N409AZ

Part: FAIRING — CHAFED (ZONE 500) · airframe 126,679 hrs · 25,532 cycles

LT O/B FLAP FAIRING 573BB SEAL RETAINER AND SEAL ARE CHAFED

Part: BEAM — CRACKED (ZONE 400) · airframe 126,679 hrs · 25,532 cycles

#1 PYLON AFT STINGER FAIRING INTERNAL I/B I-BEAM BROKEN PIECE

Part: SKIN — CHAFED (ZONE 500 FLAP) · airframe 126,679 hrs · 25,532 cycles

LEFT WING AFT FLAP L\E CHAFED BEYOND LIMITS

Part: RETAINER — CHAFED (ZONE 600) · airframe 126,679 hrs · 25,532 cycles

RT I/B FLAP FAIRING 671DB I/B SEAL RETAINER AND SEAL ARE CHAFED

Part: SKIN — GOUGED (NR 1 SLAT) · airframe 126,679 hrs · 25,532 cycles

#1 SLAT I/B SURFACE GOUGED

Part: ANGLE — CRACKED (ZONE 400) · airframe 126,679 hrs · 25,532 cycles

NUMBER 1 PYLON INTERNAL UPPER O/B ANGLE CRACKED AT TOP SIDE OF FRAME SEEN THROUGH O/B ACCESS PANEL 436AL

Part: STRUCTURE — CRACKED (ZONE 400) · airframe 126,679 hrs · 25,532 cycles

NUMBER 1 PYLON INTERNAL O/B CORD CRACKED AND BROKEN ON FWD AND AFT ENDS SEEN THROUGH ACCESS PANEL 436AL

Part: FLAP SYSTEM — FAULTED · airframe 125,091 hrs · 24,931 cycles

ON APPROACH TO KRFD CREW REPORTED EXECUTING GO-AROUND DUE TO WIND SHEAR/UNSTABLE APP. ON FLAP RETRACTION EICAS LE SLAT SYM. EXTRA CONTROL FORCES RIGHT YOKE TO REMAIN LEVEL. ATI QUICK REFERENCE HANDBOOK PROCEDURES COMPLIED WITH. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. ON ARRIVAL, THE AIRCRAFT WAS GROUNDED FOR CONDITIONAL INSPECTIONS AND ASSOCIATED MAINTENANCE. WORK IN PROGRESS.

Part: UNKNOWN — ODOR (CABIN) · airframe 124,549 hrs · 24,737 cycles

DURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED WITH LEFT AND RIGHT PACKS IN OPERATION EXHAUST SMELLS IN THE THE FLIGHT DECK WERE NOTED. SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER B767 AMM 05-51-56 SATISFACTORY. NO SIGNS OF OIL CONTAMINATION. WITH LEFT AND RIGHT ENGINES ENGAGED AND ISOLATED FROM APU BLEED AIR, NO FAULTS FOUND. NO SMOKE OR FUMES IN CABIN. WITH LEFT AND RIGHT PACKS AND ENGINES ENGAGED AND TRIM AIR VALVES FULLY OPEN IAW B767 21-51-00, FAULT NOT DUPLICATED. WITH APU BLEED AIR ONLY AND TRIM AIR VALVES FULLY OPEN LEFT AND RIGHT PACKS WERE ENGAGED. NO FAULTS FOUND. COOLING PACK SYSTEM CHECKS GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 124,528 hrs · 24,731 cycles

DURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED, LEFT EMERGENCY LIGHTS INOPERATIVE. FORWARD EMERGENCY LIGHT BATTERY REMOVED AND REPLACED. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 123,519 hrs · 24,378 cycles

POST FLIGHT, CREW REPORTED EMERGENCY LIGHTS SWITCH COVER WILL NOT STAY CLOSED. REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH GUARD IAW B767 SWPM 20-83-11. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: COWLING — DAMAGED (ZONE 400) · airframe 123,088 hrs · 24,212 cycles

#2 ENGINE I/B CORE COWL HAS A HOLE IN THE UPPER AFT EXTERIOR NAC 220-225

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 123,088 hrs · 24,212 cycles

FIRST OFFICER INBOARD SEAT TRACK CRACKED.

