Overweight Socata TB9 Stalls During Takeoff at Zborowo Airfield

Casualties unknown • Zborowo (EPZB), PL

A Socata TB9 experienced a loss of control during takeoff from a wet grassy runway, resulting in a dynamic stall and collision with obstacles.

What happened

On 9 October 2024, a pilot operating a Socata TB9, registration SP-FNL, attempted a takeoff from the wet grassy runway at Zborowo airfield (EPZB). The flight was planned with three passengers. Due to approaching low clouds and rain, the pilot had kept the engine running at idle for approximately 35 minutes while waiting for the weather to improve.

As the aircraft accelerated down the runway, it experienced an unusually long takeoff run, reaching 650 meters before reaching 60 knots. Upon reaching this point, the pilot attempted to rotate the aircraft. The aircraft climbed only 2 to 3 meters before the pilot, attempting to avoid a house ahead, initiated a left turn. During this maneuver, the pilot pulled the control column back significantly, inducing a sudden increase in the angle of and a dynamic stall. The aircraft's tail struck the runway, causing the plane to roll onto its right wing and strike two fences before coming to a stop. There were no fatalities and no injuries to the pilot or passengers, though the aircraft sustained substantial damage, including the separation of the left wing.

The investigation

The PKBWL investigation examined the aircraft's technical condition, the pilot's weight and balance calculations, and the meteorological conditions at the time of the accident. The investigation reviewed the engine's performance, the fuel used, and the pilot's previous experience with the Socata TB9. Investigators also analyzed the aircraft's mass and center of gravity (CG) relative to its maximum takeoff mass (MTOM) and evaluated the likelihood of carburetor icing given the high humidity and prolonged idling.

Findings

  • The aircraft's MTOM was exceeded by 34 kg because the pilot used an incorrect empty mass of 650 kg instead of the actual 685 kg in his calculations.
  • The aircraft's center of gravity was positioned at the extreme rear of the allowable envelope, contributing to a nose-up tendency.
  • Carburetor icing was a probable factor, as high humidity and a long period of engine idling likely reduced engine power, extending the takeoff run.
  • The pilot failed to abort the takeoff after the run exceeded the expected length for a wet, grassy surface.
  • The pilot had very limited experience with this specific aircraft type, having performed only one prior 40-minute familiarization flight.

Probable cause

The accident was caused by the aircraft exceeding its maximum takeoff mass and operating with an extremely rearward center of gravity, compounded by probable carburetor icing that reduced engine power and extended the takeoff run.

Frequently asked questions

What happened in the 2024-10-09 SOCATA, TB-9 Tampico accident near Zborowo (EPZB), PL?

A Socata TB9 experienced a loss of control during takeoff from a wet grassy runway, resulting in a dynamic stall and collision with obstacles.

What aircraft was involved and where did it happen?

The accident on 2024-10-09 involved a SOCATA, TB-9 Tampico, registration SP-FNL, operated by Prywatny (Private), at Zborowo (EPZB), PL.

What was the probable cause of the accident?

The accident was caused by the aircraft exceeding its maximum takeoff mass and operating with an extremely rearward center of gravity, compounded by probable carburetor icing that reduced engine power and extended the takeoff run.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2024-0113/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.

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