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Cessna 210 — registry & accident history

Compiled from FAA & NTSB records · as of Jul 25, 2026

There are 663 Cessna 210 airframes on record (built 1957–1981), 188 currently registered. 27 have one or more NTSB accident records (29 records total, 3 with a fatal highest-injury classification). Data as of Jul 25, 2026.

663
Airframes
188
Registered
1957–1981
Years
29
NTSB records

Recent Cessna 210 accidents

  1. N9417TOct 25, 2025No injuries
  2. N9433TMay 20, 2023Minor

    A fuel leak caused by an age-degraded fuel pressure sender hose, which resulted in fuel starvation and a loss of engine power. Contributing to the accident was inadequate maintenance.

  3. N9468TNov 27, 2022No injuries

    The nose landing gear retract arm separation for reasons that could not be determined.

  4. N7350EMay 15, 2021Serious

    A total loss of engine power due to a malfunction of the fuel flow manifold valve.

  5. N9622TOct 26, 2020Fatal

    The pilot’s improper decision to fly into icing conditions with an airplane that was not equipped for icing, which led to structural icing and a subsequent loss of airplane control, and the pilot’s impairment from carbon monoxide poisoning due to a cracked heat exchanger. Contributing to the accident was the pilot’s self-induced pressure to complete the flight due to the incoming adverse weather conditions and the inadequate inspection of the cabin air heat exchanger.

  6. N9540TAug 26, 2020No injuries

    The failure of the engine-driven hydraulic pump, which resulted in the main landing gear not fully extending and locking into place during landing. Contributing to the accident was the failure of the emergency gear extension system for reasons that could not be determined.

  7. N81KDNov 2, 2018Fatal

    The non-instrument-rated pilot's improper decision to conduct a flight in which instrument meteorological conditions existed along the route of flight, which resulted in spatial disorientation and a loss of airplane control.

  8. N7330ESep 20, 2017No injuries

    Partial retraction of the main landing gear during the landing roll for reasons that could not be determined because postaccident examination and functional testing of the gear revealed no anomalies.

Cessna 210 aircraft