N152DL

Part: SLIDE — BLOWN (R1 DOOR) · airframe 125,045 hrs · 22,893 cycles

RETURN TO GATE FOR REMOVING NO REVS, R1 SLIDE BLEW. REPLACED DOOR SLIDE. SYSTEM OPERATION IS NORMAL

Part: SKIN — DAMAGED (NR 7 SLAT WEDGE) · airframe 124,321 hrs · 22,775 cycles

NR 7 SLAT T/E WEDGE INBD EDGE AFT, HAD BENT SKIN AND SEPARATED FORM COMPOSITE. REPAIRED IAW SRM 51-70-10.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 "J" CHORD AT STA 566 IN FLC IS CORRODED. REPLACED J CHORD.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 CORROSION ON KEEL BEAM WEB AT STA 965. REPAIRED PER ERA 584052-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 AT FLC MAIN CARGO DOOR AT STA 524 AND STA 569 HAS CORROSION ON LOWER CHORD. REMOVED CORROSION AT FLC STA 569. FOUND TO BE OUT OF LIMITS. REPAIRED PER ERA 5847132-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 1097-1200 IS CORRODED ALONG ENTIRE LENGTH. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 762 CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 965-987 CORRODED. REPLACED SEAT TRACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 124,321 hrs · 22,775 cycles

AFT EXTERIOR FUSELAGE SKIN IS CRACKED EXTENDING FROM RIVET HEAD STATION 1725 STRINGER 7R (VERIFIED WITH HFEC SURFACE SCAN). REPAIRED PER SRM 53-80-01 (LP 1436589)

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 NR 1 PYLON UPPER LINK I/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING. REPLACED BUSHING.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVELCORROSION ON S34L STA 453 REPAIRED STRINGER S34L STA 453 PER SRM 53-00-03 (LP 1436930)

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 NO.1 PYLON UPPER LINK I/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING. REPLACED BUSHING. (LP 1436667)

Part: PANEL — WORN (LE SLAT) · airframe 124,321 hrs · 22,775 cycles

# 6 SLAT SPRING LOADED PANEL AT OUTBOARD END OF SLAT WORN THRU ON LEADING EDGE REPAIRED PANEL PER SRM 57-10-17 (LP 1434234)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK LBL 88 STA 920 CORRODED. REPLACED SEAT TRACK (LP 1433561)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK LBL 88 STA 1097 CORRODED. REPLACED SEAT TRACK (LP 1433563)

Part: STRINGER — CORRODED (BS 1351-1373) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

STRINGER 36L BETWEEN BS 1351 AND 1373 HAD CORROSION IN CENTER SECTION, FOUND OUT OF LIMITS. REPLACED THE STRINGER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2SHEAR TIE CORRODED AT STA 1241 BETWEEN S35R AND 36R BLEND AND CHECK LIMITS. REPLACED SHEAR TIE. (LP 1421261)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 SHEAR TIE CORRODED AT STA.1307 BETWEEN S39L AND 39R. FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1420767)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1540 BEWEEN S39L 38L CORRODED, BLEND AND CHECK LIMITS. REPLACED SHEAR TIE. (LP 1421250)

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 NO 1 PYLON, UPPER LINK I/B BUSHING ON WING SIDE SHOWS SIGNS OF PITTING. REPLACE BUSHINGS ON CWO 115958-0003. (LP1420523)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 SHEAR TIE STA 1540 39R-39L CORRODEDREMOVED AND REPLACED SHEAR TIE. (LP 1420435)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 CORROSION ON S37R STA 434 REMOVED COROSION 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS REMOVED DAMAGED STR AREA AND INSTALLED STR REPAIR AND SPLICE PIECE. (LP 1419808)

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 NO.1 PYLON UPPER LINK O/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING REMOVED AND REPLACED BUSHING ON CWO 115959-0005. (LP 1420526)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 STR 39R BETWEEN STA 412-434 CORRODEDREMOVED CORROSION ON STR 39R 100% MATERIAL LOSS. REMOVED DAMAGED STRINGER AND REPLACE WITH NEW STRINGER

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 CORROSION ON S36R STA 430 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS REPLACED WITH NE STRINGER AND INSTALLED NEW STRINGER (LP 1419804)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

SHEAR TIE @STA 434 BETWEEN STR 36R-37R CRACKED REMOVED AND REPLACED SHEAR TIE AT STA 434 BETWEEN STR 3612-37R (LP 1419810)

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 NO 1 PYLON UPPER LINK, O/B BUSHING ON UPPER MOUNT ON WING SIDE SHOW SIGNS OF PITTING. REPLACED BUSHING ON CWO 115958-0003. (LP 1420528)

Part: BUSHING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 NO.1 PYLON FWD BUSHING ON UPPER LINK SHOWS SIGNS OF PITTING. REPLACED (LP1418700)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 SHEAR TIE @ STA 412 BETWEEN STR 36R-37R CORRODED OUT OF LIMITS. REPLACED SHEAR TIE. (LP1418076)

Part: SHEAR TIE — CORRODED (BS 1417) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

SHEAR TIE CORRODED AT BS 1417 BETWEEN STRINGERS 39L AND 39R, FOUND OUT OF LIMITS. THE SHEAR TIE WAS REPLACED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 STRINGER CLIP @ STA 1540 STR 39R.REPLACED STRINGER CLIP (LP 1416198)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 124,321 hrs · 22,775 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 1201-1439 IS CORRODED ALONG THE ENTIRE LENGTH. REPLACED SEAT TRACK. (LP1415508)

Part: WEDGE — DAMAGED (LE SLAT) · airframe 124,321 hrs · 22,775 cycles

#10 SLAT T/E EDGE WEDGE, I/B T/E HAS DAMAGE & COMPOSITE EXPOSED C/W SRM 51-70-10. (LP 1425960)

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 123,594 hrs · 22,669 cycles

CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED ALL BULBS. SYSTEM OPERATION IS NORMAL.

