N353AZ

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 113,249 hrs · 21,347 cycles

EMERGENCY EXIT SIGN BY L1 DOOR DOES NOT ILLUMINATE DURING LIGHT TEST. REMOVED AND REPLACED POWER SUPPLY IAW B767 AIRCRAFT MAINTENANCE MANUAL 33-51-07. OPS CHECKED GOOD.

Part: HANDLE — INOPERATIVE (COCKPIT WINDOW) · airframe 113,059 hrs · 21,268 cycles

FIRST OFFICER'S WINDOW HANDLE DOES NOT LOCK IN PLACE. OPS CHECK OF FIRST OFFICERS WINDOW HANDLE IN ACCORDANCE WITH SUPPLEMENTAL MAINTENANCE MANUAL 56-11-02 NO FAULTS NOTED. WINDOW SECURED IN CLOSED POSITION WITH NO DEFECTS.

Part: WARNING LIGHT — ILLUMINATED (ZONE 800) · airframe 112,551 hrs · 21,059 cycles

LEFT FORWARD EMERGENCY DOOR EICAS AND RIGHT EMERGENCY DOOR LIGHT ILLUMINATED IN CRUISE. INDICATION WHEN AWAY LATER IN FLIGHT. SYSTEM TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 65130 CATEGORY C. CORRECTIVE ACTION DUE ON 20 AUGUST 2025.

Part: PROXIMITY SENSOR — OUT OF LIMITS (ZONE 800) · airframe 112,551 hrs · 21,059 cycles

LEFT FORWARD EMERGENCY DOOR EICAS AND RIGHT EMERGENCY DOOR LIGHT ILLUMINATED IN CRUISE. INDICATION WHEN AWAY LATER IN FLIGHT. SYSTEM TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 65130 CATEGORY C. CORRECTIVE ACTION DUE ON 20 AUGUST 2025. REMOVED AND REPLACED S193 OVERWING EMERGENCY EXIT HATCH SENSOR IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 52-71-01. OPERATIONAL CHECK GOOD. DEFERRAL 65130 CLEARED.

Part: WARNING MESSAGE — ILLUMINATED · airframe 112,435 hrs · 21,021 cycles

ON DESCENT AT FLIGHT LEVEL 190 EICAS MESSAGE RIGHT EMERGENCY DOOR CAME ON. WENT OUT AT ABOUT 15,000 FEET. PRESSURIZATION APPEARED NORMAL. SYSTEM DEFERRED 64622, MINIMUM EQUIPMENT LIST C. ACCOMPLISHED PROXIMITY SENSOR ELECTRONICS UNIT TEST FOR TARGETS S193 AND S217 NO DEFECTS NOTED. CONFIRMED BOTH EMERGENCY DOORS ARE FLUSH WITH AIRCRAFT BODY. REMOVED, INSPECTED AND REINSTALLED SIDEWALL PANEL AT R1 IN ACCORDANCE WITH BOEING 767 AIRCRAFT MAINTENANCE MANUAL 25-21-00. NO DEFECTS NOTED. DEFERRAL 64622 CLEARED.

Part: STRINGER — CORRODED (ZONE 100) · airframe 112,243 hrs · 20,935 cycles

CORROSION ON STR 34R BETWEEN FSTA 452 AND FSTA458 IN LOWER LOBE OF FLC

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 112,243 hrs · 20,935 cycles

STA 1197+132, UPPER CHORD CORRODED UNDER NUTPLATES IN MULTIPLE AREAS

Part: TRAY — CRACKED (ZONE 100) · airframe 112,243 hrs · 20,935 cycles

FLC PDU 2R HAS A CRACKED MOUNTING TRAY

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,243 hrs · 20,935 cycles

STA 1219 S38L-S37L SHEAR TIE CORRODED

Part: ANGLE — CRACKED (ZONE 100) · airframe 112,243 hrs · 20,935 cycles

STA 1087 RBL 35 ANGLE CRACKED

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,243 hrs · 20,935 cycles

STA 1219 RBL 30 UPPER CHORD CORRODED

Part: ANGLE — CRACKED (ZONE 100) · airframe 112,243 hrs · 20,935 cycles

STA 1087 LBL 35 ANGLE ON FRAME CRACKED

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 112,243 hrs · 20,935 cycles

STA 1395 S39L STRINGER FRAME CLIP CORRODED

Part: SKIN — CRACKED (ZONE 200) · airframe 112,243 hrs · 20,935 cycles

R1 DOOR HAS 2EA CRACKS IN 2 LWR HOLES AT AFT CORNER OF DOOR CUTOUT

Part: WINDOW — MALFUNCTIONED (ZONE 200) · airframe 111,986 hrs · 20,834 cycles

PRIOR TO DEPATURE CREW REPORTED, FO #2 WINDOW WILL NOT LATCH PROPERLY. R2 WINDOW OPERATIONAL CHECK GOOD IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 56-11-02.

Part: HANDLE — FAULTED (SLIDING WINDOW) · airframe 111,763 hrs · 20,727 cycles

FIRST OFFICER'S HANDLE WILL NOT STAY IN CLOSED POSITION. PER IAI 767-300 MAINTENANCE MANUAL 56-11-00, INTEGRITY AND SECURITY CHECK OF R2 WINDOW SATISFACTORY. NO FAULTS FOUND.

