N105UA

Part: LIGHT — INOPERATIVE (SEAT 34C) · airframe 88,909 hrs · 10,202 cycles

DURING CABIN CHECK FOUND SEAT 34C EMERGENCY LIGHT NOT ILLUMINATE . EMERGENCY LIGHT REPLACED AND OPS CHECKED NORMAL.

Part: SKIN — DAMAGED · airframe 88,208 hrs · 10,131 cycles

LEFT LOWER SIDE OF L2 DOOR SCRATCHED WITH A PUNCTURE INTO ACFT SKIN. FOUND CRACK BS 720 TO 740 STRINGERS 26-27L AREA TEMP REPAIRED ACC SRM 53-00-01 PG102 ALLOW DAMA GE 2 CHART AREA D REV 97. CRACK STOP HOLES DRILLED OUT, RIVETS REPLACED BY FASTENER AND COVERED WITH HST. NDT INSPECTION PERF AC C 51-00-00 P6 PROC 4 REV 152

Part: SKIN — DAMAGED (L2 DOOR) · airframe 88,208 hrs · 10,131 cycles

LEFT LOWER SIDE OF L2 DOOR SCRATCHED WITH A PUNCTURE INTO THE SKIN BS 720 - 740 STRINGERS 26-27L FOUND A CRACK, TEMPORARY REPAIRED ACCOMPLISEHD IAW SRM 53-00-01 PG 102, REV 97. CRACK STOP HOLES DRILLED, RIVETS REPLACED. NDT INSPECTION PERF IAW 51-00-00 P6 PROC 4 REV 152

Part: LIGHT — BROKEN (CABIN) · airframe 88,105 hrs · 10,121 cycles

IAW A-CHECK, SEAT ELECTRIC LIGHT STRIP AT 33 HJK BROKEN. REPLACED ELECTRIC LIGHT STRIP IAW MM 33-51-12-201-C03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,758 hrs · 10,086 cycles

SEAT 40C EMER EXIT LIGHT INOPERATIVE. REPLACED EMER EXIT LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 87,758 hrs · 10,086 cycles

SEAT 54H - 59H EMER EXIT LIGHTS INOPERATIVE. SECURED CONNECTOR AT SEAT 54HJK. OPERATIONS CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,391 hrs · 10,046 cycles

PER A CHECK, DOOR SLIDE LIGHT AT DOOR 4R, INOPERATIVE. RECHARGED BATTERY, NOW WORKING. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,391 hrs · 10,046 cycles

PER A CHECK, AISLE EMER EXIT LIGHT AT SEAT 16, INOPERATIVE, RELAMPED. OPERATIONS CHECKED OK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 980, FLOORBEAM CHORD CORRODED, REPAIRED IAW ECRA 5310-06685 REV A. RII ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,582 hrs · 9,967 cycles

STATION 980, FLOORBEAM CHORD CORRODED. REPAIRED IAW ECRA 5310-06685 REV A. RII ACCOMPLISHED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

SKIN REPAIR WAS ACCOMPLISHED AT BS 180, BETWEEN 47L & 47R. REPAIRED IAW ECRA 5330-05494.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

A REPAIR WAS INSTALLED AT STATION 670 - 682, STRINGER 36R - 37R. REPAIRED IAW ECRA 5330-05501.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,582 hrs · 9,967 cycles

LEFT FUSELAGE SKIN AT WATER TANK OTBD VENT, BS 2090 CORROSION. REPAIRED IAW ECRA 5330-05485.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STRINGER 1120 RT TENSION TIE SLOPE SHEAR WEB FOUND CRACKED AT FWD INBD AREA. WEB REPAIRED IAW SRM 53-40-30 REP 3 & ECRA 5310-06666.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,582 hrs · 9,967 cycles

STATION 1300 - 1320, LBL 33, LONGITUDINAL FLOORBEAM FOUND CORROSION. REPAIRED IAW ECRA 5320-02656.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,582 hrs · 9,967 cycles

MAIN DECK STATION 1300 - 1320, RBL 33, LONGITUDINAL FLOORBEAM FOUND CORROSION. REPAIRED IAW ECRA 5320-02656.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

CRACK FOUND IN BS 2658 BULKHEAD WEB, IN AREA OF LBL 30 & WL 265. PERMANENT REPAIR ACCOMPLISHED IAW ECRA 5310-06671 REV A.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 86,582 hrs · 9,967 cycles

NUMBER 1 PYLON RT 452ER ACCESS DOOR SURROUND SKIN CRACK REPAIRED AT NAC STATION 228 IAW ECRA 5430-02065 REV A.

Part: STRINGER — DAMAGED (NR 3 PYLON) · airframe 86,582 hrs · 9,967 cycles

NUMBER 3 PYLON CAVITY LOWER STRINGER REPAIRED AT NAC STATION 363.53 TO 376.435. ACCOMPLISHED PERMANENT REPAIR IAW ECRA 5410-01817.

Part: LENS — CRACKED (EXIT SIGN) · airframe 86,582 hrs · 9,967 cycles

FOUND UPPER DECK LT & RT DOOR EXIT SIGN LENS CRACKED. REPLACED UPPER DECK LT & RT DOOR EXIT SIGN. OPERATIONS CHECKED OK IAW AMM 33-51-02 REV 177 & AMM 33-51-00 REV 177.

Part: LIGHT — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND DOOR 5 LAVATORY RT WALL MOUNTED EEL CABLE ASSEMBLY & LIGHT ASSEMBLY DAMAGED. REPLACED THE DOOR 5 RT WALL MOUNTED EEL CABLE ASSEMBLY & LIGHT. OPERATIONS CHECKED OK IAW AMM 33-51-12 REV 177 & AMM 33-51-00 REV 177.

Part: LIGHT — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND CABIN MAIN ENTRY DOOR 5 LT LAVATORY LT WALL MOUNTED EEL CABLES LIGHT ASSEMBLY DAMAGED. REPLACED CABIN MAIN ENTRY DOOR 5 LT LAVATORY LT WALL MOUNTED EEL CABLES LIGHT ASSEMBLY. OPERATIONS CHECKED OK IAW AMM 33- 51-12 REV 177 & AMM 33-51-00 REV 177.

Part: CABLE — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND UPPER DECK STAIR WALL MOUNTED AREA EEL COVER & CABLE ASSEMBLY DAMAGED. REPLACED UPPER DECK STAIR WALL MOUNTED AREA EEL COVER & CABLE ASSEMBLY. OPERATIONS CHECKED OK IAW AMM 33-5 1-12 REV 177 & AMM 33-51-00 REV 177.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

BS 1740 - 1960, STRINGER 46L-46R, FUSELAGE SKIN FOUND PITTING. PITTING WAS REMOVED IAW ECRA 5330-05477.

Part: CABLE — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND CABIN 1RT MAIN ENTRY DOOR GALLEY AREA, EEL MOUNTED CABLES & LIGHT ASSEMBLY DAMAGED. REPLACED CABIN 1 RT MAIN ENTRY DOOR RT GALLEY AREA, EEL MOUNTED CABLES & ASSEMBLY. OPERATIONS CHECKED OK IAW AMM 33- 51-12 REV 177 & AMM 33-51-00 REV 177.

Part: SIGN — BROKEN (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND TWO EACH EXIT SIGNS BROKEN NEAR G7 GALLEY AISLE. REPLACED TWO EACH EXIT SIGNS NEAR G7 GALLEY AISLE. OPERATIONS CHECKED OK IAW AMM 33-51-03 REV 177 & AMM 33-51-00 REV 177.

Part: CABLE — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND CABIN RT NR 4 DOOR AREA, G5 GALLEY EMER LT CABLE ASSEMBLY, 1 EA DAMAGED. REPLACED RT NR 4 DOOR AREA, G5 GALLEY EMER LT CABLE ASSEMBLY. OPERATIONS CHECKED OK IAW AMM 33-51-12 REV 177 & AMM 33-51-00 REV 177.

Part: CABLE — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND CABIN LT DOOR AREA, G5 GALLEY EMER LT CABLE ASSEMBLY, 2 EACH DAMAGED. REPLACED LT NR 4 DOOR AREA, G5 GALLEY EMER LT CABLE ASSEMBLY2 EACH. OPERATIONS CHECK OF AMM 33-51-12 REV 177 & 33-51-00 REV 177.

Part: CABLE — BROKEN (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND CABIN NR 1 DOOR GALLEY AREA, LT GALLEY MOUNTED EEL CABLES & LIGHT ASSEMBLY DAMAGED. REPLACED CABIN NR 1 DOOR GALLEY AREA, LT GALLEY MOUNTED EEL CABLES & LIGHT ASSEMBLY. OPERATIONS CHECKED OK IAW AMM 33-51-12 REV 177 & AMM 33-51-00 REV 177.

Part: CABLE — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

FOUND CABIN MAIN ENTRY DOOR 3 LT & RT LAVATORY WALL MOUNTED EEL CABLES & LIGHT ASSEMBLY DAMAGED. REPLACED THE MAIN ENTRY DOOR 3 AREA LAVATORY WALL MOUNTED EEL CABLES & LIGHT ASSEMBLY. OPERATIONS CHECKED OK IAW AMM 33-51-12 REV 177 & AMM 33-51-00 REV 177.

Part: FAN — FAILED (CARGO BAY) · airframe 83,676 hrs · 11,354 cycles

DUE TO DIVERSION, FOR SMOKE & ODOR IN THE CABIN, BULK CARGO VENTILATION FANS OVERHEATED & INOPERATIVE. REPLACED BULK CARGO VENT FAN IAW AMM 21-26-06. ACCOMPLISHED FIM TASK 21-00. TASK 808. NO SMELL OF ODOR OR SMOKE IN CABIN.

Part: SKIN — CRACKED (NR 4 PYLON) · airframe 86,582 hrs · 9,967 cycles

NUMBER 4 PLYON SKIN CRACKED AT 482ER ACCESS DOOR LOWER AFT CORNER. NR 4 PYLON SKIN CRACKED 482ER ACCESS DOOR LOWER AFT CORNER REPAIRED IAW ECRA 5430-020 57.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1220 FRAME DOUBLER, FOUND CRACK BETWEEN STRINGER 8L & 9L. STATION 1220 FRAME DOUBLER R & R IAW SRM 51-40-02 REV 94 & DWG 65B26275 REV C & REFER ECRA 5310-06670.

Part: LIGHT — DAMAGED (CABIN) · airframe 86,582 hrs · 9,967 cycles

SEVERAL SEATS FOUND WITH DAMAGED EMER LIGHTS 9J, 14B, 9B, 16B, 7B, 7J & 1K. REPLACED SEAT EMER LIGHTS AT POSITIONS & CARRIED OUT OPERATIONAL TEST, FOUND NORMAL IAW CMM 25-25-73 REV J.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,569 hrs · 7,734 cycles

PER A CHECK, SEAT 41 LT, EEL STRIP INOPERATIVE. REPLACED EEL STRIP. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,569 hrs · 7,734 cycles

PER A CHECK, SEAT 19 RT, EEL STRIP INOPERATIVE. REPLACED EEL STRIP. OPERATIONS CHECKED OK.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1220 LT TENSION TIE FWD & AFT CHANNEL, FOUND 4 EACH FASTENER HOLES CRACKED. ACCOMPLISHED EA 5310-05635 OP 19 REV A. REPAIRED STATION 1220 LT TENSION TIE FWD & AFT CHANNEL IAW SRM 53-40-30 REPAIR 1 FIG 201 REV 94.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1120 LT FRAME DOUBLER, FOUND 1 EACH FASTENER HOLE CRACKED. STATION 1200 LT DOUBLER R & R IAW DWG 65B26275 & PL 65B26275 REV D & ECRA 25310 06682.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1120 LT FWD CHANNEL, FOUND 1 EACH FASTENER HOLE CRACKED. STATION 1120 LT FWD CHANNEL REPAIRED IAW EA5310-05635 OP 19 & SRM 53-40-30 REV 94.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1180 RT TENSION TIE FWD & AFT CHANNEL, FOUND 2 EACH FASTENER HOLES CRACKED. ACCOMPLISHED EA 5310-05635 OP 19 REV A. REPAIRED STATION 1180 RT TENSION TIE FWD & AFT CHANNEL IAW SRM 53-40-30 REPAIR 1 FIG 201 REV 94.

Part: SENSE LINE — UNSECURE (LT ENGINE) · airframe 89,707 hrs · 25,416 cycles

LEFT EPR INDICATION WENT BLANK ON TAKEOFF ROLL, STBY IND READS 00. ALL OTHER ENG INDICATIONS NORMAL. EEC OPERATING IN N1 CONTROL MODE. AUTO THROTTLE CONTINUED TO FUNCTION NORMALLY. SECURED P2 FLEX LINE TO NOSE COWL FITTING AT APPROX 9 O CLOCK. RAN ENG AT IDLE POWER & BOTH EICAS & STBY INDICATIONS NORMAL. EPR RESPONDED TO THROTTLE MOVEMENT.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1180 LT TENSION TIE FWD CHANNEL, FOUND 1 EACH FASTENER HOLE ELONGATED. ACCOMPLISHED EA 5310-05635 OP 14 REV A REPAIRED STATION 1180 RT TENSION TIE FWD CHANNEL IAW SRM 53-40-30 REPAIR 2 FIG 201 REV 94.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1120 RT SIDE, TENSION TIE FRAME DOUBLER, FOUND ONE EACH FASTENER HOLE CRACKED. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5310-06681 PART 1 B.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1140 RT TENSION TIE FRAME DOUBLER, 2 EACH FASTENER HOLES CRACKED. STATION 1140 TENSION TIE DOUBLER REPLACED IAW SRM 53-40-07 REPAIR 2 REV 94 & DWG 65B01750 REV C.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1120 RT TENSION TIE FWD CHANNEL, 2 EACH FASTENER HOLES CRACKED & AFT CHANNEL FOUND EXISTING REPAIR. ACCOMPLISHED EA5310-05635 OP 19 REV A. REPAIR STATION 1120 RT TENSION TIE FWD CHANNEL IAW SMR 53-40-30 REPAIR 1 FIG 201.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1140 RT TENSION TIE FAIL SAFE CHORD, 2 EACH FASTENER HOLES CRACKED. ACCOMPLISHED REPAIR ON STATION 1140 RT TENSION TIE FAIL SAFE CHORD IAW SRM 53-40-07 REPAIR 10 FIG 201 REV 94.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

AD 2012-22-03 MAIN DECK L1 DOOR UPPER MAIN SILL, STATION 460, WEB CRACKED. INTERIM REPAIR CARRIED OUT IAW ECRA 5310-06665 PART 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

AD 2012-22-03 MAIN DECK L1 DOOR UPPER MAIN SILL STATION 460 WEB CRACKED. INTERIM REPAIR CARRIED OUT IAW ECRA 5310-06665 PART 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,582 hrs · 9,967 cycles

MAIN DECK ZONE C STATION 900, LBL 11 - RBL40 FLOORBEAM UPPER CHORD CORRODED. MAIN DECK ZONE C STATION 900, LBL 11 - RBL 40 FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-20-51 FIG 201 REPAIR REV 94.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,582 hrs · 9,967 cycles

MAIN DECK ZONE C STATION 900, LBL 11 TO RBL 40 FLOORBEAM UPPER CHORD CORRODED. FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-20-51 FIG 201 REPAIR REV 94.

Part: BATTERY — DISCHARGED (CABIN) · airframe 86,567 hrs · 9,965 cycles

SEATS 19H - 22H EMER EXIT LIGHTS DIM. LET BATTERIES CHARGE & OPERATIONS CHECKED OK IAW MM 33-51-00-501. LIGHT BRIGHTNESS NORMAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK SEAT TRACK FOUND CORRODED FROM STATION 1830 - 1870 LBL 33. REPLACED SEAT TRACK IAW DWG XPL 69B17959, SRM 51-40-05 & GMM 05-35-50 REV 5 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK SEAT TRACK FOUND CORRODED FROM STATION 1830 - 1870 LBL 11. REPLACED SEAT TRACK IAW DWG PXL 69B17959, SRM 51-40-05 & GMM 05-35-50 REV 55.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK SEAT TRACK FOUND CORRODED FROM STATION 1830 - 1870 RBL 11. REPLACED SEAT TRACK IAW DWG XPL 69B17959 REV A, SRM 51-40-05 REV 90 & GMM 05 -35-50 REV 55.

Part: LIGHT — INOPERATIVE · airframe 82,210 hrs · 9,565 cycles

FOUND EMER LIGHT INOPERATIVE AT DOOR 2R. REPLACED THE RT NR 2 DOOR SLIDE EMER LIGHT & TESTED IAW AMM 33-51-06 REV 169 FOUND PASSED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOORBEAM WEB FOUND CRACKED AT STATION 1660 RBL 33. REPAIRED IAW SRM 53-00-51 PG 201 REV 90.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

FLOORBEAM CORROSION AROUND SCREW HOLE. FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-00-51 FIG 101.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR STRAP CHANNEL FOUND CORROSION AT STATION 1700 RBL 11. REPAIRED IAW SRM 51-40-02 & 53-00-52 REPAIR 5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR INTERCOSTAL FOUND CORROSION AT STATION 1660 LBL 20. REPLACED IAW DWG 146U5620 & SRM 51-40-02 REV 90.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

CORROSION ON CABIN FLOOR PANEL SUPPORT AT STATION 1660 - 1680 RBL 40. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 5 REV 90.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR STRAP CHANNEL FOUND CORRODED AROUND SCREW HOLE AT STATION 1790 LBL 12. CORRODED FLOOR SUPPORT REPLACED IAW DWG 140U5287 REV W DWG 146U5251 REV F & SRM 51-4 0-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR INTERCOSTAL STATION 1660 - 1640 BL0 FOUND CORRODED. REPLACED IAW DWG 146U5620 & SRM 51-40-02 DRV 9 0.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR INTERCOSTAL STATION 1795 LBL 12 - RBL 8 FOUND CORRODED. CORRODED INTERCOSTAL REPLACED IAW DWG 146U5620 SHT 10 REV A & SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK SEAT TRACK FOUND CORROSION FROM STATION 1890 - 1910 LBL 33. REPAIRED IAW SRM 53-00-52 REPAIR 9 & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR STRAP CHANNEL FOUND CORROSION AROUND SCREW HOLE AT STATION 1795 RBL 11. CORROSION FLOOR SUPPORT REPLACED IAW DWG 140U5287 REV W & 146U5251 REV F & SRM 51-40 -02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR INTERCOSTAL FOUND CORRODED AT STATION 1700 - 1720 RBL 27.5. REPLACED IAW DWG 146U5253 SHT 28 & SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR INTERCOSTAL FOUND CORROSION AT STATION 1780 - 1795 LBL 5. FLOOR SUPPORT REPLACED IAW SRM 51-40-02 & DWG 146U5620 SH 10 REV A.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR INTERCOSTAL STATION 1740 - 1760 LBL 5.5 FOUND CORRODED. FLOOR SUPPORT REPLACED IAW SRM 51-40-02 & DWG 146U5620 SHT 10 REV A.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 82,210 hrs · 9,565 cycles

CABIN FLOOR PANEL UPPER CHORD FOUND CORROSION AT STATION 1660 LBL 30. CABIN FLOOR PANEL UPPER CHORD AT STATION 1660 LBL 30. REPAIRED IAW SRM 53-60-51 FIG 201 REPAIR 1. NDT INSP IAW 5946 & BSOPM 20-20-02. NO CRACKS FOUND.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MD FLOORBEAM FOUND CORROSION STATION 1700 RBL 19 TO 25. REPAIRED IAW SRM 53-60-51 REPAIR 1 FIG 2 01 REV 90. BSOPM 20-20-02 & CONDUCTIVITY TESTED IAW 5946 REV AA INSTEAD OF HFEC INSPECTION.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MID FLOOR STRAP CHANNEL FOUND CORROSION AT 1770 - 1800 RBL 40. REPAIR IAW SRM 53-00-52 FIG 201 RPE 5 & SRM 51-40-02. NDT INSP IAW PT6 51-00-00 PROC 23, NO CRACKS FOUND.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

CABIN FLOOR PANEL SUPPORT FOUND CORROSION AT STATION 1660 - 1680 LBL 40. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 5 & SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MID FLOOR INTERCOSTAL AT STATION 1795 RBL 11 FOUND CORROSION. REPLACED IAW DWG 140U5607 REV B & SRM 51-60-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

FLOORBEAM FOUND CORROSION AROUND SCREW HOLE. REPAIRED IAW SRM 53-60-51 RPR 1 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,210 hrs · 9,565 cycles

MAIN DECK FLOOR PANEL SUPPORT FROM STATION 1830 - 1890 LBL CORROSION. REPAIRED IAW SRM 53-00-52 REPAIR 5 & SRM 51-40-02. NDT INSP IAW PT6 51-00-0 0 PROC 23. NO CRACK FOUND.

Part: SCAVENGE PUMP — FAULTY (NR 1 ENGINE) · airframe 82,163 hrs · 9,561 cycles

NUMBER 1 ENG OIL TEMP AT TAKEOFF WAS 177 DEGREES & READING 28 QTS. MAINTAINED CLIMB UP TO 4000 FT. NR 1 ENG POWER WAS REDUCED & TEMP WENT TO 180 DEGREES & FLIGHT CREW SHUTDOWN ENG. REPLACED SCAVENGE PUMP IAW AMM 79-21-04-401, OIL TEMP THERMOCOUPLE IAW AMM79-34-01-401 & NR 3 SCAVENGE FLEX TUBE. ACCOMPLISHED HIGH POWER ENG RUN & REPORTED FINDINGS.

Part: SKIN — DENTED (FUSELAGE) · airframe 79,810 hrs · 9,329 cycles

ARC DENT WAS FOUND ON EXTERIOR FUSELAGE SKIN OF THE BULK CARGO DOOR FWD LWR CORNER STATION 1968 SIAW NDT PART6 51-00-00, NO CRACKS INDICATIONS.

Part: OXYGEN MASK — OUT OF ADJUST (COCKPIT) · airframe 79,524 hrs · 9,300 cycles

CAPTAIN`S 02 MASK, RESET & TESTED. SLIDE BAR STICKS & DIFFICULT TO RESET. ADJUSTED THE MASK TEST SLIDE & REINSTALLED O2 MASK.

Part: BRAKE — FIRE (NR 6) · airframe 79,187 hrs · 9,264 cycles

POSITION 6 BRAKE HAD FLAMED UPON SPOT IN. REPLACED BRAKE UNIT FOR NR 6. CHECKED AROUND BRAKE ASSEMBLY, NO DAMAGE FOUND. CLEANED UP, NO HYD LEAK FOUND.

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 79,063 hrs · 9,251 cycles

ENG 2 LOOP 2 DISPLAYED ON LOWER EICAS.

Part: UNKNOWN — MALFUNCTIONED (FIRE WARNING) · airframe 79,034 hrs · 9,247 cycles

ENG 2 LOOP A RESET CB P6 PNL, FIRE TEST IAW MAT, FAILED.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 79,021 hrs · 9,246 cycles

PRIOR TO PUSH CAPTAIN REPORTED STATIC ON HEADSET. FURTHER TO PTT 0212012 STATIC RETURNED ON CAPTS ACP. ACP REPLACED CHECKED AGAIN & NOW OPERATIONS OKAY.

Part: ACTUATOR — FAILED (LT BLG) · airframe 78,681 hrs · 9,213 cycles

BLG STEERING MALFUNCTION ON PUSHBACK FROM GATE. RT SIDE TURNS, LT SIDE FAILS TO MOVE. CHECKED HISTORY, NON FDE. FOUND MESSAGE 'LEFT BODY GEAR LEFT ACTUATOR LOCK SWITCHES DISAGREE'. REPLACED LT BLG, LT ACTUATOR IAW AMM. GROUND TEST & LEAK CHECK PASSED.

Part: DUCT — COLLAPSED (COCKPIT) · airframe 78,129 hrs · 9,155 cycles

OBSERVERS GASPER BEHIND FIRST OFFICER SEAT HAS NO AIRFLOW. FLEX HOSE ASSEMBLY BEHIND HAS COLLAPSED DUE TO SPIRAL SUPPORT SEPARATION BEHIND VENT. REPLACED FLEX DUCT AT FIRST OBSERVERS SEAT.

Part: DOOR — MISSING (CART ELEVATOR) · airframe 78,118 hrs · 9,154 cycles

UPPER DECK CART ELEVATOR DOOR DAMAGED. FOUND UPPER DECK CART ELEVATOR VIEW WINDOW MISSING. DEACTIVATED CART LIFT SYSTEM.

Part: LIGHT — INOPERATIVE (SEATS 54L - 59L) · airframe 78,028 hrs · 9,145 cycles

IAW A-CHECK, SEAT 54 RIGHT TO 59 RIGHT, SEAT EMERGENCY LIGHT INOPERATIVE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 78,028 hrs · 9,145 cycles

IAW A-CHECK, SEAT 54 RIGHT TO SEAT 59 RIGHT, SEAT EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTOR WHERE IT SPLITS OFF. SECURED FEEDER CONNECTOR.

Part: SKIN — DELAMINATED (LT WING) · airframe 77,699 hrs · 9,112 cycles

FOUND DELAMINATION OF LT WING, INBD UPPER FIXED T/E SKIN PANEL. TAP TESTED AND CONFIRMED DELAMINATION ENTIRE LENGTH OF PANEL DIAGRAM SENT TO TOMC OVER 50 PERCENT DELAM, IN ZONE 1 & 2 IAW SRM 51-70-02 DAMAGE BEYOND SRM LIMITS.

Part: STRUCTURE — TORN (GALLEY FLOOR) · airframe 77,627 hrs · 9,105 cycles

FOUND GALLEY 422 FLOOR EXTRUSION TORN. EXTRUSION REPLACED AND CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 77,627 hrs · 9,105 cycles

DURING CM 8401 CHECK, FOUND SEAT 53ABC TO 60ABC EMERGENCY LIGHT NOT ILLUMINATED. SEAT 60ABC EMERGENCY LIGHT CONNECTOR SECURED AND CHECKED NORMAL.

Part: LIGHT — BROKEN (SEAT ROW 56C) · airframe 77,364 hrs · 9,079 cycles

EMERGENCY LIGHT AT 56C BROKEN. NEW EMERGENCY LIGHT INSTALLED, OK.

Part: LIGHT — INOPERATIVE (SEAT 13AB) · airframe 77,161 hrs · 9,059 cycles

UPPER DECK SEAT 13AB, SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,161 hrs · 9,059 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT FEEDER CABLE, OPS CHECKED OK.

Part: FAN — FAILED (CABIN) · airframe 77,076 hrs · 9,050 cycles

CREW NOTICED AN ACRID ODOR AND HAZE IN THE CABIN NEAR DOOR 3RT. IT DISSIPATED AFTER A PERIOD OF TIME. CABIN CREW REPORTED BLUE HAZE WITH ELECTRICAL ODOR AT R2 & 3 DOORS. CHECKED FOR THE CAUSE OF ODOR PER MM. FOUND NO EVIDENCE. NO FAULTS FOUND. GASPER FAN MAKES A PULSATING NOISE WHILE PERFORMING SMOKE-FUMES CONDITIONAL INSPECTION, DEACTIVATED GASPER FAN, PULLED AND SAFETIED CIRCUIT BREAKER. REPLACED GASPER FAN ASSY PER MM, 21-24-01 PG 901, OPS CHECKED OKAY.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 76,782 hrs · 9,020 cycles

R5 LAVATORY SMOKE ALARM SOUNDED ON DESCENT. NO FIRE OR SMOKE NOTED FOUND LAVATORY SMOKE DETECTOR BAD. SMOKE DETECTOR REPLACED. OPS CHECKED OK IAW MM 26-13-00 PG 501.

Part: TIRE — FAILED (MLG) · airframe 76,759 hrs · 9,017 cycles

LEFT BODY GEAR OUTBOARD AFT TIRE BLOWN ON LANDING. REPLACED BOTH NR 11 AND NR 12 WHEEL REF MM.

Part: DRAIN LINE — CLOGGED (HUMIDIFIER) · airframe 76,715 hrs · 9,012 cycles

WATER LEAKING FROM BELLY UNDERNEATH FWD CARGO AREA. FOUND HUMIDIFIER WATER DRAIN RELIEF VALVE LINE ACCUMULATED WITH ICE BLOCKS ON BILGE AREA. SUSPECT AIRPLANE WATER DRAIN LINE BLOCKED, ALLOWING RELIEF VALVE TO OPEN AND OVERFLOW WATER THROUGH RELIEF LINE. REF MM 21-71-00 PG 5, ITEM 2(8) AND MM 21-71-09 PG 402, FIG A. DRAIN CLOGGED.

Part: LEG ASSY — UNDERSERVICED (NLG) · airframe 76,618 hrs · 9,003 cycles

NLG DID NOT RETRACT, RTFL DUE HISTORY OF NLG OLEO PRESSURE LOSS AND RETRACTION DAMAGE TO STA 340 BULKHEAD BRACKET AND ATTACHED HYDRAULIC LINE, CARRY OUT CONTROLLED NLG RETRACTION USING HYDRAULIC RIG TO DETERMINE POSSIBLE CAUSE OF DAMAGE. RETRACTION CATTIED AND FOUND DAMAGE CAUSED BY UNDER INFLATED OLEO LEG. FOLLOWING COMPLETION OF FACT FINDING GEAR SWING AND NOSE OLEO SERVICING COMPLETE GEAR SWING TO VERIFY RESULTS OF NOSE OLEO SERVICE TROUBLESHOOTING. GEAR SWING COMPLETED ALL FOUND SATIS

Part: OXYGEN BOTTLE — LOW PRESSURE (PAX) · airframe 76,573 hrs · 8,998 cycles

PAX OXYGEN PRESSURE LOW ON EICAS - 1590 PSI. REPLACED PAX OXYGEN BOTTLE AND INDICATED 1710 PSI. LEAK CHECKED OK.

Part: BATTERY — INOPERATIVE (DOOR) · airframe 76,509 hrs · 8,992 cycles

LEFT UPPER DECK DOOR BATTERY INOPERATIVE. CONFIRMED WEAK BATTERY FOR LEFT UPPER DECK DOOR. REPLACED BATTERY ASSY, OPS CHECKED OKAY.

Part: FAN — FAULTY (CABIN) · airframe 76,496 hrs · 8,989 cycles

UPPER RECIRC FAN STATUS MESSAGE. REPLACED UPPER FAN, OPS CHECK LEAK CHECK GOOD.

Part: SEAL — DAMAGED (L2 DOOR) · airframe 76,475 hrs · 8,987 cycles

L2 DOOR HAS A LOUD PRESSURE SQUEAL. DURING PRESSURIZATION CHECK FOUND FOUR SMALL LEAKS ON L2 DOOR. APPLIED SEALANT. DOOR SEAL HAS CHUNK MISSING IN UPPER FWD CORNER. PRESSURIZED AIRCRAFT TO 3.7, NO LEAKS NOTED,

Part: BOLT — SHEARED (WINDSHIELD WIPER) · airframe 76,250 hrs · 8,962 cycles

CAPTAIN'S WINDSHIELD WIPER NOT SEATED PROPERLY, VIBRATES. CHECKED AND FOUND WIPER ATTACHED BOLTS CORRODED AND SHEARED. NEW BOLTS INSTALLED IAW AMM. CAPTAINS WIPER OPERATION CHECKED NORMAL.

Part: LIFE VEST — MISSING (SEAT 33H) · airframe 76,236 hrs · 8,961 cycles

SEAT 33H MISSING LIFE VEST. INSTALLED VEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,236 hrs · 8,961 cycles

SEAT 9K EMEGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AT SEAT 9K AND OPS CHECKED PER 800008420 A CHECK WITH NO FAULTS NOTED.

Part: STRUT — DEFLATED (NLG) · airframe 75,847 hrs · 8,919 cycles

DEFLATED NLG STRUT AND DR-2L CAME IN CONTACT WITH ENTRY STAND. GRIT BAR ATTACH BRACKETS AND RODS DAMAGED. FOUND BROKEN LIFTER ASSY FOR GIRT BAR AT DOOR 2L. REPLACED LIFTERS. ALSO REPLACED RODS. ITEMS 17, 19 AND 21.

Part: PANEL — MISSING (NR 1 NACELLE) · airframe 75,764 hrs · 8,912 cycles

DURING ARRIVAL WAC FOUND NR 1 ENGINE OUTBD PANEL 452DL MISSING. IAW EC-RA AREA INSPECTED NO DAMAGED AND INTERIM REPAIR PERFORMED PANEL FABRICATED ECRA 5462-01002 REV A. REMOVED INTERIM REPAIR AND INSTALLED NEW PANEL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,750 hrs · 8,911 cycles

PER A CHECK, FOUND SEAT EEL FROM 45L TO 53 L, NOT WORKING. REPLACED BATTERY PACK AT DOOR 4L. TEST OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,750 hrs · 8,911 cycles

PER A CHECK, FOUND SEAT EEL FROM 45L TO 53L, NOT WORKING. ORDERED BATTERY, PCN 585-4495 OVER THRESHOLD OF DOOR 4L. LEFT HANGING OPEN FOR ACCESS TO BATTERY. OSTF# T1720, FROM DEN. REPLACED BATTERY PACK AT DOOR 4L. TEST OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,750 hrs · 8,911 cycles

PER A CHECK, ROW 43L TO 33L, SEAT EEL DIM. REPLACED BATTERY AT DOOR 3L TEST OKAY.

Part: LIGHT — UNSECURE (CABIN) · airframe 75,656 hrs · 8,901 cycles

EXIT LIGHT FWD LAV WALL 1R FALLING OFF. SECURED LIGHT FITTING.

Part: LIGHT — UNSECURE (CABIN) · airframe 75,656 hrs · 8,901 cycles

EXIT LIGHTS LAV 101 FALLING OFF. LIGHTS REFITTED.

Part: START VALVE — FAULTY (NR 2 ENGINE) · airframe 75,529 hrs · 8,889 cycles

CREW REPORT: NO ROTATION ON NR 2 ENGINE AT START WITH A CORRESPONDING NO START VLV & STARTER CUTOUT MSG. START VALVE OPEN LIGHT REMAINS ON WITH START VALVE CONFIRMED CLOSED. REPLACED START VALVE PER MM AND CHECKS OKAY.

Part: ACM — SEIZED (AC BAY) · airframe 75,529 hrs · 8,889 cycles

NOISE AND SMOKE NEAR AUX GALLEY JUST PRIOR TO LANDING. CREW REPORT ODOR SMELL, VIBRATION,ABNORMAL NOISE NEAR DOOR 2 GALLEY FLOOR AREA AND FOLLOW BY PACK NR 1 STATUS MSG. CHECK RECIR FAN, CHILLER, OVEN, GAL AND CABIN LIGHT, LAC NR 3 AND PACK NR 2, NR 3 ALL CHECK OK PER MM. FOUND PACK NR 1 ACM SEIZE REF TO DF653 FOR WORK DONE. REPLACED NR 1 ACM, DURING OPS CHECK, COMPRESSOR DISCHARGE TEMP HI. STATUS MSG "PACK 1" DISPLAYED. PACK IS LOCKED OUT WITH DF STICKER ON PACK SWITCH. REPLACED NR 1 PACK COMPRESSOR OUTLET TEMP SENSOR - T1612 -- OPERATIONAL CHECK OF NR 1 PACK SYSTEM OK.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY WALL EEL INOP: AFT WALL CROSS AISLE LEFT SIDE. REPAIRED DEFECTIVE CONNECTOR AND REPLACED EEL LAMP.

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY LIGHT INOP: CREW REST CEILING. REPLACED LAMPS AND REPAIRED ASSY LEN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY LIGHTT INOP: DOOR 5 LEFT SLIDE ILLUM. REPLACED BATTERY PACKS.

Part: LIGHT — UNSECURE (CABIN) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY WALL EEL INOP: MID GLY LEFT WALL. SECURED LOOSE EEL LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY LIGHT INOP: DOOR 5 RIGHT SLIDE ILLUM. REPLACED DEFECTIVE LAMPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY LIGHT INOP: SEAT 53 RIGHT EEL. REPLACED DEFECTIVE LAMPS.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,302 hrs · 8,867 cycles

EMERGENCY EXIT SIGN INOP: DOOR 4 RIGHT LWR EEL EXIT. REPLACED DEFECTIVE LAMPS.

Part: O-RING — LEAKING (OIL LINE) · airframe 75,226 hrs · 8,859 cycles

NR 1 ENGINE INFLT SHUTDOWN, RETURNED TO FIELD. FOUND LEAK AT JOINT OF LUBE AND SCAV PUMP AND DAMPENER. O-RING 'V' WORN AND SPLIT IN TWO. NEW O-RING FITTED AND AREA CLEANED. CARRIED OUT IAW JRH TEST NR 3. CREW REPORTED OIL PRESSURE AT IFS 65 AND DROPPING, MAX TEMP 152 DEG OIL UPLIFT 24 QTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,965 hrs · 8,830 cycles

DOOR 2L EMERGENCY SLIDE LIGHT INOP. REPLACED LAMP IN NEW LIGHT ASSY, INSTALLED ASSY OPS CHECK GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 74,965 hrs · 8,830 cycles

EMERGENCY LIGHT ALONG DOOR 5R GALLEY WALL INOP. FOUND DISCONNECTED. RECONNECTED UNDER SEAT 60 HJK. CHECKS NORMAL.

Part: COMPUTER — FAULTY (HF COMM) · airframe 74,951 hrs · 8,829 cycles

LEFT HF RADIO WILL NOT TRANSMIT. MSG 23039 & 23034 NOTED. LEFT HF TRANSCEIVER REPLACED & BITE PASS. BUT LEFT HF RECEIVE OK TRANSMIT FAIL ON ALL 3 ACP. AMU TRIED NO JOY. FIM 23-11 TASK836 FOLLOW ITEM B2 CCT CHECK OK. LEFT CMC SWAP WITH RIGHT CMC TRIED. LEFT HF WORK OK. CMC RETURNED TO ORIGINAL POSITION. FOLLOWED FIM 23-11-TASK 8 36, REPLACED LEFT CMC REF MM, ACCOMP LEFT HF CMC GROUND TEST. TEST PASSED.

Part: CIRCUIT CARD — FAULTY (FUEL SYSTEM) · airframe 74,938 hrs · 8,828 cycles

TOTAL INDICATED FUEL DROPPED 3700 POUNDS IN 10 MINUTES. FOUND CTR TANK DENSITOMETER VALUE FLUCTUATING FROM 6.8 TO 7.0 CAUSING THE FQTY TO FLUX BY APPROX 3K WITH 91K IN TANK. SUSPECT DENSITOMETER IS BAD. REPLACED DENSITOMETER IN CENTER FUEL TANK AND COMPLETED DRY BITE TEST. TEST PASSED NEED TO ACP CMCS GROUND TEST WITH 1412 GALS FUEL. COMPLETED CMCS GROUND TEST AFTER FUEL WAS ADDED. REPLACED A9 CARD PER MM, OP CHECKED GOOD PER MM.

Part: FAN — FAULTY (CABIN) · airframe 74,892 hrs · 8,824 cycles

LOWER LEFT RECIRCULATION FAN STATUS MESSAGE. PULLED BREAKER CLOSED MANUAL HUMIDIFIER VALVE AND POSITIONED HUMID SWITCH TO OFF AND PLACARD, PER MEL. RELAY 585-0949, FAN 563-9043. REMOVED & REPLACED LEFT LOWER RECIRCULATION FAN IAW AMM, OP CHECK GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (CABIN) · airframe 74,691 hrs · 8,806 cycles

CONTINUOUS CHIME FROM DOOR-3L LAV FORWARD UNIT. REPLACED IOEU ABOVE LAV. SYSTEM OPS OKAY.

Part: OVERHEAT LOOP — FAILED (NR 3 NACELLE) · airframe 74,177 hrs · 8,758 cycles

NR 3 ENGINE OVERHEAT LOOP 'A" FAULT. REPLACED FIRE OVERHEAT DETECTOR TS684 PER AMM.

Part: UNKNOWN — ODOR · airframe 74,166 hrs · 8,757 cycles

ELECTRICAL BURNING ODOR.

Part: RUB STRIP — DAMAGED (THRUST REVERSER) · airframe 74,098 hrs · 8,750 cycles

NR 3 ENGINE LEFT REVERSER REAR RUBSTRIP WORN AND CRACKED. SUPPLEMENTAL DATA UPDATE, REMOVED DAMAGED RUB STRIP ON NR 3 ENG LT REV HALF. COMPLETED REMOVAL OF NR 3 ENG REV UP TO STEP F.(5) PER MM. NEED TO CONTINUE FROM STEP F.(6) PER MM. CONTINUED FROM STEP 2F ( 6) PG 403 TO PG 407 OF MM 78-31-01. INSTALL NR 3 ENGINE THRUST REVERSER PER MM. STARTED LEFT NR 3 ENG. THRUST REVERSER HALF COMPLETED INSTALLATION PER MM TO TASK H NR 20 AT PAGE 416 CONT OF AMIS ITEM 0982087. CONTINUED INSTALLATION THRU STEP (27) P. NEED TO CONTINUE TO END. ACCOMPLISHED INSTALLATION FROM STEP 28 PG 418 TO END.

Part: HEAT SHIELD — MISSING (NR 1 OIL TANK) · airframe 73,663 hrs · 8,707 cycles

NR 1 ENGINE OIL TANK HEAT SHIELD MISSING UP TO THE FIRST CLAMP. LESS THEN 40 PERCENT. REMOVED DAMAGED HEATSHIELD. INSTALLED REPLACEMENT HEAT SHIELD.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 73,109 hrs · 8,653 cycles

EMERGENCY LIGHTS ILLUMINATED SEATS 19-22 RT SIDE. REPLACED BATTERY M6006, OPS NORMAL.

Part: WIRE — DAMAGED (APU) · airframe 72,911 hrs · 8,637 cycles

APU SHUT DOWN. FOUND WIRE FROM PIN A12 CONNECTOR DM7847CA TO CONNECTOR D95004 PIN E SHORT TO SHIELD. ALSO SEVERAL WIRES IN SAME HARNESS FOUND DAMAGED. RPL'D APU BAY HARNESS W7242 AND CLAMPS WDM AND MM. APU START, RUN, AND SHUTDOWN NORMAL.

Part: APU — SHUTDOWN (APU BAY) · airframe 72,890 hrs · 8,635 cycles

APU AUTO SHUTDOWN. NEED MORE TIME FOR T-S.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,593 hrs · 8,607 cycles

EMERGENCY LIGHT INOP FWD SILL DOOR 2 LEFT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,593 hrs · 8,607 cycles

EMERGENCY LIGHT INOP CEILING UPPER DECK ROW 15. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,593 hrs · 8,607 cycles

EMERGENCY LIGHT INOP CROSS AISLE DOOR 2R AND 2L. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,593 hrs · 8,607 cycles

EMERGENCY LIGHT AT SEAT 46 LEFT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,583 hrs · 8,606 cycles

D' ZONE SEATS A-G READING LIGHTS INOP. D-ZONE CTR SECTION ROWS 34-41DEFG INOP^18FEB SFO INF- :ZONES C+D CENTER COLUMN UNCONTROLLABLE. RPL'D LAC NR 2, NO HELP. P :FOUND DAMAGED CABLE NEAR 34D FROM FLOOR TO SEU. INSTALLED ANOTHER CABLE. PROBLEM STILL EXISTS. INSTALLED DATABASE, ALL FUNCTIONS WORK FINE.

Part: SHUTOFF VALVE — FAULTY (BLEED SYSTEM) · airframe 72,437 hrs · 8,594 cycles

RIGHT WING BLEED OVERHEAT, FLIGHT DIVERTED. NR 3 ENGINE BLEED DOES NOT INDICATE OFF ON SYNOPTIC PAGE WITH ALL FOUR ENGINES RUNNING AND NR 3 ENGINE BLEED SWITCH IN OFF POSITION. CMC MESSAGE 36272 BLEED 3 PRSOV SOLENOID FAILED OPEN. CYCLED SWITCH, AND ADVANCED THROTTLE, NO HELP. WITH NR 3 & NR 4 BLEED SWITCH OFF AND ISOLATION VALVE CLOSED, RIGHT WING DUCT PRESSURE INDICATES ZERO, BUT NR 3 BLEED VALVE SYNOPTIC IS AMBER AND IN TRANSIT. REPLACED NR 3 PRSOV PER MM. LEAK CHECKED OKAY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,413 hrs · 8,591 cycles

UPPER DECK FLOORBEAM STA 1020 LBL 6 UPPER T-CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SECTION OF T-CAP. SPLICED IN NEW SECTION PER SRM 53-10-07, FAA FORM 8100 -9, & ECRA 5310-05444. EVERY 3,000 CYCLES PERFORM DETAILED VISUAL INSP OF REPAIR AREA. AT EVERY 6,000 CYCLES PERFORM HFEC INSP OF REPAIR AREA. INITIAL RE-INSPECTIONS TO BEGIN AT PTC 20,000. CURRENT PTC IS 8591.^13FEB OPB INF- :MF8649 CREATED TO RE-CHECK EVERY 3000 CYCLES.

Part: CONTROL UNIT — FAILED (EMERGENCY LIGHTS) · airframe 72,141 hrs · 8,564 cycles

CONTROL PANEL FOR LIGHTS IN UPPER DECK GALLEY IS INOPERATIVE, ALSO UNABLE TO CONTROL FROM PANEL AT 1L. E-ZONE LIGHTS WERE INOPERATIVE BUT ABLE TO RECOVER WITH OVERRIDE AT DOOR 2R, ALSO FASTEN SEAT BELT AND NO SMOKING SIGNS INOP IN E-ZONE, AUDIO IN E-ZONE ALSO INOPERATIVE. UPPER DECK 3 OUT 4 RECESSED LIGHTS IN AFT PART OF CABIN ARE INOPERATIVE. REPLACED UPPER DECK CCTM PER MM. REPLACED CENTRAL MANAGEMENT UNIT PER MM, OPS NORMAL.

Part: CONTROLLER — FAULTY (INTERPHONE) · airframe 72,141 hrs · 8,564 cycles

UNABLE TO MAKE CALLS OUT FROM AFT CREW REST ON THE INTERPHONE, CAN RECEIVE CALLS THOUGH. REPLACED LAC#4 PER MM, SYSTEM NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,085 hrs · 8,558 cycles

EMERGENCY LIGHT INOPERATIVE. RELAMPED, OP CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 72,085 hrs · 8,558 cycles

EMERGENCY LIGHT ROW 41 LT INOPERATIVE. RESECURED CONNECTOR. OP CHECKED NORMAL.

Part: SEAL — DAMAGED (NLG STRUT) · airframe 71,896 hrs · 8,539 cycles

ON PUSH BACK SYD USED A SUPER TUG. NOISES HEARD IN NOSE GEAR DURING PUSH. GEAR DISAGREE CAUTION MESSAGE, (GEAR LEVER WAS NOT JAMMED IN THE OFF POSITION). ALSO HAD A GEAR DOOR ADVISORY MESSAGE, WENT AWAY. FOUND NOSE GEAR STRUT FLAT. REPLACED SEALS AND PACKING REF MM. ACCOMPLISHED LANDING WITH DEFLATED STRUT CHECK IAW MM 5-51-55. PERFORMED GEAR SWING, WHICH WAS SUCCESSFUL AND INSPECTION PERFORMED RII INSPECTION.

Part: LINE — CRACKED (SCAVANGE PUMP LT) · airframe 71,843 hrs · 8,531 cycles

UNWANTED FUEL TRANSFER INTO CENTER TANK. LT SCAVENGE LINE CRACKED. OLD LINE REMOVED. INSTALLED AND SAFETIED NEW LT SCAVENGE LINE.

Part: LIGHT — LOOSE (CABIN) · airframe 71,694 hrs · 8,514 cycles

EMERGENCY EXIT LIGHT LOOSE ON BULKHEAD. SECURED EMERGENCY LIGHT. OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,572 hrs · 8,503 cycles

DOOR 2R GALLEY LOWER SIDEWALL EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,572 hrs · 8,503 cycles

UPPER DECK CEILING 15AB EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,572 hrs · 8,503 cycles

UPPER DECK SEAT 16AB EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,572 hrs · 8,503 cycles

SEAT ROW 56ABC EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,572 hrs · 8,503 cycles

SEAT ROWS 45 TO 53 HJK EMERGENCY LIGHTS IS INOP. FOUNDED SHORT AT SEAT 49 HJK. RELAMPED EMERGENCY LIGHT AT 49 HJK. CHECKS NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 71,572 hrs · 8,503 cycles

DOOR 4L EXIT EMERGENCY SIGN IS INOPERATIVE. REPLACED DOOR 4L EXIT EMERGENCY SIGN, CHECKS NORMAL.

Part: WINDOW FRAME — LOOSE (CABIN) · airframe 71,514 hrs · 8,497 cycles

SEAT 45K, 51A, WINDOW FRAME LOOSE PER LOTECH. SECURED FRAME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY LIGHTS AT 37KJ INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY AT 37AB INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY AT SEAT 50 KJ INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY LIGHTS AT 6KJ INOP. RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENGY EXIT LIGHT AT 3 RIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY AT SEAT 45 KJ. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY LIGHT AT 47 SEAT KJ INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

LIGHT AT 8AB INOP. RELAMPED EMERGENCY LIGHT .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,120 hrs · 8,459 cycles

EMERGENCY AT 20AB INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,647 hrs · 8,409 cycles

EMERGENCY EXIT LIGHTS INOP DOOR 2 GALLEY AREA 2 EA LIGHTS LOWER WALL LEFT AND RIGHT. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,647 hrs · 8,409 cycles

EMERGENCY EXIT LIGHT INOP IN FLIGHT DECK CEILING. RELAMPED, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,647 hrs · 8,409 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 14. RELAMPED, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,647 hrs · 8,409 cycles

EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 13. RELAMPED, OPS CHECKS NORMAL.

Part: FAIRING — CRACKED (NR 4 PYLON) · airframe 69,684 hrs · 8,309 cycles

LARGE CRACK ON NR 4 ENGINE PYLON AT ATTACHMENT JOINTS. ACCOMPLISHED INSP OF NR 4 PYLON SAILTAIL FAIRING PER MM. ALL NORMAL, NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,601 hrs · 8,299 cycles

SEAT ROW 41HJK EMERGENCY LIGHT IS INOP. RELAMPED, CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,601 hrs · 8,299 cycles

RIGHT OVERWING EMERGENCY LAMP INOP. REPLACED OVERWING LIGHT ASSY. TESTED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,601 hrs · 8,299 cycles

SEAT ROW 55HJK EMERGENCY LIGHT IS INOP. RELAMPED, CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,601 hrs · 8,299 cycles

DOOR 1L FWD SILL EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, CHECKED NORMAL.

Part: LIGHT — UNSECURE (L1 DOOR) · airframe 69,026 hrs · 8,231 cycles

DOOR 1L EMERGENCY LIGHTS FELL OFF. SECURED EMERGENCY LIGHT FITTINGS, NOW NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 68,268 hrs · 8,147 cycles

22H SEAT MOUNTED EEL LIGHT MISSING. REPLACED EEL LIGHT AT 22H. OPS OKAY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 67,827 hrs · 8,096 cycles

FOUND AFT EMERGENCY WALL LIGHT WIRE BROKEN BY R5 DOOR WHEN PULLING UP FLOOR MAT FOR REPLACEMENT. REPLACED AND SECURED AFT WALL EMERGENCY LIGHT. CHECKS NORMAL.

Part: BATTERY — FAULTY (APU) · airframe 67,698 hrs · 8,080 cycles

APU AUTO SHUTDOWN AND UNABLE TO APPLY POWER TO AIRCRAFT. FOLLOWING APU BATTERY AND APU BATTERY CHARGER REPLACEMENT PROBLEM PERSISTS. AFTER TROUBLESHOOTING MAIN AIRCRAFT BATTERY REPLACED AND POWER RESTORED TO AIRCRAFT. GROUND POWER AND APU POWER OPERATION NORMAL. BATTERY BORROWED PART FITTED. PART NR 4579, SERIAL NR 066068 MAIN BATTERY POSITION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,583 hrs · 8,068 cycles

CROSSAISLE EMERGENCY LIGHT LT INOP, BETWEEN DOORS 2LT AND 2RT, RT MOST LT. REPLACED LAMP, CHECKED OK.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 67,583 hrs · 8,068 cycles

NR2 LT MAIN ENTRY DOOR GIRT BAR ENGAGEMENT IS POOR AND ARM-DISARM HANDLE IS NOT SMOOTH. FOUND SKIRT PULLING ON GIRT MAKING INHIBITING GIRT BAR MOVEMENT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,583 hrs · 8,068 cycles

'E' ZONE CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. CHECKS OK.

Part: GIRT BAR — OBSTRUCTED (L5 DOOR) · airframe 67,583 hrs · 8,068 cycles

NR5 LT MAIN ENTRY DOOR GIRT BAR TO FLOOR FITTING ENGAGEMENT IS POOR WHEN SLIDE IS ARMED. FOUND SLIDE SKIRT INHIBITING GIRT BAR MOVEMENT. ADJUSTED SKIRT AND ALL OPS ARE NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,228 hrs · 8,027 cycles

BURNING ODOR IN COCKPIT, CREW FOLLOWED FM PROCEDURES. SECURED EQUIP COOLING FANS. ODOR SEEMED TO SUBSIDE.

Part: FAN — FAULTY (CABIN) · airframe 67,229 hrs · 8,027 cycles

ACFT EXPERIENCED SMOKE IN COCKPIT. SECURED EQUIP COOLING FANS. ODOR SEEMED TO SUBSIDE. REPLACED EQUIP COOLING EXHAUST VALVE DUE TO BURNING ODOR IN COCKPIT. TEST PASSED WITH NO MSGS. ALSO GALLEY FAN STATUS MSGS. SYS NORMAL WITH NO ODOR.

Part: LIGHT — UNSECURE (CABIN) · airframe 67,118 hrs · 8,016 cycles

EMERGENCY PATH LIGHT LOOSE AT CORNER OF LAC 104 AT LOCATION 2L. SECURED EMERGENCY PATH LIGHT ON CORNER OF LAV 104, OPS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,001 hrs · 8,003 cycles

FLOOR EMERGENCY LIGHT BETWEEN L2 DOOR AND R2 DOOR INOPERATIVE. RELAMPED.

Part: LIGHT — INOPERATIVE (SEAT 23C) · airframe 67,019 hrs · 8,005 cycles

SEAT 23C EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AND CHECK OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,001 hrs · 8,003 cycles

EMERGENCY LIGHT SEAT 23ABC INOP. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,001 hrs · 8,003 cycles

AFT GALLEY FLOOR EMERGENCY LIGHT LEFT SIDE IS INOP. RELAMPED.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,001 hrs · 8,003 cycles

RT OVERWING EMERGENCY LIGHT AFT TWO INOP. REPLACED FUSE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,001 hrs · 8,003 cycles

EMERGENCY LIGHT SEAT 45ABC INOP. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,001 hrs · 8,003 cycles

EMERGENCY CEILING LIGHT SEAT 52 RT SIDE INOP. RELAMPED, OPS CHECKED OKAY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 66,492 hrs · 7,939 cycles

EMERGENCY LIGHT ALONG LAV BETWEEN L3 DOOR AND R3 DOOR INOP. RESECURED LAMP CONNECTOR. OPS CHECKED NORMAL.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,492 hrs · 7,939 cycles

EMERGENCY LIGHT 3R LAV SIDEWALL INOPERATIVE. REPLACED EMERGENCY LIGHT CABLE. OPS CK NORMAL.

Part: FIRE LOOP — FALSE ACTIVATION (APU BAY) · airframe 66,178 hrs · 7,908 cycles

STATUS MSG- APU FIRE LOOP A AND B. FOUND CMC MSG 26036 AND 26037 INTERMITTENT FAULTS. ACCESSED APU COMPARTMENT & VISUALLY INSPECTED WHICH HAS NO SIGN OF REAL FIRE OCCURRED & HARDWARE DAMAGED. APU CANNOT BE USED DUE TO FIRE BOTTLE HAS BEEN DISCHARGED, REMOVED TERMINALS FROM BOTH T1814 & T1815 DET LOOPS TO PREVENT FALSE WARNING. TERMINALS ISOLATED & SECURED INDIVIDUALLY. SUSPECT UPPER APU SUPPORT LOOP ASSY AT FAULT. 585-4620 LOB'D. FIRE BOTTLE REPLACED ON DF27. SWAPPED APU LOOP A&B FIRE CARD NO HELP. CHECKED WIRE FROM D63P AND D67P TO ALL TERMINAL, GROUND TO WIRES AND WIRES TO WIRES, ALL CHECKED GOOD.

Part: CHILLER — INOPERATIVE (GALLEY) · airframe 66,178 hrs · 7,908 cycles

CHILLER C01 UPPER DECK GALLEY INOPERATIVE. CYCLED CHILLER C-B, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,926 hrs · 7,881 cycles

CTR AND RT CROSS AISLE EMERGENCY LIGHTS BETWEEN DOORS 2L AND 2R INOPERATIVE. RELAMPED. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (SEAT ROW 57L) · airframe 65,345 hrs · 7,816 cycles

EMERGENCY EXIT LIGHT INOP, SEAT ROW 57 LT. REPLACED LIGHT ASSY, OPS CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,345 hrs · 7,816 cycles

EMERGENCY EXIT LIGHT INOP. UPPER DECK CEILING ROW 14. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,345 hrs · 7,816 cycles

EMERGENCY EXIT LIGHT INOP. UPPER DECK CEILING JUST FWD OF ROW 13. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,345 hrs · 7,816 cycles

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

Part: CONNECTOR — SATURATED (EMERGENCY LIGHT) · airframe 65,345 hrs · 7,816 cycles

EMERGENCY EXIT LIGHTS VERY DIM SEAT ROWS 45 THRU 53 LT, DOOR 4 LT FWD EXIT SIGN, DOOR 4 RT AFT EXIT SIGN, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LT, AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. FOUND WATER PUDDLING IN GALLEY AREA UNDER GALLEY MAT AT EMERGENCY CONNECTOR SHORTING LIGHTS. DRIED AREA OF WATER, EMERGENCY LIGHTS OPS. CK NORMAL AT PRESENT TIME.

Part: LIGHT — INOPERATIVE (SEAT 53R) · airframe 65,345 hrs · 7,816 cycles

EMERGENCY EXIT LIGHT INOP. SEAT ROW 53, RT. REPLACED LIGHT ASSY. OPS CK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,345 hrs · 7,816 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,345 hrs · 7,816 cycles

EMERGENCY EXIT LIGHT INOP, UPPER DECK CEILING ROW 15. RELAMPED. OPS NORMAL.

Part: ELEMENT — CONTAMINATED (COFFEE WARMER) · airframe 64,985 hrs · 7,778 cycles

H21 THE COFFEE WARMER SMELLS LIKE SOMETHING IS BURNING WHEN TURNED ON. FOUND MELTED PLASTIC ON ELEMENT, CLEANED.

Part: WIRE — BROKEN (CABIN) · airframe 64,758 hrs · 7,751 cycles

EMERGENCY LIGHT ROW 53 RT INOPERATIVE. REPAIRED BROKEN WIRE IN CONNECTOR, OP CHECKS GOOD ON GROUND.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 64,758 hrs · 7,751 cycles

DOOR 5 LT MAIN GALLEY FWD AND SIDE WALL EMERGENCY LIGHT INOPERATIVE. REPLACED EEL FEEDER. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,758 hrs · 7,751 cycles

DOOR 1 RT EMERGENCY BUSSEL LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT UNIT. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,758 hrs · 7,751 cycles

DOOR 1 LT EMERGENCY BUSSEL LIGHT INOPERATIVE. RELAMPED, OP CHECKS GOOD.

Part: LAMP — INOPERATIVE (SMOKE DETECTOR) · airframe 64,758 hrs · 7,751 cycles

EQUIP COOLING SENSOR TEST FAILS. FAULTS SMOKE DETECTOR M7931. RELAMPED M7931.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 64,668 hrs · 7,741 cycles

BURNING ELECT SMELL ABOVE M41 CIRCUIT BREAKERS IN THAT AREA PULLED AND SMELL CLEARED. REPLACED M41 COFFEEMAKER, OPS CK OK. M42 COFFEEMAKER WAS ALSO REPLACED AS A PRECAUTION. UNABLE TO DUPLICATE ANY BURNED ELECTRICAL SMELLS IN THIS AREA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,176 hrs · 7,685 cycles

DOOR 2L & 2R CROSS AISLE EMERGENCY LIGHT INOPERATIVE. RELAMPED, OP CHECKS GOOD.

Part: FEEDER CABLE — FAULTY (CABIN) · airframe 64,176 hrs · 7,685 cycles

ROWS 45-54L SEAT, DOOR 4R AFT DOOR 4L FWD, MAIN GALLEY FWD AND LEFT EEL LIGHTS INOP. COMMON PROBLEM ON 84XX AIRCRAFT. REPLACED EEL FEED IN CABLE. REPLACED EEL JUMPER STRIP AND REPLACED GALLEY SIDE WALL EMERGENCY EEL LIGHT STRIP. OP CHECKS GOOD ON GROUND CHECKS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,176 hrs · 7,685 cycles

AFT MOST GALLEY L CROSS AISLE EEL LIGHT INOPERATIVE. REPLACED AFT GALLEY CROSS AISLE EMERGENCY EEL LIGHT STRIP, OP CHECKS GOOD ON GROUND.

Part: CONNECTOR — MISSING (CABIN) · airframe 64,176 hrs · 7,685 cycles

SEAT 53R EEL LIGHT INOPERATIVE. REPLACED MISSING PLASTIC CONNECTOR UNDER SEAT, OP CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,596 hrs · 7,619 cycles

EMERGENCY EXIT LIGHT INOP. DOOR 5 RT BUSSLE LIGHT. RELAMPED. OPS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,596 hrs · 7,619 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 EEL ACROSS DOOR 4 LT, AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA. FOUND AND REPAIRED WET AND CORRODED EMERGENCY LIGHT AND LAMPS ASSEMBLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,596 hrs · 7,619 cycles

UPPER DECK EMERGENCY EXIT LIGHT INOP. AT DOOR AFT CEILING LIGHT. RELAMPED. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,596 hrs · 7,619 cycles

EMERGENCY EXIT LIGHT INOP. DOOR 5 LT CEILING ENTRY LIGHT. RELAMPED. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,596 hrs · 7,619 cycles

UPPER DECK EMERGENCY EXIT LIGHT INOP, JUST FWD OF SEAT 17 CEILING LIGHT. RELAMPED. OPS NORMAL.

Part: TORQUE BOX — CRACKED (BS 860) · airframe 63,567 hrs · 7,615 cycles

FWD CARGO PIT STA. 860 BETWEEN LBL 5.5 AND RBL 5.5 HAS SUSPECTED CRACK ALONG FWD EDGE OF CTR GUIDE ON TORQUE BOX WEB. REMOVED TORQUE BOX ACCESS PNL AND STARTED TO REMOVE FASTENERS FOR REPAIR. REMOVED TORQUE BOX DAMAGED UPPER WEB SECTION. MFG REPLACEMENT SKIN AND SPLICE DOUBLER IAW SRM FOR TYPICAL WEB REPAIRS. ALL COMPONENTS NEED TO BE REINSTALLED. BEGAN INSTALLING DBLR AND ROLLER TRAY ASSY. COMPLETED INSTALLATION OF FASTENERS IN ROLLER TRAYS AND INSTALLED PANEL.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 63,517 hrs · 7,608 cycles

DOOR 1R UPPER BEAM CRACKED AT THE NR 9 NUT PLATE ATTACH HOLE. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE, FILLER & CLIP.

Part: BEAM — CRACKED (R5 DOOR) · airframe 63,517 hrs · 7,608 cycles

DOOR 5R UPPER BEAM CRACKED AT THE 8TH & 10TH FASTENER HOLE FROM FWD END. MAJOR REPAIR ACCOMPLISHED: INSTALLED REINFORCING REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,517 hrs · 7,608 cycles

FOUND AFT CARGO DOOR CUT OUT UPPER FWD CORNER FUSELAGE SKIN CRACKED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED: INSTALLED 5 PIECE REINFORCING REPAIR.

Part: BEAM — CRACKED (L2 DOOR FRAME) · airframe 63,517 hrs · 7,608 cycles

DOOR 2L UPPER BEAM CRACKED AT 8TH, 9TH, & 10TH FASTENER HOLES FROM FWD END. MAJOR REPAIR ACCOMPLISHED: INSTALLED REINFORCING REPAIR. ACPD ON KAL SHOP DOCUMENTS.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 63,517 hrs · 7,608 cycles

DOOR 1L UPPER BEAM CRACKED AT THE NR 8,9,10,& 11 FASTENER HOLES FROM FWD END. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR ANGLE, FILLER AND CLIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,517 hrs · 7,608 cycles

EMERGENCY LIGHT ABOVE DOOR 3R INOP. RELAMPED, OPS CK OK.

Part: REFLECTOR — BROKEN (EMERGENCY LIGHT) · airframe 63,517 hrs · 7,608 cycles

EMERGENCY LIGHT REFLECTOR HSG BROKEN AT UPPER DECK CEILING FWD CTR EMERGENCY LIGHT. REPLACED LIGHT ASSY, OP CHECK OK.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 63,517 hrs · 7,608 cycles

EMERGENCY LIGHT BATTERY WILL NOT HOLD CHARGE AT DOOR 1L. REPLACED BATTERY, EMERGENCY LIGHT OPS CHECKED OK.

Part: FRAME — CRACKED (BS 1265) · airframe 63,517 hrs · 7,608 cycles

FOUND LT BS 1265 FRAME WEB & INTERCOSTAL CRACKED AT THE NR 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED: REPLACED THE FRAME CHORD, FRAME WEB, INTERCOSTAL WEB & CHORD.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK RT BS 1120, TENSION TIE AFT SIDE CRACKED APPROX 12 IN. FROM FRAME. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA OF TENSION TIE, INSTALLED REINFORCING REPAIR.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK LT BS 1220, TENSION TIE CRACKED AT 2 FASTENER HOLES ON FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA OF TENSION TIE, INSTALLED REINFORCING REPAIR.

Part: FRAME — DAMAGED (BS 1180) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK RT BS 1180, FRAME CRACKED AT 1 FASTENER HOLE AT TENSION TIE ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED REPAIR.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK LT BS 1140, FAIL SAFE CHORD CRACKED AT 1 FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND INSTALLED REPAIR ANGLES.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK LT BS1160, TENSION TIE CRACKED AT 5 FASTENER HOLES, 4 FWD & 1 AFT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF TENSION TIE, INSTALLED REINFORCING REPAIR.

Part: FRAME — CRACKED (BS 1160) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK LT BS 1160, FRAME CRACKED AT 1 FASTENER HOLE AT TENSION TIE ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED REPAIR.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK BS 1120 LT SIDE TENSION TIE FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF TENSION TIE, INSTALLED REINFORCING REPAIR.

Part: FRAME — CRACKED (BS 1140) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK RT BS 1140, FRAME CRACKED AT 3 FASTENER HOLES AT TENSION TIE ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED REPAIR.

Part: FRAME — CRACKED (BS 1160) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK RT BS 1160, FRAME CRACKED AT 1 FASTENER HOLE AT TENSION TIE ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED REPAIR.

Part: FRAME — CRACKED (BS 1180) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK LT BS 1180, FRAME CRACKED AT 2 FASTENER HOLES AT TENSION TIE ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED REPAIR.

Part: FRAME — CRACKED (BS 1120) · airframe 63,517 hrs · 7,608 cycles

UPPER DECK LT BS 1120, FRAME CRACKED AT 3 FASTENER HOLES AT TENSION TIE ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND INSTALLED REPAIR.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 63,517 hrs · 7,608 cycles

EMERGENCY LIGHTS FLOOD LIGHT ON DOOR 5L INOPERATIVE. CLEANED CONNECTION & TERMINAL LUG AT T-213, LIGHT OP CHECK OK.

Part: WIRE — CHAFED (FIRE LOOP) · airframe 62,371 hrs · 7,484 cycles

THE 'ENG 4 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 4 FIRE LOOP-B FIRE OR FAULT OUTPUT. CREW COMMENTS: DISPLAYED FOR 3 HOURS THEN WENT AWAY. FOUND WIRE CHAFING ON LWR FIRE LOOP WIRE AND SENSOR LOOPS CHAFING ON SUPPORT STATIONS. REPAIRED WIRES, OP CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,464 hrs · 7,375 cycles

EMERGENCY EXIT LIGHT INOP DOOR 4 LEFT BUSSLE LIGHT. RELAMPED EEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,464 hrs · 7,375 cycles

EMERGENCY EXIT LIGHT INOP AT TOP OF STAIRS UPPER DECK CEILING. RELAMPED LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,464 hrs · 7,375 cycles

EMERGENCY EXIT EEL LIGHT INOP, LOWER WALL ACROSS LAV 101. REPLACED EEL ASSY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 61,464 hrs · 7,375 cycles

EMERGENCY EXIT EEL LIGHTS INOP SEAT ROWS 45 THRU 53 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. FOUND LOOSE CONNECTION AND WATER DAMAGE. CLEANED AREA AND RECONNECTED, OP CHECKED NORMAL.

Part: PANEL — CRACKED (PYLON) · airframe 60,902 hrs · 7,312 cycles

FOUND CRACKS IN 2 DIFFERENT PYLON PANELS, 1 PANEL HAS 15 INCH CRACK AND OTHER PANEL HAS 2 CRACKS 4 INCHES LONG. OLD PANELS ARE OFF. WILL REPAIR PANEL WITH SMALL CRACKS. P/N 311U4536-3. REPLACED PANEL.

Part: BULB — DISCONNECTED (DOOR 5L) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHT INOP. AT DOOR 5 LEFT LOWER WALL EMERGENCY LIGHT. RECONNECTED AND SECURED EMERGENCY LIGHT STRIP. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHT INOP. AT DOOR 2 RIGHT CEILING ENTRY. RELAMPED. OPS. NORMAL.

Part: LIGHT — DISCONNECTED (L5 DOOR) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 5 LT LOWER WALL. RECONNECTED AND SECURED EMERGENCY LIGHT STRIP. OPS CHECK GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHTS VERY DIM ACROSS DOOR 4 LT LOWER WALL EMERGENCY LIGHT, LOWER WALL GALLEY AREA, DOOR 4 LT FWD. EMERGENCY EXIT LIGHT SIGN, DOOR 4 RT AFT EXIT EMERGENCY LIGHT SIGN AND SEAT ROWS 45 LT THRU 53 LT. REPLACED POWER FEEDER CABLE. ALL LIGHTS OPS CK NORMAL.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHTS VERY DIM ACROSS DOOR 4 LEFT LOWER WALL EMERGENCY LIGHT, LOWER WALL GALLEY AREA, DOOR 4 LEFT FWD. EXIT EEL SIGN, DOOR 4 RIGHT AFT EXIT LIGHTSIGN AND SEAT ROWS 45 LT THRU 53 LT. REPLACED POWER FEEDER CABLE. ALL LIGHTS OPS. CK. NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHT INOP AT DOOR 2 RT CEILING ENTRY. RELAMPED,OPS NORMAL.

Part: LAMP — INOPERATIVE (ROW 13) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHT INOP. UPPER DECK ROW 13 CEILING. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,804 hrs · 7,175 cycles

EMERGENCY EXIT LIGHT INOP. UPPER DECK ROW 13 CEILING. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,651 hrs · 7,160 cycles

ESCAPE SLIDE INDICATOR LIGHTS INOP, DOOR 4R & 5L. RELAMPED, OPS CHECK OK.

Part: LIGHT — BROKEN (CABIN) · airframe 59,651 hrs · 7,160 cycles

EMERGENCY LIGHT BROKEN, ROW 48LT & 58RT. REPLACED LIGHTS, OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 59,651 hrs · 7,160 cycles

EMERGENCY EXIT LIGHTS INOP, DOOR 1L, 2L, 2R, 4L CEILING ARE A, & UPPER DECK LT DOORWAY. REPLACED BATTERY PACKS AT ALL LOCATIONS. LIGHTS CHECK NORMAL.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 59,651 hrs · 7,160 cycles

SEAT TRACK SCALLOP FLANGE BROKEN, BS 1152 LBL 98.58. SPLICED IN NEW SECTION OF TRACK FROM BS 1128.5 TO 1170.5.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,232 hrs · 7,111 cycles

FLOOR EEL INOP, RT SIDE LAV 112. REPLACED BATTERY. OP CHECKS OKAY.

