Incident Overview

Date: Sunday 6 February 2005
Aircraft Type: de Havilland Canada DHC-8-315Q Dash 8
Owner/operator: Air S‚n‚gal International
Registration Number: 6V-AHL
Location: Tambacounda Airport (TUD) – ÿ Senegal
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 43
Component Affected: Left main undercarriage legLeft main undercarriage leg
Investigating Agency: ANACSANACS
Category: Accident
Air S‚n‚gal International flight 214 experienced a hard landing on runway 6 following a collision with a trench during its flight from Dakar to Tambacounda on February 5, 2005. The aircraft sustained damage to the left main undercarriage leg due to the impact, resulting in a landing on uneven terrain. The accident was attributed to a prior weight and balance assessment that was not fully realized during flight.Air S‚n‚gal International flight 214 experienced a hard landing on runway 6 following a collision with a trench during its flight from Dakar to Tambacounda on February 5, 2005. The aircraft sustained damage to the left main undercarriage leg due to the impact, resulting in a landing on uneven terrain. The accident was attributed to a prior weight and balance assessment that was not fully realized during flight.

Description

Air S‚n‚gal International flight 214 departed Dakar-Yoff Airport, Senegal, at 23:41 hours local time on February 5, 2005. The aircraft, a DHC-8-300, operated a domestic service to Tambacounda. After midnight on February 6, the flight was cleared to land on runway 6. The airplane touched down hard and went off the left side of the runway. It ran over a trench, causing the left hand main undercarriage leg to collapse. The airplane came to rest on uneven terrain at the side of the runway. Probable cause of the accident (translated from French): – Poor weight and balance assessment reported to the Pilot-in-command prior to take-off. During the flight from Dakar to Tambacounda this was not felt because the autopilot was engaged. On approach, the autopilot disengaged and induced an alteration of the speed parameters. To maintain the altitude, the pilot was obliged to increase the power resulting in a speed higher than that recommended, with poor control of the airplane in short final. – After the runway excursion, the plane’s contact with the trenches and sand piles caused by works, contributed to the degradation of certain parts of the aircraft.

Primary Cause

Poor weight and balance assessment prior to takeoff.Poor weight and balance assessment prior to takeoff.

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