N1608

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 84,569 hrs · 10,905 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 36AB AND 39AB. RESECURED CONNECTOR AT 36AB AND RETERMINATED CONNECTOR AT 39AB. SYSTEM OPERATION IS NORMAL. (LP 6119345)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 84,072 hrs · 10,842 cycles

EMERGENCY AISLE LIGHT AT SEAT 37F INOP. FOUND BROKEN WIRE AT CONNECTOR. RETERMINATED PER B767-300 WDM 33 -51-18 AND SWPM 20-42-01. OPS CK GOOD. OK FOR SVC. (LP6381040)

Part: DUCT — LEAKING (GROUND A/C) · airframe 83,729 hrs · 10,785 cycles

SHIP 1608; FLIGHT 2353 - DIVERTED - CREW REPORTED CABIN ALTITUDE WARNING SOUNDED AND CABIN ALTITUDE AT 10.5K. OPERATIONAL DECISION MADE TO MANUALLY DEPLOY MASKS AND TO DIVERT TO TAMPA DUE TO EXCESSIVE CABIN ALTITUDE. CORRECTIVE ACTION: AFTER INSPECTION OF LEFT PACK FOUND GROUND AIR CONNECTOR DUCT LEAKING, RECONNECTED SEALS AND CLAMP AND FOUND RIGHT PACK AT LOW FLOW CONTROL VALVE DUCT PERRY SEALS MISSING. REPLACED SEALS ON DUCTS. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,460 hrs · 10,748 cycles

FOUND RIGHT CEILING EMERGENCY LIGHTS FROM SEATS 18-29 AND EXIT SIGN ABOVE MID LAV INOPERATIVE. REPLACED BOTH BATTERY AND POWER PACK. SYSTEM OPERATION IS NORMAL.

Part: FUSE — DEFECTIVE (POWER SUPPLY) · airframe 81,016 hrs · 10,503 cycles

R2 EMERGENCY SLIDE ILLUMINATION LIGHT IS INOPERATIVE. FOUND FUSE OF M733 POWER SUPPLY DEFECTIVE. REPLACED FUSE AND DOOR SLIDE LIGHT. SYSTEM OPERATION IS NORMAL.

Part: STRINGER CLIP — CRACKED (BS 1654) · airframe 80,143 hrs · 10,418 cycles

STA 1654.5 S3R STRINGER CLIP FOUND CRACK AND REPLACED. (LP 0838191)

Part: STRINGER CLIP — CRACKED (BS 1678) · airframe 80,143 hrs · 10,418 cycles

STA 1678 STRINGER CLIP FOUND CRACK AT S-3R AREA AND REPLACED. (LP 0838188)

Part: SEAT TRACK — CORRODED (BS 785-830) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 STA 785, STA 819, STA 830 FOUND CORRODED AND REPAIRED. (LP 0834216)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,200 hrs · 10,425 cycles

DURING INSPECTION, CORROSION FOUND AT DRAIN MAST STA 1407 ON FUSELAGE SKIN C/W ER/A 572980-14 AND SRM 53-00-01.

Part: SEAT TRACK — CORRODED (BS 1109-1131) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 STA 1109, STA 1131 FOUND CORROSION AND REPAIRED. (LP 0834222)

Part: SEAT TRACK — CORRODED (BS 1197-1208) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 BETWEEN STA 1197+88 AND STA 1208 FOUND CORROSION OUT OF LIMITS AND REPAIRED. (LP 0834219)

Part: SEAT TRACK — CORRODED (BS 841-966) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 BETWEEN STA 841 AND STA 966 FOUND CORROSION AND REPAIRED. (LP 0834212)

Part: SEAT TRACK — CORRODED (BS 841-1097) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 BETWEEN STA 841 AND STA 1097 FOUND CORROSION ALL OUT OF LIMIT AND REPAIRED. (LP 0825888)

Part: SEAT TRACK — CORRODED (BS 1186-1197) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 BETWEEN STA 1186 AND STA 1197+88 FOUND CORROSION ALL OUT OF LIMITS AND REPAIRED. (LP 0825896)

Part: SEAT TRACK — CORRODED (BS 1097-1131) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 BETWEEN STA 1097 AND STA 1131 FOUND CORROSION AND REPAIRED. (LP 0825886)

Part: SKIN — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 FUSELAGE SKIN AT STA 1395- 1417 S35R - S36R FOUND CORROSION AFT DRAIN MASK. C/W ERA 572980-14

Part: SEAT TRACK — CORRODED (BS 751-841) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 BETWEEN STA 751 AND STA 841 FOUND CORROSION REPAIRED PER SRM 53-00-52. (LP 0825906)

Part: SEAT TRACK — CORRODED (BS 1098-1230) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT LBL 88.5 BETWEEN STA 1098 AND STA 1230 FOUND CORROSION ALL OUT OF LIMIT AND REPAIRED. (LP 0825901)

Part: SEAT TRACK — CORRODED (BS 841-1098) · corrosion level 2 · airframe 80,143 hrs · 10,418 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT LBL 88.5 BETWEEN STA 841 AND STA 1098 FOUND CORROSION OUT OF LIMIT C/W SRM 51-40-02. (LP 0824880)

Part: SKIN — DAMAGED (BS 1873-1881) · airframe 80,143 hrs · 10,418 cycles

FUSELAGE SKIN AT STA 1873-1881 RBL 8 TO RBL 10 TOP AREA PUNCH REPAIRED PER ERA 573005-14. (LP 0823269)

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 79,750 hrs · 10,379 cycles

7+20 HRS INTO FLT ORANGE GLOW TOP OF PILOT FWD WINDOW. AUDIBLE "POP" AND OUTER PANE SHATTERED. WINDOW HEAT TURNED OFF. NO AIR LEAK. DIFF PRESSS STABLE FL360 .79M SAT 55. REPLACED CAPT FWD WINDSHIELD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 79,406 hrs · 10,344 cycles

FLOOR PROXIMITY EMERGENCY LIGHTS WILL NOT ILLUMINATE AT SEATS 20B, 34F AND 40F. FOUND WIRE CONNECTOR DISCONNECT. CONNECTED THE WIRE.

Part: LIGHT — INOPERATIVE (SEAT 23F) · airframe 76,897 hrs · 10,093 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE AT SEAT 23F. SECURED THE EMERGENCY LIGHT.

Part: CABLE — OUT OF POSITION (EMERGENCY EXIT) · airframe 75,673 hrs · 9,976 cycles

EMERGENCY EXIT LEAKING AT SEAT 21A. FOUND LEFT FORWARD OVERWING EXIT STEP SUPPORT CABLE HANGING OUT 6 INCHES. REPLACED AND SECURED.

Part: WIRE — OPEN (EMERGENCY LIGHTS) · airframe 75,485 hrs · 9,958 cycles

DURING A SERVICE CHECK, FOUND ROW 36 RIGHT LIGHT WITH AN OPEN WIRE BEHIND CONNECTOR. REPAIRED THE WIRE. SYSTEM OPS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 39G) · airframe 75,442 hrs · 9,953 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT SEAT 39G. REPLACED THE LIGHTS, SYSTEM OPS NORMAL.

Part: OXYGEN MASK — NO TEST (SEATS 5BC) · airframe 74,553 hrs · 9,842 cycles

OXYGEN MASK DID NOT DEPLOY AT SEATS 5BC. RESTOWED MASK AND PERFORMED MANUAL DROP. PASSED TEST.

Part: OXYGEN MASK — NO TEST (SEATS 18 GF) · airframe 74,553 hrs · 9,842 cycles

OXYGEN MASK DID NOT DEPLOY AT SEATS 18G/F. RESTOWED MASK AND PERFORMED MANUAL DROP TEST. TEST PASSED.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 74,397 hrs · 9,821 cycles

PERFORMED AN AIR TURNBACK DUE TO A LHR FOLLOWING LOSS OF BOTH AUTO CABIN PRESS CONTROL SYSTEMS. REPLACED BOTH AUTO 1 AND AUTO 2 CONTROLLERS AND OUTFLOW VALVES. SYS CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 72,842 hrs · 9,625 cycles

EMERGENCY EXIT SIGNS AT L1 & R2 DOORS ARE INOPERATIVE. FOUND PUSHED BACK PIN AND BROKEN LOCK AT POSITION 1 CONNECTOR D017P. REPLACED THE CONNECTOR, AND BATTERY PACK. SYSTEM OPS NORMAL.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 72,832 hrs · 9,624 cycles

FOUND CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SKIN. C/W ERA 555445-14.