Part: LAMP — INOPERATIVE (CABIN) · airframe 59,232 hrs · 7,111 cycles

EMERGENCY LIGHT INOP, CEILING ROW 13. REPLACED EMERGENCY LAMP. OP CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,232 hrs · 7,111 cycles

SEAT EEL INOP, ROWS 32, 33, 34 RT. REPLACED BATTERY. OP CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,232 hrs · 7,111 cycles

EMERGENCY EXIT SIGN INOP, DOOR 3 RT AFT SIDE. REPLACED BATTERY. OP CHECKS OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,232 hrs · 7,111 cycles

FLOOR EEL INOP, BETWEEN MID LAVS 111 & 112. REPLACED BATTERY. OPS OKAY.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 59,012 hrs · 7,090 cycles

MAIN DECK SEAT 5F EMERGENCY EXIT MISSING COVER PLATE. EEL STRIP REPLACED AND OPS CHECK OK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 58,661 hrs · 7,053 cycles

SEAT ROW 55 HJK - 60 HJK EMERGENCY LIGHTS INOP. FOUND UNDER SEAT CONNECTOR DISCONNECTED. RECONNECTED. OP CHECKS NORMAL.

Part: CABLE — DEFECTIVE (EMERGENCY LIGHT) · airframe 58,661 hrs · 7,053 cycles

SEAT 3J FWD AND AFT EMERGENCY LIGHT IS INOP REPLACED BAD UNDERSEAT CABLE. CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,661 hrs · 7,053 cycles

SEAT 4F FWD EMERGENCY LIGHT IS INOP. LAMP FOUND DEFECTIVE. REPLACED LAMP. OP CHECKS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 58,297 hrs · 7,016 cycles

EEL LIGHT AT 5A FOUND BROKEN. *S/D* FOUND LIGHT BROKEN. REPLACED EEL ASSY, OPS OKAY.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,565 hrs · 6,941 cycles

EEL INOP:ALL RT FIRST CLASS IB AND OB SEATS. SUSPECT WIRE HARNESS FAULTY. REPLACED HARNESS AT 1J, SECURED ALL DISTURBED AREAS. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY LIGHTS INOP, SEAT 5A AFT SECTION. FOUND FAULTY LIGHT ASSY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY LIGHT INOP:DR5L DOOR BUSTLE LT. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY LIGHTS INOP, ALL D ZONE RT SEATS. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK OP CHECKED GOOD. AC OK FOR SAERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY EXIT SIGN INOP:DR3R EEL EXIT SIGN FWD OF DOOR. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY LIGHT INOP, FWD GALLEY RT WALL. SECURED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY LIGHT INOP, SEAT 48 LT. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,565 hrs · 6,941 cycles

WALL EEL INOP:AFT GALLEY FWD LWR WALL ACROSS FROM DOOR 4L. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY LIGHTS INOP:ALL C ZONE CEILING LT AND RT SIDES. FOUND FAULTY BATTERY. REPLACED BATTERY PACK OP CHECKED GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,565 hrs · 6,941 cycles

EMERG LT INOP:CEILING BETWEEN MID LAVS. SUSPECT BATTERY ASSEMBLY. REPLACED BATTERY ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 57,565 hrs · 6,941 cycles

EMERGENCY EXIT SIGN INOP, R1 DOOR EMERGENCY LIGHT EXIT SIGN AFT OF DOOR. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,565 hrs · 6,941 cycles

EEL INOP:SEAT 3A AFT SECTION. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 57,565 hrs · 6,941 cycles

WALL EEL INOP:LWR WALL BETWEEN MID LAVS. FOUND LIGHT ASSEMBLY AND FEEDER CABLE DAMAGED. REPLACED LIGHT ASSEMBLY AND FEEDER CABLE OP CHECKED GOOD. AC OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 57,271 hrs · 6,915 cycles

EMERGENCY LIGHT STRIP ON STAIRWELL AND AISLE IN UPPER DECK COMES ON AND OFF. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: STRIP — BROKEN (CABIN) · airframe 57,199 hrs · 6,907 cycles

AFT EMERGENCY LIGHT STRIP BROKEN OFF HALF AT SEAT 5F.

Part: SMOKE WARNING — FALSE ACTIVATION · airframe 57,094 hrs · 6,895 cycles

'SMOKE DR 5 REST' EICAS CAUTION MESSAGE DISPLAYED. ACCOMPLISHED CREW REST SMOKE DETECTION SYSTEM TEST PER MM 26-14-20 ALL 4 DETECTORS CHECK NORMAL ALSO ACCOMPLISHED GROUND TEST OF RECIRCULATION FANS TEST PASSED. TRIED TO DUPLICATE PROBLEM SYSTEM ALL TEST PASSED. AC OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,991 hrs · 6,880 cycles

DR 4 LT EMERGENCY SILL LIGHTS INOP. REPLACED BATTERY ON CHARGER. OP CK NORMAL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 56,991 hrs · 6,880 cycles

EMERGENCY LIGHT ROW 1J AFT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROW 3A) · airframe 56,991 hrs · 6,880 cycles

EMERGENCY LIGHT ROW 3A AFT INOP. REPLACED LIGHT CABLE. OP CHECKS OK.

Part: LIGHT — INOPERATIVE (ROW 32ABC) · airframe 56,991 hrs · 6,880 cycles

EMERGENCY LIGHT ROW 32ABC INOP. REPLACED CABLE. OP CK NORMAL.

Part: LIGHT — INOPERATIVE (ROW 4A) · airframe 56,991 hrs · 6,880 cycles

EMERGENCY LIGHT ROW 4A AFT INOP. RELAMPED, OP CHECKS OK.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,991 hrs · 6,880 cycles

EMERGENCY LIGHT ROW 61 RH INOP. REPLACED EEL CABLE. OP CK NORMAL.

Part: O-RING — LEAKING (L2 SLIDE BOTTLE) · airframe 56,511 hrs · 6,830 cycles

OVERWATER CHECK FOUND DOOR 2L SLIDE BOTTLE PRESSURE OUT OF GREEN BAND. FOUND FAULTY O-RING. REPLACED SLIDE RAFT ASSEMBLY. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,041 hrs · 6,782 cycles

SEAT 49A SEAT EEL LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,041 hrs · 6,782 cycles

SEAT 3A AFT EEL LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,041 hrs · 6,782 cycles

SEVERAL EEL LAMPS INOP NEAR DOOR 4L. REPLACED BATTERY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,041 hrs · 6,782 cycles

EEL CEILING LIGHT NEAR SEAT 23A INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,575 hrs · 6,735 cycles

SEAT 3A FWD EMERGENCY LIGHT IS INOP. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,575 hrs · 6,735 cycles

DOOR 3R FWD SILL & DOOR 4L BOTH SILLS EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,575 hrs · 6,735 cycles

DOOR 4 LEFT CEILING EMERGENCY LIGHT IS INOP. RELAMPED.

Part: WIRE — FAILED (NR 3 FIRE LOOP) · airframe 55,175 hrs · 6,697 cycles

F-C REPORTED FIRE LOOP A 3 ENG. REPLACED WIRES W3506-503 AND 506 REF SWP 20-30-11, CHECKED ROUTING OF WIRES ON AC 8174 ENG 3-4, AC 8105 ENG NR 3, WIRES ROUTED DIFFERENTLY, REROUTED REPLACED WITH CORRECT CLAMPS. ACCOMP TEST REF MM26-11-00, OPS CHECK PASSED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 55,105 hrs · 6,683 cycles

WALL EEL INOP LEFT SIDE AFT GALLEY. SECURED LOOSE CONTACT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,105 hrs · 6,683 cycles

EMERGENCY LIGHT INOPERATIVE DOOR 5L SLIDE ILLUM. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,105 hrs · 6,683 cycles

EEL LIGHTS INOP AT SEATS 39 ABC & 56 HJK. RELAMPED.

Part: SWITCH — DIRTY (FIRE DETECTION) · airframe 55,105 hrs · 6,683 cycles

FIRE EXT SQUIB TEST PANEL FAILS TO ILLUM ENG 1 WITH TEST SW 1. SUSPECT DIRTY SWITCH CONTACTS. CLEANED CONTACTS OPS CHECK NORMAL. AC OK FOR SERVICE.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,105 hrs · 6,683 cycles

EMERGENCY LIGHT INOPERATIVE SEAT 3J FWD SECTION. REPAIRED BROKEN WIRE ASSEMBLY

Part: CONNECTOR — INOPERATIVE (ROWS 3A) · airframe 54,670 hrs · 6,637 cycles

EMERGENCY LIGHT ROWS 3A AFT, 3J FWD & 61CB ARE INOP. RESECURED CONNECTOR.

Part: LIGHT — UNSECURE (ROW 35ABC) · airframe 54,670 hrs · 6,637 cycles

EMERGENCY LIGHT ROW 35ABC INOP. RESECURED LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,670 hrs · 6,637 cycles

EMERGENCY LIGHT SEAT 5E FWD INOP. 11-01-07 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,450 hrs · 6,614 cycles

THE 5A EXIT LIGHT INOP. *S/D* REPLACED EXIT EEL LIGHT AT DOOR 5A. OP CHECKS OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,247 hrs · 6,590 cycles

EEL AT AFT GALLEY XAISLE INOP. 10-5-07 RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,247 hrs · 6,590 cycles

EMERGENCY CEILING LIGHTS INOP AT ROW 13 & ROW 32L. 10-5-07 RELAMPED EMERGENCY CEILING LIGHTS IN BOTH SEAT POSITIONS. OP CHECKS NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,247 hrs · 6,590 cycles

EEL AT 39 ABC INOPERATIVE. 10-05-07 RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,339 hrs · 6,496 cycles

SEATS 3J & 32ABC EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LAMP ASSY. CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,339 hrs · 6,496 cycles

AFT CREW REST CEILING EMERGENCY LIGHT IS INOP. REPLACED ASSY. CHECKS OKAY.

Part: LIGHT — INOPERATIVE (SEAT 3A) · airframe 53,095 hrs · 6,468 cycles

SEAT 3A EMERGENCY LIGHT STRIP INOPERATIVE. *S/D* REPLACED LIGHT ASSY AND OP CHECKS NORMAL.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 53,074 hrs · 6,465 cycles

EMERGENCY LIGHTS BY SEATS 35-44 HJ TURN ON UNCOMMANDED. *S/D* REPLACED POWER SUPPLY AT DOOR 3R.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 52,793 hrs · 6,440 cycles

MAIN CABIN EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY. TESTED EMERGENCY LIGHTS SEVERAL TIMES, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,367 hrs · 6,395 cycles

WALL EEL INOP: UPPER DECK LT WALL ACROSS FROM LAV 124. FOUND INOP LAMP ASSY. REMOVED LAMP, PARTS IN AREA. LAMP ON AOG.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 52,367 hrs · 6,395 cycles

EMERGENCY LIGHT INOP COCKPIT CEILING. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,367 hrs · 6,395 cycles

WALL EEL INOP: UPPER DECK LT WALL ACROSS FROM LAV 124. REPLACED EEL LITE ASSY. CHECKED OK

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,367 hrs · 6,395 cycles

EEL INOP: SEAT 32 LEFT. REPLACED LAMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,937 hrs · 6,344 cycles

EMERGENCY LIGHTS FROM ROWS 22GH TO 26GH & 35HJK TO 44HJK ARE INOPERATIVE. BATTERY PACK INOPERATIVE. REPLACED BATTERY PACKS IN BOTH POSITIONS. ALL EEL OP CHECK NORMALLY.

Part: LAMP — INOPERATIVE (ROW 32ABC) · airframe 51,937 hrs · 6,344 cycles

EMERGENCY LIGHT ROW32 ABC INOPERATIVE. RELAMPED EMERGENCY LIGHTS. OP CHECKED NORMALLY.

Part: LAMP — INOPERATIVE (DOOR SLIDE 5L) · airframe 51,937 hrs · 6,344 cycles

EMERGENCY DOOR SLIDE LIGHT 5L & 5R INOP. RELAMPED SLIDE LIGHT, BOTH POSITIONS. BOTH OP CHECK NORMALLY.