Part: SEAL DEPRESSOR — DAMAGED (ZONE 200) · airframe 123,088 hrs · 24,212 cycles

MCD CUTOUT FORWARD LOWER CORNER DAMAGED

Part: SEAL DEPRESSOR — DAMAGED (ZONE 200) · airframe 12,088 hrs · 24,212 cycles

MCD CUTOUT AFT LOWER CORNER DAMAGED

Part: STRINGER — CRACKED (ZONE 200) · airframe 123,088 hrs · 24,212 cycles

STRINGER CAP CRACKED @ STA 340,S24R

Part: SKIN — DAMAGED (ZONE 100) · airframe 123,088 hrs · 24,212 cycles

LMLG WHEEL WELL FUSELAGE FORWARD OF BODY DOOR IS DAMAGED AT AND AROUND DOUBLER REPAIR

Part: SKIN — DAMAGED (ZONE 500) · airframe 123,088 hrs · 24,212 cycles

LW LEADING EDGED HAS COMPOSITE DAMAGE.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 123,088 hrs · 24,212 cycles

FIRST OFFICERS FWD SEAT TRACK CRACKED

Part: SKIN — ABNORMAL (ZONE 100) · airframe 123,088 hrs · 24,212 cycles

HOLE IN SKIN FOUND @ STA 344, S21R

Part: SUPPORT — CRACKED (ZONE 500) · airframe 123,088 hrs · 24,212 cycles

LW, T/E, I/B FLAP ANGLE GEARBOX SUPPORT PLATE CRACKED

Part: SKIN — CRACKED (ZONE 200) · airframe 123,088 hrs · 24,212 cycles

L1 DOOR CUTOUT AFT LOWER CORNER CRACKED

Part: SKIN — CRACKED (ZONE 200) · airframe 123,088 hrs · 24,212 cycles

R1 DOOR CUTOUT AFT LOWER CORNER CRACKED

Part: WINDOW — INOPERATIVE · airframe 120,924 hrs · 23,422 cycles

DURING ROUTINE MAINTENANCE, R2 WINDOW DIFFICULT TO CLOSE. ADJUSTED R2 WINDOW IAW B767 AMM 56-11-02. OPERATIONAL AND LEAK CHECK GOOD. FAULT NOT DUPLICATED.

Part: PANEL — FAULTY · airframe 119,534 hrs · 22,976 cycles

POST FLIGHT, CREW REPORTED OVERHEAD EMERGENCY DOOR LIGHT KEEPS BLINKING/FLASHING ON AND OFF. NO EICAS MESSAGE INDICATIONS OR FAULTS WITH PRESSURIZATION NOTED. SYSTEM DEFERRED-27030 MEL CAT C. REMOVED AND REPLACED ANNUNCIATOR PANEL IAW B767 AMM 33-16-02. SYSTEM OPERATIONAL CHECK IAW B767 AMM 33-16-02 GOOD. FAULT NOT DUPLICATED. NO ADDITIONAL SYSTEM FAULTS NOTED.

Part: BEAM — CORRODED · corrosion level 2 · airframe 119,427 hrs · 22,936 cycles

#2 PYLON OUTBOARD HYDRAULIC BAY DOOR CUTOUT LOWER BEAM FWD END NUT PLATE BROKEN AND BEAM CHAFFED. REMOVED AND REPLACED #2 PYLON OUTBOARD HYDRAULIC DOOR LOWER BEAM IAW B767 SRM 51-40-02

Part: PLATE — CRACKED · airframe 119,427 hrs · 22,936 cycles

#2 PYLON STRINGER FAIRING 447DB FORWARD OUTBOARD ATTACH ANGLE FLANGE CRACKED LOWER ON PYLON. REMOVED AND REPLACED SPLICE FLANGE ON #2 PYLON V WEB IAW B767 SRM 51-40-02

Part: BRACKET — CRACKED · airframe 119,427 hrs · 22,936 cycles

#2 PYLON INBOUND HYDRAULIC BAY DOOR 447BL ACCESS HYDRAULIC DRAIN LINE AFT SUPPORT BRACKET CRACKED. REMOVED AND REPLACED AFT HYDRAULIC DRAIN LINE SUPPORT IAW B767 SRM 51-40-02.

Part: FLAP — DELAMINATED · airframe 119,427 hrs · 22,936 cycles

UPPER SURFACE OFF TRAILING EDGE OUTBOARD FLAP DELAM AREA 46" INBOARD FROM OUTBOARD EDGE AND 10" FROM TRAILING EDGE. REPAIRED DAMAGE ON RIGHT WING OUTBOARD FLAP UPPER SKIN IAW B767 SRM 51-70-06 AS DIRECTED BY SRM 57-53-01.

Part: SPLICE PLATE — CHAFED · airframe 119,427 hrs · 22,936 cycles

#2 PYLON OUTBOARD SIDE ACCESS 447AR PANEL AFT MATING FLANGE CHAFFED. REMOVED, FABBED AND INSTALLED REPLACEMENT AFT MATING FLANGE IAW B767 SRM 51-40-02 PARA 9 AND BOEING DRAWING 313T3310.

Part: NONE — NONE · airframe 119,427 hrs · 22,936 cycles

#12 SLAT HAS AREA OF DELAMINATION ON UPPER TRAILING EDGE WEDGE. REPAIRED AREA OF DELAMINATION ON #12 SLAT TRAILING EDGE WEDGE IAW B767 SRM 51-70-10.

Part: SLAT — CRACKED · airframe 119,427 hrs · 22,936 cycles

GOUGE IN BOTTOM SIDE OF UPPER TRAILING EDGE OF LEFT WING NUMBER 3 SLAT LOCATED APPROXIMATELY AT OSS 734.74. REPAIRED BOTTOME SIDE OF THE UPPER TRAILING EDGE WEDGE AT #3 SLAT IAW B767 51-70-10 PER 5743-02 REAPIR 1 OF THE B767 SRM.

Part: FRAME — CORRODED · airframe 119,427 hrs · 22,936 cycles

T FRAME AT AFT END OF KEEL PANEL 139BL IS CORRODED. T FRAME BLENDED AND REPLACED AS REQUIRED IAW B767 SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101 DETAIL VII B767 SRM 51-40-05 FIG 6 AND B767 SRM 51-40-02 PARA 4

Part: SLAT — DENTED · airframe 119,427 hrs · 22,936 cycles

#1 SLAT HAS DENT ON UPPER TRAILING EDGE WEDGE. DENT REPAIRED AT 250 FARENHEIT UNDER VACCUM IAW B767 SRM 51-70-10. DENT LENGTH 8 INCHES BY 21 INCHES

Part: RIB — CRACKED · airframe 119,427 hrs · 22,936 cycles

LEFT WING NOSE FORMER AT WING STATION 450 CRACKED. REMOVED AND REPLACED CRACKED FORMER AT LOWER STATION 450 IAW B767-300 SRM 51-40-02.

Part: BRACKET — CRACKED · airframe 119,427 hrs · 22,936 cycles

FORWARD INBOARD UPPER ATTACH ANGLE IS CRACKED ON P34 PANEL IN MEC. REMOVED AND REPLACED MOUNTING BRACKET FWD INBD UPPER ON P34 PANEL IN MEC IAW B767 SRM 51-40-02 AND B767 SRM 51-40-05.

Part: FAIRING — CRACKED (ZONE 100) · airframe 119,427 hrs · 22,936 cycles

DMI 26031, L/P 572823-5 FOUND ON WALK- FWD OF MLG DOOR, STA 599, CRACK 9 IN. LONG FILLER SHEET METAL. AWAITING EO REPAIR FROM ENGINEERING. AMES N/R 139923-0100-0011,ATI REV 1 ITEM 13: PER CUSTOMER REQUEST: C/W ATI EO 53-767-7984, FVCI EO 21176.1 (REPAIR- LH SKIN UNDERWING FAIRING, STA. 952.65, P/N 149T7401-123.

Part: NONE — NONE · airframe 119,381 hrs · 22,921 cycles

SUPPLEMENTAL-ENROUTE KTPA TO KILN, RIGHT ENGINE UNCOMMANDED SHUTDOWN. SUSPECTED OIL PRESSURE BELOW 10 PSI WINDMILL. ENGINE BOTTLE 2 DISCHARGE DUE TO LOOP FAIL AND UNCOMMANDED RIGHT ENGINE SHUTDOWN. DIVERSION TO KCVG. EMERGENCY DECLARATION WITH AIR TRAFFIC CONTROL AT KCVG. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS TAKEN. AIRCRAFT GROUND FOR FAULT ISOLATIO. POWERPLANT INSPECTION IDENTIFIED EXTERNAL AND INTERNAL DAMAGE BEYOND LIMITS. REMOVED AND REPLACED THE #2 ENGINE. ALL OPERATIONAL AND LEAK CHECKS SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.