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Last updated: 20 November 2019
Statuts:Enquête Officielle
Date:mercredi 23 mars 2011
Heure:22:50
Type/Sous-type:Silhouette image of generic FA10 model; specific model in this crash may look slightly different
Dassault Falcon 100
Compagnie:Aviation Transport Solutions LLC
Immatriculation: N303FZ
Numéro de série: 218
Année de Fabrication: 1989
Equipage:victimes: 0 / à bord: 2
Passagers:victimes: 0 / à bord: 1
Total:victimes: 0 / à bord: 3
Dégats de l'appareil: Substantiels
Conséquences: Written off (damaged beyond repair)
Lieu de l'accident:Jeffersonville-Clark Regional Airport, IN (JVY) (   Etats-Unis d'Amérique)
Phase de vol: A l'atterrissage (LDG)
Nature:Affaires
Aéroport de départ:Hamilton Airport, OH (HAO/KHAO), Etats-Unis d'Amérique
Aéroport de destination:Jeffersonville-Clark Regional Airport, IN (JVY/KJVY), Etats-Unis d'Amérique
Détails:
A Falcon 10 business jet, N303FZ, was substantially damaged when it departed the runway during landing at Clark Regional Airport (KJVY), Indiana. The captain, first officer, and sole passenger were not injured.
The captain was the pilot-flying during the accident flight. After departure, the flight had to circumnavigate around numerous thunderstorms that affected the planned route of flight. When the flight was within 25 nautical miles (nm) of its intended destination, the flight crew cancelled the instrument flight plan and concluded the flight under visual flight rules.
The captain noted the wind was from 310 degrees at 19 knots, gusting 27 knots. A 5 nm straight-in final approach was flown to runway 36 (5,500 feet by 100 feet). The captain reported that the landing reference speed (Vref) was 110 knots, which included a 5 knot gust factor. As the airplane touched down on its main landing gear, it encountered a wind gust that raised the left wing. The captain corrected with a left roll input as he simultaneously reduced the airplane's pitch in an attempt to place the nose wheel onto the runway, but the airplane became airborne and drifted off the runway. The airplane touched down for the second time in the grassy area alongside the runway where the subsequent landing roll was completed without further incident. The captain reported that there were no preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane.

A postaccident examination of the airframe revealed that the right main landing gear had shifted/twisted inside the wheel well damaging both forward and aft spar assemblies. Additionally, the aft movement of the nose landing gear had damaged the forward pressure bulkhead. Both engines appeared to have ingested foreign object debris past their first compressor stages.

Probable Cause:

PROBABLE CAUSE:
The pilot's failure to maintain control of the airplane during landing in strong and gusty wind conditions.

Accident investigation:
cover
Investigating agency: NTSB
Status: Investigation completed
Duration: 300 days (10 months)
Accident number: CEN11LA265
Download report: Summary report

Sources:
» NTSB


Photos

photo of Dassault-Falcon-100-F-GHSK
accident date: 23-03-2011
type: Dassault Falcon 100
registration: F-GHSK
 

Plan
Ce plan montre l'aéroport de départ ainsi que la supposée destination du vol. La ligne fixe reliant les deux aéroports n'est pas le plan de vol exact.
La distance entre Hamilton Airport, OH et Jeffersonville-Clark Regional Airport, IN est de 152 km (95 miles).

Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus à ce jour.
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