Part: UNKNOWN — UNKNOWN (FUEL SYS) · airframe 51,937 hrs · 6,344 cycles

UNWANTED FUEL TRANSFER. FOUND NR 3 AFT OVERRIDE PUMP DISCHARGE CHECK VALVE MISSING PIN FOR DRAIN HOLE. REQ PER MM 28-31-11 ITEM 1D. REPLACED CK VLV WITH PIN INSTALLED. PROBLEM PERSISTED. PERFORMED TANK ENTRY & TROUBLESHOOTING. FINALLY REPLACED DENSITOMETER, COMPENSATOR & TANK PROBE. RETURNED TO SERVICE WITH NO RECURRENCE OF UNWANTED FUEL TRANSFER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,442 hrs · 6,286 cycles

FOUND DOOR 1L EMERGENCY SLIDE ILLUMINATION LIGHT INOP. RELAMPED, OP CHECKED OK.

Part: LIGHT — INOPERATIVE (C ZONE AT LAV 11) · airframe 51,442 hrs · 6,286 cycles

FOUND EEL INOP, C ZONE AT LAV 110 SIDEWALL. FOUND EEL STRIP BROKEN. REPLACED EEL STRIP, OP CHECKED OK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,442 hrs · 6,286 cycles

FOUND EEL'S INOPERATIVE AT SEATS 3A-AFT, 4A-AFT, 5A-AFT, 5F-AFT. RELAMPED EACH SEAT POSITION, ALL OP CHECKED OK FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 51,442 hrs · 6,286 cycles

FOUND DENT AND SCRATCH BELOW AND FWD OF R5 DOOR ON BLUE STRIPE. DENT MEASURES 3 INCHES BY 4 INCHES BY .125 INCH DEEP, AREA BURNISHED AND INSPECTED FOR CRACKS, NONE NOTED. CONT OF AMIS ITEM 53120 -AREA BLENDED AND HFEC ACP REF UA-EVA-60656, INSTALLED DOUBLER REPAIR. SET UP REPEAT FOLLOW-UP INSP. SUSPECT IMPACT BY GROUND EQUIPMENT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,442 hrs · 6,286 cycles

RIGHT OVERWING AFT EMERGENCY ILLUM LIGHT INOPERATIVE. RELAMPED, OP CHECKED OK.

Part: FIRE LOOP — FALSE INDICATION (CARGO BAY) · airframe 51,321 hrs · 6,270 cycles

FLIGHT DIVERTED DUE TO FWD CARGO FIRE WARNING. SUPPLEMENTAL DATA UPDATE FWD CARGO RED FIRE WARNING ILLUM DURING CRUISE. ARMED & DISCHARGED FIRE BOTTLES. ACFT DIVERTED TO APW WESTERN SAMOA. NO EVIDENCE OF FIRE DISCOVERED. IDENTIFIED FAULTS IN BOTH A & B LOOPS. REPLACED BOTH SMOKE DETECTORS. OP CHECKED OK. RETURNED TO SERVICE. SUSPECT MOISTURE CONDENSED IN SENSING TUBES LEADING TO FALSE SMOKE READINGS. CARGO INCLUDED BEES & DRY-ICE COOLED CARGO.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,728 hrs · 5,871 cycles

EMERGENCY LIGHT INOP DOOR 3L BUSTLE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,728 hrs · 5,871 cycles

EEL INOP AT SEATS 5J FWD AND CREW REST STAIRS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 47,728 hrs · 5,871 cycles

EMERGENCY LIGHT INOP DOOR 2R BUSTLE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 47,728 hrs · 5,871 cycles

WALL EEL LIGHTS BETWEEN MID-LAVS INOPERATIVE. REPLACED CABLE & CONNECTORS. SUSPECT DAMAGE FROM DRINK CARTS & CABLES NOT PROPERLY POSITIONED NEXT TO SEAT TRACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,249 hrs · 5,817 cycles

BOTH SEAT EMERGENCY LIGHTS INOP AT 2J.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 45,459 hrs · 5,613 cycles

EEL INOP AT SEAT 22 LEFT BOTH SECTIONS AND SEAT 3J FWD SECTION. REPAIRED CONNECTOR AT SEAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,459 hrs · 5,613 cycles

EEL INOP ON WALL BETWEEN LAVS 111 & 112. REPAIRED FEEDER WIRE ON FLOOR.

Part: SLIDE — FAILED

SLIDE SUFFERED DAMAGE DURING DEPLOYMENT TO INFLATABLE, ABRASIONS ON EXPOSED HOSES AND 3 HOSES FAILED HYDRO TESTING. LEAKING AT THE WELDED AREA ON TUBING. SLIDE DAMAGED DUE TO IMPROPER HANDING AFTER DEPLOYMENT. REPAIRED INFLATABLE HOLES AND REPLACED HOSES.

Part: HYDRAULIC SYSTEM — LEAKING (NR 2) · airframe 42,450 hrs · 5,255 cycles

FLIGHT LOST ALL QUANTITY IN THE NR 2 HYD SYS. LOSS OF FLUID DUE TO CHAFED THRUST REVERSER RETURN HYDRAULIC LINE. MAINTENANCE ALSO NOTED LEAK AT PUMP FLANGE. LEAK AT PUMP FLANGE POSSIBLY DUE TO PUMP FAILURE DUE TO SUBSEQUENT FLUID STARVATION. SYDMM ACCOMPLISHED PERMASWAGE REPAIR OF DAMAGED LINE. NO ADDITIONAL HYD PUMP INFORMATION AVAILABLE FROM OSV AT THIS TIME.

Part: SLIDE — TORN (CABIN)

DEPLOYED SLIDE, FOUND TEAR IN FLOOR. SLIDE LEAKS IN INFLATABLE AND AT ASPIRATOR FLAPS. SLIDE SENT TO OEM (GOODRICH) FOR REPAIR. REPLACED GIRT AND ASPIRATOR.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 40,759 hrs · 5,045 cycles

ABORTED TAKEOFF AT 160 KTS DUE TO SURGE IN NR 2 ENGINE. DETERMINED SURGE DUE TO A BIRD INGESTION. ALL SURGE CHECKS PER AMM ACCOMPLISHED AND NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,468 hrs · 5,009 cycles

AFT PIT FRAME 1920 T-CHORD EXFOLIATED AT RBL 57. MAJOR REPAIR ACCOMPLISHED. REPLACED CORRODED T-CHORD SECTION.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 40,468 hrs · 5,009 cycles

AFT PRESSURE BULKHEAD (STA 2360) HAS 2 EACH DENTS JUST BELOW WL 274.87 AT RBL 45 AND RBL 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED 2 EACH REPAIR DOUBLERS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,468 hrs · 5,009 cycles

BULK CARGO PIT FRAME STA 1920 UPPER CHORD AFT FLANGE IS EXFOLIATED UNDER NUT PLATES AT LBL 20, RBL 3, 6 & 12, LBL 20, RBL 3, RBL 6, RBL 12. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW CHORD SECTION.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,465 hrs · 5,006 cycles

UPPER T-CHORD ON THE FRAME AT BS 1780, APPROX RBL 27 HAS A DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE, SHIMS, INTERCOSTAL WEB & FILLERS.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,465 hrs · 5,006 cycles

UPPER T-CHORD ON THE FRAME AT BS 720, APPROX RBL 15 HAS A DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLES, SHIMS AND FILLER.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 40,465 hrs · 5,006 cycles

AFT CARGO COMPARTMENT FLOORBEAM AT STA 1820 BL0 DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CHORD REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,465 hrs · 5,006 cycles

UPPER DECK FLOORBEAM WEB IS DENTED AND CRACKED STA 380 RBL 14. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED WEB, TAPER SHIM & STIFFENER REPAIRS.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,465 hrs · 5,006 cycles

RIGHT NR 5 MED, FWD FRAME INBOARD WEB CRACKED AT LOWER DOOR HINGE AREA. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,465 hrs · 5,006 cycles

LEFT NR 5 MED, FWD FRAME INBOARD WEB IS CRACKED AT LOWER DOOR HINGE AREA. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: CONTROL UNIT — OVERHEATED (PAX O2 SYSTEM) · airframe 39,107 hrs · 4,826 cycles

PASSENGER EMERGENCY OXYGEN SYSTEM PROBLEM. PASSENGER OXYGEN QUANTITY AT 800 PSI AND DECREASING. *SUPPLEMENTAL DATA UPDATE* A VOLTAGE AVERAGING UNIT INTERNALLY OVERHEATED AND BURNED THE CIRCUIT BOARD, CAUSING FAILURE OF THE PASSENGER INDICATION SYSTEM. THE UNIT WAS REPLACED.

Part: VANE — BROKEN (NR 2 ENGINE) · airframe 38,222 hrs · 4,695 cycles

NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. READINGS DROPPED AFTER A/C REACHED ALTITUDE. THE 7TH STAGE COMPRESSOR BLADE FAILED AT THE ROOT AND DAMAGED THE HPC, CAUSING THE ENGINE TO SURGE. T HE BLADE FAILURE WAS CAUSED BY THE VANE ARM ON THE 6TH STAGE VSV BEING BROKEN AT THE 6 O'CLOCK POSITION. THE ENGINE WAS REMOVED AND OVERHAULED.

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT) · airframe 34,571 hrs · 4,182 cycles

RETURNED TO THE FIELD DUE TO LANDING GEAR HANDLE WOULD NOT RAISE PAST LEVER LOCK AFTER TAKEOFF. NO EICAS MESSAGES APPEARED.

Part: LIGHT — MISWIRED (CABIN) · airframe 33,621 hrs · 4,030 cycles

LEFT HAND FUSELAGE EMERGENCY LIGHT AT MOST FORWARD POSITION INOP. FOUND LIGHT ASSEMBLY WIRED WRONG (POWER TO GROUND). REWIRED LIGHT ASSEMBLY AND REPLACED FUSE. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,621 hrs · 4,030 cycles

EMERGENCY LIGHT INOP AFT UPPER DECK CEILING BETWEEN SLIDE DOORS. REPLACED LAMP, CHECKED OK.

Part: ENGINE — FAILED (NR 2)

APPROXIMATELY THREE HOURS AFTER TAKEOFF, NR 2 ENGINE OIL QUANTITY SHOWED 5 QUARTS SLOWLY GOING TO ZERO, 30-45 MINUTES LATER OIL PRESSURE STARTED DECREASING. ENGINE SHUTDOWN AT 72 PSI OIL PRESSURE. WIND MILLING OIL PRESSURE 6 PSI OIL TEMP 47 DEGREES.

Part: COMPRESSOR BLADE — CRACKED (NR 4 ENGINE)

NR 4 ENGINE FAILED DURING TAKEOFF ROTATION. AIRCRAFT RETURNED TO FIELD. HIGH PRESSURE COMPRESSOR 11TH STAGE BLADE FAILED DUE TO FOD. ENGINE WAS REPLACED.

Part: FUSE PIN — OUT OF POSITION (NR 1 PYLON)

NUMBER ONE PYLON INBOARD STRUT SPRING BEAM FUSE PIN MIGRATED OUT OF POSITION. *S/D* EXISTING FUSE PIN AND NUT REMOVED AND REPLACED WITH NEW PARTS. ANALYSIS OF REMOVED FUSE PIN AND NUT DID NOT REVEAL ANY DISCREPANCIES. PARTS SENT TO BOEING FOR FURTHER ANALYSIS. FUSE PIN (P/N 310U2301-120).

Part: O-RING — CUT (NR 1 ENGINE)

NR 1 ENGINE OIL QUANTITY SLOWLY DROPPED TO ZERO. SHUT DOWN ENGINE AND RETURNED TO HNL. REPLACED ENGINE. AT ENGINE DISASSEMBLY, FOUND OIL LEAK AT NR 3 BEARING SCAVENGE OIL TEMP PROBE. O-RING WAS DAMAGED. REPLACED PROBE AND O-RING.

Part: DOOR POWER LIGHT — FAILED TEST (UPPER DECK DOOR)

LEFT STRETCHED UPPER DECK DOOR POWER LIGHT FAILED TEST. REPLACED BATTERY PACK AND ANNUNCIATOR MODULE.