Loss of Control in Flight · NTSB SEA08FA161

CESSNA 441 — Sunriver, OR

1 fatal
DateJuly 16, 2008
LocationSunriver, OR
AircraftCESSNA 441
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceApproach-VFR go-around Loss of control in flight
Pilot age50
Pilot total time965 hrs · Building experience
Time in type277 hrs
Fatalities1

Probable cause

The pilot's misjudged landing flare and improper recovery from a bounced landing, and the pilot's failure to maintain directional control during the go-around after one of the airplane's propellers struck the runway.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C

What happened

The pilot was executing a day visual flight rules full-stop landing and touched down on the main landing gear near the approach end of the runway. Soon after the initial touchdown, the airplane became airborne again. Instead of initiating a go-around, the pilot attempted to continue the landing sequence. During that attempt, the airplane bounced on the runway three or four times, each time the rebound back into the air and the runway contact was more severe. During the last contact the airplane impacted the runway with sufficient force to result in the failure of the right main landing gear actuator rod, and in the right propeller contacting the runway surface multiple times. The pilot then initiated a go-around, but since the right engine had failed due to the multiple propeller strikes, the airplane produced asymmetrical thrust and began to roll to the right, veering off the right side of the runway. Soon thereafter its right wing collided with a tree and the airplane impacted terrain in an open field. The airplane was consumed by fire shortly after the collision. Postcrash inspection found no evidence of mechanical failure or malfunction with the airframe or either engine.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →