AIR TRANSPORT INTERNATIONAL INC
Also recorded as: AIR TRANSPORT INTERNATIONAL INC, Air Transport International LLC
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
Operated by Air Transport International (per NTSB report)
Not yet finalized — may be revised.Operated by Air Transport International (per NTSB report)
Not yet finalized — may be revised.Operated by Air Transport International LLC (per NTSB report)
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
7,735 reports on file — showing most recent 50.
NUMBER 2 PYLON AFT SECTION V-WEB AREA HAS INBOARD VERTICAL STIFFENER CRACKED
NUMBER 2 PYLON AFT SECTION V-WEB HAS OUTBOARD VERTICAL STIFFENER CRACKED
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
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.
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.
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.
PANEL 611PT DISBONDED INNER AND OUTTER SKINS EXCEEDING SRM REPAIR LIMITS
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.
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.
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.
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.
NUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL O/B WEB STIFFENER IS CRACKED IN LOWER RADIUS REFERENCE AMES WO N503AZ-28 NR 193266-0400-0076
NUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL SUPPORT WEB IS CRACKED REFERENCE AMES WO N503AZ-28 NR 193266-0400-0075
REJECTED TAKE OFF DUE TO LOW SPEED REJECT 60 AND 65 KNOTS. LOST BOTH EICAS SCREENS. STANDBY ENG BACKUP DID NOT WORK. ENG OIL PRESSURE ON LT SIDE REACHED RED LINE. ENGINE OIL TEMP ON LT SIDE REACHED 83 AND RT SIDE -16. EICAS MESSAGE DISAGREE STANDBY INVERTER OIL TEMP INDICATOR ON RT SIDE TEMPORARILY BLANKED. CREW DID NOT DECLARE EMERGENCY. ACFT WAS GROUNDED FOR INSPECTION AND MAINT. FOUND ALL INDICATIONS TO BE IN NORMAL CONFIGURATION AT BLOCK IN. LT EICAS FOUND EICAS DISAGREE & STANDBY INVERTER. RT EICAS HAD EICAS DISAGREE ONLY. CLEARED MESSAGES AND BIT BOTH EICAS NO CODES DISPLAYED. CLEANED WATER FOUND IN GALLEY AND IN E&E BAY. CLEANED ALL WATER IN GALLEY & TRAY. TIGHTENED LOOSENED SCREW IN TRAY ALLOWING WATER TO SEEP DOWN. WATER FOUND UNDER LT EICAS COMPUTER. CLEANED WATER & CONDENSATION. R & R LT EICAS COMPUTER. OPS CHKD GOOD. HIGH POWER ENG RUN NOTED NO FAULTS. ALL WORK ACCOMPLISHED IAW FIM 31-41 FAULT TREE 808, AMM 31-41-02, AMM 24-33-03, AMM 20-60-07, B767 AMM 20-60-06
LOWER EMERGENCY HARNESS POUCH TORN. PLACED ON TIME LIMITED ITEM 73971 PER ATI-8-14E-CARGO_TAPE. DUE 30 SEPTEMBER 2026.
SPARE LIFE VEST MISSING FROM SUPERNUMERARY STORAGE CUPBOARD BY L1 DOOR. MINIMUM EQUIPMENT LIST ATI-25-62-01-01 CATEGORY D. DUE 04 OCTOBER 2026. INSTALED LIFE VEST IAW AMM 25-11-01.
LEFT WING L/E UPPER SUPPORT STRUCTURE HAS CRACKAT LOCK FASTENER AFT END, VERIFIED BY EDDY CURRENT AROUND LES 506
NUMBER 1 ENGINE PYLON AFT NACELL STRUT FAIRING 437DB (STRINGER) INTERNAL WEB CRACKED.
R2 WINDOW WILL NOT CLOSE AND LOCK. OPERATIONAL CHECK OF R2 WINDOW IN ACCODRANCE WITH B767 AMM 56-11-02 REMOVED FOD FOUND IN R2 WINDOW TRACK. CLOSED, LATCHED AND LOCKED R2 WINDOW IAW B767 IAI SUPPLMENTAL AMM 56-11-02.
LEFT WING L/E INTERNAL LOWER SUPPORT STRUCTURE HAS CRACK, VERFIED BY EDDY CURRENT, JUST OUTBOARD OF FUEL PANEL, REFERENCE AMES WO N503AZ-28 NR 193266-0500-0024
EMERGENCY ESCAPE SLIDE PANEL MISSING FASTNER APPROXIMATELY LEFT FORWARD WIND. APPLIED SPEED TAPE TO PANEL IN ACCORDANCE WITH ATI GENERAL MAINTENANCE MANUAL 8.14D. TIME LIMITED ITEM 73720 INITIATED IAW ATI-8.14D-SPEED-TAPE DUE 21 SEPT 2026. REPLACED FASTENER ON EMERGENCY ESCAPE SLIDE PANEL IAW B767 AMM SRM 51-40-02. DEFERRAL 73720 CLEARED.
EMERGENCY ESCAPE SLIDE PANEL MISSING FASTNER APPROXIMATELY LEFT FORWARD WIND. APPLIED SPEED TAPE TO PANEL IN ACCORDANCE WITH ATI GENERAL MAINTENANCE MANUAL 8.14D. TIME LIMITED ITEM 73720 INITIATED IN ACCORDANCE WITH ATI-8.14D-SPEED-TAPE DUE 20 SEPTEMBER 2026.
DURING OK TO INSTALL LT INBD ELEVATOR FOUND INBD CORNER EDGE TO BE DAMAGED.
DURING LFEC OF RH SIDE OF 1809 INTERNAL SECTION HAD CRACK INDICATION AT AREA 3 TOP OUTBOARD FASTENER USING SPOT AND RING PROBES.
LEFT WING L/E NR 6 SLAT LOWER TRAILING CLOSEOUT PANEL SUPPORT BRACKET JUST OTBD OF MID AUX TRACK, IS CRACKED. REFERENCE AMES WO N617AZ-20 NR 192362-0500-0011
O/B HYDRAULIC BAY DOOR FWD HINGE EXCESSIVE PLAY
NR 2 ENGINE STRUT FAIRING 447DB OTBD STIFFENER AND WEB CRACKED.
R2 WINDOW CRANK SHIFTS SIDE TO SIDE WHEN OPENING WINDOW. APPEARS TO BE LOOSE. TIGHTENED AND RETORQUED R2 WINDOW CRANK IAW B767 SRM 51-40-02 AND B767 AIPC 56-11-04-01. OPERATIONAL CHECK GOOD.
CHAFE DAMAGE ON THE NR 2 ENGINE, FWD NACELLE STRUT UPPER SKIN AT NSTA 150.9
DURING DAILY CHECK FOUND CENTER PEDESTAL FLASHLIGHT BRACKET BROKEN. PLACED ON DEFERRAL 73254 MINIMUM EQUIPMENT LISTING ATI-25-63-04-01 CATEGORY C. DUE 25 MAY 2026. REMOVED AND REPLACED CENTER PEDESTAL FLASHLIGHT BRACKET IAW B767 AMM 25-64-00, B767 IAI SUPPLEMENTAL 25-60-00 AND DRAWING 25-767-01002-REV 04 SHEET 6, AND B767 SRM 51-40-02. DEFERRAL 73254 CLEARED.
RIGHT WING UPPER SKIN HAS CORROSION AT WBL 109.9 AND 70 INCHES FWD OF REAR SPAR.
FOUND CRACK ON UPPER ANGLE ON FRONT SPAR ABOVE PDU LES150-148
FRAME AT REAR OF HYD BAY NAC 375, IB ANGLE ON AFT SIDE OF FRAME IS CRACKED.
MAIN CARGO DECK DOOR LATCH CAM HOOK AT STA. 430 HAS CORROSION REFERENCE AMES WO N617AZ-20 NR 192362-0800-0005
MAIN DECK CARGO DOOR LATCH CAM HOOK AT STA. 480 HAS CORROSION REFERENCE AMES WO N617AZ-20 NR 19236208000004
FRAME AT REAR OF HYD BAY NAC 375, OB ANGLE ON AFT SIDE OF FRAME IS CRACKED. REFERENCE AMES WO N617AZ-20 NR 192362-0400-0050
L1 DOOR LOCKING PAWL BROKEN. REMOVED AND REPLACED L1 DOOR INTERLOCK PAWL IAW B767 AMM 52-11-26. OPERATIONAL CHECK GOOD.
CORROSION ON THE LOWER SURFACE OF THE RIGHT WING LOWER SKIN
AT AROUND 80KTS WITH REVERSER DEPLOYED HAD ONE LOUD BANG FROM LEFT ENGINE WITH A FLAME. NO ABNORMAL ENGINE INDICATIONS NOTED. LANDED WITHOUT INCIDENT. ACCOMPLISHED GENERAL VISUAL INSPECTION OF LEFT ENGINE IAW B767 AMM 71-00-00. ENGINE RUN NOTED NO DEFECTS. PULLED DATA FROM QUICK ACCESS RECORDER. REVIEWED AND FOUND TO BE SATISFACTORY SHOWING NO ABNORMALITIES. AIRCRAFT OK FOR SERVICE.
BS 246 FLOORBEAM HAS A CRACKED VERTICAL STIFFENER ON FORWARD SIDE OF BEAM AT LBL 40
EMERGENCY ESCAPE HARNESS BAG IS TORN. REMOVED AND REPLACED EMERGENCY HARNESS BAG IAW B767 IAI AMM 25-60-00.
AT FL350, MASTER WARNING, AURAL ALARM, AND CABIN ALTITUDE. CABIN ALTITUDE 10, 000, CABIN ALTITUDE ON AUTO 2 WAS NOT RESPONDING IN MANAUL OR AUTO 1. CREW INITIATED DIVERSION. CREW DECLARED. LANDED WITHOUT INCIDENT. POST FLIGHT WALK AROUND WAS NORMAL. AIRCRAFT WAS GROUNDED FOR INSPECTION AND MAINTENANCE. IAW B767 FIM 21-31 FAULT TREE 803 NO FAULTS NOTED. OPERATIONAL AND EXTERIOR INSPECTION OF OUTFLOW VALVE IAW B767 AMM 21-31-04 NOTED NO FAULTS. OVERBOARD EXHAUST VALVE CHECK GOOD IAW B767 AMM 21-58-05. REMOVED AND REPLACED CABIN ALTITUDE AUTO PRESSURE CONTROLLER IAW B767 AMM 21-31-02. PRESSURE LEAK CHECK NOTED NO FAULTS IAW B767 AMM 05-51-4. OPERATIONAL CHECK GOOD.
CRACK NOTED AT PYLON NR 1 I/B SIDE PYLON STRUCTURE BRACKET NEXT TO ACCESS PANEL 437BR FWD LOWER CORNER REFERENCE XTREME WO 014592 NRC 512
LEFT OVERWING ESCAPE SLIDE COMPARTMENT OPEN. RESECURED LEFT WING AFT OFF-WING SLIDE COMPARTMENT DOOR. VERIFIED ALL LATCHES ARE ENGAGED AND DOOR IS FAIR WITH FUSEALGE REFERECNE B767 AMM 25-65-08.
FOUND INTERCOSTAL SUPPORT APPROX AT STA 1339 AND RBL 33 WITH CORROSION REFERENCE XTREME WO 014592 NRC 939
LEADING EDGE SLAT DISAGREE EICAS MESSAGE IN THE AIR AFTER MOVING FLAP LEVER TO 1. AIR TRAFFIC CONTROL DECLARED EMERGENCY ON BEHALF OF THE FLIGHT CREW. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS GROUNDED FOR INSPECTION AND MAINTENANCE. COMPLIED WITH B767 FIM 27-81-00-990-806 AND B767 FIM 27-51-00-990-808. SYSTEM CHECK GOOD NO FAULTS NOTED. GENERAL VISUAL INSPECTION AND OPERATIONAL CHECK OF FLAPS AND SLATS NOTED NO FAULTS.
ENGINE NR 2, SHIP FAIRING FWD SECTION FWD LOWER BRACE FRAME FROM INB TO O/B, FOUND OUT OF LIMITS AND WITH ELONGATED HOLES. REFERENCE XTREME WO 014592 NRC 884
LEFT WHEEL WELL ON THE H BEAM IS A HYDRAULIC LINE B NUT THATS SITTING RIGHT IN FRONT OF THE CUSHION CLAMP AND BRACKET, AND THE BRACKET IS CORRODED.
# 2 PYLON PRECOOLER EXHAUST DUCT IS KNIFE EDGE AT A COUPLE SPOTS
CRACK FOUND AT FORWARD ENTRY DOOR CUT OUT AFT LOWER CORNER BETWEEN STA 340- STA 332 - 1" ABOVE S-20L