Statuts: | Accident investigation report completed and information captured |
Date: | mercredi 23 novembre 1983 |
Type/Sous-type: |  de Havilland Canada DHC-6 Twin Otter 300 |
Compagnie: | Austin Airways |
Immatriculation: | C-GTLA |
Numéro de série: | 632 |
Année de Fabrication: | 1979 |
Moteurs: | 2 Pratt & Whitney Canada PT6A-27 |
Equipage: | victimes: 0 / à bord: 2 |
Passagers: | victimes: 4 / à bord: 5 |
Total: | victimes: 4 / à bord: 7 |
Dégats de l'appareil: | Perte Totale |
Conséquences: | Written off (damaged beyond repair) |
Lieu de l'accident: | 0,4 km (0.3 milles) de Lansdowne House Airport, ON (YLH) ( Canada)
|
Phase de vol: | En approche (APR) |
Nature: | Transport de Passagers Nat. |
Aéroport de départ: | Sandy Lake Airport, ON (ZSJ/CZSJ), Canada |
Aéroport de destination: | Lansdowne House Airport, ON (YLH/CYLH), Canada |
Détails:A DHC-6 Twin Otter passenger plane, operated by Austin Airways, was damaged beyond repair in an accident near Lansdowne House Airport, ON (YLH).
There were 2 crew and 5 passengers on board of which 4 passengers were asphyxiated in the post crash fire. The 1 surviving passenger suffered serious injuries and the crew escaped with minor or no injuries.
The airplane operated on a domestic flight from Sandy Lake Airport, ON (ZSJ). Visibility at Lansdowne House was poor due to heavy snow snowfall
After executing an overshoot, the captain flew a second circuit without losing sight of the airfield. The aircraft turned toward the runway. The pilot called 'runway in sight' and shortly thereafter, the co-pilot noticed the radio altimeter pass through 200 feet. Moments before impact, the captain reported to the 1st officer that he was encountering whiteout conditions and moved to advance the power levers.
The aircraft was in line with the runway when it struck the snow-covered ice surface of the lake, about 1200 feet short of the runway threshold. The nose gear assembly was broken off at first impact. The aircraft then slid and rotated 180 degrees counter clockwise, struck large rocks on the shore and stopped 600 feet short of the runway.
The rear spars of each wing were separated from the fuselage; the fuel tanks were ruptured and the fuel lines were broken. Fire broke out on impact.
Probable Cause:
The final report did not contain a Probable Cause statement.
Sources:
» CASB Final Report
»
The Montreal Gazette - Nov 24, 1983
Opérations de secours
CASB issued 4 Safety Recommendations
Issued: -- | To: DoT Canada | CASB-85-21 |
In accordance with Department of Transport criteria for the installation of VASIS, a VASIS (or some other approved
equipment for visual assistance in judging from the cockpit the aircraft\'s position relative to the desired approach slope) be installed on Runway 26 at Lansdowne House, Ontario. |
Issued: -- | To: DoT Canada | CASB-85-22 |
The Department of Transport amend Air Navigation Order Series VII Number 2 paragraph 18(4) and Air Navigation Order Series VII, Numbers 3 and 6, paragraphs 19(4) to require @hat in all cases the information described in subsection (3) of the aforementioned paragraphs be pictorially depicted. |
Issued: -- | To: DoT Canada | CASB-85-23 |
The Department of Transport amend its procedures for conducting elective maintenance on navigational and communications equipment to prescribe minimum weather conditions below which elective maintenance shall not be conducted. (The CASB suggests that such weather minima should in no case be less than VFR flight minima and that higher minima may be warranted in some locations) |
Issued: -- | To: DoT Canada | CASB-85-24 |
The Department of Transport effect wide dissemination of Information from this accident for safety educational purposes, particularly as it pertains to:
a) the advisability of maintaining company air-to-ground transceivers in good working order and of air crews making use of all available communications equipment to remain abreast of information pertinent to their flight;
b) the importance of clear and disciplined inter-crew communications in flights conducted in both VFR and IFR flight conditions;
c) the importance of cargo being restrained sufficiently well to remain secured if the aircraft is exposed to survivable impact forces; and
d) the hazard of whiteout conditions and the adverse effect which obscuring ground-based weather phenomena such as blowing snow can have on flight visibilities while approaching to land. |
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Photos
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 Sandy Lake Airport, ON et Lansdowne House Airport, ON est de 375 km (234 miles).
Accident location: Approximate; accuracy within a few kilometers.
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.