Crash of a Canadair CL-415 in Moosehead Lake

Date & Time: Jul 3, 2013 at 1415 LT
Type of aircraft:
Operator:
Registration:
C-FIZU
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Wabush - Wabush
MSN:
2076
YOM:
2010
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12500
Captain / Total hours on type:
120.00
Copilot / Total flying hours:
1700
Copilot / Total hours on type:
138
Aircraft flight hours:
461
Circumstances:
On 03 July 2013, at about 1415 Atlantic Daylight Time, the Government of Newfoundland and Labrador Air Services Division Bombardier CL-415 amphibious aircraft (registration C-FIZU, serial number 2076), operating as Tanker 286, departed Wabush, Newfoundland and Labrador, to fight a nearby forest fire. Shortly after departure, Tanker 286 touched down on Moosehead Lake to scoop a load of water. About 40 seconds later, the captain initiated a left-hand turn and almost immediately lost control of the aircraft. The aircraft water-looped and came to rest upright but partially submerged. The flight crew exited the aircraft and remained on the top of the wing until rescued by boat. There was an insufficient forward impact force to activate the onboard 406-megahertz emergency locator transmitter. There were no injuries to the 2 crew members. The aircraft was destroyed. The accident occurred during daylight hours.
Probable cause:
Findings as to causes and contributing factors:
- It is likely that the PROBES AUTO/MANUAL switch was inadvertently moved from the AUTO to the MANUAL selection when the centre pedestal cover was removed.
- The PROBES AUTO/MANUAL switch position check was not included on the Newfoundland and Labrador Government Air Services CL-415 checklist.
- The flight crew was occupied with other flight activities during the scooping run and did not notice that the water quantity exceeded the predetermined limit until after the tanks had filled to capacity.
- The flight crew decided to continue the take-off with the aircraft in an overweight condition.
- The extended period with the probes deployed on the water resulted in a longer take-off run, and the pilot flying decided to alter the departure path to the left.
- The left float contacted the surface of the lake during initiation of the left turn. Aircraft control was lost and resulted in collision with the water.
Findings as to risk:
- If safety equipment is installed in a manner that hampers its access and removal, then there is an increased risk that occupants may not be able to retrieve the safety equipment in a timely manner to ensure their survival.
- If individuals are not trained on safety equipment installed on the aircraft, then there is an increased risk that the individuals may not be aware of how to effectively use the equipment.
- If a checklist does not include a critical item, and flight crews are expected to rely on their memory, then there is a risk that that item will be missed, which could jeopardize the safety of flight.
- If flight crews do not adhere to standard operating procedures, then there is a risk that errors and omissions can be introduced, which could jeopardize the safety of flight.
- If a person is not restrained during flight and the aircraft either makes an abrupt manoeuvre or loses control, then that person is at a much greater risk of injury or death.
- If an overweight take-off is carried out, there may be an adverse effect on the aircraft’s performance, which could jeopardize the safety of flight.
- If companies do not have procedures for recording overweight take-offs and flight crews do not report them, then the overall condition of the aircraft’s structures will not be accurately known, which could jeopardize the safety of flight.
- If organizations do not use formal and documented processes to manage operational risks, there is an increased risk that hazards will not be identified and mitigated.
- If organizations do not have measures in place to raise awareness of the potential impact of stress on performance or to promote the early recognition and mitigation of stress, then there is an increased risk that errors will occur when an individual is affected by stress that has become chronic.
Other findings:
- Utilizing the locking position of the PROBES AUTO/MANUAL switch for the MANUAL selection allows the switch to be inadvertently moved from the AUTO to the MANUAL position.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Grand Lac Germain: 1 killed

Date & Time: Apr 1, 2007 at 0700 LT
Operator:
Registration:
C-FTIW
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Seven Islands - Wabush
MSN:
31-7752123
YOM:
1977
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5475
Captain / Total hours on type:
790.00
Circumstances:
The aircraft, operated by Aéropro, was on a visual flight rules (VFR) flight from Sept-Îles, Quebec, to Wabush, Newfoundland and Labrador. The pilot, who was the sole occupant, took off around 0630 eastern daylight time. Shortly before 0700, the aircraft turned off its route and proceeded to Grand lac Germain to fly over the cottage of friends. Around 0700, the aircraft overflew the southeast bay of Grand lac Germain. The pilot then overflew a second time. The aircraft proceeded northeast and disappeared behind the trees. A few seconds later, the twin-engine aircraft crashed on the frozen surface of the lake. The pilot was fatally injured; the aircraft was destroyed by impact forces.
Probable cause:
Finding as to Causes and Contributing Factors:
1. The aircraft stalled at an altitude that was too low for the pilot to recover.
Findings as to Risk:
1. The aircraft was flying at an altitude that could lead to a collision with an obstacle and that did not allow time for recovery.
2. The steep right bank of the aircraft considerably increased the aircraft’s stall speed.
3. The form used to record the pilot’s flight time, flight duty time, and rest periods had not been updated for over a month; this did not allow the company manager to monitor the pilot’s hours.
4. At the time of the occurrence, the Aéropro company operations manual did not make provision for the restrictions on daytime VFR flights prescribed in Section 703.27 of the Canadian Aviation Regulations.
Other Findings:
1. The fact that the aircraft was not equipped with a flight data recorder (FDR) or a cockpit voice recorder (CVR) limited the information available for the investigation and limited the scope of the investigation.
2. Since the aircraft was on a medical evacuation (MEDEVAC) flight, the company mistakenly advised the search and rescue centre that there were two pilots on board the aircraft when it was reported missing.
Final Report:

Crash of a Cessna 402C near Wabush

Date & Time: Oct 22, 1995 at 1907 LT
Type of aircraft:
Registration:
N67850
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Auburn – Montreal – Schefferville
MSN:
402C-0410
YOM:
1980
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Cessna 402, with five persons on board, took off from Auburn, Indiana, USA, around 0630 local time (1130 Coordinated Universal Time (UTC)) for Schefferville, Quebec, with stops en route. Their final leg was from Montreal International (Dorval) to Schefferville, with Wabush, Newfoundland, as the alternate, and they took off at 1523 EDT (1923 UTC). The flights were conducted in accordance with instrument flight rules (IFR). While in cruising flight and west of Wabush, the pilot requested the weather conditions for Schefferville and Wabush. Because of poor conditions in Schefferville, the pilot decided to fly to his alternate, Wabush. During the ILS approach for runway 01, the aircraft was too high to complete the approach, and the pilot requested and received clearance to execute another one. During the missed approach, the pilot proceeded an unknown distance outbound and turned back toward the airport. During the inbound leg, the aircraft contacted trees on the side of a mountain, at an indicated altitude of 2,460 feet asl, and decelerated over a distance of about 900 feet. The aircraft came to rest 23 nautical miles north of the airport, on the extended centre line of runway 01, on a heading of 186 degrees magnetic. The aircraft crashed probably at just after 1907 ADT (2207 UTC) during the hours of darkness. All five occupants were injured.
Probable cause:
The pilot did not follow the missed approach procedure as published, particularly with regard to minimum altitudes, and the aircraft crashed on the side of a mountain.
Final Report:

Crash of a De Havilland DHC-2 Beaver into Lake O'Keefe: 4 killed

Date & Time: Aug 7, 1975
Type of aircraft:
Registration:
CF-BPA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wabush - Wabush
MSN:
1612
YOM:
1965
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The single engine airplane departed Wabush on a forest fire patrol. In unknown circumstances, the airplane went out of control and crashed into Lake O'Keefe and sank by 80 feet of water. The wreckage was found few hours later about 60 km southwest of Wabush and all four occupants were killed, among them two government conservation officers working as forest rangers for the Newfoundland Department of Natural Resources.

Crash of a BAe 125-400A in Wabush: 8 killed

Date & Time: Nov 11, 1969 at 1830 LT
Type of aircraft:
Operator:
Registration:
CF-CFL
Survivors:
No
Schedule:
Churchill Falls - Wabush - Montreal
MSN:
25193/NA725
YOM:
1969
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The twin engine aircraft departed Churchill Falls Airport at 1800LT on a flight to Montreal with an intermediate stop in Wabush (Labrador City). On final approach, the crew encountered poor weather conditions and failed to realize his altitude was insufficient. Out of track, the airplane struck trees then crashed on a mountainous terrain located few km from the airport. The controller at Wabush Airport informed Moncton ATC about the disappearance of the aircraft and SAR operations were initiated. All eight occupants were killed, among them Donald J. McParland, President of Churchill Falls (Labrador) Corporation, his assistant John Lethbridge, Eric Lambert and three employees of the Acres Canadian Bechtel.
Probable cause:
It was determined that the aircraft was off course on approach after the crew referred to the wrong NDB. Low visibility caused by poor weather conditions was a contributing factor.