N153DL

Part: SUPPORT BRACKET — CRACKED (NR 2 PYLON) · airframe 113,336 hrs · 21,220 cycles

WHILE PERFORMING NR 2 ENGINE CHANGE EXPOSED PYLON INSPECTION FOUND PYLON AFT FINGER SEAL SUPPORT BRACKET CRACKED AND DAMAGED. REPLACED SKIRT ANGLE & RUB STRIP.

Part: BULKHEAD — CORRODED (LT MLG WW) · corrosion level 2 · airframe 111,714 hrs · 20,967 cycles

CORROSION LEVEL 2 LEFT MLG WHEEL WELL FWD SPAR BULKHEAD AT BS 955 LBL 70 FOUND CORROSION. REPAIRED PER ERA 555745-14.

Part: FORK — CORRODED · airframe 111,982 hrs · 21,006 cycles

DURING C CHECK, CORROSION WAS NOTED UNDER THE FORK FITTING. COMPLIED WITH ERA 555745-14

Part: SKIN — CRACKED (BS 1725) · airframe 111,711 hrs · 20,966 cycles

FUSELAGE SKIN AT BS 1725, STRINGER 7R FOUND CRACKED. REPAIRED IAW SRM 53-80-01 AND ERA 555753-14.

Part: SKIN — CRACKED (BS 687) · airframe 111,711 hrs · 20,966 cycles

HFEC INSPECION FOUND ONE CRACK ON THE SKIN ALONG THE EDGE OF THE COVER PLATE AT BS 687 BETWEEN STRINGERS 36 AND 37R. DAMAGE CUT OUT IAW SRM 53-00-01. NO CRACK FOUND AND REPAIRED THE SKIN.

Part: SKIN — CRACKED (BS 687) · airframe 111,711 hrs · 20,966 cycles

HFEC INSPECTION FOUND ONE CRACK ON THE SKIN ALONG THE EDGE OF THE COVER PLATE AT BS 687 BETWEEN STRINGERS 36 AND 37R. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DELAMINATED (NR 9 SLAT) · airframe 111,711 hrs · 20,966 cycles

RIGHT WING NR 9 SLAT INBD EDGE FOUND DELAMINATED. REPAIRED IAW SRM 51-70-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 110,267 hrs · 20,738 cycles

R4 DOOR OUTSIDE EMERGENCY LIGHT OUT. REPLACED THE LAMPS. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 110,237 hrs · 20,730 cycles

LADDER EXIT SIGN FOUND INOPERATIVE AND RELAMPED. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 110,237 hrs · 20,730 cycles

FORWARD EXIT SIGN FOUND INOPERATIVE AND RELAMPED. SYSTEM OPERATION IS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 110,214 hrs · 20,725 cycles

LAVATORY 202 WALL MOUNT EMERGENCY LIGHT CLEAR LENS MISSING. REPLACED THE LENS. SYSTEM OPS NORMAL.

Part: FRAME — CRACKED (BS 1809 BULKHEAD) · airframe 110,477 hrs · 20,770 cycles

BS 1809 BULKHEAD LT FORWARD OUTER FRAME CRACKED. REPAIRED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 111,138 hrs · 20,873 cycles

DURING WALK AROUND FOUND FUSELAGE SKIN CORROSION AT STA 1583 BETWEEN S-25R AND S-25L. REPAIRED PER ERA 543061-14.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 106,143 hrs · 20,090 cycles

FOUND EMERGENCY ESCAPE LIGHT AT SEAT 39AB INOPERATIVE. MAINTENANCE CONFIRMED LIGHT BULB ASSEMBLY AND POWER AT WALL WORKS BUT BOTH WIRES SHOW OPEN BETWEEN WALL AND LIGHT BULB ASSEMBLY. REPLACED HARNESS AT 39AB CONNECTED LIGHT BULB ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — CRACKED (BS 1809) · airframe 104,238 hrs · 19,812 cycles

BS 1809.5, INSPECTION AREA, LT SIDE FWD OUTER CHORD HAS 3 INCH CRACK. REPAIRED IAW ERA 536828-14AD.

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 106,758 hrs · 20,193 cycles

GROUP A, HOLE NR 1 HAS CRACK INDICATION AT .288, REWORKED ON AMDS 5724-01010-06.

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 106,758 hrs · 20,193 cycles

GROUP A, HOLE NR 1 HAS CRACK INDICATION AT .288, REWORKED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 102,728 hrs · 19,608 cycles

LOWER BULKHEAD FOUND DAMAGED STRINGER 32R. REPAIRED IAW ERA 532913-14.