Part: PUMP — MAKING METAL (HYD SYSTEM) · airframe 122,405 hrs · 22,516 cycles

LT HYDARULIC LOW PRESSURE LIGHT FOLLOWED LT HYD QUANTITY LIGHT FOUND DP INDICATOR BLOWN OUT OF FILTER MODULE. CHECK EDP CASE DRAIN FILTER AND PRESSURE FILTER. CHECKED EDP CASE DRAIN FILTER AND PRESSURE FILTER. FOUND METAL IN BOTH, FLUSHED LEFT HYD SYSTEM. REPLACED DIFFERENTIAL PRESSURE INDICATOR AND REPLACED #1 ENG EDP

Part: INTERCOSTAL — DAMAGED (BS 132.5-138) · airframe 120,156 hrs · 22,203 cycles

RIGHT SIDE INTERCOSTAL BETWEEN STA 132.5 TO STA 138 WL 216 DAMAGED REPAIRED PER ER/A 573595-14. (LP 0863257)

Part: SHEAR TIE — DAMAGED (BS 196.5) · airframe 120,156 hrs · 22,203 cycles

SHEARTIE AT STA 196.5 BETWEEN STR 30-31 RIGHT DAMAGED. REPLACED PER ERA 573383-14. (LP 0863211)

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 120,156 hrs · 22,203 cycles

RIGHT HAND FUSELAGE SKIN SECTION 41 DAMAGED. REPAIRED PER ERA 573383-14. (LP 0863191)

Part: FRAME — DAMAGED (BS 148.5) · airframe 120,156 hrs · 22,203 cycles

FRAME AT STA 148.5 WL 210 DAMAGED REWORKED INNER AND OUTER FRAME CHORDS TO ORIGINAL CONTOUR @ STA 148.5 WL 210. REPAIRED PER ERA 568021-14. (LP 0863239)

Part: SHEAR TIE — DAMAGED (BS 188.5) · airframe 120,156 hrs · 22,203 cycles

SHEAR TIE AT STA 188.5 BETWEEN STR 30-31 RIGHT DAMAGED REMOVED AND REPLACED SHEAR TIE PER ERA 573383-14. (LP 0863232)

Part: FRAME — DAMAGED (BS 138.5) · airframe 120,156 hrs · 22,203 cycles

FRAME AT STA 138.5 WL 210 DAMAGED. REPAIRED PER ER/A 573595-14 (LP 0863248)

Part: FRAME — DAMAGED (BS 132 BULKHEAD) · airframe 120,156 hrs · 22,203 cycles

BULKHEAD FRAME AT STA 132.5 BETWEEN WL 207-220 DAMAGED. REPAIRED PER ER/A 568021-14. (LP 0863234)

Part: SUPPORT BEAM — CORRODED (LT WING TE FLAP) · airframe 116,893 hrs · 21,737 cycles

LEFT WING TE FLAP SUPPORT BEAM CORRODED. REPAIRED IAW ERA 565532-14.

Part: SUPPORT BEAM — DAMAGED (RT WING TE FLAP) · airframe 116,893 hrs · 21,737 cycles

RIGHT WING INBD FLAP SUPPORT BEAM DAMAGED. REPAIRED IAW ER/A 565521-14.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 116,893 hrs · 21,737 cycles

LT ELEVATOR SKIN DAMAGED, UPPER SURFACE I/B END C/W SRM 55-20-01.

Part: FAIRING — CRACKED (TE FLAP) · airframe 116,893 hrs · 21,737 cycles

RIGHT WING, INBOARD FLAP, OUTBOARD FLAP TRACK FAIRING, AFT FAIRING CRACKED ON LEADING EDGE. REPAIRED SRM 57-53-70.

Part: OVEN — SMOKE (GALLEY) · airframe 116,679 hrs · 21,709 cycles

REPORTED SMOKE AND FUMES FROM FORWARD GALLEY OVEN DURING TAXI OUT. REPLACED THE OVEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 116,118 hrs · 21,626 cycles

DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHT FWD LEFT NOT ILLUMINATING WHEN SELECTED ON. REPLACED THE LIGHT. SYSTEM OPS NORMAL.

Part: ACOUSTIC PANEL — DELAMINATED (THRUST REVERSER) · airframe 115,478 hrs · 21,522 cycles

LEADING EDGE THRUST REVERSER ACOUSTIC PANEL DELAMINATED AT 5 0' CLOCK POSTION. REPAIRED IAW ERA 469315-14MA.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 115,373 hrs · 21,506 cycles

EMERGENCY LIGHTS AT SEATS 21-32GF ARE INOPERATIVE. REPLACED CHARGER. SYSTEM OPERATION IS NORMAL.

Part: FUSE — NO TEST (EMERGENCY LIGHTS) · airframe 114,423 hrs · 21,364 cycles

FOUND LEFT SIDE ROW 21-23 EMERGENCY LIGHT INOPERATIVE DURING SERVICE CHECK. REPLACED F1 FUSE ON M9009 POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: WIRE — CUT (EMERGENCY LIGHTS) · airframe 114,423 hrs · 21,364 cycles

EMERGENCY LIGHTS AT SEAT 19ABC ARE INOPERATIVE. MAINTENANCE FOUND 1 OF THE WIRE CUT. SPICED AND REPAIRED. SYSTEM OPERATION IS NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 114,042 hrs · 21,309 cycles

R1 LAVATORY SMOKE DETECTOR SOUNDED DURING FLIGHT NO EVIDENCE OF SMOKE RED DETECTOR LIGHT REMAINED FLASHING FOR DURATION OF FLIGHT. INSPECTED R1 LAVATORY TEMP INDICATOR STRIP AND FUSIBLE FIRE EXTINGUISHER TIP CHECKS GOOD. PERFORMED LAV SMOKE DETECTION TEST. SYSTEM OPERATION IS NORMAL.

Part: SEAL DEPRESSOR — CRACKED (FUSELAGE) · airframe 113,102 hrs · 21,153 cycles

FOUND 1/2" CRACK AT FWD CGO LOWER AFT SIDE DEPRESSOR SEAL. REPLACED FWD CARGO DEPRESSOR SEAL.

Part: BRAKE — LEAKING (MLG) · airframe 112,746 hrs · 21,101 cycles

DURING AIRCRAFT ARRIVAL TO STAND FOUND BRAKE AND WHEEL WITH HYDRAULIC LEAKS, FUMES AND SMALL FLAMES ON IT. WHEEL REPLACED. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 111,926 hrs · 20,968 cycles

AFT GALLEY 403, LEFT EMERGENCY WHITE LIGHTS ARE INOPERATIVE. REPLACED THE LIGHT. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 111,605 hrs · 20,921 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 16B ARE INOPERATIVE. FORWARD TO MCO/PLACARD RECONNECTED EMERGENCY PATH LIGHT ELECTRICAL CONNECTOR. SYSTEM OPERATION IS NORMAL. MCO/PLAC REMOVED

Part: SKIN — CORRODED (FUSELAGE) · airframe 113,634 hrs · 21,237 cycles

CORROSION AT THE LOWER EDGE OF THE LEFT SIDE AFT LAVATORY WASTE TANK OVERBOARD VENT, LOCATED AT STA 1574 AND STRINGER S-25L. THE EXPOSED CORROSION IS APPROXIMATELY 3½ FWD/AFT AND CRACKING OCCURRED FROM THE VENT TO TWO FASTENERS WHICH HAVE PULLED THROUGH THE SKIN.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 108,679 hrs · 20,461 cycles

EMERGENCY EXIT LOWER INDENTIFIER IS INOPERATIVE. MAINTENANCE REPLACED M9011 BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 108,309 hrs · 20,403 cycles

EMERGENCY LIGHTS IN CEILING SEATS 30AB AND 39AB ARE INOPERTATIVE. MAINTENANCE FOUND CONNECTOR TO OVERHEAD PANEL AT 36AB BROKEN AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — CONTAMINATED (EXTERIOR) · airframe 108,250 hrs · 20,391 cycles

LIGHT EMERGENCY EXTERIOR SPOT LIGHT APPEARS TO BE FULL OF WATER AT TIME OF INSPECTION. MAINTENANCE CHECK AS FOR PROPER SEAL, RELAMPED AND SYSTEMS OPEATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,755 hrs · 19,869 cycles

FLIGHT DECK OVERHEAD DOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND BATTERIES. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,175 hrs · 19,415 cycles

AIRCRAFT RIGHT SIDE EMERGENCY LIGHTS FOUND INOPERATIVE DURING SERVICE CHECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 99,622 hrs · 19,189 cycles

LEFT INBD AFT FLAP LOWER SURFACE INBD AREA DAMAGED, REPAIRED WITH HOT BOND IAW SRM 57-53-01. REPAIR 1, FIG 201 AND SRM 51-70.

Part: SKIN — NOT REPORTED · airframe 109,553 hrs · 20,597 cycles

SECTION I OF ER/A 513895-14 ISSUED TO ACCOMPLISH SKIN REPAIRS ALONG STR-6L AT FS317, 374, AND 407. REPAIRS ARE BEING ACCOMPLISHED IAW SRM W/ DEVIATIONS, REF ER/A 513895-14.

Part: FLOORBEAM — DAMAGED (BS 1518) · airframe 99,567 hrs · 19,179 cycles

BS 1518, LBL 15-68 FLOORBEAM UPPER TEE DAMAGED. REPAIRED IAW ER/A 520555-14.

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 99,567 hrs · 19,179 cycles

BS 654+121, RBL 30 - 51 FLOORBEAM FOUND CORRODED. REPAIRED IAW SRM 53-00-51. REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 1416) · corrosion level 2 · airframe 99,567 hrs · 19,179 cycles

MAIN DECK BS 1416 RBL 2 - 4 FLOORBEAM CORRODED. REPAIRED IAW SRM 53-00-51.

Part: FLOORBEAM — CRACKED (BS 347) · airframe 99,567 hrs · 19,179 cycles

BS 347 RBL 22 FLOORBEAM CRACKED. DAMAGED FLOORBEAM REPAIRED IAW SRM 53-00-51.

Part: CIRCUIT BREAKER — FAULTED (EMERGENCY LIGHTS) · airframe 98,737 hrs · 19,071 cycles

DURING CLIMB, AT 10000 ALL EMERGENCY LIGHT ILLUMINATED FOR A FEW MINUTES. AT FL370 THE FIRST 8 ROWS AND THE LAST 8 ROWS OF COACH LIGHT ILLUMINATED WITH THE COCKPIT SWITCH IN THE ARMED POSITION. MX RESET RIGHT WING ESCAPE LIGHT CIRCUIT BREAKER P36. OPS CHECK OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 98,230 hrs · 19,008 cycles

THREE EMERGENCY LIGHTS, LT ISLE IN CEILING INOPERATIVE. FOUND DISCONNECT D01084 LOOSE, SECURED. SYS OPS IS NORMAL.

Part: DISCONNECT UNIT — LOOSE (EMERGENCY LIGHTS) · airframe 98,230 hrs · 19,008 cycles

F/A REPORTED EMERGENCY EXIT SIGNS INOPERATIVE. MX FOUND DISCONNECT, D01084, LOOSE. SECURED. SYS OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 98,108 hrs · 18,994 cycles

EMERGENCY LIGHTS FROM 21FG TO 31FG ARE INOPERATIVE. MX REPLACED BATTERY PACK AND RACK M9009. SYS OPS IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,461 hrs · 18,916 cycles

PILOT REPORTED CIRCUIT BREAKER FOR EMERGENCY LIGHTS, TRIPPED. MX REPLACED THE RT BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 97,479 hrs · 18,918 cycles

F/A REPORTED EMERGENCY FLOOR LIGHTS WILL NOT TURN OFF IN CABIN. MX REPLACED FOUR BATTERIES. SYS OPERATION IS NORMAL.

Part: SKIN — DAMAGED (BS 374) · airframe 96,912 hrs · 18,851 cycles

LIGHTNING STRIKE AT BS 374 AT S6L REMOVED DAMAGE WITH SKIN CUTOUT IAW SRM 53-00-01. REPAIR 1HFEC INSPECT CUTOUT IAW SRM 53-00-01, REPAIR 1 FABRICATED AND INSTALLED DOUBLER TREATED AND PAINTED IAW SRM 53-00-01, REPAIR 1 C/W PERMANENT REPAIR IAW ERA 513895-14, REV ORIG.

Part: SKIN — DAMAGED (BS 317 S6L) · airframe 96,912 hrs · 18,851 cycles

LIGHTNING STRIKE BS 317 AT S6L. REMOVED DAMAGE IAW SRM 53-00-01. INSPECTED CUTOUT IAW SRM 53-00-01 REPAIR, FABRICATED, AND INSTALLED DOUBLER IAW SRM 53-00-01, REPAIR 1. C/W PERMANENT REPAIR IAW ERA 513895-14, REV ORIG.

Part: SKIN — DAMAGED (BS 402 S6L) · airframe 96,912 hrs · 18,851 cycles

LIGHTNING STRIKE AT BS 402 AT S6L. REMOVED DAMAGE IAW SRM 53-00-01. REPAIR, FABRICATED AND INSTALLED DOUBLER TREATED AND PAINTED IAW SRM 53-00-01. REPAIR 1 C/W PERMANENT REPAIR IAW ERA 513895-14, REV ORIG.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,593 hrs · 18,180 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 24F ARE INOPERATIVE. MX REPLACED THE WIRE ASSY TO THE SIDEWALL. SYS OPS IS NORMAL. MCO/PLAC REMOVED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 95,859 hrs · 18,712 cycles

EMERGENCY AISLE LIGHT AT SEAT 33F ARE INOPERATIVE. MX FOUND BROKEN WIRE AT SEAT 33F AND REPAIRED. SYS OPS IS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,859 hrs · 18,712 cycles

COCKPIT EMERGENCY LIGHTS ARE INOPERATIVE. MX REPLACED THE LIGHT ASSY AND BATTERIES. SYS OPS IS NORMAL.

Part: SKIN — DAMAGED (BS 1373 S30R) · airframe 94,614 hrs · 18,553 cycles

FUSELAGE SKIN DAMAGED BS 1373 AFT OF AFT CARGO DOOR, DENTED AND GOUGED. REPAIRED FUSELAGE SKIN DAMAGE IAW ERA 507643-14.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 92,691 hrs · 18,310 cycles

EMERGENCY LIGHTS AT SEAT 16FG WERE INOPERATIVE. MAINTENANCE REPLACED THE MISSING WIRE ASSEMBLY AND REPINNED THE CONN SYSTEM, OPERATION IS NORMAL.

Part: FITTING — CRACKED (LT WING) · airframe 92,045 hrs · 18,233 cycles

CRACK INDICATION FOUND DURING AFT PITCH LOAD FITTING BOLT HOLE INSPECTION ON THE LEFT WING INBD BOLT HOLE. INDICATION WAS REMOVED WITHIN SP LIMITS BY OPENING HOLE TO 0.656. ERA BEING ISSUED TO ADDRESS LACK OF AVAILABLE SELF LEVELING WASHERS ERA 501250-14AD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 91,515 hrs · 18,171 cycles

EMERGENCY TRACK LIGHTS AT 23F ARE INOPERATIVE. MAINTENANCE SECURED LOOSE CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 89,659 hrs · 17,953 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT 33F DAMAGED AND REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 88,703 hrs · 17,842 cycles

FLIGHT CREW FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT SEAT 16AB, SOCKET BROKEN AT SEAT 25AB, WIRE BROKEN AT SEAT 32FG, AND A LIGHT INOPERATIVE AT SEAT 20FG. MAINTENANCE RE-TERMINATED SEAT 16AB CONNECTOR, REPLACED SEAT 25AB PATH LIGHT, RE-TERMINATED SEAT 32FG CONNECTOR, AND RE-LAMPED SEAT 20FG EMERGENCY LIGHT PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,768 hrs · 17,729 cycles

EMERGENCY LIGHTS AT ROWS 20-30DEF ARE INOPERATIVE, THE BATTERY PACK WAS REPLACED. SYS OPS IS NORMAL.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 87,634 hrs · 17,713 cycles

DURING DRC FOUND EMERGENCY LIGHTS AT ROWS 20FG-31FG INOPERATIVE. MAINTENANCE REPLACED THE FUSES IN THE BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,941 hrs · 17,634 cycles

EMERGENCY LIGHTS AT 32F ARE INOPERATIVE. MX REPLACED THE KEY PLUG. SYS OPS IS NORMAL.

Part: FAILSAFE — CRACKED (BS 955 FRAME) · airframe 82,392 hrs · 17,078 cycles

DURING THE INSPECTION OF THE BS 955, REAR SPAR BULKHEAD SIDE FRAME AND FAILSAFE STRAP, A CRACK INDICATION AND CORROSION WERE FOUND ON THE RT SIDE FAILSAFE STRAP AND CORROSION WAS FOUND ON THE SKIN. REPAIR IAW ERA 479000-14.

Part: FAILSAFE — CRACKED (FS 966) · airframe 82,392 hrs · 17,078 cycles

CRACKS WERE FOUND DURING INSPECTION OF THE FAILSAFE FITTING IN THE RT AND LT MLG WHEEL WELLS. REPAIR IAW ERA 479807-14.

Part: FAILSAFE — CORRODED (BS 955) · airframe 82,392 hrs · 17,078 cycles

WHILE ACCOMPLISHING INSPECTIONS OF THE FS955 REAR SPAR BULKHEAD SIDEFRAME AND FAILSAFE STRAP FOR AND CORROSION AND FATIQUE CRACKS IAW DAL DI 01-086393-12-AD ON 2/2/10, A CRACK INDICATION AND CORROSION WERE FOUND ON THE LT SIDE FAILSAFE STRAP AND CORROSION ON THE SKIN. APPLIED PERMANENT REPAIR IAW ERA 479649-14AD ORIG.

Part: FAILSAFE — CORRODED (BS 955) · airframe 82,392 hrs · 17,078 cycles

WHILE ACCOMPLISHING INSPECTIONS OF FS955 REAR SPAR BULKHEAD SIDE FRAME AND FAILSAFE STRAP FOR CORROSION AND FATIGUE CRACKS IAW S.I. 01-086393-12AD, A CRACK INDICATION AND CORROSION WERE FOUND ON THE RT SIDE FAILSAFE STRAP AND CORROSION WAS FOUND ON THE SKIN.

Part: ANTENNA — INOPERATIVE (ATC) · airframe 81,922 hrs · 17,016 cycles

BOTH ATC 1 AND 2 FAILED. R & R UPPER ATC ANTENNA IAW MM. INSPECTED CONNECTOR. NTF. MFG DM1301354-001. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,030 hrs · 16,911 cycles

L-3 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED L-3 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD.

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 76,358 hrs · 16,376 cycles

NR 2 ENGINE FAILED TO START ON TAXI OUT. MANUALLY OPENED START VALVE. ENGINE DIDN'T ROTATE. REMOVED DAMAGED STARTER. DUE TO STARTER VALVE MAY HAVE CLOSED DURING START AND REOPENED. REPLACED VALVE ALSO AS PRECAUTION. STARTER AND VALVE REPLACED PER AMM.

Part: FLOORBEAM — CORRODED (BS 720) · airframe 72,129 hrs · 15,898 cycles

FWD CARGO STATION 720 LBL 41 CARGO FLOORBEAM UPPER CHORD FWD BOTTOM SIDE CORRODED. REPAIRED PER 53-00-07D FIGURE 801D ON NR APP509228 AT HMV3/PSV 17.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 72,129 hrs · 15,898 cycles

AFT CARGO STATION 1197+132 LBL 41 CARGO FLOORBEAM FWD FACE UPPER CHORD NUT SIDE CORRODED. REPAIRED ON APP514981 PER 53-00-07D FIGURE 801D AT HMV3/PSV17.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 72,129 hrs · 15,898 cycles

AFT CARGO STATION 1197+22 RBL 41 FLOORBEAM UPPER CHORD FWD SIDE CORRODED. REPAIRED PER 53-00-07D FIGURE 801 ON NR APP515053 AT HMV3/PSV17.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 72,129 hrs · 15,898 cycles

AFT CARGO STATION 1197+88 RBL 41 CARGO FLOORBEAM FWD FACE UPPER SURFACE AND BOTTOM SURFACE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NR APP515160 AT HMV3/PSV17.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 72,129 hrs · 15,898 cycles

AFT CARGO STATION 1197+88 RBL 27 TO RBL 33 FLOORBEAM TOP SURACE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NR APP5155574 AT HMV3/PSV17.

Part: FLOORBEAM — CORRODED (BS 1502) · airframe 72,129 hrs · 15,898 cycles

BULK CARGO STATION 1502 CABIN FLOORBEAM LOWER SURFACE CORRODED FROM RBL 7 TO RBL 42. REPAIRED PER 53-00-51D FIGURE 101 ON APP504362.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 72,129 hrs · 15,898 cycles

AFT CARGO STATION 1197+44 RBL 41 CARGO FLOORBEAM UPPER CHORD CORRODED. REPAIRED ON NR APP515129 PER 53-00-07D FIGURE 801D ON HMV3/ PSV17.

Part: FRAME — CRACKED (BS 1809) · airframe 72,129 hrs · 15,898 cycles

BS 1809 OUTER FRAME FOUND CRACKED AT FRAME RADIUS BETWEEN STRINGER 7R AND 8 R APPROX 3/4 INCH. REPAIRED PER SRM 53-80-08 FIGURE 201 REPAIR 9 ON APP 502887 ON HMV 3/ PSV17.

Part: FLOORBEAM — DAMAGED (BS 434) · airframe 72,129 hrs · 15,898 cycles

FWD CARGO STATION 434 RBL 4 CARGO FLOORBEAM UPPER CHORD RIVET ADJACENT TO SCREW HOLE. UPPER CORD REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NR APP523636.

Part: FLOORBEAM — CORRODED (BS 645) · airframe 72,129 hrs · 15,898 cycles

CABIN BS645+66 AT RBL 32 FLOORBEAM UPPER CHORD CORRODED. REPAIRED PER 53-00-51 FIGURE 201 ON NR CARD APP521473 BY REPLACEMENT OF UPPER CHORD.

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 70,722 hrs · 15,737 cycles

APU FAULT LIGHT DURING START 2 ATTEMPTS. RTB, ECU FAULT FUEL CONTROL UNIT. REPLACED FUEL CONTROL UNIT PER M/M.

Part: UNKNOWN — UNKNOWN (APU) · airframe 70,541 hrs · 15,717 cycles

AFTER STARTING APU DUCT PRESS NEVER ROSE ABOVE 10 PSI WITH PACKS OFF. SHUT DOWN AND RESTARTED WITH NO SUCCESS. REPLACED TOTAL PRESSURE SENSOR, NO HELP. APU EGT AT 522 DEG C. IN DUCT PRESSURIZATION MODE. PER FIM AND APU SHOP 500 DEG C MAX NEEDS APU. REMOVED APU PN 3800298-1-5 SN P-1706 PER MM. INSTALLED APU PER MM 49-11-01. NO HELP. REPLACED ECU NO HELP. REINSTALLED ORIGINAL REPLACED SURGE VALVE CHECKS GOOD MCO AND PLAC REMOVED MFG P/N 979806-12.

Part: LINE — LEAKING (BRAKES) · airframe 66,590 hrs · 15,235 cycles

ON TAXI OUT IN DUB ANOTHER A/C REPORTED HYD LEAK ON RT MAIN GEAR. TOWED BACK TO GATE IN DUB. MTC FOUND NR 8 BRAKE LINE LEAKING. CAPPED OFF LINE AND SECURED. SVCD HYD. INSTALLED TEMP LINE. BLED LINE. LIMITED TO 350 HRS WITH 175 HR REINSPECT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,490 hrs · 15,223 cycles

EMERGENCY LIGHTS ON SEAT ROWS 32AB TO 40AB INOP C/A. REPLACED BATTERY CHARGER PACK M9010. OPS CHECK GOOD. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: MODULE — MALFUNCTIONED (SPOILERS) · airframe 64,731 hrs · 15,012 cycles

SPOILERS MSG SPOILERS LIGHT ILLUMINATED WITH SPEEDBRAKE HANDLE DOWN. ACCOMPLISHED T/S PER FIM 27-09-00/101 FIG 103. LIGHT GOES OFF, SYS OK NOW.

Part: APU — MAKING METAL (APU BAY) · airframe 63,980 hrs · 14,916 cycles

APU AUTO SHUTDOWN. BITE CHECK OF ECU SHOW APU STARTER REPLACED SAME, NO HELP. FOUND CHIP DETECTOR FULL OF METAL SHAVINGS. REMOVED AND REPLACED APU ASSY PER AMM. GROUND RUNUP LEAK CHECK GOOD.

Part: METERING VALVE — FAILED (NLG STEERING) · airframe 62,991 hrs · 14,797 cycles

T/O ABORTED AT 30 KNOTS DUE TO INABILITY TO MAINTAIN DIRECTIONAL CONTROL WITH RUDDER PEDAL STEERING, AC DRIFTED RAPIDLY LEFT WITH FULL RIGHT RUDDER APPLIED WITH BOTH ENGINES AT T/O POWER. STEERING CONTROL DURING TAXI APPEARED NORMAL. REPLACED STEERING METERING VALVE.

Part: PRESSURE SWITCH — FAILED (BOOST PUMP) · airframe 62,128 hrs · 14,684 cycles

RIGHT CENTER FUEL PUMP PRESSURE LIGHT INOP. REPLACED RIGHT OVERRIDE BOOST PUMP PRESSURE SWITCH.

Part: OVEN — BURNED (MID GALLEY) · airframe 60,290 hrs · 14,451 cycles

ON ARRIVAL F/A`S NOTICED A BURNED PLASTIC SMELL COMING FROM MID GALLEY NEAR ROW 5. REMOVED BURNT PLASTIC FROM TRAYS IN NUMBER 2 OVEN MID GALLEY. OVEN CHECKS GOOD. NO PLASTIC SMELL WHILE USING OVEN OR AFTER TURNING OVEN OFF. MCO AND PLACARD REMOVED.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 60,003 hrs · 14,410 cycles

EMERGENCY EXIT LIGHTS ON RT SIDE FROM MID GALLEY TO ROW 19 INOP. FOUND FUSE ON BATTERY PWR SUPPLY BLOWN. REMOVED AND REPLACED SAME, CHECKS GOOD.

Part: LOGIC CARD — LOOSE (E/E BAY) · airframe 59,678 hrs · 14,362 cycles

FIRE/OVERHEAT SYS EICAS ADVISORY ILLUMINATED DURING TAKEOFF. RESEATED CARDS. UNABLE TO DUPLICATE. TESTED SYSTEM.

Part: BUTTON — LACK OF LUBE (COCKPIT) · airframe 58,667 hrs · 14,208 cycles

AFTER T/O GEAR HANDLE WOULD NOT MOVE TO UP. IAW QRH USED LOCK OVERRIDE SWITCH TO RAISE HANDLE. GEAR HANDLE FELT STIFF WHILE RAISING IT. GEAR HANDLE CAME DOWN NORMALLY. PERFORMED BITE CHECK ON PSEU, NO FAULTS. FOUND MANUAL OVERRIDE BUTTON STUCK IN LUBED SHAFT ASSEMBLY AND PERFORMED GEAR HANDLE CHECK PER MM, OPS CHECK OK.

Part: INFLATOR — UNSERVICEABLE (OVERWING SLIDE) · airframe 56,886 hrs · 13,944 cycles

WORKING C/N C07234480 REPLACE LEFT SIDE OVERWING SLIDE INFLATOR S/N DL257. DISARMED LEFT SIDE OVERWING SLIDE PER M/M 25-65-02-004-001. REPLACED SLIDE INFLATOR. ARMED LEFT SIDE OVERWING SLIDE PER M/M 25-65-00-442-010 STEP 6 OF THE M/M, C/W SQUIB TEST, NR 2 EMG DID NOT TEST. FOUND ACTUATOR EXTENDED AND SQUIB FIRED. NOTE SPOILER WAS IN THE STOWED POSITION. REPLACED SPOILER ACTUATOR OVERRIDE OFF WING ESCAPE SLIDE.

Part: FITTING — CORRODED (T/E FLAP) · airframe 55,839 hrs · 13,797 cycles

DURING PSV IN ATLANTA, FOUND HOLES CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 089397-14MA REVISION A, REPAIR NR 4.

Part: FITTING — CORRODED (T/E FLAP) · airframe 55,839 hrs · 13,797 cycles

DURING PSV IN ATLANTA, FOUND A HOLE CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 089397-14MA REVISION A, REPAIR NR 1.

Part: DRAIN LINE — CLOGGED (E/E COMP) · airframe 54,957 hrs · 13,668 cycles

LEFT FWD LAV FLUID (2 GALS) CAME UP FROM UNDER FLOORBOARDS AT FWD ENTRY DOOR. FOUND FWD LAV, FWD GALLEY AND LEFT DOOR DRAIN LINE CLOGGED. CLEARED LINE, OPS CHECK GOOD. INSPECTED E/E COMP, ALL CHECK NORMAL.

Part: PRESSURE SWITCH — FAULTY (NR 2 ENGINE) · airframe 51,843 hrs · 13,200 cycles

DURING TAKEOFF AND CLIMB GOT A R ENG FUEL FILTER MESSAGE. MESSAGE GOES OUT BELOW 88 PERCENT N1. RETURNED TO JFK AFTER DUMPING FUEL. LANDED BELOW MAX LDG WEIGHT. FOUND DIFF PRESS SWITCH AT FAULT REPLACED SAME R/U AND LEAK CK OK. MAIN FUEL FILTER CLEAN. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: BATTERY — DISCHARGED (OVERWING SLIDE) · airframe 50,815 hrs · 13,027 cycles

WHILE PERFORMING AN ETOPS PRE-DEPARTURE CHECK THE EMERGENCY ESCAPE LEFT OVERWING SLIDE SQUIB FAILED. REPLACED BATTERY CHECKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 49,195 hrs · 12,740 cycles

ON L/O TEST, FOUND SQUIB TEST 1 AND 2 HAD ESCAPE SLIDE LIGHTS OUT FOR OVERWING SLIDES. REPLACED M962 POWER SUPPLY AND BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,023 hrs · 12,716 cycles

DURING ETOPS L/O CHECK, FOUND EMERGENCY LIGHT AT DOOR 3R INOP. RELAMPED, OP CK GOOD.

Part: SLIDE — UNSERVICEABLE (LT OVERWING) · airframe 47,957 hrs · 12,531 cycles

LEFT WING OVERWING SLIDE DEPLOYED DURING TAXI FROM HANGAR TO LINE. REPLACED DOOR ACTUATOR.

Part: FRAME — CRACKED (NR 1 ENGINE) · airframe 47,746 hrs · 12,496 cycles

ON MTC CHECK FOUND 6.75 INCH CRACK AT TURBINE REAR FRAME. REPLACED ENGINE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,167 hrs · 12,391 cycles

RT SIDE AFT FUSELAGE EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OK.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 47,165 hrs · 12,389 cycles

AUTO PRESS CONTROLLER 1 AND 2 FAILED. F/A REPORTED FUMES IN AFT CABIN. RESET CONTROLLERS, NO FAULTS. RAN PACKS, OK. RAN ENGINES AND PRESSURIZED, ALL OK. NO ODORS NOTED IN CABIN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,309 hrs · 12,248 cycles

OVERWING EMERGENCY ESCAPE SYS SQUIB TEST 1 FAILED ON LEFT SIDE. TEST 2 FAILED ON RIGHT SIDE. REPLACED EMERGENCY BATTERIES M961 AND M962 PER M/M. ALL SQUIB, TESTS OK.

Part: FITTING — MISMANUFACTURED (LT WING) · airframe 44,721 hrs · 11,941 cycles

DURING ACCOMPLISHMENT OF REWORK TO THE LT STRUT AS DETAILED IN THE STRUT IMPROVEMENT PROGRAM THE INBOARD AFT PITCH LOAD FITTING WAS INCORRECTLY MACHINED. REPAIR ER/A 398045-14AD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 44,661 hrs · 11,933 cycles

OVERHEAD EMERGENCY LIGHT INOP AFT CABIN. REPLACED POWER SUPPLY.

Part: CHARGER — FAILED (CABIN) · airframe 42,576 hrs · 11,624 cycles

LEFT EMERGENCY SLIDE SQUIB TEST FAILED DURING EPDC TEST. REPLACED CHARGER M00962 AND BATTERY. ESCAPE SLIDE SQUIBS TEST GOOD.

Part: POWER SUPPLY — SHORTED (CABIN) · airframe 40,688 hrs · 11,277 cycles

STROBE LIGHT PWR SUPPLY UNIT IN OVHD BEGAN MAKING CLICKING SOUND 1.5 HRS INTO FLT. GOT PROGRESSIVELY WORSE WITH OCCASIONAL SPARKING. DISCONNECTED CANNON PLUG SOUND AND SPARKING STOPPED. REPLACED POWER SUPPLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,619 hrs · 11,260 cycles

ON FINAL APPROACH, F/A'S REPORTED BURNING RUBBER ODOR IN AFT CABIN, RIGHT SIDE, LAST ROW OF SEATS NEAR CLOSET. IT QUICKLY DISSIPATED AND DID NOT RETURN. INSPECTED AFT CABIN, LAV, GALLEY, EEMK KIT AND ROCKWELL COLLINS EQUIPMENT. NO ODORS OR DEFECTS NOTED.

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 40,484 hrs · 11,234 cycles

SMOKE AND ELECTRICAL SMELL CAME FROM BEHIND COFFEEMAKERS IN AFT GALLEY ON CAPTS SIDE. ALL C/B''S IN GALLEY PULLED AND BOTH UTILITY BUSSES SWITCHED OFF. SMOKE DISSIPATED. INSPECTED CHILLER AREA AND WIRING IN AFT CARGO BIN. NO DEFECTS NOTED. FOUND HEAVY ELECTRICAL ODOR AT COFFEEMAKERS ON CAPTS SIDE. REPLACED BOTH COFFEEMAKERS AND RAN POWER IN AFT GALLEY FOR 30 MINS TO ALL ELECTRICAL COMPONENTS. NO SMELL OR SMOKE EVIDENT.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 40,210 hrs · 11,189 cycles

CREW MEMBERS SMELLED ACRID POSSIBLE ELECTRICAL ODOR EMANATING FROM OVERHEAD REAR GALLEY. AFT GALLEY EQUIPMENT DEACTIVATED AS A PRECAUTION. MTC PERFORMED INSPECTION TO AFT GALLEY AND ABOVE CEILING. NO SMELL NOTED. FOUND NR 4 AND 6 OVENS WITH PLASTIC MELTED ON THE BOTTOM OF THE FAN/HEATING ELEMENT SHROUD. REPLACED OVENS, OPS OK.

Part: BATTERY PACK — INOPERATIVE (RT OVERWING) · airframe 39,778 hrs · 11,113 cycles

DURING L/O, FOUND SQIB TEST 1 FAILS EMERGENCY ESCAPE SLIDE LT AND SQUIB TEST 2 FAILS EMERGENCY ESCAPE RT. REPLACED BATTERY PACK, SYSTEM OPS CHECK NORMAL.

