N331AZ

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 112,861 hrs · 25,917 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 111,172 hrs · 25,198 cycles

INTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. EMERGENCY LIGHTING BATTERY REMOVED AND REPLACED PER B767 AMM 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL MAINTENANCE ITEM 52497 CLEARED.

Part: SKIN — CRACKED (ZONE 400) · airframe 111,163 hrs · 25,197 cycles

CRACK ON #2 ENGINE PYLON I/B SIDE INNER SKIN FOR ACCESS PANEL 444AL

Part: ACCESS PANEL — DAMAGED (ZONE 300) · airframe 111,163 hrs · 25,197 cycles

VERTICAL STAB LE PANEL 321E BLEND OUTS OUT OF LIMITS.

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 111,163 hrs · 25,197 cycles

FLC ROLLER TRAY AT STATION 654-790 BL 7 RH HAS CRACKS AND A DENT

Part: ROLLER TRAY — CRACKED (ZONE 100) · airframe 111,163 hrs · 25,197 cycles

ALC ROLLER TRAY STA1275 LBL 21 IS CRACKED

Part: DUCT — WORN (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

#2 OTBD CORE COWL PRECOOLER EXHAUST DUCT IS WORN MISSING MATERIAL ALONG THE L/E

Part: SEAL — WORN (ZONE 500) · airframe 111,163 hrs · 25,197 cycles

LEFT WING TRAILING EDGE PANEL 551QB HAS A WORN SEAL

Part: SKIN — DAMAGED (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

DURING HFEC OPEN FASTENER HOLE ROTARY SCAN, DEFECT INDICATIONS WERE NOTED AT THE BOTTOM TWO FASTENER HOLES. LOCATED BETWEEN S-19R AND LWR MAIN SILL CHORD, B STA 332-339.

Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 111,163 hrs · 25,197 cycles

LEFT WING FIXED LEADING EDGE INTERCOSTAL AT LWS 520 CRACKED.

Part: SUPPORT ANGLE — CRACKED (ZONE 300) · airframe 111,163 hrs · 25,197 cycles

VERT STSB ACCESS PANEL 324AL, FWD SUPPORT ANGLE LH O/B & RH O/B CRACKED AT LWR FASTENERS.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 111,163 hrs · 25,197 cycles

ALC DOOR FWD SCUFF PLATE CRACKED STA 1277

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 111,163 hrs · 25,197 cycles

ALC DOOR MID SCUFF PLATE CRACKED REF 47637REA04 IR

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

FORWARD LOWER CARGO AFT SECTION AT FLOOR SUPPORT INTERCOSTAL AT LBL 20 BETWEEN STATIONS 720-740 HAS CORROSION AROUND NUTPLATES,

Part: SEAL — CHAFED (ELEVATOR) · airframe 111,163 hrs · 25,197 cycles

ELEVATOR SEAL PANEL IS CHAFFED

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 111,163 hrs · 25,197 cycles

1809 BULKHEAD HORIZONTAL CHORD IS CRACKED ON LH SIDE AT LBL28.5

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

FLC STA 575 RBL36 CORROSION ON INTERCOSTAL OUT OF LIMITS

Part: SUPPORT — CRACKED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

AFT LOWER CARGO FLOOR SUPPORT CRACKED STA 1461-1480, ABOVE S35R

Part: SUPPORT WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

FLC FLOOR WEB CORRSION STA 566-588 LBL17-23

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

FLC STATION 566 RBL 28-38 CORRODED BEYOND LIMITS

Part: SKIN — CRACKED (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

L-1 DOOR CUTOUT AFT LOWER CORNER CRACKED S19L BODY ARM 332-339

Part: GROUND STUD — WORN (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

P32 GROUNDING STUD LOOSE/WORN

Part: CLOSEOUT PANEL — CRACKED (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

P-32 DRIP PAN CORNER DAMAGE AND CRACKED

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

CORROSION LOWER CARGO AT 8L PDU NUTPLATE CORRODED

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

CORROSION STA 624-630, RBL 38-42

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 111,163 hrs · 25,197 cycles

CORROSION AT INTERCOSTAL STA 522-544, LBL 26

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 111,163 hrs · 25,197 cycles

FLOOR SUPPORT STA 1087 LBL22 CRACKED

Part: ACCESS PANEL — PUNCTURED (ZONE 400) · airframe 111,163 hrs · 25,197 cycles

LEFT GENERATOR P31 PANEL PUNCTURED

Part: CLOSEOUT PANEL — WORN (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

LEFT GENERATOR P31 PANEL GROUNDING STUD LOOSE/WORN

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 111,163 hrs · 25,197 cycles

FLOOR SUPPORT CRACKED AT STA1087, RBL22

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

CAPTAIN'S FORWARD INBOARD SEAT TRACK IS CRACKED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 111,163 hrs · 25,197 cycles

FIRST OFFICER'S FORWARD OUTBOARD SEAT TRACK IS CRACKED

Part: STRINGER SPLICE — CRACKED (ZONE 400) · airframe 111,163 hrs · 25,197 cycles

NUMBER 1 ENGINE PYLON I/B AFT FAIRING (STINGER) PANEL SUPPORT CRACKED

Part: SCREW — UNKNOWN (WINDOW) · airframe 109,157 hrs · 24,407 cycles

R2 WINDOW WILL NOT CLOSE. FAULT ISOLATED TO HANDLE ASSEMBLY. AIRCRAFT GROUNDED FOR MAINTENANCE. REMOVED AND REPLACED RIGHT NO. 2 WINDOW MECHANISM SCREW ASSEMBLY IAW B767 AMM 56-11-04. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,846 hrs · 24,280 cycles

FIRST OFFICER'S R2 WINDOW STUCK IN OPEN POSITION. OPERATED WINDOW IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 56-11-02. WINDOW FULLY CLOSED AND SEALED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,728 hrs · 24,234 cycles

FIRST OFFICER'S #2 WINDOW WILL NOT CLOSE AND SECURE. VERIFIED SECURITY AND INTEGRITY OF OPENABLE MECHANISM AND CLOSED WINDOW IAW B767 AMM 56-11-00. COMPLIED WITH ADJUSTMENT OF THE FIRST OFFICER'S OPENABLE WINDOW AND OPERATIONAL CHECK GOOD PER B767 AMM 56-11-02.

Part: ESCAPE REEL — UNWANTED DEPLOY (NR 3) · airframe 107,531 hrs · 23,797 cycles

POSITION #3 RAPID DESCENT DEVICE IS DEPLOYED UPON LANDING. SYSTEM DEFERRED 38167, MEL CAT C. INSTALLED POSITION #3 RAPID DESCENT DEVICE IAW B767 MAINTENANCE MANUAL 25-61-03. DEFERRAL 38167 CLEARED.

Part: SKIN — PUNCTURED (TAILCONE) · airframe 107,293 hrs · 23,704 cycles

TAILCONE UPR SKIN PUNCTURED APPROX STA 1905 LBL 10

Part: FAIRING — CRACKED (NR 2 NACELLE) · airframe 107,293 hrs · 23,704 cycles

#2 ENG PYLON TO WING FAIRING 447DB HAS A CRACKED BULKHEAD. REF FAS WO FS220060 NON ROUTINE 00174

Part: FRAME — CRACKED (BS 903)

MAIN FRAME STA 903 LBL89 INNER CHORD IS CRACKED.

Part: BEAM — CRACKED (ZONE 500) · airframe 107,293 hrs · 23,704 cycles

L/H WING O/B FLAP I/B #2 SUPPORT 1-2-3 BEAM HAS (1) HOLE MARKED IN RED SHARPIE. THAT HAS SEVERAL OPEN HOLE INDICATIONS OF DEFECTS NOTED AT THE 6 OCLOCK POSITION. VISSUAL DAMAGE NOTED ON THE I/B SIDE OF HOLE. REF FAS WO FS220060 NON ROUTINE 00586

Part: SUPPORT FITTING — CRACKED (ZONE 500) · airframe 107,293 hrs · 23,704 cycles

(2) FASTENER HOLES WITH CRACK INDICATIONS ON REAR SPAR FITTING OF FLAP SUPPORT # 1 ON THE OUTER HALF OF THE O/B FITTING. REF FAS WO FS220060 NON ROUTINE 00580

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 107,293 hrs · 23,704 cycles

SLAT #8 HAS A DENT AND POSSIBLE CRACK LEADING EDGE UPPER EXTERNAL SURFACE INBD END. REF FAS WO FS220060 NON ROUTINE 00518

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 107,293 hrs · 23,704 cycles

RH HORIZONTAL STABILIZER FWD #1 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00451

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 107,293 hrs · 23,704 cycles

RH HORIZONTAL STABILIZER AFT #7 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00456

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 107,293 hrs · 23,704 cycles

RH HORIZONTAL STABILIZER FWD #2 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00452

Part: BEAM — CORRODED (ZONE 600) · airframe 107,293 hrs · 23,704 cycles

CORROSION AREA ON BEAM PN 113T1911-40 BETWEEN WS841.20 & WS811.20 APPROX IN LENGTH 30".

