Flugunfall 24 MAR 2001 einer de Havilland Canada DHC-6 Twin Otter 300 F-OGES - Saint-Barthélémy
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Status:Accident investigation report completed and information captured
Datum:Samstag 24 März 2001
Zeit:16:28
Flugzeugtyp:Silhouette image of generic DHC6 model; specific model in this crash may look slightly different
de Havilland Canada DHC-6 Twin Otter 300
Fluggesellschaft:Air Caraïbes
Kennzeichen: F-OGES
Werknummer: 254
Baujahr: 1969
Betriebsstunden:35680
Anzahl Zyklen der Zelle:89331
Triebwerk: 2 Pratt & Whitney Canada PT6A-27
Besatzung:Todesopfer: 2 / Insassen: 2
Fluggäste:Todesopfer: 17 / Insassen: 17
Gesamt:Todesopfer: 19 / Insassen: 19
Opfer am Boden:Todesopfer: 1
Sachschaden: Zerstört
Konsequenzen: Written off (damaged beyond repair)
Unfallort:Saint-Barthélémy (   Saint-Barthélemy)
Flugphase: Annäherung (APR)
Betriebsart:Internationaler Linienflug
Flug von:Sint Maarten-Juliana Airport (SXM/TNCM), Sint Maarten
Flug nach:Saint-Barthélémy Airport (SBH/TFFJ), Saint-Barthélemy
Flugnummer:1501
Unfallbericht:
The Twin Otter plane was on a 10-minute inter island flight between St. Maarten and Saint-Barthélémy and approached Saint-Barthélémy from the West for a visual approach and landing on runway 10. While on finals over the 'Col de la Tourmente', the aircraft was seen making a sharp turn to the left. The Twin Otter struck a house on the 'Col de la Tourmente' and caught fire. A man on the ground was also killed and his wife was injured. While on finals the captain probably
selected "beta reverse range" on the propellers in order to slow down. Upon vigorously pushing back the power levers to their normal position, an asymmetric power condition developed. The Twin Otter rolled to the left and crashed.
Saint-Barthélémy is known for the difficult approach to the airport and pilots flying into Saint-Barthélémy need to have a special certification. After overflying 'Col de la Tourmente' a quick steep descent has to be made to land at runway 10, a 2100 feet runway which ends up in sea. The aircraft overfly the 'Col de la Tourmente' at a height of 10 m or less.

Probable Cause:

PROBABLE CAUSES: "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.
The investigation could not exclude three other hypotheses which can nevertheless be classified as quite unlikely:
- A loss of control during a go-around.
- A loss of control due to a stall.
- A loss of control due to sudden incapacitation of one of the pilots.
The Captain's lack of recent experience on this airplane type, the undeniable difficulty of conducting an approach to runway 10 at Saint-Barthélemy and the pressure of time during this flight were contributory factors. The low height at which the loss of control occurred was an aggravating factor."

Accident investigation:

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Investigating agency: BEA France
Status: Investigation completed
Duration: 2 years and 4 months
Accident number: BEA F-ES010324
Download report: Final report

Informationsquelle:
» SKYbrary 
» AP
» BEA (Bureau Enquetes-Accidents)
» Reuters


Sicherheitsempfehlungen
The BEA recommended the French DGAC and European JAA to demand the installation of flight recorders on aircraft capable of carrying 9 or more passengers with an MTOW of 5700kg or less.

Fotos

photo of DHC-6-Twin-Otter-300-F-OGES
accident date: 24-03-2001
type: de Havilland Canada DHC-6 Twin Otter 300
registration: F-OGES
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Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Sint Maarten-Juliana Airport to Saint-Barthélémy Airport as the crow flies is 32 km (20 miles).
Accident location: Exact; deduced from official accident report.

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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DHC-6 Twin Otter

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