N499AZ

Part: BRACKET — CRACKED (ZONE 200) · airframe 91,879 hrs · 1,664 cycles

DURING SERVICE CHECK FOUND R2 WINDOW WILL NOT CLOSE. REMOVED AND REPLACED R2 WINDOW CARRAGE MECHANISM BRACKET IN ACCORDANCE WITH B767 SRM 51-40-02. RIG CHECK AND OPERATIONAL CHECK GOOD IN ACCORDANCE WITH B767 AMM 56-11-02.

Part: SKIN — CRACKED (ZONE 200) · airframe 91,301 hrs · 16,427 cycles

CRACK IN FUSELAGE SKIN BS 1629.5 TO 1645.0 AT FUSELAGE STRINGER 14R ABOVE WATER LINE 241, B767

Part: WARNING MESSAGE — ILLUMINATED (FLAP SYS) · airframe 90,345 hrs · 16,007 cycles

DURING CLIMB OUT "TE FLAP DISAGREE" EICAS AND TRAILING EDGE LIGHT ILLUMINATED. CREW COMPLIED WITH ATI QUICK REFERENCE HANDBOOK PROCEDURES AND ALT FLAP RETRACTION. FLIGHT CONTINUED UNAFFECTED. ON APPROACH TO KAUS, THE CAPTAIN DECLARED MAYDAY AND KAUS AIR TRAFFIC CONTROL DECLARED AN EMERGENCY DESCENT. THE LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS . ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 27-51-26, FAULT ISOLATED TO FLAP HANDLE RVDT #1 M604 UNABLE TO HOLD RIG. INBOARD SLAT POSITION 2 TRANSDUCER OUT OF RIG. UNIT RE-RERIGGED IAW BOEING 767 AIRCRAFT MAINTENANCE MANUAL 27-81-00. THROUGH CONSECUTIVE FLAP/SLAT CYCLING NO FAULTS WERE NOTED. OPERATIONAL CHECK SATISFACTORY.

Part: DUCT — CRACKED (ZONE 500) · airframe 90,278 hrs · 15,971 cycles

NO. 1 ENGINE OTBD THRUST REVERSER PRE-COOLER RAM AIR DUCT IS CRACKED AT A PREVIOUS WELD REPAIR.

Part: COVER PLATE — CORRODED (ZONE 600) · corrosion level 2 · airframe 90,278 hrs · 15,971 cycles

RIGHT WING FUEL BOOST PUMP COVER PANELS 631AB AND 632AB ARE CORRODED AND WORN.

Part: FRAME — GOUGED (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#2 ENG CORE COWL O/B INSIDE 2ND FRAME LOWER FROM AFT HAS GOUGE. REPAIRED WITH 8110-3.

Part: RETAINER — BROKEN (ZONE 500) · airframe 90,278 hrs · 15,971 cycles

LEFT IB TRAILING EDGE FLAP SEAL RETAINER FOUND CRACKED. 8110-3 USED TO REPAIR AFTER FABRICATION AND CHEMICAL CONVERSION COATING, SINCE CHROME ACID ANODIZE CANNOT BE ACCOMPLISED.

Part: ATTACH BRACKET — BROKEN (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#2 PYLON, IB SIDE, ATTACH BRACKET FOR FAIRING 447DB IS BROKEN. REQUIRED 8110-3 DUE TO CHEMICAL CONVERSION IN LIEU OF SULFURIC ACID ANODIZING.

Part: DOOR — DAMAGED (ZONE 100) · airframe 90,278 hrs · 15,971 cycles

AFT CARGO COMPARTMENT, E6 SHELF DOOR IS DAMAGED. HAECO WO 320009 NON ROUTINE 46740

Part: THRUST REVERSER — WORN (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

NO. 1 ENGINE OTBD TR INNER C DUCT WALL IS WORN AT BETWEEN APPROX 1 AND 2 O'CLOCK POS. RESULTING IN MAJOR REPAIR 8110-3.

Part: THRUST REVERSER — WORN (LEFT) · airframe 90,278 hrs · 15,971 cycles

#1 ENGINE INBD T/R INNER C DUCT WALL IS WORN IN 2 LOCATIONS AT APPROX 1 AND 2 O'CLOCK POS. REQUIRED MAJOR REPAIR 8110-3. 4" X .4" AND 3" X.3" LONG AND WIDE.

Part: RETAINER — DAMAGED (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#2 ENGINE INBD TR, AFT LOWER SIDEWALL SEAL IS DAMAGED. HAECO WO 320009 NON ROUTINE 46712

Part: SEAL — WORN (ZONE 300) · airframe 90,278 hrs · 15,971 cycles

LEFT HORIZONTAL STABILIZER TO BODY UPPER BLADE SEAL 313BLX (BANANA FAIRING) HAS WORN EDGE ON LOWER SIDE AND FORWARD SIDE 8 EACH. REPAIRED WITH FAA 8110-3.