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2

RH HORIZONTAL STABILIZER FWD #6 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00455

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 107,293 hrs · 23,704 cycles

RH HORIZONTAL STABILIZER FWD #3 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00453

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 107,293 hrs · 23,704 cycles

RH HORIZONTAL STABILIZER FWD #4 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00454

Part: FRAME — CRACKED (ZONE 200) · airframe 107,293 hrs · 23,704 cycles

MAIN FRAME STA 903.5 RBL 89 INNER CHORD IS CRACKED. REF FAS WO FS220060 NON-ROUTINE 00115

Part: FRAME ANGLE — CRACKED (ZONE 100) · airframe 107,293 hrs · 23,704 cycles

MAIN FRAME STA 903 LBL89 INNER CHORD IS CRACKED. FASWO FS220060 NON-ROUTINE 00116

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 107,293 hrs · 23,704 cycles

RH HORIZ STAB UPPER SURFACE HAS AREA OF BARE METAL AND SURFACE CORROSION BETWEEN FRONT AND REAR SPARS JUST OB OF STAB TO BODY FAIRING. REF FAS WO FS220060 NON ROUTINE 00219

Part: WINDOW — INOPERATIVE · airframe 106,740 hrs · 23,497 cycles

PRIOR TO DEPARTURE, FIRST OFFICER'S R2 WINDOW DIFFICULT TO OPEN. UNLOCK HANDLE DOES NOT SEAT IN THE OPEN POSITION. SECURED ROLL PIN IN LOCK HANDLE AND SAFETIED PIN. OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 56-11-00. NO ADDITIONAL FAULTS NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (MAIN DECK CARGO) · airframe 103,369 hrs · 22,420 cycles

ENROUTE MAIN CARGO DECK A-2 SMOKE DETECTION AMBER LIGHT ON CENTER CONSOLE WITH NO INDICATION OF SMOKE, MASTER CAUTION OR EICAS INDICATIONS. CREW DECLARED EMERGENCY AND DIVERTED TO KMSP. UPON LANDING NO THERMAL HOT SPOTS DETECTED BY FIRE CREW. MAIN DECK CARGO FREIGHT WAS OFFLOADED TO FACILITATE INSPECTION. GENERAL VISUAL INSPECTION OF UPPER CARGO. NO DEFECTS NOTED. INITIATED DEFERRAL MAINTENANCE ITEM CAT C. AICRAFT RELEASED TO SERVICE. FLIGHT CONTINUED TO DESTINATION STATION KSMF WITH NO FAULTS PRESENT FOR DURATION OF FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR 2A IAW B767 IAI MM 26-14-01. OPERATIONAL CHECK SATISFACTORY. DEFERRAL MAINTENANCE ITEM 21070 CLEAR.

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 103,208 hrs · 22,369 cycles

VERTICAL STABILIZER LEFT SIDE SKIN PANEL WAS DELAMINATED BEYOND SRM LIMITS. REMOVED AND REPLACED CORE AND INNER SKIN AND REPAIRED PER AMES ENGINEERING DOCUMENT 47447REA02 REV IR AND APPROVED BY DERT-710167-SW ON 8110-3 DATED 1-19-21.

Part: FAILSAFE — CRACKED (BS 955) · airframe 103,208 hrs · 22,369 cycles

PERFORMED A CRACK TRIM OUT OF THE RIGHT SIDE FAIL STRAP PER AMES ENGINEERING DOCUMENT 472070RD04.RIGHT SIDE STA 955 REFERENCING BOEING SERVICE BULLETIN 767-53A0100 AND BOEING SERVICE BULLETIN 767-53-0116.

Part: SKIN — CRACKED (FUSELAGE) · airframe 102,618 hrs · 22,183 cycles

MAINTENANCE, DURING ROUTINE OPERATIONS AT CVG, DISCOVERED ON 331AZ A CRACK IN THE SECTION 46 FUSELAGE SKIN AT THE FORWARD JAMB OF THE RIGHT AFT LOWER CARGO DOOR, PN 146T3510, AT STA 1270, NEAR DOOR STOP NUMBER 10. THE SKIN IS MADE FROM 2024-T3 X 0.210 CLAD ALUMINUM, PER B767300 SRM 51-00-04, TABLE 3. THE SKIN IS CLASSIFIED AT PRIMARY STRUCTURE, FCBS, AND PSE PER B767-300 SRM 51-00-04, FIGURE 1. WORK IN PROGRESS.

Part: SPEAKER — SMOKE (COCKPIT) · airframe 95,820 hrs · 20,063 cycles

VISUAL SMOKE EMITTING FROM CAPTAIN'S SPEAKER ON POWER TRANSFER TO GROUND POWER UNIT. DURING A DETAILED VISUAL INSPECTION OF CAPTAIN'S SIDE CONSOLE, DETERMINED THE SOURCE OF THE ODOR AND SMOKE COMING FROM CAPTAIN'S SPEAKER IAW AMM 20-60-01. REMOVED AND REPLACED THE SPEAKER IAW AMM 23-51-02. OPS CHECKED SATISFACTORY. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE.