Crash of a De Havilland DHC-2 Beaver near Cassiar: 1 killed

Date & Time: Sep 22, 1996 at 2024 LT
Type of aircraft:
Operator:
Registration:
C-FIBP
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Watson Lake - Desolation Lake
MSN:
787
YOM:
1955
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot, sole on board, was completing a positioning flight from Watson Lake to Desolation Lake. While cruising at an altitude of 5,000 feet, the single engine aircraft struck trees and crashed in a wooded area located in hilly terrain, about 114 km southwest from Watson Lake. The wreckage was found a day later and the pilot was killed.

Crash of a De Havilland DHC-3 Otter near Alliford Bay: 3 killed

Date & Time: Aug 18, 1996 at 1950 LT
Type of aircraft:
Operator:
Registration:
C-GCMY
Flight Phase:
Survivors:
No
Site:
Schedule:
Tasu - Alliford Bay
MSN:
22
YOM:
1953
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The float-equipped, turbine-engine, DHC-3 Otter departed from Tasu, British Columbia, at about 1940 Pacific daylight saving time (PDT), with the pilot and two passengers on board, on a charter, visual flight rules (VFR) flight to Alliford Bay, 26 nautical miles to the north. When the aircraft did not arrive at destination, the operator initiated a search. The aircraft wreckage was located the following day, 18 nautical miles (nm) south of Alliford Bay, in rugged terrain at an elevation of 1,700 feet above sea level (asl). The aircraft was destroyed, and there were no survivors.
Probable cause:
The pilot probably made a navigational error because of restricted visibility in fog and light drizzle and entered the wrong valley, and he delayed his decision to reverse course until he was unable to avoid the weather.
Final Report:

Crash of a Douglas C-54A-15-DC Skymaster near Bronson Creek: 1 killed

Date & Time: Aug 14, 1996 at 1200 LT
Type of aircraft:
Operator:
Registration:
C-FGNI
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bronson Creek - Whitehorse - Wrangell
MSN:
10389
YOM:
1944
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
12500
Captain / Total hours on type:
1500.00
Copilot / Total flying hours:
2900
Copilot / Total hours on type:
420
Aircraft flight hours:
50754
Circumstances:
The DC-4 aircraft (serial number 10389) was on a visual flight rules flight from Bronson Creek, British Columbia, to Wrangell, Alaska, with a crew of three and about 16,600 pounds of cargo on board. The departure from the remote mining strip was uneventful until the aircraft approached 1,500 feet above sea level, when the crew heard a whining noise in their headsets. Believing that the whining was caused by an inverter problem, they switched inverters, but the problem persisted. Electrical instrument indications in the cockpit then became erratic, and the number 2 engine, on the left wing, began to misfire; its fire warning light in the cockpit illuminated briefly, but without the accompanying bell. The captain confirmed visually that the number 2 engine was on fire and the crew carried out the engine fire drill; however, the fire did not extinguish. The captain commenced a right-hand turn to return to the Bronson Creek airstrip, and announced to the crew that the number 2 engine had separated from the wing. The captain applied maximum power to the three remaining engines; however, the aircraft began to lose altitude. Both pilots held the rudder and aileron controls at full right deflection in an attempt to prevent the aircraft from yawing or rolling to the left. The aircraft was shaking violently at that time, and the crew members were unable to read any of the engine or flight instruments. At about 50 feet above ground level, just short of the Iskut River, the pilots closed the throttles. The aircraft descended rapidly, and the burning left wing struck a tree just as the fuselage contacted the surface of the river. The three occupants escaped the burning aircraft, and the first officer and load master swam to safety. The captain is missing and is presumed to have drowned. The aircraft was destroyed.
Probable cause:
The n°2 engine separated from the aircraft as a result of an intense fire in the wing. The loss of the engine rendered the aircraft uncontrollable, and the pilots were forced to land in the river
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 in Markham Bay: 2 killed

