Crash of a De Havilland DHC-2 Beaver near Golden

Date & Time: Oct 1, 1986
Type of aircraft:
Operator:
Registration:
C-FJOQ
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
1070
YOM:
1957
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, under the supervision of his employer/instructor, had set out to practise solo take-offs and landings in order to qualify for a float endorsement. During a take-off attempt from the river, the aircraft porpoised, cleared the water momentarily with the left and then the right float, swerved left, and struck the river bank in a level attitude. The aircraft then rolled and came to rest, partially submerged, on its left side. A fire started in the engine compartment but lasted for a short time only. The seriously injured pilot was rescued by the aircraft owner who swam across the river.
Probable cause:
The pilot, although experienced in the operation of wheel-equipped aircraft, had limited experience with aircraft on floats. His solo flying experience on float-equipped aircraft was less than one hour and was from the same location the day before the accident. The river flowed at about five knots in the direction of take-off. The water level of the river was low, and, as a result, sand bars were both above and just below the water surface. Because of these conditions, the average usable width of the river for take-offs and landings was less than 100 feet. The river had one prominent bend in the area where the aircraft commenced its take-off and another just downstream of the occurrence site. The riverbank on the left, in the direction of take-off, had tall trees up to the water's edge. The pilot suffered injuries during the crash; the lap belt had a Sliding friction-type buckle that loosened during the crash, and there was no shoulder harness installed in the aircraft. It is probable that the pilot's injuries would have been less serious if he had had a better restraint system. Although the pilot had successfully taken off and landed on the river the day before the accident, the conditions of that area were unsuitable for his limited float-flying experience. When the pilot could not establish directional control during the take-off, a prudent decision would have been to reject, rather than to continue. The supervising pilot should have realized that the conditions of the river were not suitable as a practice area for any pilot, particularly for a pilot whose float-flying experience was limited.

Crash of a De Havilland DHC-2 Beaver in Dease Lake: 5 killed

Date & Time: Sep 27, 1986 at 1735 LT
Type of aircraft:
Operator:
Registration:
C-GAEE
Survivors:
Yes
Schedule:
Atlin - Dease Lake
MSN:
724
YOM:
1954
Flight number:
2653
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The pilot and five passengers boarded the float-equipped Beaver aircraft in Atlin, BC, and departed on a visual flight rules (VFR) flight to Dease Lake at 1618 Pacific daylight time (PDT). The flight arrived over Dease Lake at 1735 and proceeded northward over the lake's east shore. Approximately one and one-half miles from the south end of the lake, the aircraft turned to the south to descend for a landing in the middle of the lake. The aircraft was in a fairly steep constant descent when it struck the water. It then nosed over and came to rest with only the bottom of the fuselage visible. The fuselage floated for about 10 minutes, then sank in 120 feet of water. The landing area was approximately one mile from the south end of the lake. The pilot escaped with serious injuries. The five passengers did not exit the aircraft and drowned.
Probable cause:
The cause of the accident is that the pilot did not recognize the glassy-water conditions and did not use the glassy-water landing technique. The following findings were reported:
- Glassy-water conditions prevailed at the time of the landing.
- The aircraft struck the water at a high rate of descent, in a nose-down attitude.
- The passenger pre-flight briefing/card did not adequately prepare passengers to deal with emergency water evacuation.
- The pilot was certified and qualified for the flight in accordance with existing regulations.
- The aircraft was certified, equipped, and maintained in accordance with existing regulations and approved procedures.
- There was no evidence found of any airframe failure or system malfunction prior to or during the flight.
- The weight and centre of gravity were within the prescribed limits.

Crash of a De Havilland DHC-2 Beaver in Tow Hill: 1 killed

Date & Time: Sep 1, 1986
Type of aircraft:
Operator:
Registration:
C-FOMI
Flight Phase:
Survivors:
Yes
Schedule:
Masset - Prince Rupert
MSN:
1204
YOM:
1958
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
En route from Masset to Prince Rupert, the pilot encountered low ceiling. While cruising at a very low altitude, the aircraft struck tree tops and crashed in a wooded area located about 25 km east of Masset. A passenger was killed while three other occupants were injured.
Probable cause:
The pilot was flying under VFR mode in IMC conditions. At the time of the accident, visibility was below minimums.

Crash of a De Havilland DHC-2 Beaver in Border Beacon

Date & Time: Jan 10, 1986
Type of aircraft:
Registration:
C-GUBD
Flight Phase:
Survivors:
Yes
MSN:
747
YOM:
1954
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances. There were no casualties.

Crash of a De Havilland DHC-2 Beaver in Wollaston Lake: 4 killed

Date & Time: Jan 8, 1986 at 1300 LT
Type of aircraft:
Operator:
Registration:
C-FMPQ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wollaston Lake - La Ronge
MSN:
1604
YOM:
1965
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
5500
Captain / Total hours on type:
500.00
Circumstances:
The aircraft departed the Welcome Bay ice strip at Wollaston Lake, Saskatchewan. This was the second leg of a flight that originated at La Ronge, Saskatchewan. On board were two Royal Canadian Mounted Police (RCMP) pilots, another member of the force, and an inspector from the Saskatchewan Department of Public Works. Witnesses stated that the aircraft took off normally, levelled momentarily, then climbed steeply into cloud Moments later, they heard the engine noise increase abruptly, then decrease rapidly, followed by a sound similar to a backfire. When the aircraft reappeared, it was in a steep, nose down, right-wing-low attitude. It crashed on the ice, one mile north of Welcome Bay; all four occupants sustained fatal injuries.
Probable cause:
The following findings were reported:
- Aircraft control was lost for undetermined reasons.
- The pilot departed Wollaston Lake into known icing conditions in an aircraft that was not certified for flight into such conditions.
- There was no evidence of any airframe failure or system malfunction prior to or during the flight.
- The flight crew was certified and qualified for the flight in accordance with existing regulations.
- The aircraft was certified, equipped, and maintained in accordance with existing regulations and approved procedures.
- The aircraft's weight and centre of gravity were within the prescribed limits.

Crash of a De Havilland DHC-2 Beaver in Merrill Pass: 3 killed

Date & Time: Sep 26, 1985 at 1230 LT
Type of aircraft:
Operator:
Registration:
N5317G
Flight Phase:
Survivors:
No
Site:
Schedule:
Hidden River - Willow
MSN:
617
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4900
Captain / Total hours on type:
1200.00
Aircraft flight hours:
7640
Circumstances:
The aircraft collided with terrain in a mountain pass at an elevation of 3,600 feet msl. The pilot obtained a weather briefing at 1329 gmt on 9/26/85 at which time Merrill Pass was forecast to be closed by 1100 adt due to deteriorating weather. The last radio communication with the aircraft was at 1803 gmt when contact was made with McGrath FSS. At this time the pilot made a pilot report stating the weather at Merrill Pass was marginal; 2 miles visibility with snow and occasional moderate turbulence. The wreckage was located on 9/29/85 and indicated the aircraft contacted the terrain in a relatively level attitude with considerable airspeed. All three occupants were killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. (c) in-flight planning/decision - improper - pilot in command
2. (f) improper use of procedure - pilot in command
3. (c) flight into known adverse weather - continued - pilot in command
4. (f) weather condition - turbulence
5. (f) weather condition - snow
6. (f) weather condition - obscuration
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: maneuvering
Findings
7. (c) terrain condition - mountainous/hilly
8. (c) altitude - not maintained - pilot in command
Final Report:

Crash of a De Havilland DHC-2 Beaver near Tutna Lake: 4 killed

Date & Time: Aug 18, 1985 at 1403 LT
Type of aircraft:
Registration:
N68085
Survivors:
No
Site:
Schedule:
Anchorage - Tutna Lake
MSN:
1332
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4190
Captain / Total hours on type:
406.00
Aircraft flight hours:
9018
Circumstances:
The aircraft crashed on the side of a mountain at an elevation of 2,200 feet approximately 3 miles from its intended destination, a remote lake. Purpose of the flight was to discharge caribou hunters into an area where caribou were spotted early that day. The aircraft was destroyed by fire. Inspection of the wreckage failed to reveal a mechanical failure/malfunction. All four occupants were killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: maneuvering
Findings
1. (f) terrain condition - mountainous/hilly
2. (c) in-flight planning/decision - poor - pilot in command
3. (c) proper altitude - not maintained - pilot in command
Final Report:

Crash of a De Havilland DHC-2 Beaver near Barham

Date & Time: Nov 10, 1984 at 0930 LT
Type of aircraft:
Operator:
Registration:
VH-IDH
Flight Phase:
Survivors:
Yes
Schedule:
Barham - Barham
MSN:
1534
YOM:
1963
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
At a height of approximately 50 feet after take-off the engine suddenly lost all power. The pilot was able to glide the aircraft over several drainage banks, two fences and an irrigation canal but a high rate of descent developed and the aircraft landed heavily and overturned. Fire broke out and the central section of the fuselage was burnt out. The pilot, sole on board, was slightly injured.
Probable cause:
The investigation was hampered by the extent of fire damage and the cause of the loss of engine power was not positively established.
Final Report:

Crash of a De Havilland DHC-2 Beaver in Jamie Lake: 1 kiled

Date & Time: Aug 14, 1984
Type of aircraft:
Registration:
C-FEYZ
Flight Phase:
Survivors:
Yes
MSN:
556
YOM:
1953
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
14000
Circumstances:
Shortly after takeoff from Jamie Lake near Watson Lake, while climbing, the left wing struck a tree. The aircraft lost height, overturned and crashed. The pilot was killed while the passenger, his son, was injured.

Crash of a De Havilland DHC-2 Beaver in Ketchikan: 2 killed

Date & Time: Jul 26, 1984 at 1200 LT
Type of aircraft:
Operator:
Registration:
N4787C
Survivors:
Yes
Site:
Schedule:
Yes Bay - Ketchikan
MSN:
1330
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3586
Captain / Total hours on type:
1510.00
Circumstances:
The pilot flew into a canyon with a climb-out gradient in excess of the aircraft capability and collided with the upsloping terrain. The pilot said he had hit a downdraft and turned away from the rising terrain just as collision occurred. Surviving passengers do not recall any turbulence or sinking sensation before the crash. The pilot did not report any turbulence or downdrafts anywhere except at the accident site. Two passengers were killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: maneuvering
Findings
1. (f) terrain condition - mountainous/hilly
2. (c) in-flight planning/decision - improper - pilot in command
3. (f) aircraft performance, climb capability - exceeded
4. (c) clearance - inadequate - pilot in command
5. (c) proper climb rate - not possible - pilot in command
Final Report: