20 fatalities

TX1501 Crash Near Saint-Barthélemy: Fatal Loss of Control on Final Approach (F-OGES)

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 accident appears to result from the Captain's use of the propellers in the reverse beta range, to improve control of his track on short final. 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)Source recordUpdated 2026-09-03Data APIEditorial standards
Aircraft registered F-OGES
Aircraft registered F-OGES. Photo: Aero Icarus from Zürich, Switzerland / CC BY-SA 2.0, via Wikimedia Commons

Aircraft TX1501 crashed near Saint-Barthélemy after a left turn and dive on final approach to runway 10. All 19 occupants and one person in a nearby house died. The captain's use of reverse beta propellers was the probable cause.

Flight Details and Final Communications The aircraft departed Saint Maarten Airport for Saint-Barthélemy Airport under callsign TX1501, carrying 17 passengers and two pilots. The captain was pilot flying at a cruise level of 1,500 feet. The crew left the Sint Maarten Juliana aerodrome frequency when abeam Fourchue, the circuit entry point located three nautical miles northwest of Saint-Barthélemy. They subsequently announced passing the 'Fourchue' reporting point on the Saint-Barthélemy Information frequency, followed by a report of passing the 'Pain de Sucre' reporting point for a final approach to runway 10. This was their last communication. ## Accident Sequence As the aircraft began its short final before the La Tourmente pass, several witnesses, including the AFIS agent, observed it turn left into a steep bank angle before diving toward the ground. The aircraft crashed near a house and caught fire. All occupants perished, along with one person who was inside the house. ## Probable Cause and Contributing Factors The official investigation determined the accident resulted from the captain's use of the propellers in the reverse beta range to improve track control on short final. A strong thrust asymmetry when exiting the reverse beta range caused loss of yaw control, followed by loss of roll control. The investigation could not exclude three other hypotheses—loss of control during a go-around, loss of control due to a stall, or loss of control due to sudden incapacitation of one pilot—but classified these as quite unlikely. Contributory factors included the captain's lack of recent experience on this airplane type, the difficulty of the approach to runway 10 at Saint-Barthélemy, and time pressure during the flight. The low altitude at which the loss of control occurred was an aggravating factor.

Frequently asked questions

What happened in the 24 Mar 2001 De Havilland DHC-6 Twin Otter accident near Saint-Barthélemy-Rémy de Haenen (Saint-Jean-Gustave III), Saint-Barthélemy?

Aircraft TX1501 crashed near Saint-Barthélemy after a left turn and dive on final approach to runway 10. All 19 occupants and one person in a nearby house died. The captain's use of reverse beta propellers was the probable cause.

Were there any fatalities in the 24 Mar 2001 De Havilland DHC-6 Twin Otter accident?

The accident was fatal, resulting in 20 fatalities.

What aircraft was involved and where did it happen?

The accident on 24 Mar 2001 involved a De Havilland DHC-6 Twin Otter, registration F-OGES, operated by Air Caraïbes, at Saint-Barthélemy-Rémy de Haenen (Saint-Jean-Gustave III), Saint-Barthélemy.

What was the probable cause of the accident?

The accident appears to result from the Captain's use of the propellers in the reverse beta range, to improve control of his track on short final. A strong thrust asymmetry at the moment when coming out of the reverse beta range would have caused the loss of yaw control, then roll control of the aircraft.