Part: SPLICE STRAP — BROKEN (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#1 PYLON, SPLICE STRAP 313T2380-604 IS BROKEN. HAECO WO 320009 NON ROUTINE 46707

Part: LATCH — DAMAGED (ZONE 800) · airframe 90,278 hrs · 15,971 cycles

FWD CARGO E/E LATCH ENTRY DOOR DAMAGED AT LOWER LEFT CORNER OF DOOR. HAECO WO 320009 NON ROUTINE 46697

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 90,278 hrs · 15,971 cycles

FUSELAGE STA 632, S31L - S32L SHEAR TIE TO BODY ANGLE FRAME FOUND CRACKED, INTERM REPAIR TERMINATED.

Part: SUPPORT — CRACKED (ZONE 600 SLAT) · airframe 90,278 hrs · 15,971 cycles

CRACK FOUND ON RIGHT WING NO. 8 SLAT INBOARD LEADING-EDGE SUPPORT.

Part: SPLICE PLATE — WORN (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

NR 2 PYLON I/B SPLICE PLATE P/N313T3310-636 FOR PANEL 447AL REQUIRES FABRICATION FOR HAECO N/R 46280. REF HAECO WO 320009 NON ROUTINE 46678

Part: LIMITER — GOUGED (THRUST REVERSER) · airframe 90,278 hrs · 15,971 cycles

#2 ENGINE I/B T/R STOP POD FITTING HAS GOUGE. HAECO WO 320009 NON ROUTINE 46615

Part: SKIN — WORN (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#1 PYLON FAN COWL SUPPORT BEAM, UPPER SURFACE OF UPPER SKIN PANEL IS WORN FROM APPROX NAC STA 145-150 ON LH AND RH SIDES. REF HAECO WO 320009 NON ROUTINE 46629

Part: LIMITER — GOUGED (THRUST REVERSER) · airframe 90,278 hrs · 15,971 cycles

#1 ENGINE O/B T/R STOP PAD FITTING HAS GOUGE, STREAMER ATTACHED. HAECO WO 320009 NON ROUTINE 46607

Part: BRACKET — CHAFED (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#2 ENG PYLON HOLD OPEN ROD STORAGE BRACKET CHAFFED O/B SIDE. HAECO WO 320009 NON ROUTINE 46650

Part: BEAM — GOUGED (THRUST REVERSER) · airframe 90,278 hrs · 15,971 cycles

#1 ENGINE OTBD T/R LOWER EDGE FRAME IS GOUGED (6 O'CLOCK POS). REF HAECO WO 320009 NON ROUTINE 46560

Part: SUPPORT BEAM — GOUGED (ZONE 600) · airframe 90,278 hrs · 15,971 cycles

RH MLG SUPPORT BEAM LOWER SURFACE HAS MULTIPLE GOUGES SPORADICALLY THOUGHOUT. HAECO WO 320009 NON ROUTINE 46469

Part: SUPPORT BEAM — GOUGED (ZONE 700) · airframe 90,278 hrs · 15,971 cycles

LMLG SUPPOER BEAM LOWER SURFACE HAS MULTIPLE GOUGES SPORADICALLY THROUGHOUT. REF HAECO WO 320009 NON ROUTINE 46467

Part: SKIN — DAMAGED (ZONE 500 FLAP) · airframe 90,278 hrs · 15,971 cycles

LH WING INBD AFT FLAP OTBD END UPPER SURFACE SKIN HAS EDGE DAMAGE. HAECO WO 320009 NON ROUTINE 46446

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 90,278 hrs · 15,971 cycles

LW FUEL BOOST PUMP PANELS 531AB AND 532AB ARE WORN AND CORRODED. HAECO WO 320009 NON ROUTINE 46434

Part: RIB — GOUGED (ZONE 500) · airframe 90,278 hrs · 15,971 cycles

LEFT WING REAR SPAR WS 1134, RIB HAS SMALL GOUGE. HAECO WO 320009 NON ROUTINE46344

Part: CHANNEL — CRACKED (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#1 PYLON, STRUT FAIRING AFT WEB, O/B CHANNEL IS CRACKED. REF HAECO WO 320009 NON ROUTINE 46308

Part: ATTACH BRACKET — CRACKED (ZONE 400) · airframe 90,278 hrs · 15,971 cycles

#2 PYLON, IB SIDE, ATTACH BRACKET FOR FAIRING 447DB IS BROKEN. HAECO WO 320009 NON ROUTINE 46275

Part: SKIN — CRACKED (ZONE 100) · airframe 90,278 hrs · 15,971 cycles

R1 DOOR AFT LWR CORNER 2ND OPEN HOLE FROM BOTTOM FOUND CRACKED AS MARKED. HAECO WO 320009 NON ROUTINE 46090

Part: SEAL — WORN (ZONE 300) · airframe 90,278 hrs · 15,971 cycles

HORIZONTAL STABILIZER TO BODY BLADE SEAL 314BRX (BANANA FAIRING) IS WORN ALONG EDGE. HAECO WO 320009 NON ROUTINE 46125

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 89,810 hrs · 15,782 cycles

DURING SERVICE CHECK, LINE MAINTENANCE REPORTED AISLE STAND EMERGENCY FLASH LIGHT BATTERY INOPERATIVE. FLASHLIGHT BATTERY REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 25-64-80. OPERATIONAL CHECK GOOD.

Part: SLIDING WINDOW — INOPERATIVE (L2) · airframe 89,279 hrs · 15,566 cycles

DURING SCHEDULED MAINTENANCE AND INSPECTIONS, LINE MAINTENANCE REPORTED L2 OPENABLE WINDOW VERY DIFFICULT TO CLOSE AND ENSURE SECURITY. LEFT NO. 2 WINDOW SEAL REMOVED AND REPLACED WINDOW SEAL PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL (AMM) 56-11-11. ADJUSTMENT AND OPERATIONAL PER BOEING 767 AMM 56-11-02 SATISFACTORY. PRESSURIZATION CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: LAMP — INOPERATIVE (TEST LIGHT) · airframe 89,257 hrs · 15,557 cycles

ON APPROACH NO NOSE LANDING GEAR INDICATION. CREW ELECTED TO ABORT THE APPROACH AND GO AROUND. EMERGENCY DECLARED AND LANDING WAS WITHOUT INCIDENT. MASTER DIM AND TEST SYSTEM REPLAMPED PER BOEING AIRCRAFT MAINTENANCE MANUAL 33-16-02. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED. PREVIOUSLY NOTED IN BODY OF TEXT OMITTED TO SELECT IN DROP DOWN OPTION OF PRECAUTIONARY PROCEDURES.

Part: FAILSAFE — CRACKED (ZONE 100) · airframe 78,626 hrs · 11,495 cycles

RH FAIL SAFE STRAP CRACKED

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 86,391 hrs · 14,534 cycles

#2 ENGINE OUTBOARD CORE COWL AFT LOWER INTERNAL CORNER ATTACH ANGLE AND TRIANGLE GUSSET MISSING RIVETS SHEARED.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 86,391 hrs · 14,534 cycles

VERT. STAB LH PANEL DELAMINATED

Part: NONE — CRACKED (ZONE 600) · airframe 86,391 hrs · 14,534 cycles

FLAP FAIRING 671FB SEAL RETAINER CRACKED

Part: STABILIZER — DELAMINATED (ZONE 300) · airframe 86,391 hrs · 14,534 cycles

VERTICAL L/E PANEL DIRECTLY BELOW 322BL R/H SIDE IS DELAMINATED IN 4 AREAS ON INTERNAL SKIN FOUND DURING CURSORY INSPECTION.

Part: BRACKET — CRACKED (ZONE 600) · airframe 86,391 hrs · 14,534 cycles

RH #7 SLAT TORQUE SHAFT SUPPORT CRACKED

Part: FRAME — CRACKED (BS 883) · airframe 86,391 hrs · 14,534 cycles

L/H FRAME STA 883.5 THE LOWER END OF FRAME COMMON TO STUB BEAM IS CRACKED

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 86,391 hrs · 14,534 cycles

CORROSION ON UPPER SKIN OF HORZ STAB BOX BETWEEN RIB 1 AND 2R AT FWD AREA

Part: PANEL — CRACKED (ZONE 100) · airframe 86,391 hrs · 14,534 cycles

P33 BACK PANEL CRACKED AT LOWER LEFT TRIANGLE DOUBLER

Part: BRAKE ASSY — DAMAGED (NR 6) · airframe 86,259 hrs · 14,491 cycles

POST FLIGHT WALKAROUND, #6 BRAKE ASSEMBLY CAME APART. REMOVED AND REPLACED THE #6 BRAKE ASSEMBLY IAW B767 AMM 32-45-08. OPERATIONAL CHECK GOOD. CONDITIONAL INSPECTION FOR PARTS DEPARTING AIRCRAFT SATISFACTORY. NO DAMAGES FOUND TO AIRCRAFT STRUCTURE AFT OF DEPARTED PART IAW B767 AMM 05-51-59-202-001. ALL PARTS ON #6 BRAKE WERE CONTAINED INSIDE THE BRAKE AND SHOWED NO EVIDENCE OF DEPARTURE.

Part: NONE — NONE · airframe 84,734 hrs · 13,957 cycles

PRE-DEPARTURE, LINE MAINTENANCE IDENTIFIED EMERGENCY EXIT SIGN BROKEN AT DOOR 1L. WORK IN PROGRESS.