Aircraft Description
N300ER is a 2013 Bombardier INC BD-100-1A10, a twin-engine turbo-fan aircraft registered to Registration Pending in Chesterfield, MO. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on November 25, 2013. Powered by a Honeywell AS907-1-1A engine producing 6944 pounds of thrust, N300ER is. The aircraft's Mode S transponder code is A31FC6 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N300ER was last updated on July 14, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Bombardier Aviation, based in Montreal, Quebec, Canada, is a leading manufacturer of business jets. The company produces the Challenger and Global series of large-cabin business jets, serving corporate and VIP transportation markets worldwide. AviatorDB tracks 2,968 Bombardier INC aircraft currently registered in the FAA database, including the BD-100-1A10 model.
AviatorDB has found no NTSB accident or incident reports involving N300ER. 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 |
|---|---|---|---|---|
| Mar 3, 2023 | ERA23LA135 | MINR | Fatal | The flight crew’s failure to remove the right side pitot probe cover before flight, their decision to depart with a No-Go advisory message following an aborted takeoff, and their selection of the incorrect non-normal checklist in flight, which resulted in an in-flight upset that exceeded the maneuvering load factor limitations of the airplane and resulted in fatal injuries to a passenger whose seatbelt was not fastened. Contributing to the severity of the in-flight upset were the pilot-in-command’s (PIC) decision to continue the climb and use the autopilot while troubleshooting the non-normal situation, and the PIC’s pilot-induced oscillations following the autopilot disconnecting from the out-of-trim condition. Also contributing to the accident was the crew’s inadequate crew resource management. |
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC