Student Pilot Experiences Speed Loss During Go-Around in Cessna 172S

Casualties unknown • Hüfifirn, GL, CH

A student pilot performing a solo training flight at Beaufort West experienced a significant loss of airspeed and a perceived engine failure following a hard landing and improper flap retraction.

What happened

On 2-July 2021, a student pilot was conducting a solo consolidation flight in a Cessna 172S, registration ZS-TBJ, at Beaufort West Aerodrome in the Western Cape. After successfully completing an initial touch-and-go on Runway 08, the pilot attempted a second touch-and-go. During this second attempt, a gust of wind from the right caused the aircraft to land heavily, resulting in the nose swinging to the left while the aircraft maintained high speed.

In response to the bounce, the pilot applied full power to initiate a go-around. As the aircraft climbed past 300 feet, the pilot observed that the airspeed was only 70 knots and the nose remained below the horizon. An attempt to lower the nose to regain speed resulted in the airspeed dropping further to approximately 57 knots. Believing an engine failure had occurred, the pilot notified the Aerodrome Flight Information Service (AFIS) and activated the crash alarm. After performing a teardrop maneuver and realizing the aircraft was too high for Runway 26, the pilot executed a second maneuver and landed safely on Runway 08. There were no injuries and no damage to the aircraft.

The investigation

The investigation examined the sequence of events following the hard landing and the subsequent flight characteristics. Investigators analyzed the pilot's actions regarding power application and flap configuration. The inquiry focused on why the aircraft failed to accelerate during the climb and why the pilot's attempt to lower the nose led to a further reduction in airspeed.

Findings

  • The aircraft likely bounced during the landing phase due to a wind gust and high speed.
  • The pilot failed to retract the flaps during the go-around procedure.
  • The failure to retract flaps created excessive drag, which prevented the airspeed from increasing past 70 knots during the climb.
  • When the pilot attempted to push the nose down to increase speed, the high drag from the extended flaps caused the airspeed to drop to 57 knots.

Probable cause

The student pilot bounced during a touch-and-go and neglected to retract the flaps during the subsequent go-around, leading to excessive drag that prevented proper acceleration and caused a loss of airspeed when the nose was lowered.

Frequently asked questions

What happened in the 1964-05-18 PIPER AIRCRAFT CORPORATION PA-18-150 accident near Hüfifirn, GL, CH?

A student pilot performing a solo training flight at Beaufort West experienced a significant loss of airspeed and a perceived engine failure following a hard landing and improper flap retraction.

What aircraft was involved and where did it happen?

The accident on 1964-05-18 involved a PIPER AIRCRAFT CORPORATION PA-18-150, registration HB-OWA, at Hüfifirn, GL, CH.

What was the probable cause of the accident?

The student pilot bounced during a touch-and-go and neglected to retract the flaps during the subsequent go-around, leading to excessive drag that prevented proper acceleration and caused a loss of airspeed when the nose was lowered.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/165.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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