW FAA APPROVAL MUST BE ISSUED PRIOR TO INSPECTION THRESHOLD OF 15,000 TOTAL AIRPLANE FLIGHT CYCLES.

Part: UNKNOWN — ODOR · airframe 79,478 hrs · 9,026 cycles

JACK SCREW COMPARTMENT HAS HEAVY FUEL SMELL. FUELED HORIZ STAB TANK REF MM12-11-03, NO ACTIVE LEAKS FOUND, ALSO RAN APU TO CHECK FUEL SUPPLY LINE IN AREA NO ACTIVE LEAKS FOUND.

Part: LIGHT — MISSING (CABIN) · airframe 79,478 hrs · 9,026 cycles

EMERGENCY LIGHT MISSING AT CORNER OF LAV NEAR DOOR 1 RIGHT AND PLASTIC CORNER IS BROKEN. ALL ADJACENT EMERGENCY LIGHTS ARE OPERABLE. REPLACED LIGHT ASSY.

Part: LIGHT — TORN (CABIN) · airframe 79,120 hrs · 8,986 cycles

EMERGENCY EXIT PATH LIGHTS STRIP IS TORN AT 1R. SECURED LIGHT ASSY. OPS ARE NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,927 hrs · 8,964 cycles

LT AND RT OTBD EMERGENCY LIGHT CROSS AISLE LIGHTS BETWEEN DOORS 2L AND 2R INOPERATIVE. RELAMPED, CHECKS OK.

Part: FEEDER CABLE — SHORTED (EMERGENCY LIGHTS) · airframe 78,927 hrs · 8,964 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 45L TO 53L, DOOR 4L FWD EXIT, DOOR 4R AFT EXIT, AFT GALLEY WALL LIGHTS LT FWD AND LT AISLE. COMMON PROBLEM WITH 84XX ACFT OUT OF O/H. REPAIRED WATER SOAKED EMERGENCY LIGHT STRIPS AND CORRODED CONTACTS.

Part: LIGHT — INOPERATIVE (SEAT 57L) · airframe 78,927 hrs · 8,964 cycles

SEAT 57L EMERGENCY LIGHT INOPERATIVE. SEAT 57L EMERGENCY LIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,927 hrs · 8,964 cycles

BETWEEN DOORS 3R AND 3L, LT AISLE WALL EMERGENCY LIGHT INOPERATIVE. RELAMPED, CHECKS OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 78,632 hrs · 8,929 cycles

LIGHT LOOSE AT CORNER WALL BY LAV 102. SECURED UPPER EMERGENCY LIGHT. LIGHT OPS CHECK OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 78,555 hrs · 8,920 cycles

STAIRWELL EMERGENCY LIGHT IS LOOSE. RE-SECURED LIGHT. OPS OKAY.

Part: FEEDER CABLE — INOPERATIVE (CABIN) · airframe 78,413 hrs · 8,905 cycles

EMERGENCY LIGHT INOP: DOOR 4L FWD EXIT SIGN. REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 78,413 hrs · 8,905 cycles

WALL EEL INOP: AFT GALLEY LT WALL. REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL.

Part: FEEDER CABLE — INOPERATIVE (CABIN) · airframe 78,413 hrs · 8,905 cycles

WALL EEL INOP: AFT GALLEY FWD WALL. REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,413 hrs · 8,905 cycles

LEFT SEAT 33ABC EEL STRIP INOP. REPLACED LAMP, CHECKS OKAY.

Part: FEEDER CABLE — INOPERATIVE (CABIN) · airframe 78,413 hrs · 8,905 cycles

EMERGENCY LIGHT INOP: DOOR 4R AFT EXIT SIGN. REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT ROW 45) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHT INOP. SEAT ROW 45 RIGHT. REPLACED LIGHT ASSY. OPS. CKS. NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHT INOP. DOOR 5 LEFT GALLEY LOWER AFT WALL. SECURED CONNECTOR. OPS. CKS. NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHT INOP. LOWER WALL ACROSS DOOR 3 LEFT. REPLACED LIGHT ASSY. OPS. CKS. NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHTS INOP. DOOR 2 GALLEY AREA CENTER AND RIGHT LOWER FWD WALL. RELAMPED. OPS. CKS. NORMAL

Part: LIGHT — INOPERATIVE (SEAT 37R) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHT INOP. SEAT ROW 37 RIGHT. REPLACED LIGHT ASSY. OPS. CKS. NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHT INOP. DOOR 4 RIGHT CEILING ENTRY. RELAMPED. OPS. CKS. NORMAL

Part: FEEDER CABLE — SATURATED (EMERGENCY LIGHTS) · airframe 77,835 hrs · 8,833 cycles

EMERGENCY EXIT LIGHTS INOP. SEAT ROWS 45 THRU 54 LEFT, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL EMERGENCY LIGHTS ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON AIRCRAFT. FOUND WATER PUDDLING IN GALLEY AREA UNDER GALLEY MAT AT EMERGENCY LIGHT CONNECTOR SHORTING THE LIGHTS. DRIED AREA OF WATER REPLACED POWER CABLE AND REPLACED LIGHT ASSY. EMERGENCY LIGHTS OPS. CK. NORMAL AT THIS TIME.

Part: WIRE — SHORTED (WINDSHIELD) · airframe 77,730 hrs · 8,822 cycles

CAPT ADJUSTING SUNSHADE INADVERTANTLY HIT WIRE ON TERMINAL BLOCK OF WINDOW 1L CAUSING SPARKS. CB FOR WINDOW HEAT POPPED AT THE SAME TIME, POSSIBLE LOOSE WIRE ON TERMINAL BLOCK. FOUND SHORT JUMPER WIRES ON TRIPLEX WINDSHIELDS NOT CONNECTED TERMINAL FOR BOTH LT AND RT WINDSHIELD. LT WINDOW HEAT CONTROLLER MADE STATUS MSG CAUSING SPARK JUMPER WIRE. SECURED WIRE IAW MM. ALSO, REPLACED L-WINDOW HEAT CONTROLLER IAW MM. TEST PASSED. INSTALLED JAL NON-POOL.

Part: GIRT BAR — BINDING (5R DOOR) · airframe 77,493 hrs · 8,798 cycles

DOOR 5R WILL NOT ARM. FREED FWD SLIDER ON GIRT BAR AT 5R. SLIDE ARMS NORMALLY NOW.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,277 hrs · 8,771 cycles

CEILING LIGHTS INOP LT AFT CABIN. RELAMPED, CHECKS OKAY.

Part: SKIN PANEL — DELAMINATED (SPOILER) · airframe 77,277 hrs · 8,771 cycles

NR 1 FLIGHT SPOILER UPPER AFT RIGHT SKIN PANEL CORNER APPEARS DELAMINATED. SPOILER PANEL DELAMINATED. REMOVED NR 1 FLIGHT SPOILER. NEED TO INSTALL NEW SPOILER PANEL. NEW PANEL ONSITE. WORKING PANEL INSTALLATION THEN RIGS.

Part: BULKHEAD — BLOWN (SLIDE)

UPON FUNCTION TEST, FOUND THE SLIDE RT SIDE BULKHEAD BLOWN. THIS CAUSED THE RAMP WALKWAY TO BULGE ON THE RT SIDE AND UN-EVEN TO WALK.

Part: LIGHT — INOPERATIVE (SEAT 19B) · airframe 76,621 hrs · 8,686 cycles

19B EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT. OPS CHECKED OK.

Part: FAN — FAILED (CABIN) · airframe 76,511 hrs · 8,674 cycles

EICAS STATUS MSG E&E CLNG EXH FAN. CREW REPORTED SLIGHT BURNING ODOR DETECTED WHEN MSG WAS INITIALLY DISPLAYED, ODOR HAS SINCE CLEARED. CHECKED SYS FOUND CB POPPED FOR FAN. RESET BREAKER AND TESTED SYS IN CMC AFTER A SUCCESSFUL TEST THE CB ON P415 PANEL POPPED AGAIN. SUSPECT FAN FAILED, NIL TIME FOR FURTHER TROUBLESHOOTING. REPLACED EXHAUST FAN. OPS CHECKS OK.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 76,285 hrs · 8,649 cycles

DOOR 2L ESCAPE SLIDE PRESSURE READS IN RED BAND. REPLACED DOOR 2L SLIDE ASSY.

Part: LIGHT — TORN (CABIN) · airframe 76,250 hrs · 8,645 cycles

EMERGENCY EXIT LIGHT INOP.DOOR 5 LEFT GALLEY AREA AFT. LWR LT WALL. INSTALLED NEW BULKHEAD EEL LIGHT, NO HELP. EMERGENCY LIGHT STRIP IS TORN 2 INCHES AFT OF CONNECTION FOR EMERGENCY BULKHEAD LIGHT UNDER GALLEY MAT, NEEDS NEW STRIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,250 hrs · 8,645 cycles

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

Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 76,250 hrs · 8,645 cycles

EMERGENCY EXIT LIGHTS INOP. SEAT ROWS 45 THRU 53 LT, DOOR 4 LT FWD EXIT SIGN, DOOR 4 RT AFT EXIT SIGN, LWR WALL EMERGENCY LIGHT ACROSS DOOR 4 LT, AND DOOR 4 GALLEY AREA LWR WALL EMERGENCY LIGHT. THIS IS A REPEDITIVE PROBLEM IN THIS SPECIFIC AREA ON ACFT. REPLACED FEEDER CABLE. CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,250 hrs · 8,645 cycles

EMERGENCY EXIT LIGHT INOP. FWD GALLEY CEILING LIGHT. RELAMPED, CHECKS OK.

Part: CABLE — FAULTY (CABIN) · airframe 75,739 hrs · 8,581 cycles

MAIN GALLEY EMERGENCY LIGHT FWD WALL INOP. REPLACED EMERGENCY LAMP CABLE, OP CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,739 hrs · 8,581 cycles

DOOR 4L EMERGENCY LIGHT ABOVE DOOR INOP. RELAMPED, OP CHECK NORMAL.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,739 hrs · 8,581 cycles

MAIN GALLEY EMERGENCY LIGHT LT WALL INOP. REPLACED EMERGENCY LIGHT CABLE, OP CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,450 hrs · 8,547 cycles

STRINGER 44L DAMAGED STA 440-480. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW STRINGER SECTION.

Part: TIRE — FAILED (NLG) · airframe 75,450 hrs · 8,547 cycles

LEFT NLG TIRE SHREDDED, ABORTED TAKEOFF AT 120 KNOTS. NLG TIRE SEPARATED/TREAD DEPARTED CAUSING ENGINE AND FUSELAGE DAMAGE. SEVERAL DENTS IN BOTTOM OF FUSELAGE JUST BEHIND THE E&E COMPARTMENT DOOR DUE TO LT NOSE TIRE TREAD SEPARATION. RE-CONTOURED 2 EACH DENTS. CUT OUT DAMAGED AREA NEAR E&E DOOR AND INSTALLED DOUBLER. UA-EVA-73003 B REPAIR. NR 1 AFT AND NR 2 AFT BRAKES AND WHEELS WERE REMOVED FOR AXLE INSP. RE-INSTALLED NR 1A BRAKE AND REPLACED NR 2A BRAKE. BOTH NR 1 AND NR 2 AFT TIRES HAVE BEEN REPLACED.

