N457AZ

Part: RETAINER — CRACKED (ZONE 600 FLAP) · airframe 114,854 hrs · 20,978 cycles

RIGHT WING INBOARD AFT FLAP OUTBOARD EDGE SEAL RETAINER IS DAMAGED AND BULB SEAL IS MISSING.

Part: SKIN — PUNCTURED (ZONE 800) · airframe 114,854 hrs · 20,978 cycles

HOLE IN MAIN CARGO DOOR OUTER SKIN

Part: COOLING FAN — INOPERATIVE (ZONE 200) · airframe 114,664 hrs · 20,899 cycles

DURING PRE-FLIGHT NOTICABLE SMELL OF BURNT WIRE IN THE FIGHT DECK. PLACED ON DEFERRAL 67357 MINIMUM EQUIPMENT LIST 21-58-03-01 CATEGORY C. DUE 06 NOVEMBER 2025. FLIGHT CREW DEBRIEFED AND FOUND THAT FORWARD EQUIPMENT SUPPLY FAN 1 EICAS MESSAGE AND EQUIPMENT COOLING SUPPLY FAN 1 BREAKER WAS OUT. IN ACCORDANCE WITH B767 FAULT ISOLATION MANUAL 21-58 FAULT TREE 904 PUSHED IN BREAKER. REMOVED AND REPLACED FORWARD SUPPLY FAN IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 21-58-06. OPERATIONAL CHECK GOOD. DEFERRAL 67357 CLEARED.

Part: WARNING LIGHT — ILLUMINATED (ZONE 800) · airframe 113,568 hrs · 20,401 cycles

AT 2500 MAIN CARGO DOOR ILLUMINATED WITH NO PRESSURIZATION ABNORMAL INDICATION. MASTER WARNING INDICATION FOR MAIN CARGO DOOR DISPLAYED. CREW ELECTED AIR TURN BACK TO DEPARTURE STATION KABE WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT GROUNDED FOR MAINTENANCE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 113,568 hrs · 20,401 cycles

AT 2500 MAIN CARGO DOOR ILLUMINATED WITH NO PRESSURIZATION ABNORMAL INDICATION. CREW ELECTED AIR TURN BACK TO KABE WITH AN EMERGENCY DECLARATION. LANDING UNEVENTFUL. ON ARRIVAL AIRCRAFT GROUNDED FOR MAINTENANCE. IAW ATI 767 MEL 52-71-01-02 DEFERRAL 60152 FOR MAIN DECK CARGO DOOR (MDCD) INDICATION SYS INITIATED. MDCD SENSOR S9024 SEQUENCE INDICATION CIRCUIT TO LOCK ACTUATOR ADJUSTED. FOR 11 CONSECUTIVE FLT CYCLES, NO ADDITIONAL FAULTS NOTED. GENERAL VISUAL INSPECTION OF DOOR LOCK ACTUATOR SYSTEM & WIRE SHAKE DOWN CHECK IAW SMM 52-32-12 AND AMM 20-60-03 GOOD. CHECKS OF ALL ASSOCIATED MDCD SENSOR RIGS PER SMM 52-32-SATISFACTORY. NO FAULTS FOUND. DEFERRAL MAINTENANCE ITEM 60152 CLEARED.

Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE) · airframe 112,366 hrs · 19,907 cycles

AT FL340, CREW REPORTED LOSS OF CABIN PRESSURE, EICAS MSG AND AURAL WARNINGS-MASTER CAUTION-ILLUMINATED. CREW COMPLIED WITH ATI QUICK REFERENCE HANDBOOK PROCEDURES, AND ELECTED AIR RETURN TO DEPARTURE STATION KRFD WITH AN EMERGENCY DECLARATION DUE TO OVERWEIGHT LANDING. LANDING WAS WITHOUT INCIDENT AND ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR INSPECTIONS AND MAINTENANCE. SUBSEQUENT TO COMPLIANCE OF TROUBLSHOOTING PROCEDURES PER BOEING 767 FAULT ISOLATION MANUAL 21-31-FT 803 AND BOEING 767 AIRCRAFT MAINTENANCE MANUAL 21-31-03, LINE MAINTENANCE REPORTED OUTFLOW VALVE WILL NOT ALLOW AIRCRAFT TO PROPERLY PRESSURIZE. AIR OUTFLOW VALVE ASSEMBLY REMOVED AND REPLACED. OPERATIONAL CHECK SATISFACTORY AMM 21-31-03 / 21-31-00. OVERWEIGHT LANDING CONDITIONAL INSPECTIONS GOOD PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 05-51-35. NO FAULTS FOUND. 19 JULY 2024, FUNCTIONAL FLIGHT CHECK ATN457 SATISFACTORY. NO FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (CABIN PRESSURE) · airframe 112,207 hrs · 19,844 cycles