Part: BRAKE — OVERHEATED (LT MLG) · airframe 39,314 hrs · 11,038 cycles

ON ARRIVAL, NR 5 BRAKE CAUGHT ON FIRE WITH VISIBLE FLAME. FLAME EXTINGUISHED WITH FIRE EXTINGUISHER, POWDER. PRECAUTIONARY REMOVAL OF NR 5 BRAKE IAW 32-41. CHECKED FOR HYD LEAKS OK. CHECKED FOR BURN MARKS AND HOT SPOTS. ALL OK.

Part: LIGHT — INOPERATIVE (SEAT 11 - 27)

EMERGENCY EXIT LIGHTS FROM SEAT 11 TO 27 OVERHEAD AISLE RT LIGHTS INOP.

Part: BATTERY — DISCHARGED (CABIN)

DURING SQUIB TEST, FOUND EMERGENCY ESCAPE SQUIBS NOT TESTING PROPERLY. FOUND MODULE M08962 BATTERY BAD. REPLACED SAME, ALL CKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMER EXIT)

RIGHT HAND AFT TWO WING SLIDE EMERGENCY LIGHTS ARE INOP AND R3 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED POWER SUPPLY.

Part: SKIN — DELAMINATED (NR9 LE SLAT)

WING NR 9 SLAT TRAILING EDGE WEDGE, UPPER SKIN, REPAIR FOR DELAMINATION. THE UPPER SKIN OF THE TRAILING EDGE WEDGE OF THE NR 9 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF DELAMINATION. THE DAMAGED AREA WAS CUT AWAY AND REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 366723-14AD.

Part: EICAS — MALFUNCTIONED (LEFT)

LEFT EICAS FAULT INDICATION, DIVERTED TO JFK. BITE CHECK SHOWED PROG PIN ERROR, TEST FAIL, LEFT COMP FAIL, CU CODE 0200 - 0080 DISCRETE 202 -210. REPLACED LEFT EICAS COMP AND PSEU. CHECKED FOR PUSHED BACK PINS, FOUND NONE. SYSTEM CHECKS OK. OVERWEIGHT LANDING INSPECTION PERFORMED PER 5-51-35-2. NO DAMAGE FOUND.

Part: TERMINAL — LOOSE (LT WINDOW)

STRONG SMELL OF SMOKE, LOWER CORNER OF CAPTS FWD WIND SCREEN VERY HOT. TURNED OFF WINDOW HEAT AND SMELL WENT AWAY. FOUND TERMINAL FOR LOWER CORNER LOOSE AND ARCING. CLEANED TERMINAL AND TIGHTENED SCREW. FOUND NO DAMAGE TO WINDOW AND NO FAULTS ON WINDOW HEAT CONTROLLER, ALL CHECKS NORMAL.

Part: SKIN — DELAMINATED (RT LE SLAT)

THE NR 11 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED ALONG THE O/B EDGE. THE DAMAGE MEASURES 3 X 3. THE DAMAGE WAS REPAIRED USING AN SRM COMPOSITE REPAIR AUTHORIZED BY ER/A 364970-14AD.

Part: SKIN — DELAMINATED (NR 4 LE SLAT)

THE NR 4 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED AT A LOCATION 6 INCHES FROM THE O/B END. THE DAMAGE MEASURES APPROX 4 X 4 AND WAS REPAIRED USING AN SRM COMPOSITE REPAIR PER ER/A 364971-14AD.

Part: SKIN — DELAMINATED (NR 5 LE SLAT)

THE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THTE I/B EDGE 3 FWD OF THE TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURES APPROX 5 (FWD/AFT) X 12. THE DAMAGE WAS REPAIRED WITH AN SRM COMPOSITE REPAIR PER ER/A 364968-14AD.

Part: SKIN — DELAMINATED (NR 6 LE SLAT)

THE NR 6 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THE O/B EDGE 1 FWD OF THE TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURED 2 X 2 AND WAS REPAIRED USING SRM COMPOSITE REPAIR PER ER/A 364972-14AD.

Part: SKIN — DELAMINATED (NR 2 LE SLAT)

THE NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED ALONG THE I/B EDGE 4 FWD OF THE TRAILING EDGE. THE DELAMINATED AREA MEASURES 4 X 4. THE DAMAGE WAS REPAIRED USING AN SRM COMPOSITE REPAIR AUTHORIZED BY ER/A 364969-14AD.

Part: SIGN — INOPERATIVE (CABIN)

ON L/O, FOUND RT AFT EMERGENCY EXIT SIGN INOP. REPLACED PWR SUPPLY.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY TRACK LIGHTS INOP B/C AISLE RT SIDE CLEANED AND REFASTENED CONNECTORS. SYSTEM OPS CHECKS GOOD.

Part: OVEN — SMOKING (GALLEY)

SMOKE IN GALLEY FROM OVEN. CLEANED PLASTIC FROM OVEN HEATING COILS.

Part: SKIN — DENTED (BS 1197)

A DENT WAS FOUND IN SKIN BETWEEN FRAME STATIONS 1197 + 44 AND 1197 + 66 JUST BELOW S25L. THE DAMAGE WAS CUTOUT PER SRM 53-00-01-2. THE CUTOUT IS APPROX 2.25 BY 4.75. IF REPAIR PER SRM, THE RIVET SPACING WILL CAUSE THE REPAIR TO OVERLAP THE SKIN LAP SPLICE. PER ER/A- ACCOMPLISH SOLID RIVET REPAIR PER B767-300 SRM 53-00-01, FIGURE 201 EXCEPT EXTEND LOWER END OF DOUBLER TO PICKUP SECOND ROW OF EXISTING LAP-SPLICE FASTENERS. ALODINE, FR PRIME, SEAL FAYING SURFACES, INSTALL WITH SEALANT, ID AS TIME-LIMITED (12 MONTHS SERVICE).