British Columbia

At about 1826 mountain standard time (MST), the aircraft, with the pilot and four passengers on board, departed the Calgary International Airport, Alberta, on a night instrument flight rules (IFR) flight to Hillsboro, Oregon, USA. At about 1946 the aircraft disappeared from the Vancouver Area Control Centre (ACC) radar screen in the vicinity of Castlegar, British Columbia. The Victoria Rescue Coordination Centre (RCC) was notified, and search aircraft were dispatched. Despite bi-national search cooperation and radar fixes of the aircraft's last known position (LKP), a seven-day search failed to locate the missing aircraft. An emergency locator transmitter (ELT) signal was not received. On 14 June 1996, the wreckage was located at latitude 49°14'48"N, longitude 117°03'20"W, at an elevation of approximately 6,700 feet above sea level (asl). The aircraft was destroyed by impact forces and a post-crash fire. The pilot and four passengers were fatally injured.

The Navair Charter Piper PA-31, flight FCV705, a mail courier with a crew of two, was on a night, instrument flight rules (IFR) flight plan from Williams Lake, British Columbia, to Kamloops. While the crew was conducting an instrument procedure to the Kamloops airport, they flew into an area that was clear of cloud. The captain cancelled his IFR flight plan and descended for a visual flight rules (VFR) approach to the airport. At 1902 PST, the aircraft collided with trees at an elevation of 2,400 feet above sea level (asl), seven nautical miles (nm) east-southeast of the Kamloops airport. The captain was fatally injured on impact, and the first officer was seriously injured; the aircraft was destroyed during the crash and post-crash fire.

The single engine aircraft was on a delivery flight from Campbell River to the seaplane base of Seal Cove in Prince Rupert. En route, in unclear circumstances, the aircraft crashed near Captain Cove, about 50 km southeast of Prince Rupert. Both passengers Mark Jonathan Cholomondeley and Ferlie Bating were killed while the pilot Spike Nasmyth survived.

The single-engine turbine Otter on amphibious floats departed Triumph Bay, British Columbia, at 1634 Pacific daylight saving time (PDT) with one pilot and nine passengers on board for a visual flight rules (VFR) flight to Campbell River. At 19:01:59 the pilot called Campbell River Flight Service Station (FSS) and reported that he was seven nautical miles (nm) northwest of the airport, inbound for Campbell River. Radar data from Comox indicate that, when this call was made, the aircraft was actually 11 nm northwest of Campbell River, just south of the Narrows (see map, Appendix A). At 19:02:40, the pilot was given the 1900 PDT Campbell River weather observation, which was as follows: ceiling 300 feet overcast and visibility two miles in light rain and fog. The pilot requested a special VFR (SVFR) clearance to enter the Campbell River control zone. Clearance for SVFR was delayed by Comox air traffic control (ATC) until an instrument flight rules (IFR) aircraft on approach to Campbell River had landed. At 19:03:54, the IFR aircraft reported breaking clouds at 900 feet above sea level (asl), which would be approximately 550 feet above ground level, on the ILS approach to runway 11 at Campbell River (airport elevation is 346 feet). This information was acknowledged by the turbine Otter pilot. The IFR aircraft landed at 1904, and the turbine Otter was issued an SVFR clearance at 19:04:45. Radar data indicate that, at that time, the aircraft was about one mile northwest of Tyee Spit, a frequently used, alternate landing site (water) for company aircraft when weather conditions preclude landing at Campbell River airport. Radar data indicate that, at 1906, after passing by Tyee Spit, the aircraft turned southbound and flew directly toward the airport. At about 2 1/2 miles from the airport, at 19:07:40, the aircraft turned right to a heading of approximately 310/ magnetic and flew in that general direction for about two minutes. The aircraft was on a track that was approximately parallel to the extended runway centre line, tracking outbound from the airport with the localizer and the Campbell River (YBL) non-directional beacon (NDB) to the left. The aircraft passed abeam the YBL NDB, which serves as the final approach fix (FAF) for the ILS approach to runway 11, and continued outbound. At 19:09:40, at about three miles outside the beacon, the aircraft turned left to a southerly heading toward the localizer and the YBL NDB. At 19:10:08, the pilot radioed that he was seven miles northwest; this was the last transmission received from the aircraft. At 19:10:25, radar contact was lost. The aircraft crashed into the northwest side of a 1,047-foot mountain at about the 860-foot level, in straight-and-level flight on a heading of 183/ magnetic. The pilot and seven of the passengers received fatal injuries. The two remaining passengers received serious injuries. The accident occurred at 1910 PDT during the hours of official daylight, at latitude 50/01'N, longitude 125/22'W. Official sunset in Campbell River was at 1908, and night was at 1940 PDT.

