Ontario

A de Havilland DHC-2 Beaver seaplane, registration C-FNFO, serial number 819, departed from Kakabikitchiwan Lake, Ontario, on a visual flight rules flight for Aremis Lake with only the pilot on board. Shortly after take-off, the aircraft was observed flying northbound at a very low altitude above Sabaskong Bay with the engine operating at a high power setting. The aircraft started to climb and bank to the left. The right wing struck the lower of two electrical wires strung across a channel between two islands. The aircraft was destroyed; the pilot sustained fatal injuries.

The Dassault-Breguet Falcon 20E aircraft was on an unscheduled charter cargo flight from Detroit Willow Run, Michigan, USA, to Peterborough, Ontario. The flight was being conducted at night and under instrument flight rules in instrument meteorological conditions. Nearing the destination, the flight crew received a clearance to conduct a non-directional beacon runway 09 approach at Peterborough Airport. The flight crew did not acquire the runway environment during this approach and conducted a missed approach procedure. They obtained another clearance for the same approach from Toronto Area Control Centre. During this approach, the flight crew acquired the runway environment and manoeuvred the aircraft for landing on runway 09. The aircraft touched down near the runway midpoint, and the captain, who was the pilot flying, elected to abort the landing. The captain then conducted a left visual circuit to attempt another landing. As the aircraft was turning onto the final leg, the approach became unstabilized, and the flight crew elected to overshoot; however, the aircraft pitched nose-down, banked left, and struck terrain. As it travelled 400 feet through a ploughed farm field, the aircraft struck a tree line and came to rest about 2000 feet before the threshold of runway 09, facing the opposite direction. The aircraft was substantially damaged. No serious injuries occurred.

While holding outside the control zone at Red Lake (YRL) pending a special VFR clearance, the pilot made a descending turn to avoid a flock of large birds. The right wing struck the water of Ranger Lake and the Cessna overturned. A military DHC-8 diverted to Red Lake and located the Cessna on the west side of Ranger Lake. The airplane was partially submerged and the pilot was on the wing. A floatplane (C-FVTU) subsequently picked up the pilot and returned him to Red Lake. The pilot suffered shoulder injuries, arm injuries, facial injuries and hypothermia.

The de Havilland DHC-2 Beaver seaplane departed from Big Trout Lake, Ontario, on a visual flight rules flight for Geraldton, Ontario, with a pilot and an aircraft maintenance engineer on board. After encountering adverse weather conditions en route to Geraldton, the pilot decided to divert to Pickle Lake, Ontario. At about 1430 central daylight time, the engine lost power at an altitude of about 300 feet above ground level while in the descent for Pickle Lake. The pilot turned the aircraft toward a nearby narrow river. In an attempt to restart the engine, the pilot confirmed that the fuel pressure was normal, the fuel selector was on the fullest tank (front), the throttle was at idle, the mixture was rich, and the ignition switch was on both, then he operated the wobble pump. When the engine did not restart, he switched to the centre fuel tank and operated the wobble pump again, but the engine still did not restart. He then switched back to the front tank and tried another restart, without success. He then landed the aircraft on the river at an estimated landing speed of about 40 to 45 mph. After the forced landing, the left wingtip collided with trees on the river bank, and the aircraft yawed to the left about 180 degrees and struck the river bank, breaking off the floats and the float struts. Impact with more trees on the river bank damaged the right wing and elevator. Both occupants were wearing lap belts with shoulder harnesses and were uninjured. The aircraft was substantially damaged. The pilot advised Thunder Bay flight service station by radio of the engine failure and crash and the crew were rescued two hours later.

The Thunder Airlines Limited Beech A100 King Air aircraft, serial number B108, took off at 1034 eastern daylight saving time (EDT) on a charter flight from Thunder Bay, Ontario, for Red Lake, Ontario, with two pilots and three passengers on board. After getting airborne, the aircraft pitched up to approximately 70 degrees, reaching a height estimated to be between 500 and 700 feet above ground level. It then rolled to the left, pitched steeply nose-down, and descended to the ground within the confines of the airport. The aircraft contacted the soft, level ground in a relatively level attitude and covered a distance of about 500 feet before coming to rest in a wooded area immediately beyond an elevated railroad bed and track. The cabin remained intact during the crash sequence, and all occupants escaped without any injuries. The aircraft was damaged beyond repair. An ensuing fuel-fed fire was rapidly extinguished by airport emergency response services (ERS)
personnel.

With one pilot and one passenger, the Mitsubishi MU-2B-40 Solitaire aircraft, serial number 410 S.A., departed on a night instrument flight rules flight from Parry Sound / Georgian Bay Airport, Ontario, destined for Toronto / Lester B. Pearson International Airport. Prior to departure, the pilot received his instrument flight rules clearance via telephone from the Sault Ste. Marie flight service station with a clearance valid time of 2118 eastern daylight time from Toronto Area Control Centre and a clearance cancel time of 2135. When the pilot did not establish communications with Toronto Area Control Centre within the clearance valid time, the Area Control Centre supervisor commenced a communication search. At 2151, he confirmed with Parry Sound / Georgian Bay Airport personnel that the aircraft had departed 10 to 15 minutes earlier. The aircraft was assumed missing and the Rescue Coordination Centre in Trenton, Ontario, was notified. Search and rescue was dispatched and three days later the aircraft wreckage was located one nautical mile west of the airport. Both of the aircraft occupants were fatally injured. The aircraft disintegrated as it cut a 306-foot swath through the poplar forest. The accident occurred at night in instrument meteorological conditions.

On final approach to Muskoka Airport, while on a cargo flight from Kitchener-Waterloo Airport, the twin engine aircraft descended too low in a slight nose down attitude when it collided with trees and crashed on the ground. Both occupants were seriously injured and the aircraft was damaged beyond repair. At the time of the accident, ceiling was at 1,000 feet with 10 km visibility and wind from 140 at 2 knots.

Wasaya Airways Ltd. Flight 804, a Hawker Siddeley 748-2A, serial number 1750, landed at Kasabonika, Ontario, on a freight flight from Pickle Lake, Ontario. During the landing roll, the aircraft could not be stopped and overran the runway by about 450 feet. The captain, the first officer and one of the freight handlers suffered minor injuries; the other freight handler was not injured. The aircraft was destroyed.

A Voyageur Airways Beechcraft A100 aircraft, C-GILM, was on a flight from Winnipeg International Airport Winnipeg International Airport, MB (YWG) to Sioux Lookout Airport, ON (YXL). The crew of two pilots and two paramedics had completed a medevac flight and were returning to Sioux Lookout without a patient on board. The weather was reported to be: wind 060 degrees at two knots, visibility three statute miles in freezing drizzle, and ceiling overcast at 400 feet AGL. The First Officer was at the controls as they attempted two full NDB approaches for runway 34, each of which resulted in a missed approach. The captain then took control of the aircraft and conducted a full NDB approach for runway 34. On final approach, the crew had the runway in sight and the aircraft was lined up, but the aircraft was high on the approach. The captain called for full flap and pushed the props up to help slow the aircraft down. The aircraft developed a high rate of descent that was not fully countered before the aircraft contacted the runway firmly with the left main landing gear. The aircraft was taxied part way to the company ramp before the aircraft began pulling to the left very noticeably. The scissors had failed and the main wheels were turned slightly off-line. While conducting a heavy-landing inspection, company maintenance and operational personnel determined that in addition to the damage to the scissors for the left main landing gear, the rear spar of the left wing had failed in the vicinity of a pass-through hole for the flap actuator. The damage is reported to be overload in nature and consistent with the effects of landing hard on the left main wheel. During the approaches, the aircraft was above cloud during the penetration turns and was only in cloud during the final approach phases. A small amount of ice accumulated on the aircraft while in cloud (about 1/8th to 1/4 inch on the spinner remained after landing) but the de-ice equipment was working and was used.

Bearskin Flight 310, a Beech 99, was inbound to Webequie Airport (YWP) on a scheduled passenger flight from Fort Hope Airport (YFH). The flight crew completed an approach to Webequie based on visual cues, GPS and ADF. The flight crew lowered the landing gear about three miles from the runway and set full flap on final approach. The captain reportedly initiated the flare at about 50 feet and the nose of the aircraft came up, but the descent was not arrested before the aircraft struck the runway. The aircraft's wings and tail reportedly had a small amount of residual ice at landing. Winds on the surface were northwest at five to ten knots but the winds aloft were reported to be easterly at up to 50 knots. Examination of the aircraft at the terminal building led the crew to call company maintenance for an inspection. Inspection of the aircraft revealed that the left wing spar was broken, the left wing skin was wrinkled and the left engine was drooping. There were no injuries reported.