Part: WIRE — EXPOSED (CONNECTOR) · airframe 74,982 hrs · 8,494 cycles

FOUND WIRING EXPOSED AT CONNECTOR M157. FOUND PLUG AT M157 OK. WIRES GOING TO CONNECTOR DM519 HAD SHORTED. REPAIRED ALL 12 WIRES GOING TO CONNECTOR. RECONNECTED AND ALL OPS RETURNED TO NORMAL.

Part: SKIN — CRACKED (NR 4 PYLON) · airframe 74,748 hrs · 8,468 cycles

NR 4 PYLON RT SIDE SKIN CRACKED AT ACCESS PLATE 482 ER CUTOUT. INSTALLED REPAIR. ACPD ON JOCR 540089.

Part: SKIN — DENTED (FUSELAGE) · airframe 74,748 hrs · 8,468 cycles

FUSELAGE SKIN DENTED AT BS 1840-1860, STR 46R-47R. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER.

Part: CABLE — DEFECTIVE (CABIN) · airframe 74,748 hrs · 8,468 cycles

LAV 111 FWD WALL EEL INOP. REPLACED EEL CABLE, OP CHECK OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,701 hrs · 8,462 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,701 hrs · 8,462 cycles

EMERGENCY EXIT EEL LIGHT INOP, AT DOOR 4 LEFT GALLEY AREA LOWER WALL. REPLACED LAMP, CHECKS OKAY.

Part: CABLE — FAULTY (CABIN) · airframe 74,701 hrs · 8,462 cycles

EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5 RIGHT GALLEY AREA LOWER AFT WALL. REPLACED EEL CABLE. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,701 hrs · 8,462 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,701 hrs · 8,462 cycles

EMERGENCY EXIT EEL LIGHT INOP, AT SEAT ROW 24 RIGHT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,701 hrs · 8,462 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,701 hrs · 8,462 cycles

EMERGENCY EXIT LIGHT INOP. ACROSS DOOR 4 LEFT LOWER WALL. RELAMPED LIGHT, CHECKS OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,701 hrs · 8,462 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 55 RIGHT. RESECURED EMERGENCY LIGHT CONNECTOR, OPS CHECK NORMAL.

Part: HOOK — DISCONNECTED (L2 RAFT LATCH) · airframe 74,227 hrs · 8,407 cycles

DOOR 2L SLIDE PAN COVER DETACHING FROM DOOR. FOUND DOOR 2L SLIDE RAFT LATCH HOOK DISCONNECTED FROM DOOR STRUCTURE LATCH BRACKET. SECURED SLIDE RAFT AND DOOR, OPS CHECK OKAY.

Part: FIRE LOOP — FAULTY (NR 3 ENGINE) · airframe 72,802 hrs · 8,246 cycles

NR 3 ENGINE FIRE LOOP INDICATION. FLT DIVERTED. TRIED NEW FIRE DET CARD YL PA12, NO HELP. RETURNED TO ORIG. TROUBLESHOT LOOP ASSY PER WDM26-11-34, FOUND UPPER AFT LOOP TS681 (A) TO (GRND) NOT OPEN. REPLACED UPPER AFT FIRE DETECTOR ASSY (TS681), GROUND TEST NORMAL, SYS OK.

Part: LIGHT — MISSING (CABIN) · airframe 72,668 hrs · 8,231 cycles

SEAT 38C EMERGENCY LIGHT ASSY IS MISSING. REPLACED LIGHT ASSEMBLY. OPS CHECK IS NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 72,668 hrs · 8,231 cycles

EMERGENCY LIGHT ASSY IS MISSING AT 33C. REPLACED EMERGENCY LIGHT AT SEAT 33C, OPS CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 72,668 hrs · 8,231 cycles

EMERGENCY LIGHT ASSY IS MISSING AT 20C.

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 72,562 hrs · 8,221 cycles

EMERGENCY EXIT LIGHT BROKEN, HALF OF THE EMERGENCY LIGHT IS ILLUMINATED AT SEAT ROW 33 LEFT. RELAMPED EMERGENCY LIGHT, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,562 hrs · 8,221 cycles

EMERGENCY EXIT EEL LIGHT IS INOP AT SEAT ROW 23 LEFT. REPLACED LIGHT, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,562 hrs · 8,221 cycles

SEAT ROW 34ABC EMERGENCY LIGHT IS INOP. REPLACED LAMP, OP CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 72,562 hrs · 8,221 cycles

EMERGENCY EXIT LIGHT IS BROKEN, HALF OF EMERGENCY LIGHT IS ILLUMINATED AT SEAT ROW 21 LEFT. REPLACED EMERGENCY LIGHT ASSY AND CHECK OK.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 72,562 hrs · 8,221 cycles

EMERGENCY EXIT SIGN INOP ACROSS DOOR 4R UPPER WALL EXIT SIGN. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 72,562 hrs · 8,221 cycles

EEL LIGHT INOP AT SEAT ROW 55 RIGHT. SECURED CONNECTOR, OPS CHECKS NORMAL.

Part: CABLE — DEFECTIVE (CABIN) · airframe 72,562 hrs · 8,221 cycles

EMERGENCY EXIT EEL 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 IN GALLEY AREA. T/S SYSTEM FOUND DEFECTIVE CABLE AND EMERGENCY LIGHTS. REPLACED CABLE AND EMERGENCY LIGHTS. GROUND FUNCTIONAL TEST OF LIGHTS GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 72,562 hrs · 8,221 cycles

EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 59 LEFT. SECURED CONNECTOR, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,028 hrs · 8,154 cycles

EMERGENCY LT INOP: DOOR 2R CEILING. RELAMPED EMERGENCY LIGHT, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,028 hrs · 8,154 cycles

EMERGENCY LIGHT INOP: DOOR 1R SLIDE ILLUM. REPLACED LIGHT ASSEMBLY, CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,028 hrs · 8,154 cycles

EEL INOP: ROW 43L. RELAMPED EEL, CHECKS OKAY.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 71,967 hrs · 8,146 cycles

RT UPPER DECK DOOR WILL NOT ARM FOR DEPARTURE. CLEANED ROLLERS AND SLIDE OF ARMING TEE. CLEANED ARMING FORK. CYCLED DOOR AND ARMING IS NOW NORMAL.

Part: ROLLER — DIRTY (RT UPPER DOOR) · airframe 71,967 hrs · 8,146 cycles

RT UPPER DECK DOOR WILL NOT ARM FOR DEPARTURE. CLEANED ROLLERS AND SLIDE OF ARMING TEE. CLEANED ARMING FORK. CYCLED DOOR AND ARMING IS NOW NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 71,678 hrs · 8,116 cycles

THE 1L FLASHLIGHT NO BLINKY. REPLACED BATTERY, OPS OKAY.

Part: HYDRAULIC SYSTEM — OVERHEATED (NR 4) · airframe 71,439 hrs · 8,090 cycles

NR 4 HYD OVERHEAT, TEMP WOULD RISE TO 96 DGR WITH ADP RUNNING, TEMP WOULD RISE TO 88 DEGREES WITH AUX PUMP RUNNING. DPI INDICATORS ARE IN ON CASE DRAIN MODULE AND RETURN FILTER MODULE. MEASURED TEMPERATURE AT RETURNED MODULE MATCHES FLIGHT DECK INDICATION AND HYD QTY IS NORMAL.

Part: SENSOR — FAULTY (HYDRAULIC SYS) · airframe 71,439 hrs · 8,090 cycles

NR 4 HYD OVERHEAT, TEMP WOULD RISE TO 96 DGR WITH ADP RUNNING, TEMP WOULD RISE TO 88 DEGREES WITH AUX PUMP RUNNING. DPI INDICATORS ARE IN ON CASE DRAIN MODULE AND RETURN FILTER MODULE. MEASURED TEMPERATURE AT RETURNED MODULE MATCHES FLIGHT DECK INDICATION AND HYD QTY IS NORMAL. REPLACED NR 4 ENG HYD TEMP SENSOR, RETURN FILTER, AND CASE DRAIN FILTERS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,439 hrs · 8,090 cycles

EMERGENCY LIGHT INOP AT 49ABC. FAULTY LAMP. REPLACED EMERGENCY LIGHT.

Part: BOTTLE — LOW (CREW OXYGEN) · airframe 71,250 hrs · 8,068 cycles

CREW OXYGEN PX READ 1560 PSI ON STS PAGE. REPLACED CREW OXYGEN CYLINDER. ACFT OK FOR SERVICE.

Part: BRAKE — SEIZED (MLG) · airframe 71,229 hrs · 8,065 cycles

LANDING GEAR NO RETRACT. RTFL. FOUND RT BLG FWD LT BRAKE SEIZED. REPLACED BRAKE. NO SHOP DATA FOR ROOT CAUSE.

Part: SLIDE — OUT OF POSITION (R5 DOOR) · airframe 71,186 hrs · 8,060 cycles

UPPER DECK R DOOR WON'T ARM. IMPROPERLY INSTALLED SLIDE. REPOSITIONED SLIDE ASSEMBLY OP CHECK GOOD. AC OK FOR SERVICE.

Part: HARNESS — FAILED (FUEL) · airframe 71,068 hrs · 8,047 cycles

FUEL IMBALANCE. FLIGHT DIVERTED. REPLACED LO-Z HARNESS IN NR 3 MAIN.

Part: BOTTLE — LOW (CREW) · airframe 69,972 hrs · 7,947 cycles

CREW AND PASSENGER OYXGEN LOW AT 1620 AND 1590 PSI RESPECTIVELY . SERVICED OXYGEN SYSTEM NO LEAKS NOTED. AC OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 69,824 hrs · 7,932 cycles

RTFL DUE TO GEAR TILT MESSAGE AND INABILITY TO RETRACT LANDING GEAR. REPLACED RT BODY GEAR TILT ACTUATOR. NO ROOT CAUSE DETERMINED FOR ACTUATOR. OSV SHOP - NO SHOP DATA FOR ROOT CAUSE. THIS SAME ACTUATOR WAS REPLACED ON THIS AIRCRAFT ON 2/18/2008.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT EEL LIGHT INOP, ACROSS LAV 104 LOWER WALL EEL. FOUND SHORTED LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OPS CHECKS NORMAL. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT EEL LIGHT INOP, ACROSS LAV 100 LOWER WALL EEL. FOUND SHORTED LIGHT ASSEMBLY BY LAV 110. REPLACED LIGHT ASSEMBLY OPS CHECKS NORMAL. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT LIGHT INOP AT STAIRS LEADING TO UPPER DECK. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT EEL LIGHT INOP, AT LEFT SIDE COAT CLOSET JUST FWD OF LAV 104 WALL EEL. FOUND SHORTED LIGHT ASSEMBLY BY LAV 110. REPLACED LIGHT ASSEMBLY OPS. CHECKS NORMAL. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT EEL LIGHT INOP, JUST AFT OF DOOR 1 LEFT WALL EEL. FOUND SHORTED LIGHT ASSEMBLY BY LAVATORY 110. REPLACED LIGHT ASSEMBLY OPS CHECKS NORMAL. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT EEL LIGHTS INOP. ALL LEFT SIDE B ZONE SEATS, SEATS 6, 7 AND 8. FOUND SHORTED WALL EEL LIGHT ASSY BY LAV 110. REPLACED LIGHT ASSEMBLY. OPS. CHECKS. NORMAL. AC OK FOR SERVICE.

