No fatalities

Simulated Engine Failure Results in Bounce and Stabilator Damage (N843KS)

Salina, KS, US

On October 27, 1997, a Beech 23 (registration N843KS) was involved in an aviation accident near Salina, KS. No fatalities were reported. Investigators recorded the probable cause as: the student pilot's excessive pull-up and the flight instructor's inadequate supervision during a simulated engine failure after takeoff, resulting in a stall/mush onto the runway. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

During a simulated engine failure at 100 feet AGL, a student pilot's control input led to a sink, collision with runway, bounce, and subsequent loss of stabilator effectiveness. The right main gear sheared off and contacted the right flap and stabilator.

Incident Overview

A Certified Flight Instructor (CFI) was conducting a training flight with a student pilot. Shortly after takeoff, at an altitude of approximately 100 feet above ground level (AGL), the CFI reduced the engine power to idle to simulate an engine failure. In response, the student pilot pulled back on the control yoke, which decreased the airspeed and resulted in a high rate of descent.

Sequence of Events

The CFI took control of the airplane and added power. However, the airplane collided with the runway and bounced, becoming airborne again. During the climb, the CFI noticed a loss of stabilator effectiveness. Despite this, the CFI was able to return the airplane to the airport and execute a landing.

Post-Landing Inspection

After landing, an inspection revealed that the right main landing gear had sheared off during the bounce. The detached gear then contacted the right flap and the right stabilator, causing damage to those components.

Contributing Factors

No contributing factors or causal links were stated in the source. The incident involved a simulated engine failure at low altitude, student control inputs, and a subsequent bounce that led to structural damage.

Frequently asked questions

What happened in the 27 Oct 1997 Beech 23 accident near Salina, KS?

During a simulated engine failure at 100 feet AGL, a student pilot's control input led to a sink, collision with runway, bounce, and subsequent loss of stabilator effectiveness. The right main gear sheared off and contacted the right flap and stabilator.

Were there any fatalities in the 27 Oct 1997 Beech 23 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 27 Oct 1997 involved a Beech 23, registration N843KS, at Salina, KS.

What was the probable cause of the accident?

the student pilot's excessive pull-up and the flight instructor's inadequate supervision during a simulated engine failure after takeoff, resulting in a stall/mush onto the runway.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X08980. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.