Part: LIGHT — DAMAGED (CABIN) · airframe 98,562 hrs · 19,023 cycles

CABIN AFT DOOR LOWER CEILING NR 2 EMERGENCY LIGHT ASSY FOUND DAMAGED. REPLACED. SYS OPS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 98,562 hrs · 19,023 cycles

NR 1 CEILING EMERGENCY LIGHT ASSY FOUND DAMAGED. REPLACED. SYS OPS NORMAL.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 98,562 hrs · 19,023 cycles

AFT RT DOOR CUTOUT EMERGENCY EXIT SIGN FOUND DAMAGED. REPLACED. SYSTEM OPS NORMAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 111,658 hrs · 20,957 cycles

SEAT TRACK FWD END BS 342 TO BS 424 RBL 88.5 CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,658 hrs · 20,957 cycles

CORROSION LEVEL 2, CABIN STA 1209 TO STA 1428 CORRODED SEAT TRACK. REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED.

Part: SCUFF PLATE — CORRODED (GIRT BAR) · airframe 111,686 hrs · 20,962 cycles

FWD DOOR AFT GIRT BAR FITTING LOWER ATTACH SCUFF PLATE MOUNT CORRODED. REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 97,405 hrs · 18,854 cycles

EMERGENCY LIGHT INOPERATIVE ON RT SIDE OF ACFT SEATS 15-19. REPLACED BATTERY PACK.

Part: WIRE — ARCED (CHILLER) · airframe 95,874 hrs · 18,667 cycles

CHILLER WIRES ARCING TO FLOORBEAM, BRACKET AND ROD END FOR POTABLE WATER TANK-BURNED FWD INBD ATTACH ROD STA 1562, BULK CARGO. MX REMOVED BRACKET AND ROD, REMOVED DAMAGE, DAMAGE WITHIN LIMITS IAW SRM 53-00-51. TREATED AND PAINTED BEAM IAW SRM 53-00-51, FIG 101 (324630). NEW BRACKET FABRICATED AND INSTALLED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 91,628 hrs · 18,131 cycles

ON DESCENT, EMERGENCY LIGHTS CAME ON. FOUND LOOSE CONNECTOR ON CHARGER. SECURED CONNECTOR AND REPLACED BATTERY PACK AT CHARGER LOCATED AT 38G. SYSTEM OPS CHECKED NORMAL PER AMM SEC 33-51.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 91,628 hrs · 18,131 cycles

ON DESCENT HALFWAY BACK IN COACH, THE EMERGENCY LIGHTS CAME ON. FOUND LOOSE CONNECTOR ON CHARGER. CONNECTED AND REPLACED BATTERY PACK AT CHARGER LOCATED AT 38G. SYSTEM OPS CHECKED NORMAL PER BAMM 767-300.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,977 hrs · 18,055 cycles

EMERGENCY LIGHT INOPERATIVE FROM ROW 15AB TO 18AB POWER SUPPLY M9011. REMOVED ALSO 15GF AND GALLEY M2 ALL ON BATTERY PACK M9011. MAINTENANCE REINSTALLED POWER SUPPLY AND FOUND L2 INBOARD AFT RED LIGHT ASSY SHORTED AND REPLACED LIGHT ASSY. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DENTED (TE FLAP) · airframe 90,296 hrs · 17,976 cycles

ON ARRIVAL FOUND SLIGHT DAMAGE TO RIGHT WING O/B FLAP UNDERSIDE. C/W REPAIR DATA B767-300 SRM 57-53-03 REPAIR 1 AND B767-300 SRM 51-70-10 REPAIR 2 FIG 203.

Part: SPAR — CORRODED (TE FLAP) · airframe 90,296 hrs · 17,976 cycles

RT WING I/B MAIN FLAP STA 124 REAR SPAR LOWER CHORD CORROSION. C/W PERMANENT REPAIR AS PER ERA 496155-14 REV A. SECTION II.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,295 hrs · 17,975 cycles

FS 1197+66 BL-28L FLOORBEAM UPPER CHORD HORIZONTAL FLANGE IS CORRODED AND REPAIRED PER B767-300 SRM 53-00-07 REPAIR 4 FIG 201 DETAIL III (NRC 52689).

Part: SKIN — DELAMINATED (TE FLAP) · airframe 90,295 hrs · 17,975 cycles

RT WING O/B TRAILING EDGE FLAP LWR SURFACE FOUND DELAMINATED AT I/B LWR SIDE. REPAIRED IAW B767-300 SRM 57-53-01 REPAIR 1 TABLE II AND SRM 51-70-01 PARA 5A FIG 9.