Part: LIGHT — SHORTED (CABIN) · airframe 69,776 hrs · 7,927 cycles

EMERGENCY EXIT EEL LIGHT INOP, TO THE RIGHT OF LAV 110 WALL EEL. FOUND EMERGENCY EXIT LIGHT SHORTED. REPLACED LIGHT ASSEMBLY OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 34HJK) · airframe 69,280 hrs · 7,876 cycles

EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 34HJK. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (SEAT 47 HJK) · airframe 69,280 hrs · 7,876 cycles

EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 47 HJK. REPLACED LIGHT ASSEMBLY.

Part: SMOKE DETECTOR — NONE (LAVATORY) · airframe 69,241 hrs · 7,872 cycles

LAV 5L 106 SMOKE ALARM INOP. OP CHECKED SMOKE ALARM PER MM 26-13-00-501. ALARM INDICATES NORMAL. AC OK FOR SERVICE.

Part: LANDING GEAR — MALFUNCTIONED · airframe 69,131 hrs · 7,863 cycles

RTFL DUE TO A PROBLEM WITH LANDING GEAR RETRACTION. REPLACED RIGHT HAND BODY GEAR TRUCK TILT POSITION ACTUATOR. OSV SHOP - NO SHOP DATA FOR ROOT CAUSE.

Part: BATTERY — FLUCTUATES (EMERGENCY LIGHTS) · airframe 69,070 hrs · 7,851 cycles

EMERGENCY FLOOR PATH LIGHTS FLICKER ON AND OFF AT ROWS 5, 6 AND 7. COULD NOT DUPLICATE FAULT. AS PRECAUTION, REPLACED M7925 BATTERY AND M6003 POWER SUPPLY PER MM 33-51-04. SHOOK HARNESSES LOCALLY -- NO FLICKERING NOTED. OBSERVED SYSTEM FOR EXTENDED PERIOD WITH NO FAULTS.

Part: SKIN — BENT (FWD CARGO DOOR) · airframe 68,845 hrs · 7,826 cycles

FWD CARGO DOOR SKIN BENT AT AFT LWR CORNER. MAJOR REPAIR ACCOMPLISHED: RMV'D DAMAGED SKIN. INSTALLED EXTERNAL DOUBLER.

Part: SKIN — CANNING (BULK CARGO DOOR) · airframe 68,845 hrs · 7,826 cycles

BULK CARGO DOOR SKIN OIL CANNING AT FWD LWR AREA. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED EXTERNAL SKIN DOUBLER.

Part: CONNECTOR — LOOSE (CABIN) · airframe 68,845 hrs · 7,826 cycles

EEL INOP SEAT 54C. SECURED CONNECTOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,519 hrs · 7,792 cycles

DOOR 5L AFT SILL EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,091 hrs · 7,748 cycles

AFT CREW REST CEILING EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSEMBLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,091 hrs · 7,748 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,091 hrs · 7,748 cycles

SEATS 4A FWD & 58 EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS, CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,091 hrs · 7,748 cycles

DOOR 5 LEFT SILL (2EA) AND DOOR 2R SILL EMERGENCY LIGHTS ARE INOP. RELAMPED.

Part: BOTTLE — LOW (CREW OXYGEN) · airframe 67,791 hrs · 7,719 cycles

CREW O2 PRESSURE SHOWS 1580. SERVICED CREW OXYGEN BOTTLE TO 1730 PSI. AC OK FOR SERVICE.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,636 hrs · 7,703 cycles

LEFT MID FLAP DELAM AND DAMAGE. LEADING EDGE INBOARD, EXTENDING OUT APPROX 5 INCHES. SUSPECT MOISTURE CONTAMINATION. REPLACED THE LT OUTBOARD FLAP PER MM-27-51-04. AC OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 67,636 hrs · 7,703 cycles

RIGHT OUTBOARD AFT FLAP HAS 3 INCH DIA HOLE, BOTTOM AT APPROX 4 FT OUT FROM INBOARDD EDGE AND 7 INCHES UP FROM T/E. REPAIRED IAW SRM 51-70-02. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,636 hrs · 7,703 cycles

EMERGENCY LIGHTS INOP AT 4E AFT, 4J AFT, 5J AFT, 43 ABC AND 58 ABC. REPLACED LIGHT ASSEMBLIES.

Part: LIGHT — LOOSE (CABIN) · airframe 67,518 hrs · 7,691 cycles

STAIR CASE TO UPPER DECK EEL LIGHT IS COMING OFF. 10-16-07 SECURED LIGHT. EEL SYSTEM READY FOR SERVICE.

Part: STRUCTURE — DAMAGED (FWD CARGO DOOR) · airframe 67,348 hrs · 7,671 cycles

FWD CARGO PIT DOOR AFT LOWER CORNER APPEARS TO BE DAMAGED.

Part: LIGHT — INOPERATIVE (SEAT 58LH) · airframe 67,200 hrs · 7,657 cycles

SEAT 58 LEFT SIDE EMERGENCY INOPERATIVE. REPLACED EMERGENCY LIGHT. OP CHECKS NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,200 hrs · 7,657 cycles

DOOR 1R SIDE SILL LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT. OP CHECKS NORMALLY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 67,008 hrs · 7,637 cycles

GEAR MONITOR, EICAS STATUS MESSAGE DISPLAYED. PRI & ALT LANDING GEAR POSITION INDICATION DISAGREE. SELECTED LANDING GEAR MAINTENANCE MESSAGE OR LOSS OF EITHER PSEU BUS OR SELECTED PSEU FAULT. 08-31-07 FOUND EICAS MSG 28649 & 28651. FOUND CIRCUIT BREAKER OPEN "CTR R MAIN 2 JETT VALVE". RESET. OPS NML. NO FOLLOWUP PROBLEMS REPORTED FOR 14 DAYS.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 66,705 hrs · 7,603 cycles

WALL EEL INOP: CROSS AISLE DOOR 5R. FOUND LOOSE CONNECTION, SECURED, CHECKS OK.

Part: FLAP — DAMAGED (LT WING) · airframe 66,705 hrs · 7,603 cycles

LEFT OUTBOARD MID TRAILING EDGE FLAP HAS A DEFLECTION IN ITS TRAILING EDGE OF 1 INCH OVER A LENGTH OF 38 INCHES. [08-14-07] EXISTING FLAP IS NOT DELAMINATED AND IS STRUCTURALLY SOUND. HOWEVER, REPLACED THE LT OUTBOARD FLAP PER MM-27-51-04. AIRCRAFT TEST FLOWN AFTER FLIGHT CONTROL CHANGE. TEST WENT WELL. AIRPLANE RETURNED TO SERVICE. SUSPECT OB MID-TRAILING EDGE FLAP CONTACTED BY GROUND EQUIPMENT & DEFORMED.

Part: FEEDER CABLE — DAMAGED (WALL: AISLE ACRO) · airframe 66,705 hrs · 7,603 cycles

WALL EEL INOP: AISLE ACROSS LAV 100. REPAIRED FEEDER WIRE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,705 hrs · 7,603 cycles

EMERGENCY LIGHT INOP: DOOR 3R SLIDE ILLUM. REPLACED LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,705 hrs · 7,603 cycles

EEL INOP: SEATS 2A & 4E AFT SECTIONS. ALSO SEAT 22 RT & ROW 34 LT. REPLACED LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,705 hrs · 7,603 cycles

EMERGENCY LIGHT INOP: CEILING ROW 24 RT. REPLACED LAMP.

Part: APU — FAULTY · airframe 66,362 hrs · 7,567 cycles

CREW REPORTS APU FLAMED OUT AT DEPARTURE TIME. FIRE CARGO AFT EICAS MSG CAME ON AFTER APU FAILED. [07-27-07] AFTER SEVERAL APU SHUT-DOWNS & ABORTED STARTS, CONDUCTED CICADA CHECK OF INLET SCREEN. CLEANED OFF LOT OFF DEAD BUGS. 10% BLOCKAGED LWR PARTS OF INLET SCREEN. APU OPERATES NORMALLY.

Part: SLIDE — FAULTY (DOOR 3L) · airframe 66,338 hrs · 7,565 cycles

DOOR 3L SLIDE PRESSURE GAUGE IS BELOW GREEN BAND.

Part: SQUIB — NO TEST (EXTINGUISHER) · airframe 66,001 hrs · 7,526 cycles

FIRE EXTINGUISHER SQUIB TEST INOPERATIVE. [06-15-07] LIGHT CIRCUIT FAILS. REPLACED LIGHT PANEL. FOUND SQUIB OP-TEST SATISFACTORILY PER MM26-21-00. A/C OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,812 hrs · 7,504 cycles

EMERGENCY LIGHT ROW 43 ABC INOPERATIVE. [SUP 06-01-07] RELAMPED ROW 43AGC.OP CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,812 hrs · 7,504 cycles

EMERGENCY LIGHT ROW 58 CEILING LIGHT RIGHT INOPERATIVE. [SUP 06-01-07] RELAMPED CEILING LIGHT. OP CHECKS NORMALLY.

Part: SQUIB — FAULTY (FIRE BOTTLE) · airframe 65,145 hrs · 7,430 cycles

AFT CARGO FIRE BOTTLE A FWD SQUIB TEST BAD. REPLACED SQUIB AND TESTED PER MMOV 26-23-02 . TESTED OK FOR SERVICE. SUSPECT INTERNAL DETERIORATION OF SQUIB.

Part: ACTUATOR — UNKNOWN (MLG) · airframe 65,132 hrs · 7,428 cycles

LANDING GEAR WON'T RETRACT; RTFL & LANDED UNDER AMBER ALERT. REPLACED RT BODY TILT ACTUATOR. CYCLED GEAR, OP CHECKED OK.

Part: CONNECTOR — FAULTY (HYDRAULIC SYS) · airframe 65,083 hrs · 7,422 cycles

RTFL UNDER AMBER ALERT DUE TO HYDRAULIC OVERHEAT MESSAGE. REPLACED TEMPERATURE TRANSMITTER FOR ENG NR 1 HYD SYSTEM PER A MM 29-32-02. NO LEAKS. AFTER REPLACEMENT INDICATION IS BLANK. SUSPECT CONNECTOR. REPLACED CONNECTOR. SYSTEM TEST OK. SUSPECT VIBRATION CAUSE INTERNAL CONNECTOR WEAR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 64,474 hrs · 7,358 cycles

EEL INOP AT 46HJK, 34ABC, 4E AFT, AND 4F AFT. RELAMPED EACH EEL, OP CHECKS OKAY FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 64,474 hrs · 7,358 cycles

EMERGENCY LIGHT AT 26R CEILING INOP. RELAMPED EEL, CHECKS OKAY FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 64,008 hrs · 7,303 cycles

EEL 4F AFT INOP. RELAMPED. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,008 hrs · 7,303 cycles

AFT LT CROSS AISLE EMERGENCY LIGHT INOP ADJACENT TO 5L. RELAMPED EEL LIGHT. OP CHECKED OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,076 hrs · 7,203 cycles

FOUND UPPER DECK LOWER EMERGENCY EEL EXIT SIGNS AT BOTH LEFT AND RIGHT EXIT DOORS INOP. REPLACED BATTERY. OP CK NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,076 hrs · 7,203 cycles

UPPER DECK LOWER WALL AISLE EMERGENCY EEL LIGHTS ACROSS LAVS INOP. REPLACED BATTERY. OP CK NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,076 hrs · 7,203 cycles

FOUND EMERGENCY EEL LIGHTS AT SEATS 12AB THRU 14AB AND 22AB THRU 26AB ARE INOPERATIVE. REPLACED BATTERY. OP CK NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 5J) · airframe 63,076 hrs · 7,203 cycles

FOUND EMERGENCY EEL LIGHTS AT SEAT 5J FWD ARE INOPERATIVE. REPLACED EEL LIGHT. OP CK NORMAL.

