Crash of a Douglas C-47B-DL in Lake Manitou

Date & Time: Mar 12, 1995
Operator:
Registration:
C-FDTT
Flight Type:
Survivors:
Yes
Schedule:
Mingan - Lake Manitou
MSN:
14170/25615
YOM:
1944
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing, one of the ski struck an ice ridge on the ground and cartwheeled. All three crew members escaped uninjured and the aircraft was damaged beyond repair.

Crash of a Cessna 402B in Le Havre-Saint-Pierre

Date & Time: Nov 23, 1994 at 1714 LT
Type of aircraft:
Operator:
Registration:
C-FFAS
Flight Type:
Survivors:
Yes
Schedule:
Lourdes-de-Blanc-Sablon - Le Havre-Saint-Pierre
MSN:
402B-0820
YOM:
1975
Flight number:
ASJ638
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
689
Captain / Total hours on type:
29.00
Aircraft flight hours:
7012
Circumstances:
The Air Satellite Cessna 402B, flight 638, took off from Lourdes-de-Blanc-Sablon, Quebec, on an instrument flight rules (IFR) flight to Havre-Saint-Pierre, Quebec, with a load of mail. At 6,000 feet above sea level (asl), meteorological conditions were visual (VMC). About 35 nautical miles (nm) from Havre-Saint-Pierre, the pilot began his descent. At 25 nm from the airport and at an altitude of 5,000 feet asl, the pilot contacted the Flight Service Station (FSS) specialist at Sept-Îles, Quebec, via the remote communications outlet (RCO). He requested weather information for Havre-Saint-Pierre Airport. The specialist gave him the latest weather report available for the Havre-Saint-Pierre FSS. The report had been issued three hours previously by Environment Canada. The meteorological sequence indicated VMC. The pilot could see the town of Havre-Saint-Pierre when he commenced his back course approach for runway 27. During the descent, the aircraft flew into snow showers. The pilot contacted the company to check the weather at Havre-Saint-Pierre Airport, and he was told there was light snow. The pilot continued the approach to the MDA indicated on the Havre-Saint-Pierre approach chart, that is, 420 feet asl. There was moderate turbulence during the approach. The pilot tried to maintain control of the aircraft while operating the radio in an attempt to obtain more detailed weather information. One of the company pilots told him the snowfall was heavier. The aircraft then banked right. The pilot corrected, and, at the same time, the wheels touched the ground. The aircraft crashed and slid on its belly about 100 feet before coming to rest. The pilot sustained minor injuries; the aircraft sustained substantial damage. The accident occurred about 1.5 nm from the threshold of Havre-Saint-Pierre runway 27 on marshy ground. The pilot remained in radio contact with overflying aircraft and said he would stay on board the aircraft until rescuers arrived. Search and rescue crews walked toward the crash site, but they were unable to find the aircraft because of the rough terrain and reduced visibility. Five hours later, a Search and Rescue helicopter located the aircraft with the aid of the direction finder. The weak signal from the emergency locator transmitter (ELT) was still readable and was received. The pilot was transported to hospital for first aid treatment.The accident occurred during the hours of darkness.
Probable cause:
The pilot continued the descent below the MDA without the required visual references.
Final Report:

Crash of a Cessna 421C Golden Eagle III in Charlevoix: 6 killed

Date & Time: Aug 3, 1994 at 1950 LT
Registration:
C-GVPB
Flight Phase:
Survivors:
No
Schedule:
Charlevoix - Trois-Rivières
MSN:
421C-0484
YOM:
1973
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
5261
Captain / Total hours on type:
1215.00
Aircraft flight hours:
3190
Circumstances:
Around 1950 eastern daylight saving time (EDT), the Cessna 421C aircraft, registration C-GVPB, operated by les Ailes de Charlevoix inc., took off on a visual flight rules (VFR) charter flight from Charlevoix Airport, Quebec, to Trois-Rivières, Quebec, with one pilot and five passengers on board. Shortly after take-off, witnesses saw greyish smoke emanating from the left engine. The aircraft entered a steep left turn followed by a descent. It then continued in the new direction. Shortly after, the aircraft yawed and entered an uncontrolled roll, nosed down, and crashed. The aircraft caught fire on impact. All six occupants were fatally injured during the impact. The aircraft was destroyed.
Probable cause:
It is probable that a loss of oil pressure in the left engine caused a loss of power just after take-off. The pilot was unable to maintain the minimum control speed (VMC) of the aircraft.
Final Report:

Crash of a Piper PA-31-310 Navajo C in Lourdes-de-Blanc-Sablon: 2 killed

Date & Time: Jan 11, 1994 at 1854 LT
Type of aircraft:
Operator:
Registration:
C-GDOU
Flight Type:
Survivors:
No
Schedule:
Saint Anthony - Lourdes-de-Blanc-Sablon
MSN:
31-7612033
YOM:
1976
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8000
Captain / Total hours on type:
1550.00
Copilot / Total flying hours:
1079
Copilot / Total hours on type:
650
Aircraft flight hours:
11050
Circumstances:
On 11 January 1994, the crew were on a chartered round-robin flight on a PA-31 Navajo, between Lourdes-de-Blanc-Sablon airport, Quebec, and St. Anthony, Newfoundland, in accordance with visual flight rules (VFR) . During the return flight, at night, the crew advised the St. Anthony flight service station (FSS) that they departed at 1813 Newfoundland standard time (NST). At 1846 NST, the crew transmitted that they were flying at 2,500 feet and that they were 32 nautical miles (nm) and 13 minutes southeast of Blanc-Sablon. Seven minutes later, the crew called the Sept-Iles FSS through the Blanc-Sablon repeater. They requested airport information and reported being 16 nm and six minutes from the airport. After receiving information on the winds and the altimeter setting, the crew reported that they would use runway 05 and would call back on final. No further transmissions were received from the crew. Fishermen found the wreckage seven months later.
Probable cause:
The cause of the occurrence could not be determined; however, it is probable that the pilots did not monitor the altimeter properly and allowed the aircraft to descend until it struck the surface of the ice.
Final Report:

Crash of a Short 330-UTT in Umiujaq

Date & Time: Dec 1, 1993 at 1510 LT
Type of aircraft:
Registration:
C-FPQE
Flight Type:
Survivors:
Yes
Schedule:
Kuujjuarapik - Umiujaq
MSN:
3124
YOM:
1988
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10122
Captain / Total hours on type:
500.00
Copilot / Total flying hours:
10000
Copilot / Total hours on type:
10
Aircraft flight hours:
1323
Circumstances:
The two pilots were transporting Hydro-Québec employees in the aircraft to allow them to check electrical facilities in several villages along the Hudson Bay coast. The aircraft departed
Kuujjuarapik, Quebec, at about 1444 eastern standard time (EST) on a flight to Umiujaq, Quebec, a distance of 86 nautical miles (nm) to the north. The pilot-in-command was flying the aircraft. After the take-off from Kuujjuarapik, the crew contacted the Kuujjuarapik Flight Service Station (FSS) to file a flight notification and request weather information. The crew received three weather reports for Umiujaq from that FSS. The flight was conducted at an altitude of 5,000 feet on an outbound track of 045 degrees from the Kuujjuarapik non-directional beacon (NDB). Thirty miles from Umiujaq, the crew commenced the descent. Seven miles from the village, the aircraft was at an altitude of 700 feet and the crew could see the ground. The crew used a global positioning system (GPS) waypoint to supplement visual navigation (before reaching a downwind position), and continued their step-down procedure to about 200 feet above ground level (agl) on a heading of 25 degrees magnetic (°M). At that altitude, the visibility was reported by the crew to be over one and one-half miles and the crew could recognize references on the ground and position the aircraft for landing. When turning onto the final approach to runway 21, the pilot-in-command initiated a turn with at least 35 degrees of bank angle, and the aircraft stalled. The pilot-in-command initiated a stall recovery and called for full power. The aircraft did not gain sufficient altitude to overfly the rising terrain, and it crashed. The two crew members and two of the passengers sustained minor injuries. They were given first aid treatment at the accident site by other passengers.
Probable cause:
The stalling speed of the aircraft increased due to ice on the leading edge of the wings and because the pilot made a steep turn; the aircraft stalled at an altitude from which the pilot was unable to recover. A contributing factor was the crew's decision to continue the visual approach into Umiujaq despite the weather conditions reported.
Final Report:

Crash of a Piper PA-31T Cheyenne II in Montreal

Date & Time: Nov 12, 1993 at 1739 LT
Type of aircraft:
Operator:
Registration:
C-GSWB
Flight Type:
Survivors:
Yes
Schedule:
Ottawa - Montreal
MSN:
31-7720013
YOM:
1977
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Montreal-Dorval Airport, the pilot contacted ATC and reported longitudinal control problems. The aircraft started to roll left and right and the pilot maintained control using considerable aileron and rudder inputs. On short final, the twin engine aircraft crash landed short of runway 24L and came to rest in a grassy area. The pilot was injured and the aircraft was damaged beyond repair.

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

Date & Time: Jul 28, 1993 at 1800 LT
Type of aircraft:
Operator:
Registration:
C-FIUS
Flight Phase:
Survivors:
Yes
Schedule:
Lake Allard - Seven Islands
MSN:
901
YOM:
1956
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Following the derailment of a train, employees of the mine company 'QIT Fer et Titane' should be transferred from Lake Allard to Seven Islands. After takeoff from Lake Allard, the engine failed. As no suitable terrain was available, the pilot initiated a 180 turn to attempt an emergency landing on the lake. During the last turn, the aircraft stalled and crashed in the lake. A passengers was rescued while five other occupants were killed.
Probable cause:
Engine failure for unknown reasons. The aircraft stalled during the last turn because its speed was insufficient.

Crash of a De Havilland DHC-3 Otter near Schefferville

Date & Time: Aug 21, 1992 at 0730 LT
Type of aircraft:
Operator:
Registration:
C-FBSF
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Schefferville - Desbergères Lake
MSN:
9
YOM:
1953
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot departed the Air Saguenay base at Squaw Lake, Schefferville in northern Quebec around 07:00 local on a VFR flight to Desbergères Lake, about 210 miles to the northwest. The float-equipped C-FBSF was carrying six passengers and equipment for hunting caribou. Weather conditions deteriorated 30 minutes into the flight. The pilot entered a narrow valley some 50 miles northwest of Schefferville, then realised he could not clear the mountain peaks because of the lower ceiling in that area. When he tried to turn around to the left he flew into a fog bank. On emerging from the fog he saw the aircraft was going to strike the mountain. He raised the nose to minimize the force of the impact and tried to set the Otter down on the mountain side. The floats slid about 150 feet along the rocky surface, then broke off. The engine struck the ground and was torn off. The engine then rolled under the aircraft and came to rest on the right side of the fuselage. The Otter came to rest on the mountainside at an altitude of 2,650 feet. All passengers had been sitting on the right side of the aircraft and the baggage and equipment was stowed on the left side. The pilot and passengers were able to evacuate the Otter and there were no injuries. As they did so the Otter caught fire and burned for 45 minutes, consuming the fuselage. The wings fell to the ground after the wing supports melted. The fire died out after all flammable material was consumed. When radio contact with the Otter was lost, search aircraft were launched and located the crash site. The occupants were spotted at 11:30 and a rescue helicopter arrived at the site at 14:00 and all were rescued. There was however no rescue for the Otter which had been completely destroyed.
Source: http://www.dhc-3archive.com/DHC-3_9.html

Crash of a De Havilland DHC-6 Twin Otter 200 in Poste-Montagnais

Date & Time: Jan 20, 1992 at 1510 LT
Operator:
Registration:
C-FHNM
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Poste-Montagnais - Seven Islands
MSN:
127
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on icy runway 18, the aircraft deviated to the left but the crew continued the takeoff procedure. At liftoff, the aircraft struck a 1,2 metre snowdrift and crashed, coming to rest upside down. Both pilots escaped uninjured and the aircraft was damaged beyond repair and later transferred to Norway on static display.

Crash of an Avro 748-272-2A in Rivière-au-Saumon

Date & Time: Nov 29, 1991
Type of aircraft:
Operator:
Registration:
C-GGOO
Flight Phase:
Survivors:
Yes
Schedule:
Rivière-au-Saumon - Quebec City
MSN:
1692
YOM:
1971
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll at Rivière-au-Saumon Airport, the right engine caught fire and exploded. The crew abandoned the takeoff procedure and completed an emergency braking maneuver. All 35 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It was determined that the aircraft's water/methanol system had been serviced from a drum containing contaminated fluid. The drum was not labelled in a properly manner.