Part: SPAR — CORRODED (TE FLAP) · airframe 90,295 hrs · 17,975 cycles

RT WING I/B FLAP STA 124 REAR SPAR LOWER CHORD CORRODED. PERMANENT REPAIR PERFORMED IAW ERA 496155-14 REV 0.

Part: FLAP — DENTED (RT WING) · airframe 90,295 hrs · 17,975 cycles

RT WING O/B FLAP LWR SIDE FOUND DENT. REPAIRED IAW B767-300 SRM 57-53-01 REPAIR 1 AND REPAIR INSTRUCTION IAW B767-300 SRM 51-70-10 REPAIR 2 FIG 203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,295 hrs · 17,975 cycles

CABIN STA 355 RBL 45-49 FLOORBEAM UPPER CHORD CORRODED. REPAIRED IAW B767-300 SRM 53-00-51 FIG 201 REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,295 hrs · 17,975 cycles

CABIN STA 287 RBL 26 FLOORBEAM UPPER CHORD CORRODED. REPAIRED IAW B767-300 SRM 53-00-51 FIG 201 REPAIR 1.

Part: WEDGE — DENTED (LE SLAT) · airframe 90,295 hrs · 17,975 cycles

LEFT WING NR 5 SLAT EXT UPPER WEDGE SURFACE DENTED. REPAIR DATA REFERENCE B767-300 SRM 57-43-02 REPAIR 1 AND THE REPAIR INSTRUCTIONS REFER B767-300 SRM 51-70-10 REPAIR 2 FIG 203.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 90,295 hrs · 17,975 cycles

LEFT WING NR 5 SLAT EXT WEDGE UPPER O/B CORNER DELAMED. REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,295 hrs · 17,975 cycles

CABIN STA 654+66 RBL 20 TO RBL 29 FLOORBEAM UPPER CHORD CORRODED. REPAIRED PER B767-300 SRM 53-00-51 FIG 201 REPAIR 1.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 90,295 hrs · 17,975 cycles

O/B MAIN FLAP LWR SURFACE MUD SECTION FOUND DELAM. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE II AND SRM 51-70-07 PARA 5A(1) FIG 9.

Part: STRUCTURE — DAMAGED (PYLON) · airframe 89,289 hrs · 17,855 cycles

PYLON REWORK IAW ERA 389666-14.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 84,659 hrs · 17,305 cycles

EMERGENCY LIGHT AT SEAT 21GF ARE INOPERATIVE. MX SECURED THE CONNECTOR AT SIDEWALL. SYS OPS IS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 84,508 hrs · 17,287 cycles

EMERGENCY LIGHT AT 35B IS INOPERATIVE. MX RE-PINNED THE HARNESS. SYS OPERATION IS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 84,508 hrs · 17,287 cycles

EMERGENCY LIGHTS AT SEAT 14B WERE INOPERATIVE. MX RE-PINNED THE HARNESS. SYS OPS IS NORMAL.

Part: CDU — FAILED (COCKPIT) · airframe 84,145 hrs · 17,246 cycles

LEFT CDU FAILED ACCOMPANIED BY A SMALL WISP OF SMOKE. SMELL AND SMOKE DISSIPATED, CIRCUIT BREAKER WAS PULLED. MAINTENANCE REMOVED LEFT CDU AND CLEANED DEBRIS. NO SMELL OR SMOKE IN AREA. SYSTEM OPERATION IS NORMAL. (2010-D1292) (DL76G102946)

Part: SPAR — DAMAGED (LT WING) · airframe 84,126 hrs · 17,244 cycles

LT FRONT SPAR WEB RIB 8 HOLE. REPAIRED IAW ERA 486556-14.

Part: FITTING — DAMAGED (LT WING) · airframe 84,126 hrs · 17,244 cycles

LT WING SKIN AFT PITCH LOAD FTG HOLES. REPAIRED IAW ERA 486412-14.

Part: SKIN — DAMAGED (LT WING) · airframe 84,126 hrs · 17,244 cycles

TOOLING DAMAGE TO LEFT WING LOWER SKIN FASTENER HOLE AFT INBOARD HOLE COMMON TO AFT PITCH LOAD FITTING, DAMAGED OCCURRED DURING THE ACCOMPLISHMENT OF SIP MOD. DISCREPANT HOLE WAS OVERSIZED AND STRAIGHT SHANK REPAIR BUSHING INSTALLED AND RE-INSTALLATION COMPLIED WITH SIP MOD PER SB 767-54-0081 (DL76G102856).

