Instructional Flight Exits Runway During Landing in Londrina

Casualties unknown • LONDRINA, PR, BR

An Aero Boero AB-115 experienced a loss of directional control on the runway during a landing demonstration, resulting in a 180-degree turn and runway excursion.

What happened

On January 24, 2016, an Aero Boero AB-115, registration PP-FGM, was conducting a cross-country navigation flight for a commercial pilot training program. The flight originated from Bauru (SBBU) and was destined for Londrina (SBLO), operated by Aeroclube de Londrina. On board were an instructor and a student pilot.

During the approach to Londrina, the instructor took control of the aircraft to demonstrate a three-point landing technique. During the flare, the aircraft descended abruptly and bounced on the runway. In an attempt to regain lift and execute a second touchdown, the instructor applied power. Upon the second contact with the ground, the aircraft yawed sharply to the left, performing a 18/0-degree turn on its axis and exiting the runway.

The investigation

The investigation examined the aircraft's handling characteristics and environmental conditions. The AB-115 features a conventional landing gear configuration with a high wing and a narrow track, which inherently complicates ground maneuverability. Furthermore, the aircraft's center of gravity is positioned just behind the main gear, making it susceptible to directional instability during crosswind conditions.

At the time of the incident, the METAR indicated a left crosswind of 070° at 08 knots, with a crosswind component of approximately 07 knots. While this wind was within the manufacturer's operational limits (10 to 13 knots for paved runways), the investigation noted that the left wind, combined with the engine torque produced by the power application, exacerbated the leftward yaw. Analysis of tower video suggested the initial touchdown was abrupt and uncoordinated, potentially causing the nose wheel to lose steering effectiveness and triggering the loss of control.

Findings

  • The primary contributing factor was the improper application of flight controls following a bounced landing.
  • The aircraft's conventional gear configuration and center of gravity made it highly sensitive to directional changes on the ground.
  • The application of power during the bounce increased engine torque, which, when paired with the existing left crosswind, intensified the leftward yaw.
  • The two crew members were uninjured, and the aircraft sustained no damage.

Probable cause

The loss of control was caused by an uncoordinated and abrupt touchdown following a bounce, which, when combined with engine torque and a left crosswind, led to a significant leftward yaw and subsequent runway excursion.

Frequently asked questions

What happened in the 2016-01-24 aircraft accident near LONDRINA, PR, BR?

An Aero Boero AB-115 experienced a loss of directional control on the runway during a landing demonstration, resulting in a 180-degree turn and runway excursion.

What aircraft was involved and where did it happen?

The accident on 2016-01-24 involved a aircraft, registration PPFGM, at LONDRINA, PR, BR.

What was the probable cause of the accident?

The loss of control was caused by an uncoordinated and abrupt touchdown following a bounce, which, when combined with engine torque and a left crosswind, led to a significant leftward yaw and subsequent runway excursion.

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