Part: STRUCTURE — INTERFERENCE (DOOR FRAME) · airframe 62,610 hrs · 7,145 cycles

DOORWAY FRAME TO SILL CLIP INTERFERES WITH FASTENER INSTALLATION AT BS 1810 STR 27R. TRIMMED OUT CLIP & INSTALLED REPAIR ANGLE. INSPECTED REPAIR. WITHIN 15000 CYCLES OF REPAIR INSTALLATION & ACP REPETITIVE INSPECTIONS AT INTERVALS NOT TO EXCEED 3000 CYCLES. SUSPECT IMPROPER REPAIR EARLIER IN VISIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,610 hrs · 7,145 cycles

EMERGENCY EXIT LIGHT INOP AT UPPER DECK LT EXIT. RELAMPED AND OP CHECKED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,610 hrs · 7,145 cycles

EMERGENCY EXIT LIGHT INOP AT UPPER DECK RT DOOR AND NUMEROUS SEAT EELS FLICKERING AT UPPER DECK FWD AREA. REPLACED BATTERY PACKS, OP CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,610 hrs · 7,145 cycles

SEVERAL CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED, OP CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,610 hrs · 7,145 cycles

DOORWAY 4L AFT EEL INOPERATIVE. RELAMPED, OP CHECKED OK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,610 hrs · 7,145 cycles

DOOR 1L EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, OP CHECKED OK

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 62,610 hrs · 7,145 cycles

EEL LIGHTS INOP AT SEATS 54C, 1J & 4A. RELAMPED, OP CHECKED OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 62,494 hrs · 7,128 cycles

FLAPS DRIVE EICAS CAUTION MESSAGE DISPLAYED. 'FLAPS DRIVE' EICAS CAUTION MESSAGE DISPLAYED. INBD OR OUTBD TE FLAP ASYMMETRY, INBD OR OUTBD TE FLAP SHUTDOWN OR L E FLAP SHUTDOWN, OR LE ELEC FLAPS DISAGREEMENT. REPLACED NR 1 FLAP LE DRIVE UNIT PER MM 27-81-03.

Part: BLADES — BIRD INGESTION (NR 1 ENGINE) · airframe 62,138 hrs · 7,088 cycles

BIRD STRIKE ON NR 1 ENGINE. ABORTED TAKEOFF AT APPROXIMATELY 153 KNOTS. EXTENSIVE FAN BLADE DAMAGE. 24 OF 38 DAMAGED BEYOND LIMTS. NOSE COWL LIP SEVERELY DENTED. ALL SURGE CHECKS INCLUDING BORESCOPE INSPECTION CHECKED OK. ALL FAN BLADES REPLACED. NOSE COWL REPLACED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,834 hrs · 7,053 cycles

ROW 44 RH EMERGENCY LIGHT INOP.

Part: SMOKE — DETECTED (CABIN) · airframe 59,855 hrs · 6,835 cycles

ELECTRICAL SMOKE IN CABIN.

Part: ASPIRATOR — DAMAGED (ESCAPE SLIDE) · airframe 59,623 hrs · 6,808 cycles

THERE WAS A LARGE HOLE FOUND ON THE UNDERSIDE OF THE ASPIRATOR DURING THE ASPIRATOR INSPECTION. ASPIRATOR DAMAGED BEYOND REPAIR. DAMAGE CAUSED BY IMPROPER PACKING. REPLACED ASPIRATOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,563 hrs · 6,800 cycles

EMERGENCY EXIT LIGHT ABOVE DOOR 3 RIGHT INOP. REPLACED LAMP.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 59,563 hrs · 6,800 cycles

CENTER LAV CROSS AISLE WALL MOUNTED EMERGENCY EEL LIGHT INOP. REPAIRED FEEDER CABLE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,563 hrs · 6,800 cycles

EMERGENCY EXIT LIGHT AT SEAT 32 HJK INOP. REPLACED LAMP.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,563 hrs · 6,800 cycles

EMERGENCY EXIT CEILING LIGHT IN FLIGHT DECK INOP. REPLACED POWER SUPPLY.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 59,563 hrs · 6,800 cycles

EMERGENCY EXIT SIGN BELOW VIDEO MONITOR AT DOOR 3 LEFT INOP. REPAIRED CONNECTOR.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 58,598 hrs · 6,693 cycles

EXISTING DOUBLER NOT PER SRM OR MM, STATION 1720-1740 AND STRINGER 38R-40R. MJR RPR, EXISTING DOUBLER NOT PER SRM OR MM, STA 1720- 1740, AND STR 38R-40R. DOUBLER REMOVED; ACCOMP HFEC INSP, NO CRACKS NOTED, REF NDT PART 6, 53-00-01. FABBED DOUBLER AND INSTALLED PER SRM 53-00-01, FIG 201. LESS THAN 5 LB SKIN TRIM OUT 3 BY 5 INCH, 2 INCH ABOVE SKIN LAP AT STR 40R.

Part: ODOR — DETECTED (CABIN) · airframe 53,647 hrs · 6,083 cycles

FA REPORTED SMELLING PLASTIC BURNING SMELL/SMOKE. F/A USED A PLASTIC COVER WHILE HEATING FOOD. PLASTIC COVERED FOOD IS NOT LOADED INTO OVENS. F/A SHOULD REVIEW CORRECT PROCEDURES FOR RECON OVENS AND NEVER PLACE ANY PLASTIC ITEMS INTO OVENS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,033 hrs · 6,003 cycles

CORROSION WAS DISCOVERED ON THE UNDERSIDE OF THE FLOORBEAM LOCATED AT STA 1100 FROM LBL 17 TO LBL 30. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR STRAP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,539 hrs · 5,930 cycles

SEAT 17L AFT EEL LIGHT STRIP WILL NOT LIGHT. REPLACED AND TESTED 17L EEL LIGHT ASSY, CHECKS OK.

Part: AILERON — MALFUNCTIONED (WING)

FLT EXPERIENCED AILERON PROBLEMS PRIOR TO LANDING. AUTOPILOT WARNING RECEIVED. DISCONNECTED AUTO PILOT. AIRPLANE COULD NOT TURN LEFT (RIGHT TURNS OK).

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 49,257 hrs · 5,483 cycles

LIGHTNING STRIKE TO FUSELAGE SKIN. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPAIRED PER SRM.

Part: ACTUATOR — FAILED (RT MLG DOOR) · airframe 48,363 hrs · 5,359 cycles

RT WING GEAR FAILED ALTERNATE EXTENSION TEST. NEITHER DOORS NOR GEAR WOULD EXTEND. FAILED ALTERNATE EXTEND ACTUATOR. REPLACED ACTUATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,742 hrs · 5,125 cycles

FORWARD SIDE OF LAV 117 EEL LIGHT INOPERATIVE. REPLACED EEL STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,742 hrs · 5,125 cycles

FORWARD SEAT EEL AT SEAT 2J IS INOPERATIVE. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,742 hrs · 5,125 cycles

CEILING EEL AT ROW 2 IS INOPERATIVE. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,742 hrs · 5,125 cycles

AFT SEAT EEL AT SEAT 5F IS INOPERATIVE. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,742 hrs · 5,125 cycles

BOTH SEAT EEL AT SEAT 1A IS INOPERATIVE. RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,742 hrs · 5,125 cycles

CEILING EEL LIGHT AT ROW 17 IS INOPERATIVE. REPLACED BATTERY PACK IN CEILING.

Part: LIGHT — LOOSE (CABIN) · airframe 46,742 hrs · 5,125 cycles

AT LAV 110 EEL LIGHT INOP. STAPLED POWER STRIP AND OPS TESTED NORMAL.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 45,902 hrs · 5,016 cycles

THE RIGHT HAND EXTERIOR SKIN WAS PUNCTURED JUST AFT OF DOOR 5R. BODY STATION 2290, NEAR STRINGER 21R. MAJOR REPAIR ACCOMPLISHED, A DOUBLER REPAIR WAS INSTALLED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,899 hrs · 4,881 cycles

EMERGENCY EXIT OVERHEAD LIGHT ASSEMBLY AT SEATS 17GH INOP. LIGHT ASSEMBLY INOP. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,929 hrs · 4,422 cycles

EEL LIGHT AT CROSSAISLE DOOR 5L AND 5R DOES NOT ILLUMINATE. *S/D* REPLACED EEL LIGHT ASSY, OPS CHECKED OK.

Part: WIRE — BROKEN (1 L DOOR)

1L MED EMERGENCY SLIDE LIGHT (ON DOOR) ILLUMINATES WHEN POWER IS OFF AIRCRAFT. THIS PROBLEM WAS CAUSED BY A DISCONTINUITY IN THE CIRCUIT. A GROUND WIRE WAS FOUND BROKEN (ROUTING OF WIRE IS FROM DX317, PIN 1 TO GD6338). WIRE W2078-001-20 WAS REPLACED (REF WDM 33-51-22).

Part: POWER PACK — INOPERATIVE (CABIN)

UPPER DECK LEFT EMERGENCY EXIT LIGHT WILL NOT TURN OFF. REPLACED POWER PACK.

Part: RETRACT MECH — OUT OF SEQUENCE (GEAR DOORS)

ON TAKEOFF, GEAR DOOR MESSAGE APPEARED ON EICAS. AFTER BECOMING AIRBORNE, LANDING GEAR HANDLE WAS RAISED AND GEAR CAME UP BUT MESSAGE REMAINED ON. LOWERED GEAR, BURNED DOWN FUEL, AND LANDED UNEVENTFULLY. *S/D* GEAR DOORS FAILED TO CLOSE DUE TO AN OUT OF SEQUENCE CONDITION OF THE ALTERNATE EXTEND MOTOR. RECYCLED LANDING GEAR ALTERNATE EXTEND SYSTEM. GEAR CYCLED AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. NO FURTHER ACTION TAKEN. NO PARTS REPLACEMENT REQUIRED. RECYCLING OF ALTERNATE EXTEND SYSTEM ACCOMPLISHED PER IRREGULAR PROCEDURES 7-52.

Part: PANEL — CRACKED (LT WING)

DURING INSPECTION AT NRT, A 41 INCH CRACK WAS FOUND ON THE LEFT WING FIXED LEADING EDGE UPPER SKIN PANEL. THE DAMAGED SKIN PANEL IS LOCATED OUTBOARD OF WS 499.02 AND INBOARD TO THE NR 2 ENGINE. ACCOMPLISHED INTERIM SANDWICH DOUBLER REPAIR. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK. PART TOTAL CYCLES, 2,663.

Part: LAMP SEGMENT — FAILED (CABIN)

EMERGENCY EXIT LIGHT INOP AT ROW 1R, LAMP SEGMENT BURNED OUT. REPLACED LAMP SEGMENT AND POWER STRIP.

Part: EEL LAMP — FAILED (CABIN)

FLOOR EEL INOP FROM ROW 24L FWD TO LAV 104 AND DOOR 2 GALLEY CROSS AISLE. REPLACED SHORTED TWO LAMP SEGMENT NEXT TO DOOR 2L.

Part: EEL WIRE — FAILED (CABIN)

EMERGENCY EXIT SIGNS AT DOOR 4 LEFT REMAIN ON AFTER TEST. RESPLICED WIRE BUNDLE.