Part: STRUCTURE — CRACKED (NR 8 SLAT) · airframe 72,559 hrs · 9,586 cycles

RIGHT WING FIXED L/E BULLNOSE CRACKED UNDER THE NR 8 SLAT 3 FT FROM OTBD END OF SLAT. COMPLIED WITH ERA 55618-14.

Part: WIRE HARNESS — DAMAGED · airframe 72,559 hrs · 9,586 cycles

FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR ROW 40AB. SCREENS DIED AND SEAT BELT SIGNS 40CD (CENTER) FLICKERING, QRM IFE POWER ISOLATED NO FURTHER ODOR DETECTED. FOUND SEAT TO SEAT HARNESS 38-39AB CUT TO SHIELD. REPLACED HARNESS, VSEBS AT 39-41, SYSTEM OPERATION IS NORMAL.

Part: PROXIMITY SENSOR — MALFUNCTIONED (R2 DOOR SLIDE) · airframe 71,704 hrs · 9,478 cycles

R2 EMERGENCY SLIDE LIGHT INTERMITTENTLY FLASHES. RESEATED PROXIMITY BOX AND CYCLED DOOR. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 84,108 hrs · 10,847 cycles

WHILE ATL FOR INSPECTIONS, MTC WAS WORKING AMDS WORKCARD 5724- 01010-03B AND FOUND A CRACK IN THE LOWER WING SKIN OF THE LH WING EXTENDING FROM FASTENER NUMBER 1 IN THE GROUP A? FASTENERS COMMON TO STR 9.5. SECTION III C/W ERA 532672-14. (LP 1814330)

Part: SKIN — CRACKED (LT WING) · airframe 84,108 hrs · 10,847 cycles

WHILE ATL FOR INSPECTIONS MAINTENANCE FOUND A CRACK IN THE LOWER WING SKIN OF THE LEFT WING EXTENDING FROM FASTENERS NUMBER 1 IN THE GROUP A FASTENERS COMMON TO STR9.5 THE CRACK IS EMANATING FROM THE INBD MOST FASTENERS ON THE FORWARD ROW OF THE GROUP FASTENER SET. SECTION II C/W ERA 532672-14. (LLP1814323)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,834 hrs · 8,530 cycles

ULTRASOUND INSPECTION INDICATES CRACKING ON BULKHEAD. COMPLETED REPAIR IAW ERA 532583-14AD, REV A.

Part: FASTENER — CRACKED (WING) · airframe 63,834 hrs · 8,530 cycles

FASTENER CRACKED. REPAIRED IAW ERA 532660-14 AD.

Part: FASTENER — CRACKED (WING) · airframe 63,834 hrs · 8,530 cycles

FASTENER CRACKED. REPAIRED IAW ERA 532672-14, REV ORIGINAL.

Part: SKIN — CRACKED (RT WING) · airframe 72,912 hrs · 9,633 cycles

FOUND A CRACK IN THE LOWER RT WING SKIN, EXTENDING FROM A FASTENER COMMON TO STRINGER 9.5. THE CRACK IS 0.180 INCHES IN LENGTH. REPAIRED IAW ER/A 532660-14.

Part: SKIN — DENTED (BS 1844 LBL 10) · airframe 53,640 hrs · 7,369 cycles

DENT ON SKIN BS 1844 LBL 10, 1 X 0.5, 0.020 INCH DEEP. PERMANENT REPAIR PERFORMED IAW PRI NR 508526-14 REV 0 AND REV 1.

Part: SKIN — DENTED (BS 1439-1461) · airframe 53,640 hrs · 7,369 cycles

FUSELAGE SKIN FOUND DENTED AT BS 1439-1461 S24R. REPAIR CARRIED OUT PER BOEING SRM 53-00-03 FIG 201 REPAIR 2.

Part: SKIN — DENTED (BS 1439-1461) · airframe 53,640 hrs · 7,369 cycles

FUSELAGE SKIN BS 1439-1461, S24R AREA FOUND ONE DENT. REPAIR CARRY OUT IAW SRM 53-00-01, FIG 201, REPAIR 1.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 53,259 hrs · 7,329 cycles

SEAT 26AB WHITE AISLE EMERGENCY EXIT PATH LIGHT INOPERATIVE. FOUND WIRES BROKEN OFF CONNECTOR AT OTBD SEAT LEG. FWD EMERGENCY EXIT PATH LIGHT AT 26AB. ALL OTHER EMER EXIT LIGHTS OPS NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,719 hrs · 6,595 cycles

FS 903 RT FRAME INNER CHORD WAS CRACKED BETWEEN STR 20R AND 21R AND WAS REPAIRED PER ERA 488821-14AD REV ORG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,719 hrs · 6,595 cycles

CABIN-STA 1480 LBL 50 FLOORBEAM FOUND CORRODED AND REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201.

Part: SKIN — DELAMINATED (RT WING LE FLAP) · airframe 47,719 hrs · 6,595 cycles

RT INBD FLAP OTBD L/E FAIRING FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA AS PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 45,733 hrs · 6,380 cycles

MAINTENANCE FOUND DURING A CHECK HARNESS DAMAGED ON EMERGENCY PATH LIGHTS SEAT 28F-40B. MAINTENANCE REPLACED SEAT HARNESS. SYSTEM OPERATION IS NORMAL.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 45,711 hrs · 6,378 cycles

MAINTENANCE FOUND DURING A CHECK HARNESS DAMAGED ON EMERGENCY PATH LIGHTS SEAT 28F-40B. MAINTENANCE REPLACED SEAT HARNESS. SYSTEM OPERATION IS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 45,173 hrs · 6,319 cycles

RIGHT PRV MESSAGE ON T/O. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 42,157 hrs · 6,014 cycles

EMERGENCY ESCAPE PATH LIGHTS INOP FROM 20A/B TO 16A/B. FOUND WIRE BROKE AND SHORTED AT SEAT 17A/B AND REPAIRED SAME. REPLACED CHARGE FUSE FOR PIN 13 AND 14 PACK M1209. CKS OK

Part: STARTER — FAILED (APU) · airframe 41,498 hrs · 5,940 cycles

APU FAILED TO START. FOUND APU STARTER INOP. REMOVED AND REPLACED APU STARTED PER MM. OPS NORMAL.

Part: FUEL FILTER — UNSERVICEABLE (NR 2 ENGINE) · airframe 40,664 hrs · 5,853 cycles

RIGHT ENGINE FUEL FILTER LIGHT AT 400. STAYED ON FOR 15 MINS IN TERM AND LEVEL OFF. FOUND FUEL FILTER DIRTY. REMOVED AND REPLACED FUEL FILTER IAW MM. OPS CHECK OK. SUMPED RT TANK. NO WATER OR DEBRIS FOUND.

Part: IGNITION SYS — WARNING LIGHT (NR 2 ENGINE) · airframe 40,642 hrs · 5,851 cycles

RT ENG IGN 1 STATUS MSG. PERFORMED TWO GOOD STARTS NR 2 ENGINE. NO MSGS NOTED.

Part: SPAR — CUT (LT WING) · airframe 40,374 hrs · 5,821 cycles

WHILE CUTTING THE LOWER WING SKIN FOR THE WINGLET MODIFICATION, THE FRONT SPAR LOWER CHORD AFT FLANGE WAS ALSO CUT AT 0 FSS 1035. THE DAMAGE WAS TRIMMED OUT AND INSTALLED A TITANIUM STRAP.

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE) · airframe 40,361 hrs · 5,820 cycles

RT ENG WOULD NOT START. RTB, RT ENG PRESS SWITCH POPPING C/B REPLACED FUEL PRESSURE SWITCH PER M/M. OP CKS GOOD RAN ENG AT IDLE, NO FAULTS NOTED. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR.

Part: PLUG — FAILED (NR 1 ENGINE) · airframe 39,633 hrs · 5,737 cycles

LEFT ENGINE IGN 1 INOP. REPLACED NR 1 ENGINE 1 IGN PLUG. RAN ENGINE, OPS OK.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 38,011 hrs · 5,553 cycles

AFTER 35 MINUTES OF TAXI, LEFT THROTTLE WAS ADVANCED AND THERE WAS NO ENGINE RESPONSE. LEFT ENGINE REMAINED AT IDLE REGARDLESS OF THROTTLE POSITION. NO EICAS MESSAGE OR EEC LIGHTS DISPLAYED. ONCE APU WAS STARTED AND ELEC PWR SWAPPED CONTROL RETURNED TO LEFT THROTTLE AND ENGINE. REMOVED AND REPLACED LT ENG EEC IAW MM, OPS CKS OK. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR.

Part: ENGINE — MAKING METAL (NR 2) · airframe 37,388 hrs · 5,478 cycles

METAL FOUND ON B-SCAV DETECTOR SCREEN. FOUND SMALL AMOUNT OF METAL DEBRIS ON MCD AND LARGE QT OF DEBRIS ON B SCAV MCDON LUBE PUMP, PER MSU REQ ENG CHG. NR 2 ENG REPLACED PER TRANS 1T161.

Part: INDICATOR — FAILED (COCKPIT) · airframe 36,106 hrs · 5,336 cycles

AT FL350 M.78 FLIGHT CREW DETECTED ACRID ODOR AND SAW A SMALL AMOUNT OF SMOKE COMING FROM ABOVE THE CENTER GLARE SHIELD. ALL OFF FLAGS APPEARED ON F/O`S IAS/MACH INDICATOR AND IAS/MACH C/B OPENED ON RT SIDE. REMOVED FO`S IAS/MACH INDICATOR. INDICATOR APPEARS TO BE SHORTED. SWAPPED F/O`S INDICATOR WITH CAPTS IAS/MACH INDICATOR. PERFORMED AIR DATA COMPUTER TEST. ALL INDICATIONS NORMAL. REINSTALLED CAPTS INDICATOR IN ORIGINAL POSITION. NEEDS INDICATOR DPN 341002534 NIS DKR 478834. INSTALLED FOS IAS/MACH INDICATOR PER MM. OPS CK GOOD.

Part: SKIN — DAMAGED (BS 1346-1365) · airframe 36,060 hrs · 5,331 cycles

FOUND FUSELAGE SKIN BLEND AT FS 1346-1365 AND STRINGERS 20-21R.

Part: SKIN — GOUGED (FS 1346-1360) · airframe 36,049 hrs · 5,330 cycles

BLENDS OF GOUGED SKIN BETWEEN STA 1346-1360, S 27R - 31R.

Part: BOTTLE — EMPTY (EVAC SLIDE) · airframe 35,701 hrs · 5,290 cycles

LEFT OVERWING SLIDE BOTTLE FOUND EMPTY DURING ROUTINE CHECK BOTTLE REPLACED.

Part: TIRE — SEPARATED (MLG) · airframe 32,816 hrs · 4,947 cycles

NR 4 TIRE HAD RECAP COME OFF ON LANDING. REPLACED NR 4 WHEEL ASSY PER MM OK FOR SERVICE.

Part: ACTUATOR — FAILED (SPOILER) · airframe 32,722 hrs · 4,935 cycles

SPOILER EICAS STATUS MSG FOUND NR 11 SPOILER ACT INOP. REPLACED BY NEW ON ACC MM 27-61-02-424-023. ALL TESTS ACC AMM 27-61-00 501 C/OU OK. INSPECTION PERFORMED.

Part: VALVE — FAILED (LT A/C PACK) · airframe 32,544 hrs · 4,913 cycles

BEFORE PUSHBACK W/L PACK OFF THE PACK OFF LIGHT WENT OUT AND THE L PACK OFF EICAS MESSAGE WAS NOT DISPLAYED. RTB, REMOVED AND REPLACED LT PACK VALVE. OPS NORMAL.

Part: SKIN — DAMAGED (BS 1362 S31-32R) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE STA 1362 BETWEEN STR 31R AND32R HAS STATIC DISCHARGE. REPAIRED PER ERA 459550-14.

Part: SKIN — GOUGED (BS 1274 S31-32R) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE STA 1274 STR 31R TO STR 32R SKIN GOUGED. REPAIRED PER ERA 459461-14 TIME LIMITED REPAIR.

Part: SKIN — GOUGED (BS 1406 S20R) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE UPPER AFT CORNER OF DOOR CUTOUT SKIN GOUGED STA 1406 AND STR 20R. REPAIRED PER ERA 459506-14 TIME LIMITED REPAIR.

Part: SKIN — GOUGED (FS 1350) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE RS AFT OF AFT PIT DOOR CUTOUT LWR SKIN SECTION STA 1350 STR 31R TO STR 27R SKIN HAS AREAS OF GOUGING. COMPLIED WITH INSTRUCTIONS OF ERA 459507-14 TIME LIMITED REPAIR.

Part: WIRE — BROKEN (BS 1219) · airframe 31,469 hrs · 4,777 cycles

BROKEN EMERG EQUIPMENT LIGHTING WIRE RIGHT SIDE STA 1219 ROW 30. REPAIRED FEEDER IAW BSWPM 20-10-13. TESTED ON OPN 6843.

Part: SKIN — SCRATCHED (BS 618-628 S23R) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE SKIN SCRATCHED BS 618-628 S23R. REPAIRED PER ERA 459504-14.

Part: SKIN — GOUGED (BS 1274 S27-28R) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE FWD SIDE OF AFT PIT DOOR CUTOUT STA 1274 BETWEEN STR 27R AND 28R SKIN GOUGED. REPAIRED PER ERA 459461-14.

Part: SKIN — GOUGED (FUSELAGE) · airframe 31,469 hrs · 4,777 cycles

FUSELAGE SKIN ON FWD AND AFT SIDE OF BULK CARGO DOOR SCRATCHED AND GOUGED. REPAIRED PER ERA 459505-14.

Part: SKIN — GOUGED (BS 1373 S28-29R) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE RS AFT OF AFT PIT DOOR CUTOUT LWR SKIN SECTION STA 1373 BETWEEN STR 29R AND STR 28R SKIN HAS PREVIOUS GOUGE, ALSO HAS GAP UNDER FASTENER. REPAIRED PER SRM 53-00-01 FIG 201 REPAIR 14.

Part: SKIN — GOUGED (BS 1774) · airframe 31,469 hrs · 4,777 cycles

EXT FUSELAGE FWD UPPER CORNER OF AFT PIT COOR CUTOUT STA 1774 SKIN GOUGED. REPAIRED PER ERA 459462-14 TIME LIMITED REPAIR.

Part: TRANSMISSION — UNKNOWN (LT ENGINE) · airframe 30,888 hrs · 4,705 cycles

RTB AFTER LGEN WAS INDICATED ON EICAS. L DRIVE LIGHT REMAIN ON. FWD TO MEL PLACARD PER 24-00-01. REMOVED AND REPLACED NR 1 ENG IDG ASSY IAW MM. PERFORMED ENG RUN PER DELTA PFH, OPS CHK OK LEAK CHK OK MSGS CLEARED MCO AND PLACARD REMOVED.

Part: LINE — BROKEN (NR 1 ENG OIL SYS) · airframe 30,785 hrs · 4,691 cycles

AT FL330 LEFT ENG OIL PRESSURE AND QUANTITY DROPPED TO ZERO. ENGINE SUBSEQUENTLY FLAMED OUT. ENGINE SHUTDOWN, CHECKLIST PERFORMED, 38K LBS OF FUEL DUMPED FROM CTR TANK. NORMAL SINGLE ENG LANDING. FOUND OIL LINE AND CLAMP GOING TO OIL PRESS TRANSMITTER BROKE. REPLACED NR 1 ENGINE PER TRANS 1T160.

Part: UNKNOWN — UNKNOWN (APU) · airframe 28,160 hrs · 4,377 cycles

NO DUCT PRESSURE WHEN APU BLEED SELECTED TO SUPPLY PNEUMATICS. FWD TO MCO AND PLAC PER MEL 49-11-01C. PERFORMED ECU BITE PROCEDURE. NO FAULTS OR MINI-FLAGS. RAN A BLEED VALVE OPS OK. PRESSURE NORMAL.

Part: CIRCUIT BREAKER — FAILED (COCKPIT) · airframe 26,236 hrs · 4,125 cycles

STANDBY BUS EICAS MESSAGE IN FLT. STBY POWER OFF LIGHT ILLUM, DID NOT EXTINGUISH WHEN BATTERY SELECTED MESSAGES INCLUDE L YAW DAMPER, L BLD ISLN VLV UTL BUSSES, L/E SLAT DISAGREE, PROBE HEAT AND AILERON LOCK OUT. REPLACED INTERMITTENT C/B, OPS NOW NORMAL.

