Crash of a Beechcraft B90 King Air in Fort Simpson: 3 killed

Date & Time: Oct 16, 1988
Type of aircraft:
Operator:
Registration:
C-GDOM
Survivors:
No
MSN:
LJ-368
YOM:
1968
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On final approach to Fort Simpson Airport, the twin engine crashed 3 km short of runway, bursting into flames. All three occupants were killed.

Crash of a Noorduyn Norseman in Quebec

Date & Time: Oct 7, 1988
Type of aircraft:
Operator:
Registration:
C-FINL
Flight Phase:
Survivors:
Yes
MSN:
275
YOM:
1943
Location:
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances somewhere in Quebec. There were no casualties.

Crash of an Avro 748-2B-FAA in Cheney: 2 killed

Date & Time: Sep 15, 1988 at 1019 LT
Type of aircraft:
Operator:
Registration:
C-GFFA
Flight Type:
Survivors:
No
Schedule:
Montreal - Ottawa
MSN:
1789
YOM:
1981
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
A BAe-748 cargo plane was destroyed when it crashed while on approach to Ottawa International Airport, ON (YOW), Canada. Both pilots were killed. The airplane had arrived at Montreal-Dorval International Airport, QC (YUL) following a cargo flight from Dayton, OH, USA. All the cargo was unloaded in Montreal and the aircraft departed at 09:58 for Ottawa on an instrument flight rules (IFR) flight plan. The en route phase of the flight were uneventful. At about 10:19, while the aircraft was in level cruise flight at 3000 feet at approximately 200 knots indicated airspeed (KIAS), the flight data recorder (FDR) recorded a full-up deflection of the left aileron and a full-down deflection of the right aileron, and the aircraft began a roll to the left at a high rate. The right aileron remained at the fully-deflected position for a period of three seconds, and then, over the next seven seconds, the deflection gradually decreased by about five degrees. During the same 10-second period, the left aileron remained nearly fully deflected for the first eight seconds, then the deflection decreased by about five degrees during the next two seconds. By this time, the aircraft had rolled through approximately 460 degrees, and the aircraft nose had dropped 20 to 30 degrees below the horizon. At this point, the ailerons suddenly returned to about the neutral position and remained there for the last three seconds of the flight. The aircraft bank angle remained at approximately 90 degrees of left bank with a maximum vertical g of 4.7 recorded. The aircraft struck the ground at an airspeed of approximately 290 KIAS after a heading change of about 75 degrees left of the cruise heading. At impact, the aircraft bank angle was nearly 90 degrees left and the pitch angle was 41 degrees down. The time from the initial aileron deflection to ground impact was approximately 18 seconds.
Probable cause:
The Board determined that the aileron control system was asymmetrically rigged, making it susceptible to aerodynamic overbalance. The operator did not conduct the required post-maintenance flight tests of the aileron control response. When the ailerons were held at full deflection by aerodynamic forces, following a large control-wheel input by the pilot, the subsequent control reaction by the pilot was inappropriate. Contributing to the accident were the design of the aileron system; ambiguous and incomplete maintenance instructions; a lack of published information for flight crew concerning aileron system performance and possible emergencies; and the presence of factors which may have led to the development of flight crew fatigue.

Crash of a De Havilland DHC-2 Beaver in Ahmic Lake

Date & Time: Jul 3, 1988
Type of aircraft:
Operator:
Registration:
C-FPSM
Flight Type:
Survivors:
Yes
MSN:
1525TB1
YOM:
1963
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
6.00
Circumstances:
The pilot had successfully completed 10 or 12 landings in other parts of the large lake. He flew the aircraft to the southeast end of the lake and carried out a successful touch-and-go landing and initiated another circuit and approach to land in the same area. Following touchdown, the right outer wing struck the water, and the aircraft nosed over and began to sink. The pilot was able to escape from the aircraft before it submerged. The pilot held a valid Airline Transport Pilot Licence and was acquiring solo time in order to obtain a float endorsement. He had completed 6.1 hours of time on the aircraft, 3.1 of this solo time. The pilot had not reported any difficulty with the previous landings; prior to this touchdown, he had to adjust his approach slightly to the right of his intended landing path to avoid water traffic. The pilot reported that the wind was blowing from about 330° at 5 to 10 knots which would have resulted in a 20° crosswind from the right of his landing path. Weather observations taken at Muskoka Airport and North Bay Airport at about the time of the occurrence reported the wind direction and speed to be 280° true at 10 gusting to 15 knots and 240° at nine knots respectively. Ahmic Lake is equidistant from these two airports, that is about 35 miles from each. Using these reported winds, this would result in a crosswind component of between 30 and 70° from the left. Damage to the aircraft's right wing and float suggested that, on touchdown, the aircraft may have been drifting to the right, resulting in the right float ploughing into the water, followed by the right wing striking the surface of the lake. Careful examination of the damaged right float confirmed that there was no evidence of collision with a floating or submerged object. The float bow had been driven upwards and inwards, resulting in overload failures in the float structure ahead of the spreader strut attachments. This damage pattern is consistent with that which would result from hydrodynamic forces acting on the float structure at touchdown with the aircraft in in a slightly nose-down attitude and drifting to the right. Damage to the right wing was also due to water impact. All float attach brackets and struts had failed under overload conditions when the aircraft nosed over. The pilot had limited experience on float-equipped aircraft and may not have recognized drift or wind direction prior to touchdown. The lake was large enough for an into wind landing. No faults were found in the aircraft's control systems or float structure which would have contributed to the accident. The damage pattern indicated that the aircraft touched down in a slightly nose-down attitude, drifting to the right. Hydrodynamic forces acting on the right float following touchdown resulted in the right outer wing striking the water. The aircraft, as a result, nosed over and sank.
Source: www.dhc-2.com

Crash of a Bristol 170 Freighter 31M in Bronson Creek

Date & Time: Jun 21, 1988 at 0832 LT
Type of aircraft:
Operator:
Registration:
C-GYQY
Flight Type:
Survivors:
Yes
Schedule:
Wrangell - Bronson Creek
MSN:
13134
YOM:
1953
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After touchdown, the aircraft went out of control, veered off runway, lost its undercarriage and came to rest. All three crew members escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Grumman G-21A Goose off Rivers Inlet

Date & Time: May 12, 1988
Type of aircraft:
Operator:
Registration:
C-FAWH
Flight Phase:
Survivors:
Yes
MSN:
1083
YOM:
1940
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While taking off from the bay at Rivers Inlet, the seaplane was caught by strong winds, causing a wing to hit the water surface. The aircraft went out of control and came to rest. All seven occupants were uninjured while the aircraft was damaged beyond repair.
Probable cause:
Caught by strong winds during takeoff.

Crash of a Swearingen SA226AC Metro II off Hamilton: 2 killed

Date & Time: Feb 11, 1988 at 0332 LT
Type of aircraft:
Operator:
Registration:
C-GJDX
Flight Type:
Survivors:
No
Schedule:
Toronto - Hamilton
MSN:
TC-211EE
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew departed Toronto-Lester Bowles Pearson Airport on a short night cargo flight to Hamilton. While descending in good weather conditions, the airplane went out of control and crashed into Lake Ontario, few km off Hamilton. Both pilots were killed.

Crash of a Swearingen SA226AT Merlin IV in Hamilton

Date & Time: Jan 12, 1988
Operator:
Registration:
C-GJWW
Survivors:
Yes
MSN:
AT-013
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For unknown reasons, the aircraft completed a gear up landing at Hamilton-Civic Airport. All three occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Britten-Norman BN-2A-6 Islander on Mt Waddington: 4 killed

Date & Time: Dec 4, 1987
Type of aircraft:
Operator:
Registration:
C-GOMC
Flight Phase:
Survivors:
No
Site:
Schedule:
Bella Coola – Campbell River
MSN:
10
YOM:
1967
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The twin engine aircraft departed Bella Coola on a scheduled service to Campbell River but failed to arrive at destination. SAR operations were initiated but eventually abandoned after few days as no trace of the aircraft nor the four occupants was found. The wreckage was never localized but it is believed the aircraft may have crashed in the Mt Waddington (4,016 meters high) area.

Crash of a De Havilland DHC-4A Caribou in Ross River: 2 killed

Date & Time: Nov 10, 1987 at 1713 LT
Type of aircraft:
Operator:
Registration:
C-GVYX
Flight Type:
Survivors:
Yes
Schedule:
Fort Nelson - Ross River
MSN:
292
YOM:
1970
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Aircraft flight hours:
11185
Circumstances:
The DHC-4A Caribou aircraft was en route from Calgary to Ross River where it was to be used to transport silver ore concentrate from the mines at Plata to Ross River. On board were two pilots, two company aircraft maintenance engineers to service the aircraft, and about 5,500 pounds of aircraft parts and equipment to support the operation of the aircraft in Ross River. One refuelling stop was made at Fort Nelson, after which the aircraft proceeded on an IFR flight plan to its destination. Ross River has no published instrument approach and is situated in a valley in mountainous terrain. It was necessary to overfly Ross River, proceed 30 miles to the northwest and complete an NDB approach at Faro where the minimum circling altitude is 2,709 feet agl. When below cloud at Faro, the aircraft must then proceed visually up the river valley to Ross River. The Caribou arrived over Faro at approximately 16:15, and an attempt was made to descend below the cloud base which was reported to be 400 to 600 feet agl. When visual reference with the ground was not made, the pilot climbed out to the southeast and informed Faro Community Airport Radio Station (CARS) that he was proceeding to his alternate, Watson Lake. In cruise flight the no. 2 engine began to lose oil, causing the oil pressure to drop to zero. The right engine was then shut down, and the propeller was feathered. A little later, the aircraft was heard flying out to the southeast for an approach to runway 26 at the Ross River Airport. On approach the landing gear had to be recycled because the nose gear did not lock down during the first attempt to lower the gear. The plane was no longer in a position to land, so the captain initiated a go-around. The aircraft passed by the town and then began to lose altitude, descending gradually into the trees. Portions of the right wing were torn off on contact with the trees, and the plane rolled to the right and nosed into the ground. The aircraft then cartwheeled over the embankment and down onto the river shore 20 feet below.
Probable cause:
The Canadian Aviation Safety Board determined that a lack of communication at the company's maintenance facility led to the dispatch of the aircraft with an unsuitable gasket in the right engine, and the subsequent loss of engine oil. A single-engine go-around was attempted when the combination of single-engine performance, a low cloud base, and high terrain surrounding a confined operating area made a successful overshoot uncertain. The flaps were fully retracted before the minimum speed for single-engine flight in the zero flap configuration was achieved.