N669US

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,018 hrs · 13,507 cycles

DURING SERVICE CHECK, FOUND UPPER DECK LEFT EXIT DOOR EMERGENCY SLIDE LIGHTS INOPERATIVE AND REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 109,781 hrs · 13,384 cycles

FLOOR EMERGENCY LIGHT BESIDE SEAT 77A TO 79A INOPERTIVE. REPLACED POWER SUPPLY WITH BATTERY ABOVE SEAT 78 AISLE. OPS TESTED OK IAW AMM 33-51.

Part: FAN — FAILED (RECIRCULATION) · airframe 108,663 hrs · 13,265 cycles

JUST AFTER TAKEOFF THE CREW RECEIVED A RECIRCULATION FAN MESSAGE AND THE F/A REPORTED SMOKE IN THE CABIN. TURNED OFF THE FANS AND SMOKE QUICKLY DISSIPATED AND FLIGHT CONTINUED. VERIFIED FAN CAUSED THE EVENT. R & R THE RECIRCULATION FAN AND FILTERS IAW AMM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 104,902 hrs · 12,832 cycles

RIGHT NR 2 DOOR UPPER DOOR HINGE CUTOUT CORNER IN THE DOOR EXTERNAL SKIN FOUND CRACK. THE CRACKED EXTERNAL SKIN AT RT NR 2 DOOR UPPER DOOR HINGE CUTOUT CORNER REPAIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,902 hrs · 12,832 cycles

SHIP 6309. 0.135"LENGTH CRACK FOUND ON AFT UPPER CORNER OF THE CUTOUT R, RT MAIN ENTRY DOOR NR 5. LEFT MAIN ENTRY DOOR NR 5 CUTOUT AFT UPPER CORNER SKIN WAS REQUIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,902 hrs · 12,832 cycles

0.135" LENGTH CRACK FOUND ON AFT UPPER CORNER OF THE CUTOUT R, RT MAIN ENTRY DOOR NR 5. RIGHT MAIN DOOR NR 5 AFT UPPER CORNER OF CUTOUT SKIN WAS REPAIRED.

Part: STOP FITTING — CRACKED (L3 DOOR) · airframe 104,902 hrs · 12,832 cycles

LEFT NR 3 DOOR CUTOUT FWD SIDE STOP SUPPORT FITTING "NR 5" FOUND CRACK. FWD SIDE NR 5 STOP SUPPORT FITTING WAS REPLACED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 104,663 hrs · 12,793 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 22C CEILING. SECURED THE ELECTRICAL CONNECTOR D13500P.

Part: ENGINE — FIRE (NR 4) · airframe 103,501 hrs · 12,665 cycles

RETURNED TO DEPARTURE, WITH THE NR 4 ENGINE SHUTDOWN. CREW REPORTED THAT THEY HAD THE NR 4 ENGINE SURGE AT 600 FT AND THEN ABOUT 15 SECONDS LATER HAD A NR 4 ENGINE FIRE WARNING. FOLLOWED QRH AND BLEW BOTH FIRE BOTTLES, FIRE WARNING EXTINGUISHED. ENGINE CHANGE IN PROGRESS.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 103,183 hrs · 12,627 cycles

L2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,106 hrs · 12,500 cycles

R3 DOOR EMERGENCY EXIT SIGN DOES NOT LIGHT. R & R BATTERY CHARGER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 101,672 hrs · 12,450 cycles

R5 EMERGENCY DOOR MOUNT LIGHT WOULD NOT TURN ON. REPLACED LIGHT ASSEMBLY WITH BATTERY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,288 hrs · 12,404 cycles

DURING NON ROUTINE LINE CHECK, UPPER DECK EMERGENCY LIGHTS INOPERATIVE AT SEATS 72-75. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51, WDM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.

Part: DOOR FRAME — CRACKED · airframe 99,497 hrs · 12,193 cycles

NR 5 MAIN CABIN DOOR CUT OUT FWD DOOR FRAME JUST BELOW S17L AREA FOUND CRACKED. CRACK CUTOUT AND REPAIRED IAW ERA 512578-14, REV ORIGINAL.

Part: RIVET — LOOSE (FUSELAGE SKIN) · airframe 99,497 hrs · 12,193 cycles

BS 2673 & 2678 RIVETS FOUND LOOSE. REPAIRED IAW ERA 518816-14, REV ORIGINAL. .

Part: FRAME — CRACKED (BS 1480) · airframe 99,497 hrs · 12,193 cycles

CRACKED FRAME WEB BS 1480, S33L BLG WHEEL WELL. REPAIRED CRACKED FRAME WEB LOCATION BS 1480, S33L IAW ERA 518819-14, REV ORIGINAL.

Part: DOOR FRAME — CRACKED · airframe 99,497 hrs · 12,193 cycles

MAIN CABIN DOOR CUTOUT FWD DOOR FRAME JUST BELOW S-17 FOUND CRACKED. CRACKED AREA CUTOUT AND REPAIRED IAW ERA 512578-14, REV ORIGINAL.

Part: STRUCTURE — CORRODED (BS 1480) · airframe 99,497 hrs · 12,193 cycles

AFT CARGO BAY STRINGER JOINT FITTING BS 1480 CORRODED. THE DAMAGED STRINGER JOINT FITTING WAS REPLACED IAW SRM 51-40-02 AND DWG:69B10501.

Part: SEAT TRACK — CORRODED (BS 2240) · airframe 99,497 hrs · 12,193 cycles

CORROSION ON SEAT TRACK BS 2240 LBL 11, WL 199.8 M/D. SEAT TRACK REPLACED IAW SRM 53-00-52, REPAIR 6.