Part: NUT — LOOSE (WINDOW) · airframe 111,175 hrs · 20,479 cycles

PRE-DEPARTURE INSPECTIONS AND MAINTENANCE CREW REPORTED CAPTAIN'S WINDOW HANDLE IS BINDING WHEN MOVING FROM LOCKED TO UNLOCKED. PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 56-11-02 LOCKING NUT ON THE LOWER AFT LINK ARM LOOSE. ADJUSTMENT OF THE LINK ARM IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 56-11-02 SATISFACTORY. NO ADDIITONAL FAULTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,406 hrs · 19,764 cycles

PRIOR TO DEPARTURE LINE MAINTENANCE REPORTED, L2 WINDOW HARD TO CLOSE. WINDOW TRACK AND SEAL WERE CLEANED AND LUBRICATED. OPERATIONAL CHECK GOOD IAW B767 AMM 56-11-02.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 108,951 hrs · 19,572 cycles

B000754 GEN BY NRC: (WHILE WORKING N/R B000741) FOUND CORROSION ON STRINGER 33R AT STA 1395

Part: STRINGER — CORRODED · airframe 108,951 hrs · 19,572 cycles

STRINGER 34R CORRODED BETWEEN STA 732 TO STA 752

Part: SUPPORT WEB — GOUGED (ZONE 600) · airframe 108,951 hrs · 19,572 cycles

R/H WING TE AFT OF LANDING GEAR SUPPORT BEAM FALSPAR WEB ACCESS HOLE LOWER EDGE LARGE TOOL MARK DAMAGES

Part: STRINGER — CORRODED (ZONE 100) · airframe 108,951 hrs · 19,572 cycles

LOWER LH FUSELAGE HAS BULGING AT APPROX FS 656 LS35 .

Part: STRINGER — BENT (ZONE 100) · airframe 102,798 hrs · 17,471 cycles

AIRBORNE/PEMCO NON-ROUTINE 1489N1 DISCREPANCY: ATI LP 512447-2: ON POST FLT FOUND DENT ON BELLY OF A/C @ STA 1793 CORRECTIVE ACTION: REMOVED & REAIRED STRINGERS 39R & 39L & INSTALL EXTERNAL DOUBLER REPAIR @ APPROX STA 1793 IAW B767-300 SRM 53-00-05, 51-40-02 & EO # 20306 REV. A

Part: SKIN — DENTED (BS 1793) · airframe 102,798 hrs · 17,471 cycles

ON POST FLIGHT INSPECTION, FOUND A DENT ON BELLY OF THE ACFT AT BS 1793. REMOVED & REPAIRED THE STRINGERS 39R & 39L & INSTALL EXTERNAL DOUBLER REPAIR IAW SRM 53-00-05, 51-40-02 & EO 20306 REV. A

Part: SKIN — DENTED (BS 1793) · airframe 102,798 hrs · 17,471 cycles

AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. ON POST FLIGHT, FOUND A DENT ON THE BELLY OF THE AIRCRAFT AT BS 1793 BETWEEN STRINGERS 39L AND 39R. REPAIRED IAW SRM 53-767-7169.

Part: PROXIMITY SWITCH — FAILED (FLAPS) · airframe 97,260 hrs · 15,733 cycles

ON ARRIVAL AT 32,000 FT, LE SLAT ASYMETRY CAUTION MESSAGE WITH FLAP/SLAT INDICATOR. INDICATION OUT OF 0, BUT NOT FLAPS 1. FLAP SELECTOR IN 0 POSITION. DECLARED AN EMERGENCY. COMPLETED CHECKLIST, FLAPS DEPLOYED TO FLAPS 20. LANDED IN EMERGENCY CONDITION. LANDING WAS WITHOUT INCIDENT AT SCHEDULED AIRPORT, AIRCRAFT GROUNDED. COMPLIED WITH PSEU BITE TEST AND IAW FIM 27-81-FT 809, FAULT ISOLATED TO THE RT OTBD PROXIMITY SWITCH NR 9 SLAT S297. VISUAL INSPECTION OF SWITCH AND WIRES NOTED DAMAGING AT THE SPLICE. REMOVED AND REPLACED THE SWITCH AND REPAIRED SHIELDED GROUND SPLICE. OPS CHECKED SATISFACTORY. CAUTION MESSAGE & LIGHT DID NOT REPEAT. AIRCRAFT RELEASED FOR SERVICE

Part: FAN — MALFUNCTIONED (RECIRCULATION) · airframe 96,174 hrs · 15,370 cycles

FORWARD EXHAUST EQUIPMENT COOLING FAN CIRCUIT BREAKER TRIPPED IN FLIGHT. OCCURED WITHIN 15 SECONDS OF UNUSUAL FAN NOISE AND BURNING ELECTRICALL ODOR. COMPLIED WITH CONDITIONAL INSPECTION 05-51-56. NO FAULTS WERE NOTED, NO BURNING ODOR OR EVIDENCE OF BURNING AND ARCING AT FORWARD EXHAUST EQUIPMENT FAN. REMOVED AND REPLACED THE AIR RECIRCULATION FAN IAW AMM 21-58-06. OPERATIONAL CHECK SATISFACTORY. NO DEFECTS NOTED. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.