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: SUPPORT — DAMAGED (ZONE 600) · airframe 95,609 hrs · 26,265 cycles

DURING INSTALLATION OF PANEL 661KB, FOUND A HOLE PARTIALLY DRILLED INTO THE RIGHT WING TRAILING EDGE HINGE POINT STRUCTURE. REPAIRED IAW AMES REA 47739REA12 WITH 8110-3 APPROVAL. REFERENCE AMES WO N761CX-57 NR 195166-0600-0140.

Part: ATTACH ANGLE — CRACKED (ZONE 400) · airframe 106,958 hrs · 20,890 cycles

NR 2 PYLON OTBD AFT ATTACH ANGLE IS CRACKED.

Part: FORMER — CRACKED (LT NR 5 SLAT) · airframe 106,958 hrs · 20,890 cycles

LE NOSE FORMER AT #5 SLAT TAI DUCT IS CRACKED

Part: FORMER — CRACKED (ZONE 500) · airframe 106,958 hrs · 20,890 cycles

LE NOSE FORMER AT LES 490 IS CRACKED

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 95,631 hrs · 25,952 cycles

PORTABLE FLASHLIGHT INDICATOR LIGHT NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-02. OPS CHECKED GOOD.

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER ONE LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (ZONE 800 LATCH) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER ONE LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER TWELVE LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER FIVE LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER SEVEN LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER SIX LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER TEN LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER NINE LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: HOUSING — CORRODED (LATCH CAM) · corrosion level 2 · airframe 95,609 hrs · 26,265 cycles

MDCD NUMBER EIGHT LATCH CAM HOUSING HAS PITTING IN PIN HOUSING

Part: SUPPORT — CORRODED (ZONE 600) · airframe 95,609 hrs · 26,265 cycles

TE UPPER PANEL SUPPORT AT WS 250 ABOVE AFT LANDING GEAR BEAM IS CORRODED AROUND NUTPLATES

Part: SUPPORT ANGLE — CRACKED (ZONE 400) · airframe 95,609 hrs · 26,265 cycles

NUMBER 2 ENGINE PNEUMATIC DUCT SUPPORT ANGLE IS CRACKED AT 3 O'CLOCK POSITION

Part: STRAP — GOUGED (ZONE 200) · airframe 95,609 hrs · 26,265 cycles

PREVIOUS BLEND REPAIR ON INNER STRAP, AUX SILL IS GOUGED

Part: SHELF — DAMAGED (ZONE 900) · airframe 95,609 hrs · 26,265 cycles

SUPERNUMERARY GALLEY SHELF IS MISSING METAL EDGE

Part: COFFEEMAKER — FAILED (ZONE 200) · airframe 95,230 hrs · 13,794 cycles

CREW REPORTED BURNING SMELL FROM COFFEE POT. CIRCUIT BREAKER TRIPPED. PLACED ON DEFERRAL 76213 NON-ESSENTIAL FURNISHINGS NEF 120 PER ATI-25-20-01-01-N2001. REMOVED AND REPLACED GALLEY OVEN HOT CUP MODULE IN ACCORDANCE WITH IAI AMM SUPP 25-31-20. OPERATIONAL CHECK GOOD. DEFERRAL 76213 CLEARED.

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. TROUBLESHOT IN ACCORDANCE WITH B757 FIM 33-51 FAULT TRE 802 AND B757 WDM 33-51-15. EXAMINED PLUG D78. NO LOOSE OR BAD PINS NOTED. RECONNECTED CANNON PLUG PER B757 AMM 33-51-07. OPERATIONAL CHECK GOOD. DEFERRAL 75954 CLEARED.

Part: EXHAUST CONE — DEFORMED (ZONE 400) · airframe 95,609 hrs · 26,265 cycles

CLEARANCE CHECK OF R ENG IB CORE COWL / EXHAUST NOZZLE FOUND GAPS OUT OF LIMITS.

Part: EXHAUST CONE — DEFORMED (ZONE 400) · airframe 95,609 hrs · 26,265 cycles

CLEARANCE CHECK OF R ENG OB CORE COWL / EXHAUST NOZZLE FOUND GAPS OUT OF LIMITS.

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