Ontario

The pilot of the Cessna 441 Conquest was conducting an international charter flight from General Mitchell International Airport in Milwaukee, Wisconsin, to Gods Lake Narrows, Manitoba. The pilot landed the aircraft at Fort Frances, Ontario, to clear customs and refuel, and then continued his visual flight rules (VFR) flight to Gods Lake Narrows. During the take-off at Fort Frances, the aircraft experienced a power loss in the left engine. The pilot elected to continue the take-off but was unable to control the aircraft after it became airborne. The aircraft veered to the left and crashed on the airfield. The accident occurred at 0425 central daylight time (CDT), at night, on the Fort Frances Municipal Airport. All seven occupants sustained minor injuries and the aircraft was damaged beyond repair.

The aircraft, a Hawker Siddeley 748 Series 2A Model 234 (HS 748) owned and operated by Air Manitoba Ltd. (Air Manitoba), took off from Winnipeg at 1438 central standard time (CST) , 10 November 1993, on scheduled flight NAM 205/ 206 that included stops at Sandy Lake, Ontario; St. Theresa Point, Manitoba; Island Lake, Manitoba; and return to Winnipeg, Manitoba. The flight was conducted in accordance with an instrument flight rules (IFR) flight plan and flight notification. On arrival at Sandy Lake at approximately 1549, the crew attempted to land but were unable to because of the low ceiling and visibility. They then diverted to St. Theresa Point, landing at 1630. A normal turnaround was completed; the number of passengers on departure was 26, and 2,086 pounds of fuel was uploaded to an estimated total of 6,700 pounds on board. The flight departed St. Theresa Point for Sandy Lake at 1720. The aircraft landed at approximately 1745 at Sandy Lake, where 22 passengers deplaned while four remained on board; the aircraft was not refuelled or otherwise serviced at Sandy Lake. During the stop, both engines were shut down. On take-off from Sandy Lake, there were two pilots, a flight attendant, and four passengers on board. The aircraft took off from runway 29 at Sandy Lake at approximately 1805 and entered a right turn. Witnesses indicate that the aircraft appeared to fly at a lower than normal height throughout the turn. After turning through approximately 120 degrees(°), the aircraft descended into 100-foot trees and crashed. The aircraft struck the ground about one nautical mile (nm) northwest of the airport. All seven occupants of the aircraft were fatally injured in the crash. The accident occurred during the hours of darkness. The wreckage was located at position latitude 53°04'71"N, longitude 93°21'38"W, at an elevation of approximately 940 feet above sea level (asl).

En route from Steinbach to Webequie, the pilot informed ATC about his position some 64 km north of Pickle Lake. Few minutes later, the twin engine aircraft crashed in unknown circumstances in the region of Nibinamik, southwest of Webequie. The wreckage was found on September 23 in an isolated area. Both occupants were killed.

Crashed in unknown circumstances while on approach to Ottawa Airport. The pilot, sole on board, was injured. The aircraft was on a delivery flight.

Crashed in unknown circumstances shortly after takeoff from Sandridge Lake. The aircraft was destroyed by a post crash fire and all four occupants were killed.

At 2043 eastern daylight time (EDT), Frontier Air Flight 1602, C-GFAW, a Beechcraft C99 Airliner, took off from Timmins, Ontario, on a scheduled domestic flight to Moosonee, Ontario. The aircraft carried a two-pilot crew, two passengers, and approximately 60 pounds of freight and baggage. The flight proceeded, via airways, to Moosonee at 7,000 feet above sea level. At 2121 EDT, the flight was cleared for an approach at Moosonee with a temporary altitude restriction of 5,000 feet. The crew elected to fly the very high frequency omnidirectional range (VOR) runway 24 approach. At 2129 EDT, the crew reported on the 061° radial of the VOR at five nautical miles (nm) outbound. Shortly after intercepting the 061° radial inbound, the crew initiated a descent to the 440-foot minimum descent altitude (MDA). While in the descent, the aircraft broke through the lowest cloud layer at 900 feet asl, approximately 9.2 nm from the VOR. At this point, both pilots had the runway lights in sight, and the captain decided to change to a visual approach and proceed inbound at 700 feet asl. Shortly after advising the co-pilot of his intentions, the captain initiated the before-landing cockpit check and selected the landing gear lever to the DOWN position. Immediately thereafter, the aircraft struck trees and crashed seven miles east-northeast of the Moosonee Airport. One of the pilot was killed while three other occupants were injured.

The twin engine aircraft was dispatched at Pelée Airport to evacuate to Windsor a patient. On board were one patient, his spouse, one ambulance officer and two pilots. Shortly after a night takeoff from runway 28, while climbing, the aircraft went out of control and crashed in Lake Erie. The copilot and the patient survived while three other occupants were killed.

Air Ontario Flight 1363, a Fokker F-28 jet, crashed during takeoff from Dryden Municipal Airport, Ontario, Canada. Of the 69 persons on board, 24 suffered fatal injuries. The aircraft in question, registration C-FONF, had suffered from a malfunctioning auxiliary power unit (APU) for the five days preceding the accident. Throughout the week preceding March 10, Air Ontario maintenance attempted, with limited success, to cure the APU problems. On March 9 it was decided to defer the repair of the APU until the aircraft returned to Toronto on the night of March 10. This meant that the aircraft was dispatched with the APU inoperable. On the morning of March 10, C-FONF departed Winnipeg on a round trip flight to Dryden, Thunder Bay and back as flight 1362/3. Since no external power unit was available at Dryden, the engines couldn't be restarted in case of engine shutdown on the ground. The flight to Thunder Bay was uneventful apart from a slight delay due to poor weather at Thunder Bay. As the aircraft was prepared for the return flight, it appeared that the aircraft was overweight as a result of ten additional passengers having transferred to the flight due to an earlier cancellation. The Air Ontario duty manager decided to off-load fuel and to arrange refuelling at Dryden. This caused an additional delay of 35 minutes. The Fokker F-28 departed Thunder Bay at 11:55 hours EST, about one hour behind schedule. The aircraft landed at Dryden at 11:39 hours CST. It began to snow lightly when the aircraft landed. Between 11:40 and 12:01, Air Ontario 1363 was refuelled with the right engine operating and with the passengers remaining on board the aircraft. This so called 'hot refuelling' procedure was followed because the APU was unserviceable. Eight passengers deplaned in Dryden and seven passengers boarded the aircraft. Meanwhile, snow was accumulating on the wings, forming a layer of 1/8-1/4 inch. No de-icing was done because de-icing with either engine running was prohibited by both Fokker and Air Ontario. The aircraft then taxied to runway 29 for departure, but was instructed to hold as there was a Cessna 150 on approach. The snow was continuing to fall heavily, becoming increasingly thick on the wings. At 12:09 the aircraft started it's takeoff roll on the slush-covered runway 29. There was an accumulation of at least one-half inch of wet, layered snow on the wings of the F-28 as it began its takeoff roll. After a longer than normal takeoff roll, the aircraft was rotated near taxiway Alpha, at approximately the 3500 foot mark. The aircraft lifted off slightly, began to shudder, and then settled back down onto the runway. The takeoff roll then continued and the aircraft was rotated a second time, finally lifting off at approximately the 5700 mark of the 6000 foot runway. It flew over the end of the runway approximately 15 feet above the ground. It thereafter failed to gain altitude and mushed through the air in a nose-high attitude, before commencing to strike trees. The aircraft crashed and came to rest in a wooded area, 3156 feet past the runway end and caught fire.

The twin engine aircraft was dispatched from Timmins to Chapleau on an ambulance flight, carrying two medical staffs and two pilots. A patient should be boarded in Chapleau and transferred to Sault Sainte Marie. Following an uneventful flight at FL120, the crew started a night descent to Chapleau. On a final NDB approach, the aircraft struck the ground and crashed 2,5 km southwest of the airport. The aircraft was destroyed and all four occupants were killed.

A Douglas DC-3C was destroyed when it crashed in Pikangikum Lake, ON, Canada. Both the pilot and the co-pilot were fatally injured in the accident. The airplane departed Red Lake Airport, ON (YRL) as Air Ontario flight 937 on a flight to Pikangikum Airport, ON (YPM). The main cargo load being carried consisted of a rubberized bladder tank containing 2,068 litres of fuel oil. Weather at the Pikangikum Airport was poor with drizzle, low clouds, and fog, with a visibility of one and one-half to two miles. The airplane was heard overflying the airport and turning over the Pikangikum Lake in preparation for a final approach and landing on runway 27. While over the water the airplane stalled and struck the ice-covered lake 180 feet south of a tree-covered island. It descended through the ice and struck the lake bottom at a depth of 8 to 12 feet. The ice thickness at the area of impact varied from one inch to three inches. Both pilots were killed.