Part: MANIFOLD — UNSERVICEABLE (NR 1 ENGINE) · airframe 24,713 hrs · 3,913 cycles

FLT CREW REPORTED NR 1 ENG OIL LOSS DIVERTED TO DXB FOR REPAIRS. ENG WAS NOT SHUTDOWN. ENG OIL TANK SERVICED. ENGINE MOTORED. LEAK TRACED TO OIL LINE TO PRESSURE TRANSMITTER AND LOW PRESSURE SWITCH. LINE AND CLAMP REPLACED AND ENGINE GROUND RUN CARRIED OK. NO LEAKAGE EVIDENT.

Part: LINE — BROKEN (NR 1 ENGINE) · airframe 24,686 hrs · 3,909 cycles

AT CRUISE ALT FL320, 3 HOURS INTO FLT, LEFT ENGINE OIL QUANTITY WENT TO ZERO. OIL PRESSURE WAS 45 PSI AND GRADUALLY DECREASED TO 11 PSI TRANSIENT 10 PSI EXPERIENCED ON FINAL APPROACH LEFT THRUST LEVER REDUCED TO IDLE. NO REVERSE. ALL OTHER ENG PARAMETERS NORMAL. OIL PUMP DISCHARGE MANIFOLD PIPE BROKEN. PIPE REPLACED. ENGINE RUN-UP 5 MIN. ALL PARAMETERS NML. NO LEAK DEBRIS. INFO ENG OIL SERVICED 48 PINTS WITH EXXON 2380 ENG OIL, MPN 1978M64G01.

Part: BATTERY — OVERHEATED (APU) · airframe 22,053 hrs · 3,538 cycles

PRIOR TO DEPARTURE BURNED SMELL REPORTED IN THE BACK OF THE CABIN. MTC FOUND THE APU BATTERY HOT. REPLACED BATTERIES AND CHARGER.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 20,150 hrs · 3,241 cycles

ABORTED T/O IN FCO 120 KNOTS NUMEROUS LIGHTS BELLS INDICATIONS ELECTRIC MALFUNCTION LOSS OF BUS ETC. C/B A-2 ON PANEL P6-1 DC STBY FOUND POPPED. REPLACED CB AND RELAY K109 STBY PWR AND RELAY K104 MAIN BATTERY.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 19,259 hrs · 3,114 cycles

THE RIGHT AND LEFT INBOARD ELEVATORS WERE FOUND WITH DAMAGE ON THE LOWER SKIN PANELS. THE DAMAGE EXTENDS THROUGH THE OUTER SKIN, INNER SKIN, AND HONEYCOMB CORE. REPAIRED PER ER/A 417308-14.

Part: ODOR — DETECTED (BUN WARMER) · airframe 14,506 hrs · 2,395 cycles

MID GALLEY BUN WARMER OVERHEATED WITH STRONG ELECTRICAL SMELL. INSPECTED BUN WARMER, FOUND VERY HOT TO TOUCH, PULLED AND SECURED C/B AND FORWARD TO MCO AND PLACARD PER MEL 25-20-01B.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 13,676 hrs · 2,257 cycles

AT DEPARTURE F/A INFORMED OF A SMOKE ODOR AT AFT RT GALLEY COFFEEMAKER AREA. REMOVED NR 1 AND NR 2 COFFEEMAKER AND FOUND WIRES OK. NOTICE AN ODOR AT NR 2 COFFEE MAKER. REPLACED NR 1 AND 2 COFFEEMAKERS IN AFT RT GALLEY. OPS OK.

Part: ACCESS DOOR — MISSING (APU) · airframe 9,219 hrs · 1,497 cycles

AFTER LEVEL LOUD BANG HEARD BY FLIGHT CREW FOLLOWED BY AIRFRAME VIBES. FLIGHT RETURNED TO ATL WHERE MTC FOUND BOTH APU ACCESS DOORS MISSING. ITEM UNDER INVESTIGATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 8,756 hrs · 1,429 cycles

FWD MID ATT SEAT FLASHLIGHT INOP. REPLACED BATTERY, OPS NORMAL.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 6,574 hrs · 1,080 cycles

FOUND FUSE BLOWN ON EMERGENCY LIGHT BATTERY CHARGER. REPLACED FUSE, OPS CHECK NORMAL.