ON CLIMB OUT CREW REPORTED, MAIN CARGO DOOR LIGHT ILLUMINATED AT FL280. PRESSURIZATION OK. CREW ELECTED AIR TURN BACK TO KLAL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. POST FLIGHT LINE MAINTENANCE VERIFIED OPERATIONAL CHECK OF MAIN CARGO DOOR GOOD. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52639 PER ATI MINIMUM EQUIPMENT LIST 52-71-01-02. MAIN DECK CARGO DOOR FORWARD INSTRUMENT PANEL CERTIFIED INOPERATIVE. AIRCRAFT RESUMED SERVICE. MAIN CARGO DOOR OPERATIONAL CHECK PER IAI SUPPLEMENTAL MAINTENANCE MANUAL 52-32-00 SATISFACTORY. NO FAULTS NOTED.

Part: WARNING LIGHT — ILLUMINATED (MAIN CARGO DOOR) · airframe 112,199 hrs · 19,841 cycles

ON CLIMB OUT CREW REPORTED, MAIN CARGO DOOR LIGHT ILLUMINATED AT FL280. PRESSURIZATION OK. CREW ELECTED AIR TURN BACK TO KLAL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52639 PER ATI MINIMUM EQUIPMENT LIST 52-71-01-02. CORRECTIVE ACTION DUE 26 JUNE 2024. AIRCRAFT RESUMED SERVICE.

Part: NUT PLATE — NONE · airframe 87,019 hrs · 11,993 cycles

MAIN CABIN - INSTALL STRUCTURAL PROVISIONS FOR ELT MOD

Part: DOOR — DELAMINATED (RT MLG) · airframe 87,019 hrs · 11,993 cycles

RH MLG DOOR AFT EDGE PANEL DISPLACED, FIBER GLASS CLOSURE PLIES FOUND DELAMINATED. UNKNOWN ON HOW DAMAGE OCCURED. AREA OF DAMAGE WAS 34" LONG.

Part: RIB — CRACKED (RT WING LE) · airframe 87,019 hrs · 11,993 cycles

RIGHT WING, FIXED LEADING EDGE , ALIGNMENT RIB AT OSS 607.247 IS CRACKED AT THE LEADING EDGE NOSE SECTION.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 111,971 hrs · 19,758 cycles

SUBSEQUENT TO SERVICE CHECK, LINE MAINTENANCE REPORTED AFT FD EMERGENCY FLASHLIGHT BATTERY REQS REPLACEMENT EMERGENCY LIGHTING FLASHLIGHT BATTERY REMOVED AND REPLACED PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 25-64-00. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: PANEL — WORN (LT WING LE) · airframe 111,965 hrs · 19,754 cycles

LEFT WING LE PANEL 521AMB HAS WORN HOLES

Part: STANCHION — CRACKED (ZONE 200) · airframe 111,965 hrs · 19,754 cycles

CRACK FOUND ON THE RIGHT SIDE OF THE FORWARD OUTER VERTICAL CHORD ON THE TOP LEFT FASTENER LOOKING AFT. CRACK EXTENDS FROM THE END PART THROUGH THE FASTENER AND UNDER THE OVERLAPPING STRUCTURE.

Part: RING ASSEMBLY — DAMAGED (T/R TORQUE BOX) · airframe 111,965 hrs · 19,754 cycles

#2 ENGINE, RH THRUST REVERSER, TORQUE BOX OUTER RING HAS FRETTING DAMAGE ON THE INNER SURFACE.

Part: LATCH — DAMAGED (FWD CARGO DOOR) · airframe 111,965 hrs · 19,754 cycles

FWD CARGO DOOR, FWD LATCH CAM HAS EDGE DAMAGE.

Part: HOUSING — DENTED (LT WINGLET LIGHT) · airframe 111,965 hrs · 19,754 cycles

LEFT WINGLET, AFT POSITION LIGHT, HOUSING IS DENTED AND GOUGED

Part: SKIN — DAMAGED (BS 412) · airframe 111,965 hrs · 19,754 cycles

ACCOMPLISH PERMANENT REPAIR OF LIGHTNING STRIKE AT STA 412, STR 30R

Part: SKIN — DAMAGED (BS 387) · airframe 111,965 hrs · 19,754 cycles

ACCOMPLISH PERMANENT REPAIR OF LIGHTNING STRIKE AT STA 387 STR 33L

Part: STRINGER — CORRODED (BS 1490 S35L) · corrosion level 2 · airframe 111,965 hrs · 19,754 cycles

AFT CARGO PIT STRINGER S35L STA 1490 LBL29 HAS CORROSION

Part: TEE ANGLE — GOUGED (ZONE 200) · airframe 111,965 hrs · 19,754 cycles

MAIN CABIN TEE ANGLE ATTACH CLIP FOR INTERCOSTAL AT STA 1043 S18L IS GOUGED ON THE LOWER ATTACH FLANGE COMMON TO THE FRAME.

Part: TEE ANGLE — GOUGED (BS 1043 S18L) · airframe 111,965 hrs · 19,754 cycles

MAIN CABIN TEE ANGLE ATTACH CLIP FOR INTERCOSTAL AT STA 1043 S18L IS GOUGED ON THE LOWER ATTACH FLANGE COMMON TO THE FRAME.

Part: STRINGER — MISLOCATED (WINGLET) · airframe 111,965 hrs · 19,754 cycles

UNABLE TO COMPLY WITH WINGLET STRINGER MOD ATI-57-767-06242, DUE TO MISALIGNMENT ISSUE OF 767-3421-9 AND 767-3421-11 STRAPS WITH EXISTING FASTENER LOCATIONS PER THE DRAWING REQUIREMENTS

Part: FRAME — NONE (ZONE 700) · airframe 111,965 hrs · 19,754 cycles

SRM 53-60-71-2R, REPAIR 2 REQUIRES ACCOMPLISHMENT TO FACILITATE RMLG SWIVEL FITTING SUPPORT REPLACEMENT

Part: RIB — DAMAGED (RT WING) · airframe 111,965 hrs · 19,754 cycles

RIGHT WING TRAILING EDGE RIB AT WSTA 534.27 HAS AN ELONGATED HOLE

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 111,965 hrs · 19,754 cycles

RIGHT WING, OUTBOARD FLAP, UPPER SURFACE, 36 INCHES+- FROM INBOARD EDGE AND 28 INCHES FROM TRAILING EDGE IS AN AREA OF DELAMINATION

Part: FRAME — CRACKED (BS 883 S19-20L) · airframe 111,965 hrs · 19,754 cycles

FRAME AT STA 883 STR 19L-20L CRACKED

Part: ATTACH ANGLE — CORRODED (BS 566) · corrosion level 2 · airframe 111,965 hrs · 19,754 cycles

FWD CARGO LOWER DOORSILL ATTACH ANGLE IS CORRODED AT NUTPLATES STA 566 RBL 35 - 37. REF HAECO WO 320005 NON ROUTINE 34777

Part: LIMITER — GOUGED (THRUST REVERSER) · airframe 111,965 hrs · 19,754 cycles

NUMBER 2 ENGINE OUTBOARD THRUST REVERSER INNER SURFACE FORWARD DOWNSTOP BASE IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34756

Part: FRAME — GOUGED (BS 1021 S18-20L) · airframe 111,965 hrs · 19,754 cycles

MAIN CABIN FRAME AT STA 1021 INNER CHORD HAS MULTIPLE GOUGES IN THE RADIUS BETWEEN STR 18L AND 20L. REF HAECO WO 320005 NON ROUTINE 34670

Part: ACCESS PANEL — GOUGED (NR 1 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#1 ENGINE NACELLE ACCESS PANEL 431AT FORWARD INBOARD MATING AREA IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34693

Part: RIB — GOUGED (THRUST REVERSER) · airframe 111,965 hrs · 19,754 cycles

#1 ENGINE, RH THRUST REVERSER FWD CORE COWL RIB IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34703

Part: LIMITER — GOUGED (THRUST REVERSER) · airframe 111,965 hrs · 19,754 cycles

#1 ENG R/H T/R INNER SIDE FWD BUMPER BRACKET GOUGED. REF HAECO WO 320005 NR 34706

Part: SKIN PANEL — GOUGED (THRUST REVERSER) · airframe 111,965 hrs · 19,754 cycles

#1 ENG R/H T/R INNER SIDE LOWER SECTION AFT OF BUMPER MOUNT BRACKET STRUCTURE HAS CHAFING DAMAGE

Part: SUPPORT FRAME — GOUGED (NR 2 NACELLE) · airframe 111,965 hrs · 19,754 cycles

TOP PORTION OF #2 ENGINE STRUT FAIRING SUPPORT STRUCTURE FRAME -136 GOUGED

Part: RIB — CHAFED (THRUST REVERSER) · airframe 111,965 hrs · 19,754 cycles

#1 ENG R/H T/R INNER SIDE FWD RIB MIDDLE SECTION HAS AREA THAT IS CHAFED. REF HAECO WO 320005 NON ROUTINE 34704

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 111,965 hrs · 19,754 cycles

RIGHT WING UPPER SKIN IS CORRODED AT WING ROOT JUST AFT OF AFT OVERWING EXIT DOOR STEP

Part: STIFFENER — GOUGED (NR 1 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#1 PYLON, HYDRAULIC BAY, BILGE AREA, 2EA WEB STIFFENERS ARE GOUGED

Part: ACCESS PANEL — WORN (NR 1 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#1 ENGINE, INBOARD ACCESS PANEL 437AR, AFT ATTACHMENT FLANGE FOUND WORN WITH A MATERIAL LOSS OF 0.026

Part: STRINGER — CORRODED (BS 1562 S37L) · corrosion level 2 · airframe 111,965 hrs · 19,754 cycles

LH SIDE LOWER STRINGER S-37L AT FWD AND AFT SIDE OF STATION 1562 HAS CORROSION

Part: DOOR SILL — CORRODED (BS 566 RBL36-38) · corrosion level 2 · airframe 111,965 hrs · 19,754 cycles

FWD LOWER CARGO DOOR SILL ATTACH ANGLE IS CORRODED AT NUTPLATES BS 566, RBS 36-BL 38

Part: WEB — CHAFED (LT WING) · airframe 111,965 hrs · 19,754 cycles

RW IB AILERON OB CLOSEOUT RIB UPPER LEADING EDGE IS CHAFFED

Part: SUPPORT — CRACKED (WS 651) · airframe 111,965 hrs · 19,754 cycles

RH WING FIXED L.E. FRAME SUPPORT STRUCTURE JUST O/B OF W.S.651 IS CRACKED

Part: SKIN PANEL — GOUGED (BS 400 S37-38L) · airframe 111,965 hrs · 19,754 cycles

FUSELAGE EXTERIOR, ZONE 100, STA 400+-, S37L - 38L +- HAS TWO (2EA) GOUGES. REF HAECO WO 320005 NON ROUTINE 34171

Part: STRUCTURE — CRACKED (BS 1810 RBL 28) · airframe 111,965 hrs · 19,754 cycles

CRACK FOUND ON THE LEFT SIDE OF HORIZONTAL INNER CHORD LOOKING AFT, R/H HORIZONTAL INNER CHORD AT STA 1809.5 RBL 28. CRACK LOCATED AT THE 7 OCLOCK POSITION ON THE LOWER ROW MOST INBOARD FASTENER EXTENDING TO THE END OF THE PART.

Part: SKIN — DENTED (BS 1390 S34-35L) · airframe 111,965 hrs · 19,754 cycles

FUSELAGE EXTERIOR, ZONE 100, STA 1390 +/- BETWEEN S34L - S35L, 27 +/- INCHES FORWARD OF BULK CARGO DOOR FORWARD EDGE, IS DENTED

Part: FORMER — CRACKED (ZONE 600) · airframe 1,111,965 hrs · 19,754 cycles

RH WING OUTBD LE HAS A CRACKED BRACKET TO THE NO.8 INBD CURATIN SPRING APPROXIMATELY WS 465. HAECO WO 320005 NON ROUTINE 34217

Part: SKIN — CRACKED (ZONE 200) · airframe 111,965 hrs · 19,754 cycles

R1 DOOR LOWER CORNER FUSELAGE SKIN AND BEARSTRAP CRACKED

Part: PANEL — WORN (NR 2 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#2 PYLON PANEL 447CL IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34048

Part: PANEL — WORN (NR 1 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#1 PYLON PANEL 437CL IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34046

Part: PANEL — WORN (NR 1 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#1 PYLON PANEL 437CR IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34047

Part: PANEL — WORN (NR 2 NACELLE) · airframe 111,965 hrs · 19,754 cycles

#2 PYLON PANEL 447CR IS WORN ON INNER SURFACE. REF HAECO WO 320005 NR 34049

Part: SKIN PANEL — MISREPAIRED (BS 654 S22L) · airframe 111,965 hrs · 19,754 cycles

INTERIM REPAIR ON FUSELAGE SKIN, STA 654+34, STR 22L REQUIRES PERMANENT REPAIR

Part: SKIN PANEL — NONE (ZONE 100) · airframe 1,111,965 hrs · 19,754 cycles

INTERIM REPAIR ON FUSELAGE SKIN, STA 408, S30L REQUIRES PERMANENT REPAIR

Part: SKIN — DAMAGED (ZONE 100)

LH FUSELAGE LIGHTNING STRIKE DAMAGE AT STATION 387 STRINGER33L

Part: SKIN — DAMAGED (ZONE 200) · airframe 111,453 hrs · 19,562 cycles

LIGHTENING STRIKE STA 742 S4R

Part: RIVET — DAMAGED (ZONE 100) · airframe 111,453 hrs · 19,562 cycles

LIGHTENING STRIKE DAMAGE AT STA 654+34 S22L

Part: SKIN — DAMAGED (ZONE 100) · airframe 111,453 hrs · 19,562 cycles

LH FUSELAGE-LIGHTENING STRIKE AT STA 408 STR 30L

Part: SKIN — DAMAGED (ZONE 200) · airframe 111,453 hrs · 19,562 cycles

LIGHTNING STRIKE DAMAGE AT STA. 676 STRINGER 3R-4R

Part: NONE — NONE

FO'S WINDOW HAS A LOCKING BRACKET ON THE ESCAPE HANDLE WINDOW. WORK IN PROGRESS.

Part: INTAKE DUCT — CRACKED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

ENGINE PRE-COOLER INLET DUCT CRACKED

Part: PANEL — CRACKED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

#2 PYLON OB ARROW HEAD PANEL CRACKED.

Part: SLAT — DELAMINATED (ZONE 500) · airframe 107,592 hrs · 18,132 cycles

#6 SLAT WEDGE DELAMINATED

Part: SEAL DEPRESSOR — GOUGED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

MDCD AFT MID UPPER SEAL DEPRESSOR GOUGED

Part: DOOR — CRACKED (ZONE 500) · airframe 107,592 hrs · 18,132 cycles

#4 SLAT OB ROD COVER DOOR CRACKED

Part: FIRE SEAL — DAMAGED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

#1 PYLON PANEL 436CL HAS DAMAGED FIRE SEAL

Part: SEAL DEPRESSOR — GOUGED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

MAIN DECK CARGO DOOR UPPER SEAL DEPRESSOR.