Part: FLOOR SUPPORT — CORRODED (BS 2270-2280) · airframe 99,497 hrs · 12,193 cycles

CORROSION FOUND ON FLOOR SUPPORT BS 2270-2280, LBL 11, WL 199.8. FLOOR SUPPORT REPLACED IAW SRM 51-40-02, PAGE 1 TO 7.

Part: STRINGER — CORRODED (BS 1600-1640) · airframe 99,497 hrs · 12,193 cycles

AFT CARGO BAY STRINGER 36L, BS 1600-1640. FOUND CORRODED. STRINGER REPAIRED IAW SRM 53-00-03, REPAIR 6.

Part: SEAT TRACK — CRACKED (BS 1000) · airframe 99,497 hrs · 12,193 cycles

SUSPECTED CRACK ON SEAT TRACK, BS 1000, LBL 98. SEAT TRACK REPLACED IAW, SRM 51-40-02, PAGE IT 07, AND DWG 140U5289-45.

Part: STOP FITTING — CRACKED (L4 DOOR FRAME) · airframe 99,497 hrs · 12,193 cycles

STOP FITTING L4 DOORWAY CRACKED. R & R IAW AMDS CARD:5310-01283-07C.

Part: SEAT TRACK — CRACKED (BS 1000) · airframe 99,497 hrs · 12,193 cycles

SUSPECTED CRACK ON SEAT TRACK BS 1000, RBL 98. SEAT TRACK REPLACED IAW, SRM 51-40-02 AND DWG 140U5289.

Part: FLOORBEAM — CORRODED (BS 480) · airframe 99,497 hrs · 12,193 cycles

FLOORBEAM BS 480, LBL60, WL 199.8 CORRODED. SECTION CUT OUT AND FABRICATED REPAIR PARTS IAW, SRM53-10-51, REPAIR 3 . HFEC INSPECTED AND NO CRACK FOUND.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 98,795 hrs · 12,104 cycles

RIGHT EXTERIOR EMERGENCY LIGHTS OUT AT 1ST AND 2ND POS. REPLACED FUSE ON POWER SUPPLY THEN OPS CHECKED GOOD IAW AMM 33-51, NRT 116646.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 96,418 hrs · 11,803 cycles

R5 DOOR SLIDE EMERGENCY LIGHT WILL NOT TURN OFF. REPAIRED BROKEN WIRE W2088-004-20 IAW SWPM 20-30-12. EMERGENCY LIGHTS TEST OK IAW AMM 33-51-00/501.

Part: SEAT TRACK — CORRODED (BS 900) · airframe 95,292 hrs · 11,676 cycles

SEAT TRACK, ZONE C BS 900, RBL98.58, FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 51-10-02. INSTALLED SEAT TRACK IAW AMM20-51-01.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 95,211 hrs · 11,664 cycles

DURING INSPECTION FOUND SEAT 22 ABC FLOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED FLOOR PROXIMITY SWITCH ASSEMBLY. OPERATIONAL CHECK OK AS PER AMM 33-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 95,094 hrs · 11,649 cycles

DURING INSPECTION, FOUND DOOR 3R EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY BATTERY AND BATTERY CHARGER PER B747-400 AMM33-51. CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,994 hrs · 11,637 cycles

DURING INSPECTION FOUND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED DOOR 3R EMERGENCY POWER SUPPLY BATTERY PER AMM 33-51. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,689 hrs · 11,601 cycles

DURING INSPECTION, FOUND DOOR MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT AND POWER SUPPLY PER WDM 33-51-41. OPS CHECKED NORMAL PER AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 94,646 hrs · 11,596 cycles

DURING INSPECTION FOUND UPPER DECK AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AT CEILING PANEL BS 970 PER AMM 33-51. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,107 hrs · 11,528 cycles

DURING INSPECTION FOUND EMERGENCY FLOOR PROXIMITY LIGHTS BESIDE SEAT 79 AND 80 WON`T TURN ON. MAINTENANCE REPLACED DEFFECTIVE M7052 POWER SUPPLY AND OPS CHECKED OK AS PER AMM NR 33-51. AIRCRAFT OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 93,917 hrs · 11,505 cycles

DURING INSPECTION FOUND POSITION DOOR 2R FLOOR PROXIMITY LIGHT NOT ILLUMINATED. MAINTENANCE REPAIRED BAD CONNECTOR AND RELAMPED. OPS CHECKED OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 93,807 hrs · 11,491 cycles

DURING INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT ROW 20-30 LEFT. MAINTENANCE RECONNECTED MODULE PIN AT ROW 20. OPERATIONAL CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,293 hrs · 11,431 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR LIGHTS AT SEATS 51ABC TO 64ABC WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHTS. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHTS WERE REPLACED.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 92,815 hrs · 11,377 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY EXIT SIGN AT DOOR R3 LOWER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FUSE. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE WAS REPLACED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 7,049 hrs · 855 cycles

DOOR 3R AND RT EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER AT DOOR 3R PER AMM 33-51. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,680 hrs · 813 cycles

DOOR 4R DOOR-MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 919,661 hrs · 11,270 cycles

DURING A MAINTENANCE VISIT, TWO OVERWING EMERGENCY LIGHTS ON THE RIGHT SIDE WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY, F4 FUSE AND THE RIGHT FORWARD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY, FUSE AND LIGHT ASSEMBLY WERE REPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 91,879 hrs · 11,260 cycles

DURING A MAINTENANCE VISIT, TWO OVERWING EMERGENCY LIGHTS ON THE RIGHT SIDE WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AT 3R. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 91,378 hrs · 11,203 cycles

DURING A MAINTENANCE VISIT, THE EXTERIOR EMERGENCY LIGHT, FIRST AND SECOND, ON THE RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. SYSTEM OPERATION WAS NORMAL AFTER THE WIRE WAS REPAIRED.