The DC-3 aircraft, with the captain, first officer, and an apprentice aircraft maintenance engineer on board, was to be ferried from Vancouver, British Columbia, to Whitehorse, Yukon. Just after take-off from runway 08, as the first officer was setting the engine power, the right propeller began to over-speed. The captain told the first officer to shut down and feather the right engine. The first officer did as instructed, and advised the Vancouver tower controller of the engine problem and that they would return to the airport to land on runway 08. The captain turned the aircraft to the right, onto downwind for runway 08; however, because the aircraft's altitude and airspeed were decreasing, the first officer advised the tower controller that they would land on runway 30. The aircraft continued to lose height, narrowly avoiding buildings in its path, and crashed to the ground, one mile short of runway 30. The three occupants were seriously injured during the impact and the post-crash fire; the captain died of his injuries eight days after the accident.

On 11 January 1995, at 0035 Pacific standard time (PST), the twin-engine Learjet 35 departed Vancouver International Airport, British Columbia, on a night, instrument flight rules (IFR), medical evacuation (MEDEVAC) flight to the Masset aerodrome, on the northern end of the Queen Charlotte Islands. On board the Learjet were a flight crew of two pilots, and a medical team consisting of two attendants and a doctor. Their mission was to evacuate a patient from Masset and deliver her to Prince Rupert for treatment; the aircraft was then to return to Vancouver. The flight-planned route was at flight level (FL) 390, direct to Sandspit then direct to Masset. Following routine communications with Air Traffic Services (ATS), at about 0144, the aircraft reported "outbound" from the Masset non-directional beacon (NDB) on the published NDB "A" instrument approach procedure to runway 12. Air Traffic Control (ATC) radar, situated near Sandspit, tracked the aircraft as it flew the approach. Radar data shows that the aircraft began a descent about 10 seconds after it had completed the procedure turn and was established on the final inbound approach track. Forty-three seconds later, at a point 8.8 nautical miles (nm) from the threshold of runway 12 and on the final, inbound track, the aircraft disappeared from radar. Department of National Defence (DND) Search and Rescue (SAR) aircraft began searching the area shortly after the aircraft was declared missing, and were later assisted by other private and military aircraft and vessels. On the second day of the search, flotsam from the aircraft was found in the area. Extensive underwater searching using sonar and underwater cameras found the aircraft wreckage on 31 January 1995, in 260 feet of water, near the last known position. The aircraft had been destroyed. The bodies of two occupants were found several days after the accident, but the other three occupants have not been found and are presumed to have been fatally injured. The accident occurred at latitude 54/08NN and longitude 131/58NW, at about 0149 PST, during the hours of darkness in unknown weather conditions.

The captain, first officer, and two passengers departed from the Fish Egg Inlet logging camp, located 56 nautical miles (nm) north of Port Hardy, British Columbia, for a 16 nm visual flight rules (VFR) flight to Pruth Bay. This was the second leg of a flight which had originated at Port Hardy. The first officer, who occupied the left pilot seat and was handling the controls, taxied the aircraft a short distance away from the dock and took off. The captain occupied the right pilot seat. As the aircraft climbed through 100 feet, and just as the flaps were retracting, the aircraft pitched up violently and stalled. The pilots were unable to regain control of the aircraft, and it crashed into the water about 100 feet from the shore and sank immediately. The captain, who sustained serious injuries from the crash, escaped from the wreckage and swam to shore. The first officer and the two passengers remained in the aircraft and drowned. When the aircraft failed to arrive at Pruth Bay, personnel from Pacific Coastal Airlines (the company) notified the Rescue Coordination Centre and started their own search. A search pilot spotted debris in the water near the logging camp at about 1430 Pacific daylight saving time (PDT) that day. He landed to investigate, found the captain on the shore nearby, and transported him to the Port Hardy hospital. The accident occurred during daylight hours at approximately 1148 PDT, at latitude 51°36'N and longitude 127°41'W. There were no witnesses, other than the aircraft captain, to this accident.

The pilot, sole on board, was engaged in a fire fighting mission in the region of Quesnel. While cruising at an altitude of 6,500 feet, the pilot realized that the oil pressure on the left engine dropped while oil was leaking. He decided to shut down the left engine but mistakenly activated the fire extinguishing system on the right engine, causing the right engine to stop as well. In such conditions, he reduced his altitude and attempted to ditch the aircraft in the Fraser River near Quesnel. The aircraft was damaged beyond repair and the pilot was slightly injured.

The amphibious DHC-2 Beaver was being operated from the Harbour Air base at Sandspit, British Columbia, located on the Queen Charlotte Islands. On the first flight on the day of the accident, the aircraft carried baggage from the Sandspit Airport to a floating fishing resort at anchor in Givenchy Bay. This bay is located in the Kano Inlet on the west coast of the Queen Charlotte Islands, 28 nautical miles (nm) west of Sandspit. On board the aircraft with the pilot was a passenger who would remain with the flight for the return trip to Sandspit. The aircraft departed Sandspit under visual flight rules (VFR) at 1015 Pacific daylight time (PDT) and landed at the fishing resort at 1039. The pilot had taken the most direct route to the destination through a low pass and over Yakoun Lake. He advised the company dispatch on the company radio frequency that the weather was quite poor along that route and that he planned to take the Skidegate Channel for the return trip. On arrival at the Givenchy resort, the aircraft was loaded with the fish to be transported to Sandspit; it then departed Givenchy at 1051. When the aircraft did not arrive at Sandspit, a search was organized. The wreckage was located at 1245 at Hunter Point, about 7 nm from Givenchy, at latitude 53°15'N, longitude 132°42'W. The accident had occurred during the hours of daylight at approximately 1100. The aircraft was destroyed and the pilot and passenger were fatally injured upon impact.

The Grumman G21A Goose (C-FUMG) departed from the Seal Cove floatplane base at Prince Rupert, British Columbia, on a charter flight to Kincolith. The aircraft carried one pilot, four passengers, and approximately 600 pounds of baggage and freight. This was the first flight of the day for the occurrence aircraft. Prior to take-off, the pilot contacted the Prince Rupert Flight Service Station (FSS)1 by radio and obtained local traffic and weather information. The aircraft took off from the water at approximately 1141 Pacific standard time (PST)2, and proceeded southbound, following the normal departure path. During the take-off and climb, one or both of the aircraft's engines did not sound as if they were operating normally. Shortly after take-off, the pilot radioed the company dispatcher at Seal Cove and reported that he was experiencing engine problems, and that he was returning to Seal Cove and would require assistance at the ramp. After the left propeller stopped rotating, the aircraft rolled to the left and descended steeply to the ground. The aircraft crashed into trees on a hillside, at an altitude of approximately 150 feet, approximately three nautical miles (nm)3 south of Seal Cove. The pilot and one passenger were fatally injured; the three other passengers received serious injuries. A search started approximately 45 minutes after the aircraft departed. The aircraft was discovered by a Coast Guard helicopter, which was able to rescue the survivors. The accident occurred during daylight hours at about 1145 PST, at latitude 54·17'N and longitude 134·14'W.