Aircraft stall and runway excursion during takeoff

No fatalities • La Ceiba-Goloson, Honduras • Takeoff (climb)

An aircraft experienced a stall and subsequent runway excursion immediately following takeoff, resulting in significant damage but no injuries.

What happened

During the initial climb phase following departure from runway 06, the flight crew performed the procedure to retract the landing gear and decrease engine power. Shortly after these actions, the aircraft entered a stall condition. This loss of lift caused the plane to descend back onto the runway surface.

Upon contacting the runway, the aircraft slid for approximately 450 metres before coming to a complete stop. Despite the impact, all 21 occupants managed to evacuate the aircraft without injury. The aircraft sustained damage that was determined to be beyond repair.

Findings

  • The loss of altitude and subsequent runway excursion were triggered by the crew reducing engine power while simultaneously retracting the landing gear during the climb.

Probable cause

The reduction of engine power during the initial climb phase led to an aerodynamic stall.

Frequently asked questions

What happened in the 1997-03-03 Let L-410 accident near La Ceiba-Goloson, Honduras?

An aircraft experienced a stall and subsequent runway excursion immediately following takeoff, resulting in significant damage but no injuries.

Were there any fatalities in the 1997-03-03 Let L-410 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1997-03-03 involved a Let L-410, registration HR-IAS, operated by Isleña Airlines - Isleña de Inversiones, at La Ceiba-Goloson, Honduras.

What was the probable cause of the accident?

The reduction of engine power during the initial climb phase led to an aerodynamic stall.

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