Part: ANGLE — CRACKED · airframe 84,053 hrs · 17,234 cycles

FOUND CLOSEOUT ANGLE CRACKED WHILE CONDUCTING INSP IAW 1T204. CONDUCTED HFEC INSP OF BOLT HOLES IAW EA 01-074944-12ADME04. NO FURTHER DAMAGE NOTED. REPLACED CLOSEOUT ANGLE IAW DWG 311T2150.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,442 hrs · 16,933 cycles

EMERGENCY LIGHTS IN CEILING, RT SIDE FIRST CLASS AISLE IS INOPERATIVE. MX FOUND THE BATTERY PACK BAD AND REPLACED THE BATTERY PACK. SYS OPS IS NOW NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,442 hrs · 16,933 cycles

EMERGENCY LIGHTS IN CEILING RT SIDE 1ST CLASS AISLE INOPERATIVE. FOUND BATTERY PACK BAD R & R BATTERY PACK CHECKS GOOD.

Part: FAILSAFE — CORRODED (FS 955) · airframe 81,440 hrs · 16,932 cycles

WHILE ACCOMPLISHING INSPECTIONS OF THE FS955 REAR SPAR BULKHEAD SIDE FRAME AND FAIL SAFE STRAP FOR CORROSION AND FATIGUE CRACKS IN ACCORDANCE WITH DAL S.I. 01-086393-12AD, A CRACK INDICATION AND CORROSION WERE FOUND ON THE RH SIDE FAILSAFE STRAP AND CORROSION WAS FOUND ON THE SKIN. REPAIRED PER ERA 480089-14AD.

Part: FAILSAFE — CORRODED (FS 955) · airframe 81,440 hrs · 16,932 cycles

A CRACK INDICATION WAS FOUND AT THE LOWER BOLT HOLE DURING ULTRASONIC INSPECTION OF THE FAIL SAFE FITTING IN THE LT MAIN LANDING GEAR WHEEL WELL PER SI 01-086393-12AD. REPAIRED PER ERA 480088-14AD.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 81,440 hrs · 16,932 cycles

FUSELAGE STRINGER LBL & RBL 85.9 FS 966 SPLICE. REPAIRED IAW ERA 480170-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,438 hrs · 16,931 cycles

EMERGENCY LIGHTS ON CEILING RT AFT SIDE INOP. REPLACED BATTERY PACK OF P/S M734.

Part: PROCESSOR — MALFUNCTIONED (TCAS) · airframe 80,010 hrs · 16,747 cycles

ON TAXI OUT TCAS PROCESSOR AND XNDR TCAS DATA MSG ON RADAR INDICATOR. REPLACED TACS PROCESSOR. SYS TEST OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: SHUTOFF VALVE — MALFUNCTIONED (LEFT) · airframe 78,478 hrs · 16,566 cycles

LEFT SYS BLEED FAILED AFTER TAKEOFF WOULD NOT RECOVER. TROUBLESHOT PER FIM REPLACED L AIR BLEED CONTROL CARD NO HELP. REPLACED LEFT HPSOV CHECKED HPSOV PEP M/M. RAN ENGINES AND THE LEFT BLEED AIR CHECKED GOOD.

Part: CONNECTOR — DIRTY (NR 1 ENGINE) · airframe 78,119 hrs · 16,525 cycles

NO OIL PRESS ON EICAS AND L ENG OIL PRESS LIGHT REMAINED ILLUMINATED ON LT ENG START ATTEMPT. TROUBLESHOT AND COMPLIED WITH QRH. CLEANED CONNECTORS OIL PRESSURE TRANSMITTER AND LOW OIL PRESSURE SWITCH. PERFORMED ENGINE RUN. ALL INDICATIONS NORMAL.

Part: APU — ODOR (APU BAY) · airframe 72,139 hrs · 15,841 cycles

STRONG OIL ODOR ENTIRE A/C W/PACKS RUNNING. INSP APU AND APU BLEED DUCT NO OIL FND. INSP PACKS BAYS NOTHING ABNORMAL. RAN PACKS INDEPENDENTLY TRYING TO DETERMINE WHICH HAD MORE SMELL. PERFORMED DUCT BURNOUT UP TO STEP 10 PER M/M 250083. REPLACED APU PER AMM. FINISHED DUCT BURNOUT PER AMM 21-00-2.

Part: LINK — UNKNOWN (TE FLAP) · airframe 72,022 hrs · 15,827 cycles

FLAP LINK REPLACED IAW EA 01-076248-12, ME07, ME08, ME09, ME,10, ME11, ME12.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 71,852 hrs · 15,808 cycles

RIGHT HYD QTY EICAS MESSAGE WITH RT HYD QTY LIGHT. RT SYSTEM QTY INDICATING 0.47 WITH RF AND DECREASING SLOWLY 5 HOURS AND 20 MIN INTO FLIGHT. REPLACED LINE WITH BORROW PART FROM AIR FRANCE. FOUND RT ENG EDP HYDRAULIC PRESS HOSE ASSEMBLY LEAKING. REPLACED HOSE ASSEMBLY RAN ENG LEAK CHECK PERFORMED FOUND NML PART PROVIDED BY AIR FRANCE, MPN AE1010744M0174.

Part: UNKNOWN — WARNING LIGHT (SLATS) · airframe 71,353 hrs · 15,747 cycles

EICAS MSG LE SLAT DISAGREE DISPLAYED. LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1, BOTH FLAP POINTERS. FSEU CHECKED, NO FAULT EPSU CHECKED FOUND SENSOR 302. FAULTY TARGET FOUND FULL OF GREASE, CLEANED SYSTEM. OPERATED SEVERAL TIMES, OP`S OK.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 70,246 hrs · 15,618 cycles

DURING ENGINE START, LT ENGINE, AS THE L FUEL CONTROL SWITCH WAS PLACED ON, THESE INDICATIONS APPEARED - 1 EICAS L ENG FUEL VLV MSG 2 ENG VLV LIGHT ON PEDESTAL ENGINE WOULD NOT START NO EGT RISE FUEL CONTROL SWITCH WAS PLACED OFF APPROX 2 MINUTES LATER THE ABOVE EICAS MSG AND VLV LIGHT EXTINGUISHED. RESTARTED ENGINE, AT GATE CHKS GOOD.

Part: PROJECTOR — OVERHEATED (FWD CBN) · airframe 68,775 hrs · 15,449 cycles

MID CABIN PROJ OVERHEATED WITH WHITE SMOKE AND ELECTRICAL ODOR. INSTALLED FWD VIDEO PROJ. MID PROJ PREVIOUSLY REPLACED WITH PROJ PER EA 01-461217-14, AND FWD POSITION EMPTY. MCO AND P REMOVED.

Part: PROJECTOR — OVERHEATED (CABIN) · airframe 68,775 hrs · 15,449 cycles

FLT CREW REPORTED THE FIRST CLASS OVERHEAD PROJECTOR, OVERHEATED WITH WHITE SMOKE AND BURNT ELECT SMELL. USED HALON FIRE BOTTLE TO EXTINGUISH ONBOARD AMT DEACTIVATED AND REMOVED PROJECTOR TO ENSURE FIRE WAS EXTINGUISHED. INSTALLED FWD VIDEO PROJ. MID PROJ PREVIOUSLY REPLACED WITH PROJ PER EA 01-461217-14 AND FWD POSITION EMPTY. MCO AND P REMOVED. DEFECTIVE PROJ REMOVED AND DELIVERED TO HANGAR FRO DESK FOR QUARANTINE.

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY) · airframe 67,180 hrs · 15,247 cycles

LT UTIL BUSS DROPPED OFF AFTER STARTING LT ENG. REPLACED ELEC SYST CONTRL PNL AND BPCU PER THE M/M. OPS CKS OK.

Part: RIB — GOUGED (RT WING) · airframe 66,939 hrs · 15,217 cycles

A GOUGE WAS FOUND ON THE INBOARD SIDE OF THE NR 4 RIB OF THE AFT WEB, RHS WING. REPAIRED PER BOEING INSTRUCTIONS AS DETAILED IN ERA 454124-14

Part: BULKHEAD — CRACKED (BS 287 LBL 25) · airframe 66,688 hrs · 15,186 cycles

THE NLG WHEELWELL, STA. 287 BULKHEAD, LBL 25 VERTICAL CHORD WAS CRACKED. THE CRACK WAS STOP DRILLED INSTEAD OF CUT OUT AS SPECIFIED IN THE SRM. THE EXISTING REPAIR WAS REMOVED AND THE CRACKED AREA CUT OUT AND A REPAIR ANGLE WAS REINSTALLED IAW THE SRM. REF AD 2005-02-02.

Part: ENGINE — FIRE (NR 1) · airframe 65,403 hrs · 15,035 cycles

LEFT ENG FIRE ON DEPARTURE RETURNING TO GIG. REPLACED NR 1 ENG PER TRAN 1T160.

Part: SWITCH — INACCURATE (FUEL CUTOFF) · airframe 65,009 hrs · 14,989 cycles

HUNG START LT ENG CRASH ENG STARTER TO EXT TAIL PIPE FIRE. REPLACED LT ENG FUEL CUTOFF SWITCH WRANG OUT, REF WDM 76-11-11 AND 28-22-21 CKS OK REQS OPS CHECK. PERFORMED ENG RUN PER MM OPS NORMAL.

Part: SENSOR — OUT OF ADJUST (NR 8 SLAT) · airframe 64,619 hrs · 14,944 cycles

ON CLIMB-OUT, SLAT ASYMMETRY LIGHT AND INDICATION WAS INTERMITTENT. REPLACED NR 8 OB SLAT SENSOR. REPLACED WIRE W480-001-18 AND PER MM. CHECKS NORMAL. SLATS CHECK NORMAL PER MM.

Part: LATCH — FAILED (LT OFFWING SLIDE) · airframe 62,602 hrs · 14,680 cycles

DURING LEFT WING SLIDE REPLACEMENT FOUND DOOR LATCH NR 3 BROKEN. REMOVED AND REPLACED LEFT OFFWING SLIDE COMPARTMENT DOOR LATCH NR 3 PER AMM.

Part: PSEU — FAILED (E/E BAY) · airframe 59,529 hrs · 14,284 cycles

AT APPROX 96 KNOTS CREW RECEIVED T/O CONFIG WARNING MESSAGE T/O WAS ABORTED A/C RETURNED TO GATE FOR REPAIRS. REPLACED PSEU M162 WAS AND FSPM M839.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 58,973 hrs · 14,203 cycles

WHILE T/S NBR 2 ENG T/R NOT STOWING, FOUND DAMAGE TO RIGHT T/R COWL. REPLACED REVERSER. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: SEAL — BLOWN (LT BLEED DUCT) · airframe 57,341 hrs · 13,967 cycles

LEFT BLEED DUCT LIGHT AND MESSAGE. FOUND SEALS BLOWN IN LEFT WING ROOT DUCT AREA. REPLACED SEALS.

Part: ODOR — DETECTED (CABIN) · airframe 51,733 hrs · 13,140 cycles

0913 13 JUL GRU 2509601- THERE WAS A MILD ELECTRICAL SMELL AROUND SEATS 11C, 12C WHICH STOPPED WHEN THOSE OVERHEAD PANEL READING LIGHTS WERE TURNED OFF ATL MCC/MC/0236Z. INSPECTED READING LIGHT PANELS AND AREA AROUND MENTIONED SEATS NOTHING ABNORMAL FOUND. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 51,103 hrs · 13,032 cycles

FOUND CHAFED WIRE AT SEAT 10A. REPAIRED WIRE. AND REPLACED FUSE. OPS CHECK OK.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 49,695 hrs · 12,768 cycles

TWO AUDIBLE STALLS INTO ATL. DURING RT ENG BORESCOPE FOUND BLADE DAMAGE ON 12TH STAGE OF THE COMPRESSOR AND 1ST STAGE OF THE HPT. REPLACED ENGINE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,858 hrs · 12,272 cycles

EMERGENCY ESCAPE SYS FAILS SQUIB TEST. REPLACED LEFT ESCAPE BATTERY PACK, OPS OK.

Part: ROD — SHEARED (WATER TANK) · airframe 44,855 hrs · 11,918 cycles

ON TAKEOFF FROM FRA HEARD BANGING SOUND, THERE AFTER LOST ALL POTABLE WATER. FOUND 2 TIE RODS SHEARED AND MAIN WATER TANK LEAKING AT LOWER FITTING AND FIBERGLASS SURROUND. DRAINED WATER TANK AND SECURED TANK WITH CARGO STRAP, WATER COMPRESSOR C/B ON P33 PNL PULLED/COLLARED. REQ TANK REPAIR AND 2 TIE RODS (P/N 381202073). FWD TO MCO AND PLACARD PER MEL 38-10-0.IPC REF 38-11-01-01.

Part: PROJECTOR — MALFUNCTIONED (CABIN) · airframe 44,854 hrs · 11,917 cycles

SMOKE SMELL FROM FORWARD PROJECTOR AREA IN MAIN CABIN AS WELL AS VIDEO CLOSET RED POWER SWITCHES 2. SMELL PERSISTED AS LONG AS POWER WAS ON THE PROJECTOR. GREEN STATUS LIGHT ON UNIT LIT. SMELL DIMINISHED WHEN CB/S PULLED. NO SMOKE SEEN ONLY BAD HOT SMELL PRESENT. REPLACED PROJECTOR WHICH WAS ALSO BAD FROM STOCK. DEFER TO MCO.

