Pilot Debrief

CESSNA 172R near Willoughby Hills, OH — 2014-08-26

Final reportCEN14FA453
Sign in to save
Date
2014-08-26
Location
Willoughby Hills, OH, USA
Airport
CGF
Aircraft
CESSNA 172R
Registration
N4207P
Category
Airplane
Highest injury
Fatal
Fatalities
4
Phase of flight
Takeoff roll

Probable cause

The pilot's failure to maintain control of the airplane while returning to the airport immediately after takeoff, which resulted in the airplane exceeding its critical angle of attack and entering an aerodynamic stall during the turn. Contributing to the accident was the pilot's inadequate preflight planning, which resulted in the airplane being over maximum gross weight and its subsequent decrease in takeoff climb performance.

Contributing factors

Contributing to the accident was the pilot's inadequate preflight planning, which resulted in the airplane being over maximum gross weight and its subsequent decrease in takeoff climb performance.

NTSB narrative

The pilot and three passengers boarded the airplane for a local flight at night. The controller cleared the flight for takeoff and observed the airplane lift off about 2,000 feet down the runway. Shortly after liftoff, the pilot contacted the controller and reported that the airplane was not "climbing fast" and that he wanted to make a left turn to return to the airport. The controller approved the left turn and observed the airplane begin a left turn and descend to impact with the terrain. A postimpact fire ensued. Examination of the accident site indicated that the airplane impacted in a steep descent. The witness observations and the impact geometry are consistent with the pilot failing to maintain adequate airspeed while turning to return to the airport, resulting in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall. A postaccident examination of the airplane and engine did not reveal any anomalies that would have prevented normal operation of the aircraft. Weight and balance calculations showed that the airplane was between 93.6 and 165.6 pounds over maximum gross weight at the time of the accident. The decreased takeoff climb performance reported by the pilot was likely due to the airplane's over gross weight condition.

Analysis

Primary failure mode
Loss of control
First missed decision gate
Pilot could have aborted takeoff when not climbing fast.

NTSB coding

Evidence available

  • Photos
  • 15 docket documents
View NTSB final reportView NTSB docket

Docket documents15

Related mishaps