20 fatalities

2001-03-24: De Havilland DHC-6 Twin Otter (F-OGES) — Air Caraïbes — Saint-Barthélemy-Rémy de Haenen (Saint-Jean-Gustave III), Saint-Barthélemy

Saint-Barthélemy-Rémy de Haenen (Saint-Jean-Gustave III), Saint-BarthélemyLanding (descent or approach)

On March 24, 2001, a De Havilland DHC-6 Twin Otter (registration F-OGES) operated by Air Caraïbes was involved in an aviation accident near Saint-Barthélemy-Rémy de Haenen (Saint-Jean-Gustave III), Saint-Barthélemy during landing or approach. 20 people were killed. Investigators recorded the probable cause as: The pilot's use of propellers in the reverse beta range caused a thrust asymmetry that led to a loss of directional and roll control. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781202809Data APIEditorial standards
Aircraft registered F-OGES
Aircraft registered F-OGES. Photo: Aero Icarus from Zürich, Switzerland / CC BY-SA 2.0, via Wikimedia Commons

A flight from Saint Maarten to Saint-Barthélemy crashed during its final approach, resulting in the deaths of all on board and one person on the ground.

What happened

On a scheduled flight from Saint Maarten Airport to Saint-Barthélemy Airport, an aircraft carrying 17 passengers and two crew members was performing a landing approach. While cruising at 1,500 feet, the crew transitioned from the Sint Maarten Juliana aerodrome frequency to the Saint-Barthélemy Information frequency. After passing the Fourchue reporting point, the flight crew reported passing the Pain de Sucre waypoint while preparing for a final approach to runway 10.

During the short final phase of the approach, near the La Tourmente pass, observers including an AFIS agent witnessed the aircraft execute a sharp left turn characterized by a steep bank and a sudden dive toward the terrain. The impact occurred near a residential structure, which subsequently caught fire. The accident resulted in 19 fatalities on board the aircraft, as well as one fatality of an individual located in the nearby house.

Findings

The investigation determined that the primary cause was the pilot's decision to utilize the propellers in the reverse beta range to assist with directional control during the final approach. This action created a significant thrust asymmetry when transitioning out of the reverse beta range, leading to a loss of both yaw and roll control.

Several secondary factors contributed to the accident, including:

  • The pilot's lack of recent experience operating this specific aircraft type
  • The inherent difficulty of performing an approach to runway 10 at Saint-Barthélemy
  • Time pressure experienced during the flight
  • The low altitude at which the loss of control occurred

Probable cause

The pilot's use of propellers in the reverse beta range caused a thrust asymmetry that led to a loss of directional and roll control.