Part: MODULE — INOPERATIVE (CABIN) · airframe 911,872 hrs · 24,224 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH LIGHT AT DOOR 3R WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACEDTHE EMERGENCY ESCAPE PATH LIGHT MODULE. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT MODULE WAS REPLACED.

Part: MODULE — INOPERATIVE (CABIN) · airframe 91,173 hrs · 11,181 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH LIGHT AT LAVATORY DOOR 2L WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR PROX LIGHT MODULE. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT MODULE WAS REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,444 cycles

DURING LCK, A CRACK WAS FOUND ON THE STA Y00 LBL 45 FRAME IN THE FWD CARGO COMPARTMENT. ER/A 495580-14 SECT I WAS ACCOMP. FOLLOW ON ACTION IS REQ FOR THIRD STAGE APPROVAL. DFRD 233849 STA MSP 09SEP11 ATA 5311 ENTR 233849 S ACCOMP ER/A 495580-14 SECT II BEFORE 20,000 A/C CYCLES. IF THIS LOG AND ER/A HAVE NOT BEEN REVISED BY 20,000 TOTAL A/C CYCLES, REMOVE A/C FROM REVENUE SERVICE. FOLLOW ON ACTION IS REQUIRED FOR STAGE III (DTA) APPROVAL FROM BOEING.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

DURING LCK, FUSELAGE SKIN PANELS REQUIRED REPAIR BY BLENDING OUT WEAR DAMAGE AT THE VERTICAL STAB SEAL INTERFACE. FOLLOW-ON SURFACE HFEC INSP ARE REQ PER EM 5331-01190, SECTION 02. BOEING SB 747-53A2470, REV 2 / FAA AD 2009-14-02. ACCOMP SURFACE HFEC INSP PER SECT II OF ER/A 491632-14AD PRIOR TO 20,000 TOTAL FC AND REPEAT AT INTERVALS NOT TO EXCEED 6,000 FC. AA 5331-01190 ADDED FOR AC 6309 ASSOCIATED ER/A 13-491632 ADDED FOR AC 6309.

Part: FITTING — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

CORROSION WAS FOUND ON BODY FAIRING CLIP STA 880 BL 0. S: 1"X0.8". REPLACED WITH NEW CLIP .

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

RADOME SUPPORT CRACK BS 134 RBL6 L=0.8". REPLACED THE SUPPORT WITH NEW ONE PER B747-400 SRM 51-40-02 P1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

CORROSION WAS FOUND ON TWO BODY FAIRING CLIPS STA 920. BL 0. S: 1"X0.8" REPLACE THE CLIPS WITH THE NEW ONE PER B747-400 SRM 51-40-02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

DURING PERFORM REPAIR A TOOL PENETRATED THE 65B07415-5 WEB AT LBL 10, STA 120 LWR LOBE FRAME FWD CARGO COMPARTMENT S=0.6" X0.8". PER ER/A 495575-14 REV O AND NRC 120/30 COMPLETED THIS WORK.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

CORROSION WAS FOUND ON BODY FAIRING SUPPORT STA 987 LBL 50.S:1"X0.8". MAINTENANCE REPAIRED SUPPORT FLANGE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

5/190 A CORROSION WAS FOUND ON SUPPORT OF BODY FAIRING STA 9875 LBL 20. S:1"X5" LOG PAGE ENTERED AND DEFERRED FOR SDR REPORTING. MAINTENANCE REPAIR 3 FIG 201 REPAIRED THE SUPPORT FLANGE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

SEVERAL CORROSION WERE FOUND ON BODY FAIRING SUPPORT STA 880 BL 0-RBL 40. S: 0.9"X0.9". MAINTENANCE REPAIRED FAIRING SUPPORT FLANGE.

Part: FAIRING — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

SEVERAL CORROSION WERE FOUND ON BODY FAIRING 880. BL 0-LBL 50. S: 0.9"X0.9". MAINTENANCE REPAIRED FAIRING SUPPORT FLANGE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

8/190 SEVERAL CORROSION WERE FOUND ON BODY FAIRING SUPPORT STA 1660. LBL 40-60. S=0.8"X0.8" LOG PAGE ENTERED AND DEFERRED FOR SDR REPORTING. MAINTENANCE PERFORM REPAIRED PER ER/A 495578-14 REV ORIGINAL. RII COMPLETED.

Part: BULKHEAD — BROKEN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

A BROKEN WEB WAS FOUND ON BULKHEAD OF FORWARD CARGO COMPARTMENT STA 720 LBL 7. S: 0.5"X0.7. REPAIRED THE WEB PER ER/A 495575-14 REV 0.

Part: SKIN — WORN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

RT FUSELAGE SKIN SEVERAL WEAR STA 2558-STA 2618. S-3R. MAXL:10" BLEND REPAIR PER ER/A 491632-14AD REV 0 THIS DAMAGE WITHIN LIMITS.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

A CRACK WAS FOUND ON FLOOR FRAME UPPER CHORD OF FWD CARGO COMPARTMENT STA 600 LBL 42. L: 2". REPLACED THE DAMAGED FLOOR FRAME PER ER/A495580-14.

Part: SKIN — WORN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

RT FUSELAGE SKIN WEAR. STA 2320-STA 2330. S-3R. L=10" REPAIR PER ER/A 491632-14AD REV 0 THIS DAMAGE WITHIN LIMITS.

Part: FITTING — BROKEN (NR 1 PYLON) · airframe 90,864 hrs · 11,144 cycles

STRUT NR 1: INSTALL FITTING OF ADP WAS BROKEN AT STRUT FT BULKHEAD. REPLACED THE FITTING WITH NEW ONE PER B747-400 SRM 51-40-02P1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

CORROSION WAS FOUND ON INTERNAL AND EXTERNAL SKIN SURFACE AT LAV TUB CUTOUT (LT) STA 2090. S-35L - S-36L. S: 1"X0.8- BLEND OUT THE CORROSION, RECORD SIZE, REPLACED THE INTERNAL DOUBLER AND RESTORED SURFACE TREAT, AND PAINT PER B747-400 SRM 53-00-01 ALLOWABLE DAMAGE 1. FIG 101 AND B747-400 SRM 51-40-02 P1 ORIG.MAT.0.071" DAMAGE DIM.L1.22" W1.01"D0.004.

Part: SKIN — WORN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

RT FUSELAGE SKIN SEVERAL WEAR STA 2380-STA 2416 S-3R. MAXL:9" BLEND REPAIR PER ERA 491632-14AD REV O THIS DAMAGE WITHIN LIMITS.

Part: SKIN — WORN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

LT FUSELAGE SKIN SEVERAL WEAR STA 2330-STA 2350. S-3L. MAXL:8" DFRD BY CUI 713978 STA PEK 28AUG11ENTR 713978 S. REPAIR PER ER/A 491632-14AD REV 0 THIS DAMAGE WITHIN LIMITS MONITOR ESTABLISHED ON L/P 0378469.

Part: BALANCE WEIGHT — CORRODED (ELEVATOR) · airframe 90,864 hrs · 11,144 cycles

LT OUTBOARD ELEVATOR ADJUST WEIGHT CORROSION. S:3"X2.5". ELEV STA 231.8. REPLACED THE ADJUST WEIGHT WITH NEW 02 P1.

Part: SKIN — WORN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

LT FUSELAGE SKIN WEAR. STA 2370. S-3L. L=2.5" BLEND REPAIR PER ER/A491632AD REV 0 THIS DAMAGE WITHIN LIMITS.

Part: BALANCE WEIGHT — CORRODED (ELEVATOR) · airframe 90,864 hrs · 11,144 cycles

LT OUTBOARD ELEVATOR BALANCE WEIGHT CORROSION. S: 2.5"X5" ELEV STA 231.8. REPLACED THE BALANCE WEIGHT WITH NEW PART PER B-747-400 SRM 51-40-02 P1 2.

Part: SKIN — WORN (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

LT FUSELAGE SKIN SEVERAL WEAR STA 2541 -STA 2598 S-3L. AXL:10" BLEND REPAIR PER ER/A 491632-14AD REV 0 THIS DAMAGE WITHIN LIMITS.

Part: GATE — CORRODED (R1 DOOR) · airframe 90,864 hrs · 11,144 cycles

LOWER SURFACE CORROSION WAS FOUND ON LOWER GATE OF RT NR 1 DOOR. S=0.2"X0.2- PER ER/A 491638-14 REV ORIG. PERFORMED THE LOWER GATE REPAIR. ORIG.MAT. 0.150" DAMAGE DIM. L20.04" W1.1" D0.04".

Part: GATE — CORRODED (L1 DOOR) · airframe 90,864 hrs · 11,144 cycles

CORROSION WAS FOUND ON LOWER GATE OF LT NR 1 DOOR. S=0.5"X0.5" PER ER/A 491637-14 REV ORIG. PERFORMED THE LOWER GATE REPAIR ORIG.MAT. 0.15" DAMAGE DIM: L2.53" W0.4" D0.03".

Part: GATE — CORRODED (L5 DOOR) · airframe 90,864 hrs · 11,144 cycles

LOWER SURFACE CORROSION WAS FOUND ON LOWER GATE OF LT NR 5 DOOR. S=0.3"X2" PER ER/A 495576-14 REV ORIG. PERFORMED THE LOWER GATE REPAIR. ORIG.MAT. 0.155" DAMAGE DIM: L1.87" W0.69" D0.108".

Part: RIB — CRACKED (RADOME) · airframe 90,864 hrs · 11,144 cycles

CRACK WAS FOUND ON RIB OF RADOME SUPPORT AT STA 134, LBL 6, L=1.5" DFRD PER B747-400 SRM 51-40-02 P1 REPLACED THE RIB WITH NEW PART.

Part: GATE — CORRODED (L2 DOOR) · airframe 90,864 hrs · 11,144 cycles

LOWER SURFACE CORROSION WAS FOUND ON LOWER GATE OF LT 2 DOOR. S=0.6"X1" PER ER/A 491636-14 REV ORIG PERFORMED THE LOWER GATE REPAIR. ORIG.MAT. 0.190" DAMAGE DIM: L1.34" W0.70" D0.051".

Part: GATE — CORRODED (L2 DOOR) · airframe 90,864 hrs · 11,144 cycles

LOWER SURFACE CORROSION WAS FOUND ON LOWER GATE OF LT NR 2 DOOR. S=0.6"X1- PER ER/A 491636-14 REV ORIG. PERFORMED THE LOWER GATE REPAIR ORIG.MAT. 0.190" DAMAGE DIM: L1.34" W0.70" D0.051".

Part: SKIN — DENTED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

DENT ON FUSELAGE SKIN (CREASE) AT STA 222, 3" BELOW CUSP LINE LONGERON 18L. COMPLIED WITH ER/A 495312-14 REV ORIGINAL SECTION 1. ACCOMPLISH CLOSE VISUAL INSP OF REPAIR AREA TO CHECK FOR LOOSE, MISSING FASTENERS REF SECTION 2 OF ER/A 495312-14 REV ORIG. ACCOMPLISH SECT 2 PRIOR TO 3000 FLIGHT CYCLES AFTER SECTION 1 AND REPEAT EVERY ASSOCIATED ER/A 14-495312 ADDED FOR AC 0885.

Part: SILL — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

LT NR 1 MAIN ENTRY DOOR UPPER SILL WEB CRACK BS 460. S-17L. L=0. 8".

Part: SILL — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

RT NR 1 MAIN ENTRY DOOR UPPER SILL WEB CRACK BS 460, S-17R, L=2".

Part: SILL — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

RT NR 1 MAIN ENTRY DOOR UPPER SILL WEB CRACK BS 460. S-17R. L=2" PER B747-400 SRM 53-10-15 R1 CATEGORY B. INSP REPEAT DETAILED INSP OF THE MAIN ENTRY DOOR 1 UPPER MAIN SILL OUTER CHORD, WEB, AND FRAME ATTACH ANGLES FOR CRACK(S). WITH 6000 FLIGHT-CYCLES FROM THE LAST INSPECTION. WITHIN 1500 FLIGHT-CYCLES AFTER THE ORIGINAL ISSUE DATE OF SB. REPEAT INTERNAL 6000 FLIGHT-CYCLES.

Part: FITTING — CRACKED (FUSELAGE) · airframe 90,864 hrs · 11,144 cycles

FOUND CRACK ON THE HOLE OF SPLICE FITTING LT OUT SIDE AT 2598 BULKHEAD. MAINTENANCE REPAIRED THE CRACKED HOLD PER ER/A491613-14AD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,072 hrs · 10,928 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR MOUNT LIGHT AT 2L WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY DOOR MOUNT LIGHT AT 2L. SYSTEM OPERATION WAS NORMAL AFTER THE EMERGENCY DOOR MOUNT LIGHT WAS REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,072 hrs · 10,928 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR 4L DOOR MOUNT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE DOOR MOUNT LIGHT. SYSTEM OPERATION WAS NORMAL AFTER THE DOOR MOUNT LIGHT WAS REPLACED.

Part: FUSE — BLOWN (CABIN) · airframe 89,072 hrs · 10,928 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY SLIDE LIGHT AT UPPER RIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE WAS REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,782 hrs · 10,895 cycles

DURING HFEC INSPECTION FOUND 2 INCH LONG CRACK AT BX 2674.85 WL 305. FWD SIDE OF FRAME. CUT OUT DAMAGE, FABBED REPAIR OUT OF 2024T3 .050", TREATED AND INSTALLED PER SRM 51-70-11 FG 201 ID TAG INSTALLED PER PS 900 5-1 INSPECTION RII MTC COMPLETE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 88,594 hrs · 10,876 cycles

DURING MAINTENANCE VISIT, THE EMERGENCY PATH LIGHT AT GALLEY G3C LEFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTORS AT THE EMERGENCY LIGHT AT PATH HAVE DISCONNECTED. MAINTENANCE REPAIRED THE CONNECTORS. SYSTEM OPERATION WAS NORMAL AFTER THE CONNECTOR WAS REPAIRED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 88,594 hrs · 10,876 cycles

DURING MAINTENANCE VISIT, THE RIGHT OVERWING EMERGENCY LIGHTS NR 1 AND NR 2 POSITION WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE EMERGENCY LIGHT ABOVE DOOR 3L. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 3,351 hrs · 426 cycles

DURING A MX VISIT THE EMERGENCY ESCAPE PATH LIGHT ALONG SEATS 77-79 UPPER DECK WERE BRIGHT AND THEN SHUTOFF INDEPENDENTLY OF OTHERS AFTER APPROX 5 SECONDS. MX R & R BATTERY PACK IN POWER SUPPLY, M334. EMERGENCY LIGHTS TESTED OK IAW AMM 35-51-04/201. ACFT IS OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,373 hrs · 10,850 cycles

DURING A MX VISIT THE EMERGENCY ESCAPE PATH FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE ON SEAT 9J. MX REPLACED 2 FLOOR LIGHT ASSEMBLIES AND REPAIRED WIRING. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT1K) · airframe 87,922 hrs · 10,791 cycles

DURING LAYOVER CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT SEAT 1K & 27C INOPERATIVE. MX REPLACED THE LENS COVER AT 27C AND THE LIGHT ASSY AT 1K. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,871 hrs · 10,786 cycles

DURING A LINE CHECK. MX FOUND THE DOOR 5L MOST AFT EMERGENCY PATH LIGHT INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 87,055 hrs · 10,675 cycles

EMERGENCY EGRESS AISLE LIGHTING INOP, ROWS 10-12. CORRECTION: SECURED ELECTRICAL CONNECTION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 85,910 hrs · 10,533 cycles

DURING LINE CHECK MAINTENANCE FOUND 2 RIGHT EMERGENCY OVERWING LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 85,910 hrs · 10,533 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHT AT G3C MISSING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: FAN — MALFUNCTIONED (CREW REST) · airframe 85,325 hrs · 10,461 cycles

DURING CRUISE, F/A REPORTED A STRONG BURNING SMELL IN THE F/A BUNK. CREW FOLLOWED QRM AND SHUT OFF ALL RECIRC FANS. SMELL DISAPPEARED. MX FOUND THE CREW REST SUPPLY FAN CIRCUIT BREAKER OUT AND REPLACED THE SUPPLY FAN. OPS TEST WAS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 84,775 hrs · 10,395 cycles

F/A FOUND EMERGENCY PATH LIGHTS NEAR DOOR 2L LAV OUT OF POSITION. MAINTENANCE FOUND WIRES BROKEN AND LIGHT ASSEMBLY MISSING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND CAP. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,504 hrs · 10,363 cycles

DURING LAYOVER CHECK, MX FOUND 2 RT OVERWING EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE POWER SUPPLY AND BATTERY. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,943 hrs · 10,362 cycles

DURING LINE CHECK LT UPPER DECK DOOR BATTERY TEST FAILED. REPLACED POWER SUPPLY AND BATTERY. CHECKS OK ACFT RETURNED TO SERVICE.

Part: CARGO TRACK — CRACKED (BS 1862) · airframe 84,223 hrs · 10 cycles

DURING "L" CHECK FOUND CRACK IN RT OTBD CARGO TRACK AT BS 1862 RT. REPAIRED IAW SRM 53-00-52.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 84,223 hrs · 10,328 cycles

DURING "L" CHECK FOUND SHORT EDGE MARGIN ON SHEAR BEAM AT MAIN DECK CREW REST. REPAIRED IAW ERA 473036-14AD AND CARD 5300-01047-01B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,389 hrs · 12,530 cycles

DURING LEAK CHECK, FUSELAGE SKIN PANELS REQUIRED REPAIR BY BLENDING OUT WEAR DAMAGE AT THE VERTICAL STABILIZER SEAL INTERFACE IAW SRM.

Part: ROD END — BROKEN (L5 DOOR) · airframe 82,807 hrs · 10,159 cycles

DURING GROUND OPERATIONS FOUND DOOR 5L DIFFICULT TO OPEN. REPLACED BROKEN ROD END AND RIGGED DOOR PER AMM 52-11-09. DOOR FUNCTION TESTED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS)

DURING OVERNIGHT CHECK FOUND OVERHEAD EMERGENCY EXIT SIGN INOP AT UPPER DECK STATION 720. MX REMOVED AND REPLACED POWER SUPPLY, AND BATTERY. OPERATIONAL CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (K)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING OVERNIGHT, FOUND EMERGENCY LIGHTS INOP AT DOOR 3 RT. MX REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHTS AT DOOR, 5 RT INOPERATIVE. MX REMOVED AND REPLACED BATTERY AND POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (K)

Part: STIFFENER — MISMANUFACTURED (FUSELAGE)

DURING L-CHECK, WHILE ACCOMPLISHING SB 747-53-2481 MODIFICATION FOUND SHORT EDGE MARGIN IN THE OVERHEAD CREW REST STIFFENER AND WEB BETWEEN BS 2280-2295, RBL 54-86. REPAIRED IAW EA 63-215027. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 79,489 hrs · 9,748 cycles

DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHTS AT ZONE B RT INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

DURING OVER NIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS FROM ROW 51 TO 65 ABC INOPERATIVE. MAINTENANCE REPAIRED LOOSE WIRE AT PIN CONNECTION. OPS CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,629 hrs · 9,501 cycles

DURING OVERNIGHT CHECK, FOUND ZONE B RIGHT SIDE FLOOR PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACCESS PANEL — LEAKING (NR 2 RESER TANK) · airframe 77,329 hrs · 9,464 cycles

2 HOURS INTO FLIGHT, THE CREW REPORTED A FUEL QUANTITY PROBLEM. ABOUT 6,000 LBS TO 7,000 LBS OF FUEL WAS LOST BY THE FIRST POSITION REPORT. FUEL FLOW ON ENGINES WAS NORMAL AND NO REPORTS OF ANY TRANSFERRING. THE FUEL LOSS STABILIZED AND NO ADDITIONAL FUEL WAS LOST EN ROUTE. ON ARRIVAL AT THE GATE THEY FOUND NR 1 ENGINE PYLON MISSING PANEL (452FL) AND FUEL LEAKING FROM A HOLE IN THE NR 2 RESERVE TANK LOWER ACCESS PANEL (553DB). MAINTENANCE REMOVED AND REPLACED PYLON PANEL (452FL) AND FUEL ACCESS PANEL (553DB). OPERATIONAL CHECKED GOOD, NO LEAKS, AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,539 hrs · 9,358 cycles

DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS ON RIGHT SIDE AFT WING TO BODY FAIRING INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CRACKED (BS 460 S10R) · airframe 76,429 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AT BS 460. REPAIRED PER EA 63-212199.

Part: STRINGER — CRACKED (BS 500 S10L) · airframe 76,429 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACKS IN STRINGER 10L AT BS 500. REPAIRED PER EA 63-212202.

Part: STRINGER — CRACKED (BS 460 S10R) · airframe 76,429 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AT BS 460. REPAIRED PER EA 63-212199.

Part: STRINGER — CRACKED (BS 480 S10L) · airframe 76,429 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AND STRINGER 10L AT BS 480. REPAIRED PER EA 63-212201.

Part: STRINGER — CRACKED (BS 500 S10R) · airframe 76,429 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AT BS 500. REPAIRED PER EA 63-212202.

Part: STRINGER — CRACKED (BS 480 S10L) · airframe 76,429 hrs · 9,342 cycles

DURING M" CHECK FOUND CRACKS IN STRINGER 10L AT BS 480. REPAIRED PER EA 63-212201.

Part: SKIN — CRACKED (BS 1480) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1480 HOLE NR 11. REPAIRED PER EA 63-211896 SECT I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED EVERY 5,500 CYCLES THEREAFTER PER SECT II OF EA 63-211896.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 75,426 hrs · 9,211 cycles

DURING OVERNIGHT CHECK, FOUND E ZONE RIGHT SIDE EMERGENCY FLOOR PATH LIGHTS INOP. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 75,356 hrs · 9,202 cycles

DURING OVERNIGHT CHECK EMERGENCY FLOOR LIGHTING AT ROWS 21 THRU 31 LEFT WERE INOP. MAINTENANCE REMOVED AND REPLACED L-2 DOOR POWER SUPPLY, FUSE AND REPAIRED WIRE. OPERATIONALLY CHECKED GOOD. AIRCRAFT HAS RETURNED TO SERVICE.

Part: CONTROLLER — ODOR (GALLEY) · airframe 74,680 hrs · 9,115 cycles

DURING FLIGHT, FLIGHT ATTENDANT REPORTED OVEN 2-7 HAS AN ODOR OF BURNED WIRE. MAINTENANCE REPLACED OVEN CONTROLLER. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,206 hrs · 9,047 cycles

DURING OVERNIGHT CHECK, FOUND EMERGENCY PATH LIGHT AT ZONE C LEFT WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,948 hrs · 9,009 cycles

DURING OVERNIGHT CHECK, FOUND FORWARD UPPER DECK EMERGENCY PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY AND POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,497 hrs · 8,817 cycles

OVERNIGHT MAINTENANCE FOUND RT OVERWING 3 EA EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,497 hrs · 8,817 cycles

OVER NIGHT MAINTENANCE FOUND RT OVERWING 3 EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,160 hrs · 8,775 cycles

DURING OVERNIGHT CHECK, FOUND UPPER DECK EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,024 hrs · 8,098 cycles

DOOR R1 EMERGENCY MOUNTED LIGHT ASSEMBLY WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 61,626 hrs · 7,384 cycles

DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,170 hrs · 7,328 cycles

DURING LINE CHECK, FOUND UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REPAIRED LIGHTS. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,923 hrs · 7,298 cycles

DURING LINE CHECK, FOUND C-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: COFFEEMAKER — SMOKE (NR 1 GALLEY) · airframe 60,503 hrs · 7,246 cycles

DURING FLIGHT, THE NR 2 COFFEEMAKER IN THE NR 1 GALLEY STARTED SMOKING. PULLED CIRCUIT BREAKER AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED COFFEEMAKER. OPERATIONAL CHECK GOOD.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 59,923 hrs · 7,178 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C-31C. REPLACED EMERGENCY LIGHT SOCKET ASSEMBLY AT SEAT 21C. OPERATIONAL CHECK GOOD.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,923 hrs · 7,178 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C-31C. REPLACED EMERGENCY LIGHT SOCKET ASSEMBLY AT SEAT 21C. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,037 hrs · 7,070 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT AND BETWEEN DOOR 2R AND 3R. REPLACED THE POWER SUPPLY FOR THE LIGHTS ON THE LEFT SIDE OF THE AIRCRAFT AND REPLACED A LIGHT ASSEMBLY TO REPAIR THE LIGHTS BETWEEN DOOR 2R AND 3R. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (ROWS 21-31) · airframe 58,661 hrs · 7,029 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21 TO 31. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: LIGHT — SMOKE (CABIN) · airframe 56,729 hrs · 6,777 cycles

DURING FLIGHT, THE SMELL OF SMOKE WAS NOTICED FROM THE FOUR AREA LIGHTS OVER THE 2R JUMPSEAT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RELAMPED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,230 hrs · 6,468 cycles

DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON LEFT SIDE FROM ROWS 21-31 AND FROM RIGHT FLIGHT ATTENDANT STATION 2 RIGHT. RELAMPED EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 52,516 hrs · 6,241 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51KJH-66KH. RECONNECTED LIGHTS AT ROW 66. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 52,285 hrs · 6,211 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-60. RESEATED CONNECTOR AT ROW 51. OPERATIONAL CHECK GOOD.

Part: OVEN — OVERHEATED (GALLEY) · airframe 51,576 hrs · 6,119 cycles

DURING FLIGHT, THE LEFT OVEN IN THE NR 1 GALLEY OVERHEATED AND SMOKED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,249 hrs · 5,722 cycles

DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 35 AND AT ROW 52R. REPLACED LAMPS, OPERATIONAL CHECK NORMAL.

Part: WIRE — DISCONNECTED (GALLEY) · airframe 45,918 hrs · 5,432 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT THE NR 1 GALLEY RIGHT WALL AND INOPERATIVE BETWEEN 51-60R. RECONNECTED WIRING. OPERATIONAL CHECK OK.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 44,000 hrs · 5,212 cycles

DURING CLIMB, THE BODY LANDING GEAR DOOR DID NOT RETRACT. AIRCRAFT RETURNED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED THE PROXIMITY SWITCH ELECTRONIC UNIT. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (ROW 51-66)

DURING LINE CHECK (PEK), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-66. RECONNECTED ELECTRICAL CONNECTOR. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — LOOSE (DOOR 5L)

DOOR 5L GIRT BAR WAS FOUND LOOSE AND HANGING INTO SLIP STREAM AFTER TAKEOFF. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED DOOR, SLIDE AND REPAIRED SKIN DAMAGE, OPERATIONAL CHECK GOOD.

Part: SWITCH — OUT OF POSITION (CABIN)

DURING LINE CHECK, FOUND A AND B ZONE FLOOR PATH EMERGENCY LIGHTS ON THE RIGHT SIDE INOPERATIVE. PLACED EMERGENCY LIGHT SWITCH TO ARM POSITION AND ALLOWED BATTERY PACKS TO CHARGE, OPERATIONAL CHECK GOOD.

Part: WIRE — FAILED (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 24H - 31H. REPAIRED WIRE. OPERATIONAL CHECK GOOD.

Part: LIGHT — LOOSE (CABIN)

DURING LINE CHECK, FOUND E-ZONE AND ROW 31HK FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHT ASSEMBLIES, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND RIGHT E-ZONE FLOOR PATH EMERGENCY LIGHTS, EMERGENCY FLOOR PATH LIGHTS AT 3R JUMPSEAT, SEAT 31HJK, SEAT 43HJK, AND FROM ROWS 36HJK TO 41HJK INOPERATIVE. REPLACED POWER SUPPLY, BULBS, AND RECONNECTED ELECTRICAL PINS, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 54 TO 66. REPAIRED WIRE, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND UPPER DECK FLOOR PATH EMERGENCY LIGHTS ON THE RIGHT SIDE OF THE DOOR INOPERATIVE. RECONNECTED LIGHTS. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51HJK TO 59HJK. RECONNECTED CONNECTOR PIN, OPERATIONAL CHECK GOOD.

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND AFT RIGHT C-ZONE EMERGENCY FLOOR PATH LIGHTS AND DOOR 3L AND 3R EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRES, OPERATIONAL CHECK GOOD.

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND FLOOR EMERGENCY PATH LIGHTS INOPERATIVE FROM ROWS 51HJK TO 64HK. RECONNECTED WIRE, OPERATIONAL CHECK GOOD.

Part: LIGHTS — DISCONNECTED (CABIN)

DURING LINE CHECK, FOUND THE FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE FROM ROWS 2B-4B, 66C, AND FROM ROWS 51H-65H. RECONNECTED LIGHTS. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK (SEL), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51GHJ-65HJK. RECONNECTED CONNECTOR PIN. OPERATIONAL CHECK OK.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND THE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51R-61R. RECONNECTED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND THE RIGHT D-ZONE AND 66ABC EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. RECONNECTED ELECTRICAL PLUGS, OPERATIONAL CHECK GOOD.

Part: LIGHT — NOT CONNECTED (CABIN)

DURING LINE CHECK, FOUND FIRST CLASS LEFT FLOOR EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHT ASSEMBLY AT ROW 4, OPERATIONAL CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 980-1000)

DURING P-CHECK, FOUND CORROSION ON THE LBL 41 SEAT TRACK FROM BS 980 - 1000. REPAIRED TRACK (P/N 140U5617-13) PER EA 63-101910.

Part: FLOOR BEAM — CORRODED (BS 460-480)

DURING P-CHECK, FOUND CORROSION ON THE FLOOR BEAM UPPER CHORDS BS 460 FROM RBL 39 - 61 AND BS 480 FROM RBL 64 - 75. REPAIRED CHORDS PER EA 63-106559.

Part: FITTING — CORRODED (NR 3 TE FLAP)

DURING P-CHECK, FOUND CORROSION IN THE NR 3 FLAP TRACK OUTBOARD SIDE FITTING AT WBL 353. REPLACED FITTING.

Part: FITTING — CORRODED (LT TE FORE FLAP)

DURING P-CHECK, FOUND CORROSION IN THE LEFT WING OUTBOARD FORE FLAP, INBOARD SEQUENCE CARRIAGE ATTACH FITTING LONG BORE. REPLACED FITTING.

Part: PIN — DISCONNECTED (CABIN)

DURING LINE CHECK, FOUND THAT THE EMERGENCY FLOOR PROXIMITY LIGHTS WERE INOPERATIVE FOR SEATS 11 TO 14JK. RECONNECTED A PIN AT 11JK, CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND THE RIGHT EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROWS 35 TO 42. RECONNECTED CONNECTOR PIN AND OPERATIONAL CHECK GOOD.

Part: POWER PACK FUSE — FAILED (CABIN)

DURING LINE CHECK, TWO RIGHT AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED RESISTOR FUSE ON THE OVERWING EMERGENCY LIGHT POWER PACK, OPERATIONAL CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN)

DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS AT SEAT ROWS 35L TO 42L WERE FOUND INOPERATIVE. RECONNECTED THE CONNECTOR PIN IN FLOOR TRACK AT SEAT ROW 42L AND OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, THE RIGHT BODY FAIRING EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, THE AFT CABIN FLOOR MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRE AT SEAT ROW 65L AND OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (EXTERIOR)

DURING LINE CHECK, THE AFT TWO EXTERIOR EMERGENCY LIGHTS LOCATED ON THE RIGHT WING TO BODY FAIRING WERE FOUND INOPERATIVE. REPLACED THE EXTERIOR EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK OK.

Part: EEL PIN — LOOSE (CABIN)

TPE - DURING LINE CHECK, THE EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 35L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE PIN, OPERATIONAL CHECK OK.

Part: EEL CONNECTOR — LOOSE (CABIN)

TPE - DURING LINE CHECK, THE FLOOR EMERGENCY OATH LIGHTS BETWEEN ROWS 36L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE LIGHT ASSEMBLY PIN AND OPERATIONAL CHECK OK.

Part: COMPRESSSOR — STALLED (NR 3 ENGINE)

DURING ROTATION, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH HIGH EGT AND WAS SHUTDOWN. THE AIRCRAFT RETURNED TO TPE WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED AND THE ENGINE WAS REPLACED.

Part: BULKHEAD — CRACKED (FS 378.43)

DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE NR 3 PYLON AFT BULKHEAD 378.43. REMOVED DAMAGE AND REPAIRED PER EA 63-096770.