Part: DOOR — DAMAGED (ZONE 500) · airframe 107,592 hrs · 18,132 cycles

#3 SLAT OB CLOSE OUT DOOR DAMAGED.

Part: COWLING — DELAMINATED (NR 1 ENG FAN) · airframe 107,592 hrs · 18,132 cycles

#1 ENGINE IB FAN COWL DELAMINATED 0.125

Part: DOOR — CRACKED (ZONE 600) · airframe 107,592 hrs · 18,132 cycles

# 10 SLAT ROD DOOR COVER IS CRACKED

Part: SEAL DEPRESSOR — DAMAGED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

FWD LOWER SEAL DEPRESSOR DAMAGED

Part: SEAL DEPRESSOR — DAMAGED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

AFT LOWER CORNER SEAL DEPRESSOR

Part: SEAT TRACK — WORN (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

FO'S AFT IB SEAT TRACK HOLES ARE WORN

Part: WEB — CRACKED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

# 1 PYLON PANEL 437DB WEB CRACKED

Part: ACCESS PANEL — PUNCTURED (ZONE 100) · airframe 107,592 hrs · 18,132 cycles

PANEL 194NR IS PUNCTURED

Part: WEB — CRACKED (ZONE 300) · airframe 107,592 hrs · 18,132 cycles

VERT STAB AUX SPAR WEB CRACKED O/B L/S FSS127

Part: BRACKET — CRACKED (ZONE 100) · airframe 107,592 hrs · 18,132 cycles

P-33 PANEL BRACKET CRACKED

Part: PANEL — CRACKED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

PYLON PANEL 447DB CRACKED WEB

Part: SKIN — CHAFED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

PANEL 447AL CHAFFED

Part: PANEL — CRACKED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

#1 PYLON PANEL 436CL HAS DAMAGED ALUMINUM

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

CAPTAINS AFT INBD SEAT TRACK, POSITION HOLES WORN / ELONGATED.

Part: WEB — CRACKED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

NO. 1 PYLON AFT MOST WEB IS CRACKED ON INBOARD SIDE OF STINGER FAIRING MOUNTING FLANGE NAC STA 407.34

Part: PANEL — CHAFED (ZONE 400) · airframe 107,592 hrs · 18,132 cycles

PANEL 432AL IS CHAFED

Part: ACCESS PANEL — DELAMINATED (ZONE 300) · airframe 107,592 hrs · 18,132 cycles

VERTICAL STAB, RIGHT HAND VERTICAL PNL @ FSS 14.128 DELAMINATED

Part: BRACKET — CRACKED (ZONE 600) · airframe 107,592 hrs · 18,132 cycles

RW INBD L/E UPPER SLAT TORQUE TUBE SUPPORT BRACKET IS CRACKED LOCATED APPROX AT LES 292

Part: WINDOW — CRACKED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

VIEW PORT INTERNAL WINDOW CRACKED ON L/H AFT PASSENGER ENTRY DOOR -L2-

Part: NONE — NONE (ZONE 300) · airframe 107,592 hrs · 18,132 cycles

LT HORZ PANEL 335AFB HAS WORN TORN SEAL

Part: WINDOW — CRACKED (ZONE 200) · airframe 107,592 hrs · 18,132 cycles

VIEW PORT INTERNAL WINDOW CRACKED ON R/H AFT SERVICE DOOR -R2-

Part: BATTERY PACK — INOPERATIVE · airframe 106,396 hrs · 17,767 cycles

ON THE GROUND, FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT POSITION BATTERY PACK IAW B767 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 105,909 hrs · 17,620 cycles

PRE-DEPARTURE MAINTENANCE REPORTS INTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. INITIATED DEFERRAL MAINTENANCE ITEM 23948, MEL CAT C. AIRCRAFT RELEASED TO SERVICE SYSTEMS OPERATIONAL CHECK IAW B767 AMM 33-51-00 SATISFACTORY. FAULT NOT DUPLICATED. DEFERRAL MAINTENANCE ITEM-23948 CLEAR.