Part: FAN — FAILED (E/E BAY) · airframe 44,241 hrs · 11,815 cycles

IN CRUISE AT FL 370 A STRONG ODOR OF BURNING PLASTIC. FOLLOWED BY FWD EQUIPMENT EXHAUST FAN C/B POPPING AND FWD EQUIPMENT EXIT FAN STATUS MSG. REPLACED FWD EQUIPMENT EXHAUST FAN PER MM. OPS CHECK NORMAL. S/N OFF 1529, S/N ON 5586A, P/N 211002542.

Part: MANIFOLD — CRACKED (#2 ENGINE) · airframe 43,538 hrs · 11,706 cycles

RT ENG FUEL MANIFOLD LEAK.REMOVED AND REPLACED FUEL PIPE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: OVEN — FAULTY (GALLEY) · airframe 43,143 hrs · 11,648 cycles

AIR TURNBACK DUE TO SMOKE IN CABIN. FOUND OVEN IN MID GALLEY AT FAULT. REPLACED SAME.

Part: HYDRAULIC SYSTEM — LEAKING (MAIN) · airframe 42,304 hrs · 11,522 cycles

CENTER SYSTEM HYD QTY STARTED DROPPING RAPIDLY. TURNED OFF CENTER SYS PUMPS AS PER POM. .35 FLUID STILL IN SYS IN CRUISE. SERVICED CENTER SYS TO FULL. RAN ALL FLT CONTROLS, FLAPS, GEAR, RUDDER, ELEV, AND STAB. NO LEAKS FOUND. DUE TO PREV CTR SYSTEM HYD LEAK.

Part: LIGHT — INOPERATIVE (MID GALLEY) · airframe 40,866 hrs · 11,283 cycles

MID GALLEY OVERHEAD EMER LTS INOP REPLACED ONE RECEPTACLE AND RELAMPED LITS OPS CK GOOD

Part: FAN — FAILED (LEFT) · airframe 39,120 hrs · 10,986 cycles

INTERMITTANT ELEC ODOR THROUGHOUT ACFT FOLLOWED BY A L RECIR FAN EICAS WITH ASSOC INOP LIGHT IN L RECIRC SWITCH ON OVERHEAD. SWITCH TURNED OFF AND CB PULLED R14. NORMAL OPS AFTERWARDS. REPLACED LT RECIRC FAN.

Part: POWER SUPPLY — INOPERATIVE (SEAT 20) · airframe 38,553 hrs · 10,898 cycles

FOUND CROSS AISLE EMERGENCY LIGHTS AT 20CDE INOPERATIVE ON EPDC. REPLACED POWER SUPPLY OPS CK OK.

Part: SWIVEL — WORN (RH MLG) · airframe 37,725 hrs · 10,761 cycles

THE RT MLG STRUT SWIVEL WAS FOUND TO HAVE CORROSION AND FRETTING DAMAGE ON THE FACE OF ONE OF ITS LUGS. CORRECTIVE ACTION: ER/A 334312-14.

Part: TUBE — CHAFED (FIRE BOTTLE) · airframe 37,723 hrs · 10,760 cycles

THE FIRE EXTINUISHER DISCHARGE SYSTEM TUBE ASSY WAS FOUND WORN DUE TO VIBRATING CONTACT WITH THE APU PNEUMATIC DUCT LOCATED IN THE LEFT SIDEWALL OF THE C-2 B/B AT FS 1351 TO FS 1439. THE (P/N 453T2620-100) TUBE ASSY WAS REPLACED REF DWG 453T2620.

Part: INSULATION — DETERIORATED (FIRE BOTTLE LINE) · airframe 37,723 hrs · 10,760 cycles

THE FIRE EXTINGUISHER DISCHARGE SYSTEM LINE INSULATION WAS FOUND DETERIORATED IN THE LEFT SIDEWALL OF THE C-2 B/B FROM FS 1351 TO FS 1439 DUE TO CHAFING WITH THE APU PNEUMATIC DUCT AT THAT LOCATION. THE (P/N 5259381800) (R-180-F) INSULATION WAS REPLACED.

Part: SKIN — GOUGED/DENTED (FS1425, S-34&35L)

FUSELAGE SKIN FS 1425, STRG 34L-35L, DENT/GOUGE REPAIR. THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 1425 OVER STRINGERS 34L AND 35L BY GROUND EQUIPMENT. THERE WAS NO DAMAGE TO THE UNDERLYING STRUCTURE. THE SKIN DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368748-14.

Part: PUMP — FAILED (LT HYD SYS)

LEFT HYD SYSTEM FLUID LOST AND SUBSEQUENT ADB FAILURE. REPLACED LT HYD PUMP, FLUSHED SYSTEM, CHANGED ALL ASSOCIATED FILTERS.

Part: SEAT — SPARKING (RT COCKPIT)

F/O SEAT INOP. WHILE MOVING SEAT ELECTRICALLY AFT A VISIBLE SPARK WAS SEEN COMING FROM RIGHT REAR LOWER PART OF SEAT (NEAR TRACK) AND SEAT JAMMED, ABLE TO MOVE MANUALLY. MAINTENANCE FOUND POWER CHORD DAMAGED. NO SPARE AT ARN FWD TO MCO, AS PER MEL 25-11-01A. PLACARD INSTALLED. PULLED F/O SEAT CB.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR)

L1 DOOR SLIDE FELL OFF DOOR AND STARTED TO UNLACE. SWAPPED DOOR SLIDE L3 TO L1, PLACED L3 SLIDE ON MCO/PLA PER MEL 52-11-04.

Part: UNION — LEAKING (NR 1 ENGINE)

EXCESSIVE OIL CONSUMPTION ON LEFT ENG OIL QTY PRIOR TO ENG START. AFTER LANDING OIL 3, AFTER ENG SHUTDOWN 7. PERFORMED CHECK OUT PER FIM 71-05-00. FOUND LEAK BELOW SERVO FUEL. UNION WAS NOT CORRECTLY INSTALLED. INSTALLED NEW UNION AND AFTER ENG RUN NO LEAKS FOUND.

Part: SKIN — DELAMINATED (NR 3 LE SLAT)

THE UPPER SKIN OF THE NR 3 SLAT T/E WEDGE WAS FOUND WITH A 6 X 13.5 DELAMINATED REPAIR. THE REPAIR WAS REMOVED, ALL DELAMINATION TO THE SKIN TRIMMED AWAY AND THEN REPAIRED PER B767 SRM 57-43-02. THE REPAIR WAS DOCUMENTED PER ER/A 366432-14.

Part: PWR SUPPLY — FAILED (CABIN)

FOUND ON OW II CHECK, EMERGENCY SEAT LIGHTS INOP SEATS 13A/BTO 22 A/B. REPLACED POWER SUPPLY. EMERGENCY LIGHTS OPS CKS OK.

Part: PSEU — FAILED (E/E COMPT)

EN ROUTE FLAP (TAKEOFF CONFIG) MESSAGE IN CRUISE FOR 10SEC. REOCCURRED WITH PROBE HEAT MESSAGE, THREE GEAR LIGHTS, FLAP WARNING AND NOSE A/G DISAGREE. NOSE GEAR A/G DISAGREE REMAINED ON THROUGHOUT REST OF FLIGHT. PSEU REPLACED AS SUSPECT COMPONENT AND AIRCRAFT TEST HOP ACCOMPLISHED, ALL SYSTEMS GOOD.

Part: COFFEEMAKER — FAILED (MID GALLEY)

NOTICED SLIGHTLY ACRID ELECTRICAL SMELL COMING FROM MID GALLEY. REPLACED NR 1 AND NR 2 COFFEEMAKERS IN MID GALLEY.

Part: WEDGE — DELAMINATED (NR 1 LE SLAT)

WING, NR 1 LE SLAT/TRAILING EDGE WEDGE : REPAIR FOR DELAMINATION. THE UPPER SKIN OF THE NR 1 LEADING EDGE SLAT TRAILING EDGE WAS FOUND WITH A 6 X 1.5 AREA OF DELAMINATION. THE AREA WAS REPAIRED IN ACCORDANCE WITH SRM 57-43-02 PER ER/A 363288 14AD.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND EMERGENCY TRACK LIGHT OUT, BEGINNING OF COACH CLASS. SPLICED IN NEW LIGHT ASSY, CKS NML.

Part: FAN BLADES — LACK OF LUBE (NR 1)

FAN VIBRATION ON LEFT ENGINE WENT TO 5.0 ON INITIAL CLIMB-OUT 4.2-4.5 IN CRUISE AT FL 310/330/350. COULD FEEL VIBS ONLY AT IDLE OR LOW PWR SETTINGS. REMOVED AND LUBED FAN BLADES PER MM. LUBED PER OPN 4021. PERFORMED ENG VIB SURVEY WITH PBS 4000 IN ACCORD WITH PREFLIGHT HANDBOOK TEST NBR 7. VIBS WITHIN ALLOWABLE LIMITS.