N479AZ

Part: DUCT — GOUGED (ZONE 400) · airframe 112,205 hrs · 20,129 cycles

NUMBER 2 ENGINE OUTBD CORE COWL PRE COOLER EXHAUST DUCT GOUGED REF. REA 47170REA600

Part: WINDOW — CRACKED (ZONE 800) · airframe 112,205 hrs · 20,129 cycles

REPAIR VIEWPORT WINDOWS PRISM ASSY. LEFT AND RIGHT AFT PASSENGER ENTRY DOOR ASSY. B767

Part: FITTING — DAMAGED (ZONE 700) · airframe 112,205 hrs · 20,129 cycles

RIGHT MLG FORWARD SIDE OF TRUCK LOWER FITTING OVERSIZED ZERT FITTING REA 47694REA02

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

BATHTUB FITTING SUPPORT AT BS 516 RBL44 CORROSION AT FASTENER ON LWR FLANGE

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

BILGE PANEL FOUND CORROSION ON INTERCOSTAL AT STA 500-522 RBL 24

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

BILGE PANEL FOR J CHORD AT STA 522-600 RBL 32-44 FOUND CORROSION

Part: SKIN — DELAMINATED (ZONE 300) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

RIGHT HORIZ STAB UPPER SKIN L/E INNER PANEL DELAMENATED PN 185T1001-2

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

BATHTUB FITTING SUPPORT AT STA 522 RBL44 CORROSION ON FASTENERS LWR FLANGE

Part: FORMER — CRACKED (ZONE 600) · airframe 112,205 hrs · 20,129 cycles

RIGHT WING LE NOSE FORMER AT 0SS 441 IS CRACKED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

BS 478-500, RBL 24, FOUND INTERCOSTAL CORRODED, 100% LOSS.

Part: FORMER — CRACKED (ZONE 600) · airframe 112,205 hrs · 20,129 cycles

RIGHT WING LE NOSE FORMER AT 0SS 430 CRACKED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

INTERCOSTAL AT STA 546-566,RBL 32 CORROSION AT NUTPLATES

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

INTERCOSTAL AT STA 566-588 RBL25 HAS CORROSION AROUND FWD FASTENERS

Part: STRUCTURE — CRACKED (ZONE 300) · airframe 112,205 hrs · 20,129 cycles

LEFT SIDE BS 1809.5 OUTER CHORD CRACKED WL 250-256, PN 148T2740-9

Part: FAILSAFE — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

FLC DOOR CUTOUT STA 566 CORROSION AT FAILSAFE STRAP AND INNER CHORD

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 112,205 hrs · 20,129 cycles

INTERCOSTAL AT STA 588-610 RBL 36 HAS CORROSION UNDER NUT PLATE

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 112,205 hrs · 20,129 cycles

INTERCOSTAL AT BS 588 - 610, RBL 32 HAS CORROSION UNDER NUTPLATES.

Part: ESCAPE REEL — UNRAVELED (ZONE 200) · airframe 112,171 hrs · 20,116 cycles

NR 4 DESCENT DEVICE FOUND UNRAVELED INSIDE STORAGE BOX. PLACED ON DEFERRAL 67494 MINIMUM EQUIPMENT LIST 25-61-01-01 CATEGORY C. DUE 10 NOVEMBER 2025. REMOVED AND REPLACED #4 DESCENT DEVICE IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 25-61-04. DEFERRAL 67494 CLEARED.

Part: BALL SCREW — SHEARED (WINDOW FRAME) · airframe 111,562 hrs · 19,898 cycles

FIRST OFFICER'S R2 WINDOW WILL NOT CLOSE. UPON INSPECTION FOUND BALLSCREW SHAFT SHEARED AT FORWARD END. REMOVED AND REPLACED R2 WINDOW BALLSCREW ASSEMBLY AND REINSTALLED ORIGINAL LOWER R2 WINDOW TRACK AND R2 WINDOW IN ACCORDANCE WITH BOEING 767 AIRCRAFT MAINTENANCE MANUAL 56-11-04 AND BOEING 767 AIRCRAFT MAINTENANCE MANUAL 56-11-02. OPERATIONAL CHECK NOTED DEFECTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 109,073 hrs · 18,920 cycles

2 EA CRACK INDICATIONS FOUND AT L1 DOOR CUTOUT LOWER AFT CORNER. INDICATION IN BEAR STRAP AND SKIN LAYERS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 109,073 hrs · 18,920 cycles

R1 DOOR CUTOUT LOWER AFT CORNER HAS BEAR STRAP AND SKIN CRACKED AS FASTENER HOLE, CORROSSION AND SCRIBE LINE AT SCUFF PLATE AREA.

Part: STRAP — CRACKED (BS 1726) · airframe 109,073 hrs · 18,920 cycles

CRACK FOUND ON STA 1725.5 FRAME RH SIDE AFT OF BULKHEAD 2ND FASTENER BELOW APU INLET DOOR INTERNAL STRUCTURE

Part: RIB — MECHANIC ERROR (RT WING) · airframe 109,073 hrs · 18,920 cycles

RH WING, OUTBOARD TRAILING EDGE, FWD OF OUTBOARD EDGE OF OUTBOARD AILERON, FLANGE HAS DRILL STRIKE

Part: RIB — MISMARKED (RT WING) · airframe 109,073 hrs · 18,920 cycles

RH WING, OUTBOARD TRAILING EDGE, FWD OF OUTBOARD EDGE OF OUTBOARD AILERON, FLANGE HAS DRILL START/STRIKE

Part: STRINGER — GOUGED (LT WING) · airframe 109,871 hrs · 16,469 cycles

LH WING INTERNAL STRINGER L-10 HAS MULTIPLE GOUGES ON THE FWD FACING SURFACE. REPAIRED STRINGER PER FLIGHT VEHICLE CONSULTING, INC (FVCI) EO# 24012-10 REV. B DTD 02/12/2024

Part: HELICOIL — STRIPPED (WINDOW FRAME) · airframe 109,073 hrs · 18,920 cycles

WINDOW FRAME 13L HAS ONE DAMAGED HELI COIL AND OUT OF ROUND HOLE

Part: SUPPORT BEAM — GOUGED (ZONE 700) · airframe 109,073 hrs · 18,920 cycles

LMLG SUPPORT BEAM HAS MULTIPLE GOUGES ON THE LOWER SURFACE OF THE BEAM, DAMAGE REPAIRED BY BLENDING

Part: FAILSAFE — CORRODED (BS 903 S19-20R) · corrosion level 2 · airframe 109,073 hrs · 18,920 cycles

MAIN CABIN - FRAME STRAP AT STA 903 BETWEEN STR 19R - STR 20R HAS EXFOLIATION CORROSION

Part: FRAME — DAMAGED (BS 903 LBL 89) · airframe 109,073 hrs · 18,920 cycles

MAIN CABIN - FRAME AT STA 903 LBL 89 HAS ONE ELONGATED HOLE REF HAECO WO 320004 NON ROUTINE 32776

Part: FRAME — CRACKED (ZONE 200) · airframe 109,073 hrs · 18,920 cycles

MAIN CABIN - FRAME AT STA 903 LBL 89 IS CRACKED AND REQ REPAIR PER ATI EO-53-767-7701. REF HAECO WO 320004 NON ROUTINE 32739

Part: FRAME — CRACKED (BS 903 RBL 89) · airframe 109,073 hrs · 18,920 cycles

WHILE PERFORMING ATI EO:53-767-7702 THE FRAME AT STA 903 RBL89 WAS FOUND TO BE CRACKED

Part: RIB — GOUGED (ZONE 500) · airframe 109,073 hrs · 18,920 cycles

LH WING INTERNAL RIB 28 INBD FACING WEB SURFACE IS GOUGED IN LINE WITH STRINGER L-9 VIEWED THROUGH ACCESS HOLE 541TB

Part: TORQUE TUBE — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 109,073 hrs · 18,920 cycles

AFT CARGO DOOR LATCH TUBE HAS CORROSION

Part: FAIRING — GOUGED (RT FLAP TRACK) · airframe 109,073 hrs · 18,920 cycles

RIGHT WING, OUTBOARD FLAP, OUTBOARD FLAP TRACK, MID FAIRING TRAILING EDGE IS IN CONTACT WITH GREASE FITTINGS AND IS GOUGED

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 109,073 hrs · 18,920 cycles

RW UPPER SKIN IS CORRODED AT TWO EACH FASTENER HOLES JUST AFT OF AFT OVERWING EXIT BS 925-928. REF HAECO WO 320004 NON ROUTINE 32248

Part: WEB — CRACKED (LT WING) · airframe 109,073 hrs · 18,920 cycles

L/H WING L/E BULLNOSE WEB IS CRACKED AT THE LOWER RADIUS IN LINE WITH THE L/E RIB BETWEEN OSS 648.595 AND OSS 694.550, PREVIOUS REPAIR IN THE SAME AREA. THRE CRACKS 6.7", 3.4", AND 0.285" IN LENGTH

Part: SUPPORT — CRACKED (RWS 694) · airframe 109,073 hrs · 18,920 cycles

RIGHT WING, OUTBBOARD FIXED LEADING EDGE, STA 694 INTERNAL LOWER SUPPORT IS CRACKED. REF HAECO WO 320004 NON ROUTINE 32193

Part: BRACKET — CRACKED (LT WING) · airframe 109,073 hrs · 18,920 cycles

LH WING INBD L/E AREA TORQUE TUBE GUIDE ATTACH BRACKET HAS MULTIPLE CRACKS AT APPROX IFSS 290. REF HAECO WO 320004 NON ROUTINE 32175

Part: SUPPORT BEAM — GOUGED (ZONE 600) · airframe 109,073 hrs · 18,920 cycles

RH MLG SUPPORT BEAM HAS MULTIPLE GOUGES ON THE LOWER SURFACE. REFER TO HAECO WO 320004 NON ROUTINE 32138

Part: ESCAPE REEL — FAILED (UNKNOWN) · airframe 107,508 hrs · 18,317 cycles

DURING ROUTINE MAINTENANCE FOUND EMERGENCY DESCENT DEVICE (THIRD FROM FRONT) TO BE UNWOUND. #4 DEVICE. INSTALLED SERVICEABLE DESCENT DEVICE IN ACCORDANCE WITH IAI MAINTENANCE MANUAL 25-61-03.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,479 hrs · 18,308 cycles

EMERGENCY DOOR DISCRETE LIGHT INTERMITTANT. NO EICAS MESSAGE DISPLAYED AND PRESSURIZATION NORMAL. SYSTEM DEFERRED 40726, MEL CAT C. N ACCORANCE WITH FAULT ISOLATION MANUAL 32-09 FAULT TREE 405 AND FAULT ISOLATION MANUAL 32-09 FAULT TREE 803 NO FAULTS NOTED. DEFERRAL 40726 CLEARED.

Part: BATTERY — INOPERATIVE (COCKPIT) · airframe 106,798 hrs · 18,055 cycles

FLASHLIGHT ON CENTER COUNSEL INOPERATIVE. SYSTEM DEFERRED 36969, MEL CAT C. REMOVED AND REPLACED CENTER CONSOLE FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL 36769 CLEARED.

Part: WINDOW — LOOSE (EMERGENCY EXIT) · airframe 105,304 hrs · 17,523 cycles

POST FLIGHT, CREW REPORTED R2 WINDOW EMERGENCY EXIT HANDLE LOOSE. SECURED AND VERIFIED THE INTEGRITY OF MOUNTING HARDWARE FOR ANGLED GEARBOX IAW B767 AMM 56-11-04. OPERATIONAL CHECK GOOD. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.

Part: BUSHING — CORRODED (ZONE 600) · corrosion level 2 · airframe 105,127 hrs · 17,468 cycles

RH MAIN LANDING GEAR AFT TRUNNION BEARING AFT LWR AT 6 "O" CLOCK POSITION HAS CORROSION

Part: SKIN — CRACKED (ZONE 500) · airframe 105,127 hrs · 17,468 cycles

LEFT WING LOWER SKIN HAS A CRACK AT STA 952 STRINGER L-9.5

Part: FLAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 105,127 hrs · 17,468 cycles

LH WING IB FLAP LOWER SURFACE HAS AREA OF BULGING SKING 65" FROM OB END OF FLAP

Part: SKIN — CRACKED (ZONE 500) · airframe 105,127 hrs · 17,468 cycles

LH WING LOWER SKIN HAS EVIDENCE OF A CRACK AT WS 980

Part: SKIN — DENTED (ZONE 100) · airframe 105,127 hrs · 17,468 cycles

PROTRUDING DENT AT BS 392 AND ABOVE STRINGER 32L

Part: SKIN — CRACKED (WNG-BDY FAIRING) · airframe 102,937 hrs · 16,800 cycles

DURING ROUTINE OPERATIONS IN SMF. MAINTENANCE DISCOVERED A CRACK IN THE LEFT-HAND STA 952.65 UNDERWING FAIRING SKIN. THE SKIN IS MADE FROM 2024-T3 X 0.050” AND CLASSIFIED AS A PRIMARY STRUCTURE. A 22” DETAILED VISUAL INSPECTION (DVI) OF THE SURROUNDING STRUCTURE IDENTIFIED NO ADDITIONAL DAMAGE. IN ACCORDANCE WITH ATI ENGINEERING ORDER 53-767-7599 REVISION IR, DATED FEBRUARY 21, 2021, A 4 INCH CRACK UNDER WING FAIRING SKIN (PIN 149T7401-123) AT STATION 952.65 WAS REPAIRED. THE CORRECTIVE ACTION IDENTIFIED WITHIN THE REPAIR ORDER CONSTITUTES A MAJOR ALTERATION CATEGORY A. THE INSPECTIONS GIVEN IN THE BASELINE ZONAL INSPECTION ARE SUFFICIENT FOR CONTINUED AIRWORTHINESS. AIRCRAFT RELEASED TO SERVICE.