AIR TRANSPORT INTERNATIONAL INC

Operated by Air Transport International (per NTSB report)

Operated by Air Transport International (per NTSB report)

Operated by Air Transport International LLC (per NTSB report)

The passenger's decision to ignore the fasten seatbelt sign, resulting in serious injury to the passenger during a turbulence encounter.

Operated by Air Transport International (per NTSB report)

The asymmetrical activation of the left wing spoiler due to a broken retraction cable during takeoff. A factor associated with the incident was the operator's inadequate inspection of the cable.

Operated by AIR TRANSPORT INTERNATIONAL (per NTSB report)

the failure of the ground crew to maintain an appropriate center of gravity while downloading cargo from the airplane. A factor was the ground crew's failure to follow established downloading procedures.

Operated by AIR TRANSPORT INTERNATIONAL (per NTSB report)

IMPROPER PREFLIGHT PLANNING/PREPARATION, IN THAT THE FLIGHT ENGINEER MISCALCULATED (MISJUDGED) THE AIRCRAFT'S GROSS WEIGHT BY 100,000 LBS AND PROVIDED THE CAPTAIN WITH IMPROPER TAKEOFF SPEEDS; AND IMPROPER SUPERVISION BY THE CAPTAIN. FACTORS RELATED TO THE ACCIDENT WERE: IMPROPER TRIM SETTING PROVIDED TO THE CAPTAIN BY THE FLIGHT ENGINEER, INADEQUATE MONITORING OF THE PERFORMANCE DATA BY THE FIRST OFFICER, AND THE COMPANY MANAGEMENT'S INADEQUATE SURVEILLANCE OF THE OPERATION.

Part: EPR SYSTEM — DETACHED (ZONE 200) · airframe 97,549 hrs · 14,869 cycles

EMERGENCY ESCAPE DESCENT DEVICE FELL FROM HOLDER DURING LANDING. PLACED ON DEFERRAL 76019 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-25-61-01-01. DUE 24 AUGUST 2026. REPLACED #3 DESCENT DEVICE IN ACCORDANCE WITH B767 AMM 25-61-05. DEFERRAL 76019 CLEARED.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 116,043 hrs · 22,025 cycles

LWW BULKHEAD STA 955 APPROX LEFT HAND BUTT LINE 86 HAS AREA OF CORROSION

Part: BUSHING — DAMAGED (ZONE 400) · airframe 95,609 hrs · 26,265 cycles

LATCH RECIEVER BUSHINGS ON NR 1 PYLON INBD SIDE HAVE BEEN OVERSIZED.

Part: DISPLAY — FAULTED (ZONE 200) · airframe 115,993 hrs · 21,458 cycles

PRIOR TO BLOCK OUT FLIGHT CREW REPORTED LEFT FLIGHT MANAGEMENT COMPUTER FAILED ALONG WITH AN ELECTRICAL SMOKE SMELL. REMOVED AND REPLACED LEFT CONTROL DISPLAY UNIT IN ACCORDANCE WITH B767 AMM 34-61-02. ACCOMPLISHED FLIGHT MANAGEMENT COMPUTER SYSTEM CONTROL DISPLAY UNIT TEST IN ACCORDANCE WITH B767 AMM 34-61-02 NO FAULTS NOTED.

Part: LONGERON SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 116,043 hrs · 22,025 cycles

LEFT OVERWING LONGERON IS CORRODED BETWEEN BS 930 - 940.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 68,916 hrs · 22,032 cycles

ROW 8 EMERGENCY LIGHT WILL NOT STAY ON PAST 4 SECONDS. PLACED ON DEFERRAL 75954 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-33-51-01-01. DUE 22 AUGUST 2026.

Part: FRAME — GOUGED (ZONE 500) · airframe 116,043 hrs · 22,025 cycles

PANEL 573BB AFT FRAME IS SEVERELY GOUGED

Part: DUCT — CRACKED (ZONE 400) · airframe 116,043 hrs · 22,025 cycles

INBD CORE COWL EXHAUST DUCT IS CHAFED ON THE LEADING EDGE

Part: BAG — TORN (ZONE 200) · airframe 113,473 hrs · 20,657 cycles

EMERGENCY ESCAPE HARNESS BAG TORN IN SEVERAL SPOTS. REMOVED AND REPLACED EMERGENCY ESCAPE HARNESS BAG IN ACCORDANCE WITH SRM 51-40-02. NO OTHER DEFECTS NOTED. DEFERRAL 75883 CLEARED.

Part: STRINGER — CRACKED (ZONE 100) · airframe 95,609 hrs · 26,265 cycles

STRINGER 25L CRACKED AT FUSELAGE BS 676.

Part: SKIN — CORRODED (ZONE 100) · airframe 116,043 hrs · 22,025 cycles

CORROSION ON SKIN AT BS 955 WHERE THE PICKLE FORK COMES IN CONTACT BELOW THE FLOOR.

Part: STIFFENER — CRACKED (ZONE 400)

PANEL 447DB WEB STIFFENER IS CRACKED

Part: ACCESS PANEL — WORN (ZONE 500) · airframe 116,043 hrs · 22,025 cycles

LEFT WING T/E PANEL 561PB HAS FASTENER HOLE ELONGATED

Part: STIFFENER — CHAFED (ZONE 400) · airframe 116,043 hrs · 22,025 cycles

#1 PYLON HYDRAULIC BAY LOWER RIBS ARE CHAFFED FROM HYDRAULIC SUPPLY HOSE.

Part: WINDOW — INOPERATIVE (ZONE 200) · airframe 128,622 hrs · 26,367 cycles

FIRST OFFICERS WINDOW DOES NOT APPEAR TO MECHANICALLY CLOSE ALL THE WAY. ADJUSTED R2 WINODW IN ACCORDANCE WITH B767 AMM 56-11-02. OPERATIONAL CHECK GOOD. ACCOMPLISHED CABIN LEAK CHECK IAW B767 AMM 05-51-24 NO LEAKS NOTED.

Part: RIB — CRACKED (ZONE 500) · airframe 116,043 hrs · 22,025 cycles

RIB AT W/S/ 499.60 CRACKED L/W L/E

Part: PACKING — FAILED (HYD SYS) · airframe 88,802 hrs · 16,945 cycles

AIRINC MESSAGE BY CREW REPORTED RIGHT HYDAULIC QUANTITY EICAS IN FLIGHT, RIGHT HYDRAULIC PUMPS SHUT DOWN AT FLIGHT LEVEL 360. RIGHT HYDRAULIC INDICATOR LIGHT CAME ON FOLLOWED BY FLUCTUATION OF PRESSURE 3000 TO 2900. ACCOPLISHED ATI QUICK REFERENCE HANDBOOK AND RIGHT HYDRAULIC SYSTEM WAS SHUT DOWN AT FLIGHT LEVEL 3. AS A PRECAUTION CREW DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED FOR INSPECTION AND MAINTENANCE. REMOVED AND INSPECTED BOTH DIFFERENTIAL PRESSURE INDICATOR AND BOTH PRESSURE SWITCHES FROM ENGINE DRIVEN PUMP PRESSURE/CASE DRAIN MODULE. REPLACED FAILED PACKINGS IN ACCORDANCE WITH B767 AMM 29-11-17. REMOVED AND REPLACED FILTER ELEMENT IN ACCORDANCE WITH B767 AMM 29-11-17. ACCOMPLISHED EXTERNAL LEAK CHECK OF PRESSURE/CASE DRAIN MODULE IAW B767 AMM 29-11-00 AFTER 5 MINUTE AT IDLE NO LEAKS NOTED.

Part: DOOR — INOPERATIVE (ZONE 800) · airframe 111,568 hrs · 22,957 cycles

DURING TAKEOFF AND LANDING HEAVY ELECTRICAL BURNING SMELL, NO SMOKE, HIGH POWER AND IDLE SEEMED TO INCREASE THE SMELL. FOUND SMELL STRONGEST IN FORWARD MAIN CARGO. NO EICAS FAULTS NOTED. MAIN CARGO DOOR INOPERATIVE. GROUND GOOD VAC INTO LOCK ACTUATOR. CLEANED CONNECTOR AND RESECURED IAW B767 SWPM 20-60-01. DOOR OPERATIONAL CHECK GOOD. RAN ENGINES AT IDLE IAW B767 AMM 71-00-00 NO FAULTS NOTED. CLEANED DIRTY E/E COOLING SUPPLY AIR INLET IAW B767 AMM 21-58-00.

Part: FRAME — CHAFED (ZONE 400) · airframe 116,043 hrs · 22,025 cycles

THE UPPER CHORD IS DEEPLY CHAFED, ON THE BULKHEAD ON TOP OF THE RIGHT PYLON, LOCATED AT THE FWD O/B CORNER OF THE 441BT PANEL.

Part: BRACKET — CRACKED (ZONE 800) · airframe 116,043 hrs · 22,025 cycles

WHILE REMOVING MDCD FWD LWR CORNER SEAL DEPRESSOR, FOUND MOUNTING CHANNEL/BRACKET TO BE CRACKED.

Part: POUCH — TORN (ZONE 200) · airframe 115,910 hrs · 21,427 cycles

LOWER ESCAPE ROPE HARNESS POUCH FOUND TORN. PLACED ON TIME LIMITED ITEM 75518 PER ATI-8.14E-CARGO_TAPE. REMOVED AND REPLACED LOWER ESCAPE HARNESS POUCH IAW AMM 25-61-00. DEFERRAL 75518 CLEARED.

Part: GUARD — FAULTED (ZONE 800) · airframe 93,345 hrs · 17,246 cycles

CREW REPORTED ON ARRIVAL ENTRY DOOR ARM SWTICH GUARD WILL NOT RETRACT. ADJUSTED ARM SWITCH GUARD IN ACCORDANCE WITH B767 AMM 20-11-00. OPERATIONAL CHECK GOOD.

Part: PAD — GOUGED (ZONE 400) · airframe 116,043 hrs · 22,025 cycles

NUMBER 1 ENGINE INBD FAN COWL HAS GOUGED RUB PAD

Part: SKIN PANEL — WORN (ZONE 600) · airframe 116,044 hrs · 22,025 cycles

RW L/E PANEL 611ST HAS 1EA FASTENER HOLE ELONGATED. ELONGATED HOLE WAS REAMED OVERSIZED TO .3745 IN. A FREEZE PLUG WAS THEN INSTALLED. THE ORIGINAL FASTENER HOLE WAS THEN LOCATED, DRILLED AND COUNTERSUNK TO ACCEPT THE OEM FASTENER FOR PANEL INSTALLATION. REFERENCE AMES WO N379AZ-25 NR 19294606000096

Part: SPLICE PLATE — CRACKED (ZONE 600) · airframe 116,044 hrs · 22,025 cycles

RW LE STA 258 LOWER SPAR FOUND CRACKED. LOWER SPLICE PLATE WAS REMOVED, FABRICATED, AND INSTALLED. REFERENCE AMES WO N379AZ-25 NR 192946-0600-0024

Part: STIFFENER — CRACKED (ZONE 400) · airframe 93,809 hrs · 17,726 cycles

NR 1 PYLON AFT V WEB O/B VERTICAL STIFFENER IS CRACKED AT LOWER EDGE

Part: CDU — SHORTED (ZONE 200) · airframe 131,419 hrs · 24,876 cycles

DURING PRE-FLIGHT CREW REPORTED CIRCUIT BREAKER A33 ON P11 HAS POPPED AND FLIGHT DECK SMELLS LIKE SMOKE/ELECTRICAL. REMOVED AND REPLACED OVERHEATED K104 MAIN BATTERY RELAY AND SHORTED LEFT CONTROL DISPLAY UNIT IAW WDM 24-51-14, WDM 247-54-71, WDM 24-33-11, WDM 33-16-12 AND AMM 24-33-00 AND B767 AMM 34-61-02. OPS CHECKED GOOD.

Part: HANDLE — FAULTED (R2 WINDOW) · airframe 114,456 hrs · 21,859 cycles

RIGHT SIDE R2 WINDOW HANDLE DOES NOT STAY STOWED VERY WELL. COMES OUT OF DETENT. ACCOMPLISHED INBOARD/OUTBOARD ADJUSTMENT OF R2 WINDOW IN ACCORDANCE WITH B767 AMM 56-11-02. OPERATIONAL CHECK GOOD.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 93,809 hrs · 17,726 cycles

CORROSION ON LOWER SIDE OF CARGO DOOR SILL AT 2ND LOCK FROM FWD END

Part: SEAL DEPRESSOR — BENT (ZONE 100) · airframe 116,043 hrs · 22,025 cycles

MAIN DECK CARGO DOOR CUTOUT, AFT LWR CORNER SEAL DEPRESSOR IS BENT UP

Part: FORMER — CRACKED (ZONE 500) · airframe 116,043 hrs · 22,025 cycles

RIB AT W.S. 430.00 CRACKED L/W L/E

Part: ELEC CONNECTOR — DIRTY (ZONE 200) · airframe 87,884 hrs · 26,325 cycles

EMERGENCY LIGHTS NOT ARMING. CLEANED EMERGENCY LIGHT PANEL ELECTRICAL CONNECTOR IAW SOPM 20-60-01. OPS CHECKED GOOD.

Part: SLIDING WINDOW — INOPERATIVE (ZONE 200) · airframe 118,093 hrs · 24,515 cycles

R2 WINDOW WILL NOT CLOSE AND LOCK. ACCOMPLISHED ADJUSTMENT OF R2 WINDOW IAW AMM 56-11-02 AT LOWER AFT AND FORWARD UPPER. OPS AND LEAK CHECKED GOOD IAW AMM 56-11-02 AND B767 AMM 51-11-00.

Part: SUPPORT ANGLE — CRACKED (NR 7 SLAT) · airframe 116,043 hrs · 22,025 cycles

NR 7 SLAT, T/E SUPPORT ANGLE CRACKED JUST INBD OF CENTER AUX ARM.

Part: LIFE VEST — TORN (ZONE 200) · airframe 94,978 hrs · 13,691 cycles

RIGHT SUPERNUMERARY SEAT LIFE VEST BAG TORN OPEN. PLACED ON DEFERRAL 74891 MINIMUM EQUIPMENT LIST CATEGORY D IAW ATI-25-25-03-01. REMOVED AND REPLACED RIGHT SUPERNUMERARY SEAT LEFE VEST IAW B767 IAI 25-63-00. DEFERRAL 74891 CLEARED.

Part: LIFE VEST — MISSING (ZONE 200) · airframe 94,978 hrs · 13,691 cycles

FIRST OBSERVER SEAT LIFE VEST MISSING. PLACED ON DEFERRAL 74890 MINIMUM EQUIPMENT LIST CATEGORY A PER ATI-25-11-02-01. INSTALLED FIRST OBSERVER SEAT LIFE VEST IN ACCORDANCE WITH AMM 25-62-00.

Part: LIFE VEST — TORN (ZONE 200) · airframe 94,978 hrs · 13,691 cycles

RIGHT SUPERNUMERARY SEAT LIFE VEST BAG TORN OPEN. PLACED ON DEFERRAL 74891 MINIMUM EQUIPMENT LIST CATEGORY D PER ATI-25-25-03-01. DUE 06 NOVEMBER 2026

Part: JACKSCREW — INOPERATIVE (ZONE 200) · airframe 130,745 hrs · 24,525 cycles

LEFT WINDOW HANDLE NOT LATCHING. CAPTAIN WINDOW. REMOVED AND REPLACED L2 WINDOW JACKSCREW ASSY IAW AMM 56-11-04. WINDOW RIGGED IAW AMM 56-11-04. PRESURIZATION TEST ACCOMPLISHED IAW AMM 56-11-00. OPS CHECKED GOOD.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 114,208 hrs · 26,479 cycles

NUMBER 2 PYLON AFT SECTION V-WEB AREA HAS INBOARD VERTICAL STIFFENER CRACKED

Part: STIFFENER — CRACKED (ZONE 400) · airframe 114,208 hrs · 26,479 cycles

NUMBER 2 PYLON AFT SECTION V-WEB HAS OUTBOARD VERTICAL STIFFENER CRACKED

Part: STIFFENER — CRACKED (ZONE 100) · airframe 114,208 hrs · 26,479 cycles

VERTICAL STIFFENER ANGLE ON FORWARD SIDE OF BS 246 FLOORBEAM, LBL 43.0, LEFT TUNNEL OF MEC IS CRACKED REFERENCE AMES WO N331AZ-40 NR 194950-0100-0064

Part: WINDOW — CRACKED (ZONE 800) · airframe 93,340 hrs · 17,243 cycles

THE INTERIOR PRISM COVER WINDOW IS CRACKED, IN THE WINDOW IN THE R4 DOOR.

Part: THRUST REVERSER — UNLOCKED (RT ENGINE) · airframe 95,582 hrs · 26,241 cycles

RIGHT ENGINE REVERSER UNLOCKED AT FLIGHT LEVEL 380. GREEN, AMBER, GREEN, AMBER NO YAW. NO CONTROL PROBLEM. LIGHT EXTINGUISHED FOR THE REMAINDER OF THE FLT. NO ABNORMAL INDS ON LANDING ROLL WITH THRUST REVERSER DEPLOYED. AIR TRAFFIC CONTROL DECLARED EMERGENCY FOR CREW. NO ABNORMAL INDICATIONS ON LANDING. AIRCRAFT WAS GROUNDED. REPAIRED WIRES W330-01TR-20, W330-015-18, W330-016-18, AND W330-02TB-20 AND CLEANED D4192P IN ACCORDANCE WITH B767 SWPM 20-10-15 AND B767 SWPM 20-61-00. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: TERMINAL — FAULTED (ZONE 200) · airframe 110,577 hrs · 32,487 cycles

DURING PRE-FLIGHT CREW REPORTED RIGHT CHART LIGHT SHOCKED PILOT WHEN TOUCHED. REMOVED AND REPLACED RIGHT CHART LIGHT IN ACCORDANCE WITH B767 AMM 33-14-00. OPERATIONAL CHECK GOOD.

Part: A/C PACK — INOPERATIVE (ZONE 100) · airframe 91,256 hrs · 13,632 cycles

RETURNED TO BLOCK DUE TO LEFT PACK TEMPERATURE EICAS, LEFT PACK INOPERATIVE AND SMOKE IN THE COCKPIT. AIRCRAFT GROUNDED FOR INSPECTION AND MAINTENANCE. ACCOMPLISHED PHASE 1 CONDITIONAL INSPECTION IN ACCORDANCE WITH B767 AMM 05-51-00 AND B767 AMM 21-00-21-102-030 NO DEFECTS NOTED. CREW RAN LEFT AND RIGHT ENGINES AND RIGHT PACK AS PART OF CONDITIONAL INSPECTION. NO SMOKE OR SMELL IN CABIN. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DEBONDED (ZONE 600) · airframe 116,043 hrs · 22,025 cycles

PANEL 611PT DISBONDED INNER AND OUTTER SKINS EXCEEDING SRM REPAIR LIMITS

Part: HANDLE — NOT SEATED (ZONE 200) · airframe 112,562 hrs · 21,254 cycles

FIRST OFFICER'S EMERGENCY EGRESS HANDLE ON EXTERIOR IS OUT. RESEATED FIRST OFFICER'S EMERGENCY EGRESS HANDLE IN ACCORDANCE WITH IAI AMM 56-11-02. OPERATIONAL CHECK GOOD.

Part: CRADLE — BROKEN (ZONE 200) · airframe 113,485 hrs · 20,724 cycles

CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER BOTTOM BROKEN. PLACED ON DEFERRAL 74109 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-25-63-04-01. DUE 23 JUNE 2026. REMOVED AND REPLACED CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER IN ACCORDANCE WITH B767 SRM 51-40-02. OPERATIONAL CHECK GOOD. DEFERRAL 74109 CLEARED.

Part: GUARD — DETACHED (ZONE 200) · airframe 105,199 hrs · 34,389 cycles

EMERGENCY LIGHT SWITCH GUARD SPRING RELEASED/DETACHED. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUARD IN ACCORDANCE WITH B767 AMM 20-11-00. OPERATIONAL CHECK IN ACCORDANCE WITH B767 AMM 33-51-08 NOTED NO FAULTS.

Part: FLASHLIGHT — DEFECTIVE (ZONE 200) · airframe 94,220 hrs · 17,727 cycles

FLIGHT DECK EMERGENCY FLASHLIGHT CAME ON IN CRUISE. RESEATED FLASHLIGHT AND IT WENT OUT. FLASHLIGHT CAME BACK ON IN DESCENT. REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY IN ACCORDANCE WITH B767 AMM 25-60-00.