Date & Time: Aug 12, 1996 at 1347 LT
Operator:
Registration:
C-GNDN
Flight Type:
Survivors:
No
Schedule:
Iqaluit - Markham Bay - Lake Harbour
MSN:
427
YOM:
1974
Flight number:
7F064
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3813
Captain / Total hours on type:
2028.00
Copilot / Total flying hours:
2724
Copilot / Total hours on type:
1000
Circumstances:
First Air 064, a DHC-6 Twin Otter (Serial No. 427), took off from Iqaluit, Northwest Territories (NWT), at 1258 Coordinated Universal Time (UTC) on a charter flight to Markham Bay, Lake Harbour, and back to Iqaluit. The aircraft was carrying six barrels of Jet B fuel to be delivered to Markham Bay, an off-strip landing site. At 1300, just after he took off, the captain told the Iqaluit Flight Service Station (FSS) specialist that the estimated time of arrival (ETA) for Markham Bay would be 1335. At approximately 1345, the crew informed First Air dispatch that they were landing at Markham Bay. After touching down, the pilot attempted an overshoot. During the attempt, the aircraft struck the ground about 200 metres past the end of the landing area, got airborne again, cleared a ridge, then crashed onto a rocky beach. A helicopter located the airplane 629 metres from the beginning of the landing area, partially submerged in water. The two pilots, the only occupants, received fatal injuries in the crash.
Probable cause:
For unknown reasons, a decision was made to overshoot even though insufficient runway remained for acceleration, take-off, and climb. Likely contributing directly to the decision to overshoot was the difficulty in controlling the aircraft on touchdown.
Final Report:

Crash of a Beechcraft D18S near Sioux Lookout

Date & Time: Jul 6, 1996
Type of aircraft:
Operator:
Registration:
C-FBGO
Flight Phase:
Survivors:
Yes
Schedule:
Fort Frances – Granite Lake
MSN:
A-865
YOM:
1952
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Fort Frances, Ontario, with the pilot and four passengers on a visual flight rules (VFR) flight to Granite Lake. The weather was overcast with good visibility on departure. However, about one-half of the way to Granite Lake, just north of Ignace, the pilot encountered an area of increasing rain and decreasing visibility. The pilot made several course deviations to find a route through the poor weather, but eventually could find neither a way out of the poor weather nor a lake with suitable conditions for landing. While manoeuvring at low level and with heavy rain obscuring the horizon, the pilot reported that the engines lost partial power because of carburettor icing. The pilot applied carburettor heat but was unable to restore engine power or sustain aircraft altitude. The pilot attempted to keep the aircraft level, and in a matter of seconds, the aircraft descended into the trees. The aircraft travelled approximately 500 feet through the trees; the left wing was torn off and a fuel-fed fire broke out almost immediately. All occupants survived the crash with minor injuries and exited the aircraft. The passenger occupying the copilot seat received burns to his upper body. The crash site was overflown about 15 minutes later by a second company pilot who transmitted a Mayday. The occupants were picked up by helicopter about one hour later
Probable cause:
The pilot continued the flight into adverse weather at low level and force-landed the aircraft into trees when the engines experienced a partial power loss that was probably caused by carburettor icing.
Final Report:

Crash of a Swearingen SA26T Merlin IIA in Whale Cove

Date & Time: Jun 20, 1996 at 1905 LT
Type of aircraft:
Operator:
Registration:
C-GTHN
Flight Type:
Survivors:
Yes
MSN:
T26-016
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Whale Cove Airport, the aircraft deviated to the left after a course of about 1,600 feet. It veered off runway, lost its undercarriage and came to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The aircraft deviated from the runway centerline after landing due to strong crosswinds gusting up to 31 knots. The certification limit for the aircraft in such conditions was 22 knots.

Crash of a De Havilland DHC-3 Otter near Cochenour

Date & Time: Jun 16, 1996 at 1914 LT
Type of aircraft:
Registration:
C-FMEL
Flight Phase:
Survivors:
Yes
Schedule:
Cochenour - Thunder Bay
MSN:
222
YOM:
1957
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The float-equipped DHC-3 (Otter), carrying the pilot and six passengers, departed the company's water base at Cochenour, Ontario, on a charter flight to Sandy Beach Lodge, located on Trout Lake approximately 25 miles to the east. The pilot levelled the aircraft and configured it for cruise flight at approximately 2,500 feet above sea level (asl). Shortly after level-off, the pilot heard a popping sound and noted a slight loss of engine power, and wisps of whitish-grey smoke entered the cabin. The aircraft instruments indicated normal engine operation, and the fire warning system did not activate. The pilot suspected that the engine had suffered a cylinder failure and turned to return to Cochenour. A passenger seated in the right front crew seat reported flames near the floor at the front, right corner of the cockpit. The pilot radioed the Thunder Bay Flight Service Station to advise of the emergency, had the passenger vacate the crew seat, and attempted to suppress the fire with a hand-held extinguisher. Thick, black smoke billowed into the cabin, restricting visibility and causing respiratory distress for all of the occupants. The pilot opened the left crew door in order to see ahead and landed the aircraft, still on fire, on McNeely Bay, the first available landing site. The aircraft landed hard but remained upright on the floats. The occupants left by the main door, with their life jackets, and were picked up almost immediately by nearby boats. The aircraft was consumed by fire within minutes after landing. The pilot suffered second degree burns to his face and right forearm, and the passenger in the right crew seat suffered burns to his right leg. The remaining five passengers escaped serious injury.
Probable cause:
Continued operation of the engine following an exhaust valve failure on the n°2 cylinder resulted in a flaming gas path near the right side of the firewall, an exhaust system overheat, and a subsequent cabin fire.
Final Report:

Crash of a Piper PA-31-325 Navajo C/R near Kangiqsujuaq: 4 killed

Date & Time: May 30, 1996 at 0804 LT
Type of aircraft:
Registration:
C-GRPM
Flight Phase:
Survivors:
No
Site:
Schedule:
Kangiqsujuaq – Kuujjuaq
MSN:
31-8012021
YOM:
1980
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The Piper Navajo PA-31 (serial number 318012021), belonging to Les transports Aéro 2000 Inc., with three passengers and one pilot on board, was on a charter visual flight rules (VFR) flight from Kangiqsujuaq, Quebec, to Kuujjuaq, Quebec. At 1056 eastern daylight saving time (EDT), the pilot contacted the Kuujjuaq flight service station (FSS) by radio and reported that he had taken off eight minutes earlier and planned to overfly the Nouveau-Québec crater. That was the last message received from the pilot. When the aircraft failed to arrive at destination at the expected time, a search was initiated. The next day, a ground search team found the aircraft. The Navajo struck the eastern slope of the Nouveau-Québec crater while in straight and level flight. The four occupants of the aircraft were fatally injured in the accident.
Probable cause:
The pilot continued flight in adverse weather and may have lost situational awareness due to incorrect information provided by the GPS. The pilot evidently did not have the visual references required to avoid striking the eastern slope of the Nouveau-Québec crater.
Final Report:

Crash of a De Havilland DHC-3 Otter near Terrace: 2 killed

Date & Time: May 9, 1996 at 1430 LT
Type of aircraft:
Registration:
C-GDOB
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Ketchikan – Prince Rupert – Dawson Creek – Buffalo Narrows
MSN:
194
YOM:
1957
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
10000
Copilot / Total flying hours:
5000
Circumstances:
The single-engine, float-equipped DHC-3 Otter departed Ketchikan, Alaska, at 0905 Pacific daylight time (PDT) on 09 May 1996 with a pilot and co-pilot on board. They were on a visual flight rules (VFR) ferry flight to Dawson Creek, British Columbia, en route to Buffalo Narrows, Saskatchewan. After a refuelling stop and weather briefing at Prince Rupert, British Columbia, the aircraft departed eastbound along the published Telkwa Pass VFR route. When the aircraft did not arrive at Dawson Creek, it was reported overdue. The next day, an extensive search for the missing Otter was commenced and wreckage was located by search and rescue aircraft at 1930 PDT, 30 miles east of Terrace, in the Telkwa Pass. The aircraft had struck mountainous terrain and was destroyed. Both occupants were fatally injured.
Probable cause:
The absence of aircraft wreckage and documentation precludes an analysis of the technical aspects of this accident. This analysis, therefore, concentrates solely on the operational aspects. The high impact speed is indicative of either a loss of control followed by a rapid descent into terrain or controlled flight into unseen terrain. Given that the pilot reported encountering snow showers within 15 miles of the accident site, it is possible that the weather continued to deteriorate and may have adversely affected the pilot's ability to maintain visual contact with the terrain.
Findings:
1. The weight and centre of gravity of the aircraft at the last take-off were estimated to have been within the prescribed limits.
2. The pilot was certified, trained, and qualified for the flight in accordance with existing regulations.
3. Marginal visual weather conditions existed in the vicinity of the accident site.
4. It is possible that deteriorating weather affected the pilot's ability to maintain visual contact with the terrain.
Causes and Contributing Factors:
It was not determined why the aircraft struck terrain; however, it is likely that the contact occurred during conditions of reduced visibility.
Final Report:

Crash of a Douglas DC-3C in Kenty Lake

Date & Time: May 5, 1996 at 1400 LT
Type of aircraft:
Operator:
Registration:
C-GCZG
Flight Type:
Survivors:
Yes
MSN:
17118/34385
YOM:
1945
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing on the icy Kenty Lake, the right ski struck a snowbank, causing the gear to collapse. All three occupants were evacuated safely while the aircraft was damaged beyond repair.