N347AZ

Part: UNKNOWN — ODOR (CABIN) · airframe 109,730 hrs · 22,190 cycles

BURNING SMELL IN FLIGHT WHEN ENGINE ANTI-ICE WAS ON. ACCOMPLISHED SMOKE/FUMES IN CABIN CONDITIONAL INSPECTION PER B767 AMM 05-51-56. AFTER 30 PLUS MINTES OF DUAL ENGINE OPERATION AT IDLE NO ABNORMAL ODORS DETECTED. EXTERNAL ENGINE TUBING INSPECTION IAW AMM 75-00-00-206-001-H00 NOTED NO DEFECTS. INSPECTED #2 ENGINE MASTER CHIP DETECTOR IAW AMM 79-21-05 NO DEFECTS NOTED. OPERATED LT & RT COOLING PACKS DURING ENGINE RUNS IAW AMM 21-00-00 NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE.

Part: ENGINE — FAULTED (LEFT) · airframe 109,725 hrs · 22,188 cycles

UPON LANDING HEARD A LOUD BANG AND FLASH OF LIGHT BOTH FROM THE LEFT SIDE OF AIRCRAFT. NO OTHER IRREGULAR ITEMS NOTED. ACCOMPLISHED EXTERIOR INSPECTION WITH NO DAMAGE, DEFECTS, OR ANY OTHER ABNORMALITIES NOTED. ACCOMPLISHED LEFT ENGINE VARIABLE STATOR VANE AND VARIABLE BYPASS VALVE ACTUATOR INSPECTIONS IN ACCORDANCE WITH MM 75-31-02 & AMM 75-32-01 NO DEFECTS NOTED. VARIABLE BYPASS VALVE RIG CHECK/ADJUSTMENT IAW AMM 75-32-02. FEEDBACK CABLE RIGGING SATISFACTORILY ALIGNED. LT & RT ENGINE FOQA DATA DOWNLOADED & REVIEWED BY ATI ENGINEERING WITH NO EVIDENCE OF LT ENGINE COMPRESSOR STALL. LT ENIGNE POWER ASSURANCE RUN TEST 12 IAW AMM 71-00-00. NO DEFECTS.

Part: WINDOW — CRACKED (ZONE 200) · airframe 10,962 hrs · 2,214 cycles

CAPTAIN'S SIDE WINDOW GLASS CRACKED WHILE CLOSING. ACCOMPLISHED L2 WINDOW INSPECTION IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 56-10-00 NO DEFECTS NOTED. NO CRACKS OR DEFECTS FOUND.

Part: PROXIMITY SENSOR — OUT OF LIMITS (ZONE 800) · airframe 109,477 hrs · 22,082 cycles

POST FLIGHT CREW REPORTED, RH FORWARD EMERGENCY DOOR DISCRETE LIGHT INTERMITTENT. DISPLAY COMES AND DISAPPEARS. LINE MAINTENANCE TRANSFERRED FAULT TO DEFERRAL MAINTENACE ITEM 63509 IAW ATI MINIMUM EQUIPMENT LIST 52-71-01-01. FOLLOWING A WIRING CHECK PER IAI WIRING DIAGRAM MANUAL 52-71-12 PROXY SENSOR S193 WAS IDENTIFED AS OUT OF LIMITS AND ADJUSTED ACCORDINGLY. SYSTEM OPERATIONAL CHECK IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 32-09-13 SATISFACTORY. SYSTEM MONITORED FOR 10 CONSECUTIVE FLIGHT CYCLES WITH NO ADDITIONAL FAULTS NOTED. DEFERRAL MAINTENANCE ITEM 63509 CLEARED.

Part: ACTUATOR — FAULTED (AUTOPILOT) · airframe 109,234 hrs · 21,997 cycles

AUTO PILOT DISCONNECTED ON DESCENT, AFTER 3RD TIME HAND FLEW AIRPLANE NOTICED A/C WOULD NOT TRIM. NO EICAS MESSAGES.COMPLETED STAB TRIM CHECKLIST. UNABLE TO GET STAB TRIM TO MOVE AND FROZEN AT 3.5 UNITS. DIVERSION TO PHNL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. FOLLOWING INSPECTIONS, EVIDENCE OF WEAR ON THE JACK SCREW ASSEMBLY AND SUSPECT BAD ROLLERS IN GIMBAL ASSEMBLY. STAB TRIM BALL SCREW ACTUATOR REMOVED AND REPLACED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 27-41-10. OPERATIONAL AND LEAK CHECK GOOD. NO ADDITIONAL FAULTS NOTED.

Part: HOUSING — CRACKED · airframe 109,203 hrs · 21,986 cycles

FLC RH AFT BALLMAT, CARGO STOP CRACKED/CORRODED ON BOTTOM SIDE

Part: SKIN — DEBONDED (ZONE 300) · airframe 109,203 hrs · 21,986 cycles

VERTICAL STABILIZER R/H EXTERNAL SKIN BETWEEN AUX SPAR AND FRONT SPAR IS DELAMINATED JUST ABOVE RIB 5

Part: STOP — LOOSE (ZONE 100) · airframe 109,203 hrs · 21,986 cycles

FLC RH AFT BALLMAT CARGO STOP LOOSE IN HOUSING

Part: SKIN — DAMAGED (ZONE 600 SPOILER) · airframe 109,203 hrs · 21,986 cycles

# 9 SPOILER HAS COMPOSITE DAMAGE ON UPPER SURFACE

Part: SCUFF PLATE — DENTED (ZONE 100) · airframe 109,203 hrs · 21,986 cycles

ALC MIDDLE SCUFF PLATE DENTED AFT SIDE

Part: FITTING — CRACKED (ZONE 300) · airframe 109,203 hrs · 21,986 cycles

1809 RIGHT FWD OUTER CHORD FITTING CRACKED

Part: SKIN — CRACKED (ZONE 200) · airframe 109,203 hrs · 21,986 cycles

L1 DOOR LWR REAR CORNER CRACKED.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 109,203 hrs · 21,986 cycles

LEFT LOWER FORWARD 1809 CHORD CRACKED.

Part: STOP FITTING — CRACKED (ZONE 200) · airframe 109,203 hrs · 21,986 cycles

FLC RH AFT BALLMAT, CARGO STOP CRACKED/CORRODED ON BOTTOM SIDE

Part: SKIN — CRACKED (ZONE 200) · airframe 109,203 hrs · 21,986 cycles

P-31 PNL BONDING STRAP ATTACHMENT STUD SKIN IS CRACKED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 109,203 hrs · 21,986 cycles

BULK CARGO CENTER FLOOR SUPPORT STA 1439 CORRODED AROUND NUTPLATE

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 109,203 hrs · 21,986 cycles

ATTACH ANGLE AT FLOOR BEAM STA1087 AT RBL 26 IS CRACKED.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 109,202 hrs · 21,986 cycles

ATTACH ANGLE AT FLOOR BEAM STA1087 AT LBL 26 IS CRACKED.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 109,203 hrs · 21,986 cycles

ALC DOOR CUT OUT, CEILING SUPPORT STA 1329 RBL 70 CRACKED

Part: SLIDING WINDOW — DIRTY (ZONE 200) · airframe 108,376 hrs · 21,684 cycles

POST FLIGHT CREW REPORTED, FIRST OFFICER'S WINDOW WILL NOT OPEN. FIRST OFFICER'S WINDOW CLEANED AND LUBED. OPERATIONAL CHECK GOOD.

Part: FLAP — DELAMINATED (ZONE 600) · airframe 105,151 hrs · 20,451 cycles

RW OB FLAP LOWER SURFACE DELAM

Part: SKIN — CRACKED (ZONE 100) · airframe 105,151 hrs · 20,451 cycles

CRACK IN SKIN AND BEARSTRAP

Part: SKIN — DELAMINATED (ZONE 300) · airframe 105,151 hrs · 20,451 cycles

VERTICAL AUX SPAR SKIN DELAMINATED

Part: SKIN — DAMAGED (ZONE 100) · airframe 105,151 hrs · 20,451 cycles

REPAIR AT STA 1329 STRR 35L NEEDS REPLACED

Part: FRAME — CRACKED (ZONE 600) · airframe 105,151 hrs · 20,451 cycles

LEADING EDGE FRAME CRACKED

Part: RIB — CRACKED (ZONE 600) · airframe 105,151 hrs · 20,451 cycles

RW FIXED LEADING EDGE FRAME CRACKED.

Part: RIB — CRACKED (ZONE 500) · airframe 105,151 hrs · 20,451 cycles

CRACK AT FIXED LWS 531

Part: RIB — CRACKED (ZONE 500) · airframe 105,151 hrs · 20,451 cycles

LW AIR LOAD RIB CRACKED.

Part: RIB — CRACKED (ZONE 500) · airframe 105,151 hrs · 20,451 cycles

CRACK AT FIXED LEADING LWS 549

Part: SKIN — DELAMINATED (ZONE 300) · airframe 105,151 hrs · 644,002 cycles

L/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATION

Part: SKIN — DELAMINATED (ZONE 300) · airframe 105,151 hrs · 20,451 cycles

L/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATION

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 104,767 hrs · 20,302 cycles

EMERGENCY FLASHLIGHT INOPERATIVE. SYSTEM DEFERRED, 38182 MEL CAT C. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL 38182 CLEARED.

Part: BEARING — CORRODED (ZONE 500) · airframe 102,810 hrs · 19,570 cycles

LH MAIN LANDING GEAR SUPPORT BEAM HAS EVIDENCE OF CORROSION ON THE FWD FACE AROUND THE TRUNNION BUSHING.

Part: BEAM — CORRODED (ZONE 500) · corrosion level 2 · airframe 102,810 hrs · 19,570 cycles

LH MAIN LANDING GEAR SUPPORT BEAM HAS EVIDENCE OF CORROSION ON THE FWD FACE AROUND THE TRUNNION BUSHING

Part: ROLLER — DISENGAGED (R2 WINDOW) · airframe 98,681 hrs · 18,283 cycles

PRE-DEPARTURE R2 WINDOW DIFFICULT TO CLOSE. LOWER AFT TRACK ROLLER DISENGAGED FROM TRACK. RE-INSTALLED TRACK ROLLER AND ADJUSTED R2 WINDOW IAW AMM 56-11-02. NO ADDITIONAL FAULTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 98,612 hrs · 18,262 cycles

PRE-DEPARTURE-ATN3406: CREW REPORTS FIRST OFFICER'S WINDOW DIFFICULT TO CLOSE. ADJUSTED FIRST OFFICER'S WINDOW RIG IAW AMM 56-11-02. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: WINDOW — CRACKED (R2) · airframe 96,943 hrs · 17,745 cycles

PRE-DEPARTURE, R2 WINDOW CRACKED WHEN FLIGHT CREW SELECTED WINDOW HEAT. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED R2 WINDOW IAW B767 AMM 56-11-02. OPERATIONAL CHECK OF R2 WINDOW AND EMERGENCY EGRESS HANDLE SATISFACTORY. NO DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NR 6 SLAT) · airframe 91,974 hrs · 16,155 cycles

LEADING EDGE ASYM MESSAGE DISPLAYED DURING DESCENT WITHOUT CREW INITIATING ANY FLAP SETTING. EMERGENCY DECLARED, CONTINUED APPROACH AND ACCOMPLISHED LE FLAP ASYM QRH CHECKLIST. LANDED WITHOUT INCIDENT . AIRCRAFT GROUNDED. COMPLIED WITH FAULT ISOLATION MANUAL 27-81-FAULT TREE 809. REMOVED AND REPLACED THE 297 PROXIMITY SENSOR ON RIGHT SLAT NR 9 OTBD IAW AMM 27-88-01. OPS CHECKED GOOD. FAULT NOT DUPLICATED. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: FMC — INOPERATIVE (COCKPIT) · airframe 91,562 hrs · 16,033 cycles

CAPTAIN'S FLIGHT MANAGEMENT COMPUTER DISPLAY UNIT SUDDENLY WENT BLANK ALONG WITH HEAVY ODOR OF ELECTRICAL SMOKE. LEFT COMPUTER DISPLAY UNIT CIRCUIT BREAKER WAS PULLED. SMOKE DISSIPATATED AND DID NOT RETURN. REMOVED AND REPLACED THE CAPTAIN'S FMC DISLAY UNIT. OPS CHECKED SATISFACTORY. NO DEFECTS NOTED.