Aircraft Description
N363CM is a Boeing 767-338, a twin-engine turbo-fan aircraft registered to Cargo Aircraft Management INC in Wilmington, OH. The registration certificate was issued on October 21, 2011. The registration is set to expire on October 31, 2027. The aircraft is configured with 351 seats. The aircraft's Mode S transponder code is A417AF (hex), used for ADS-B identification and flight tracking. N363CM was last tracked by AviatorDB near Hartsfield Jackson Atlanta International Airport (KATL) on April 2, 2026. The FAA registry record for N363CM was last updated on September 20, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Boeing 767-200, aviation's first twin-engine wide-body airliner, revolutionized commercial aviation by proving that twin-engine aircraft could efficiently operate long-haul routes previously requiring four engines. First flown on September 26, 1981, it was a low-wing twin-engine wide-body that could accommodate 210 passengers in three-class configuration. Measuring 159 feet in length with a 156-foot wingspan, it achieved a maximum range of 3,900 nautical miles and cruising speed of Mach 0.86. The aircraft was manufactured by Boeing Commercial Airplanes at their Everett, Washington facility. AviatorDB tracks 6,953 Boeing aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is B762.
AviatorDB has found no NTSB accident or incident reports involving N363CM. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Jan 29, 2021 | ENG21LA013 | MINR | Unknown | The fatigue fracture and liberation of two airfoils from a low pressure turbine stage 5 nozzle segment that impacted and damaged the downstream low pressure stage 5 blades creating an initial imbalance load in the engine’s low pressure turbine rotor sufficient to allow all the low pressure turbine blades to lose radial blade clearance, contact static structure, and to fracture transversely across the airfoil. The progressive failure of the low pressure rotor caused an increasingly imbalanced load that eventually resulted in the fracture of the oil supply tube that allowed oil to contact hot engine parts and smolder and ignite resulting in the undercowl fire. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC