Zone

Crash of a Piper PA-31-310 Navajo C near Colton: 1 killed

Date & Time: May 3, 2017 at 2030 LT
Type of aircraft:
Operator:
Registration:
C-GQAM
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Quebec - Montreal
MSN:
31-7912093
YOM:
1979
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5250
Captain / Total hours on type:
1187.00
Circumstances:
The commercial pilot departed on a planned 1-hour cargo cross-country flight in the autopilot-equipped airplane. About 3 minutes after departure, the controller instructed the pilot to fly direct to the destination airport at 2,000 ft mean sea level (msl). The pilot acknowledged the clearance, and there were no further radio transmissions from the airplane. The airplane continued flying past the destination airport in straight-and-level flight at 2,100 ft msl, consistent with the airplane operating under autopilot control, until it was about 100 miles beyond the destination airport. A witness near the accident site watched the airplane fly over at a low altitude, heard three "pops" come from the airplane, and then saw it bank to the left and begin to descend. The airplane continued in the descending left turn until he lost sight of it as it dropped below the horizon. The airplane impacted trees in about a 45° left bank and a level pitch attitude and came to rest in a heavily wooded area. The airplane sustained extensive thermal damage from a postcrash fire; however, examination of the remaining portions of the airframe, flight controls, engines, and engine accessories revealed no evidence of preimpact failure or malfunction. The fuel selector valves were found on the outboard tanks, which was in accordance with the normal cruise procedures in the pilot's operating handbook. Calculations based on the airplane's flight records and the fuel consumption information in the engine manual indicated that, at departure, the outboard tanks of the airplane contained sufficient fuel for about 1 hour 10 minutes of flight. The airplane had been flying for about 1 hour 15 minutes when the accident occurred. Therefore, it is likely that the fuel in the outboard tanks was exhausted; without pilot action to switch fuel tanks, the engines lost power as a result of fuel starvation, and the airplane descended and impacted trees and terrain. The overflight of the intended destination and the subsequent loss of engine power due to fuel starvation are indicative of pilot incapacitation. The pilot's autopsy identified no significant natural disease:however, the examination was limited by the severity of damage to the body. Further, there are a number of conditions, including cardiac arrhythmias, seizures, or other causes of loss of consciousness, that could incapacitate a pilot and leave no evidence at autopsy. The pilot's toxicology results indicated that the pilot had used marijuana/tetrahydrocannabinol (THC) at some point before the accident. THC can impair judgment, but it does not cause incapacitation; therefore, the circumstances of this accident are not consistent with impairment from THC, and, the pilot's THC use likely did not contribute to this accident. The reason for the pilot's incapacitation could not be determined.
Probable cause:
The pilot's incapacitation for unknown reasons, which resulted in an overflight of his destination, a subsequent loss of engine power due to fuel starvation, and collision with terrain.
Final Report:

Crash of a Mitsubishi MU-2B-60 Marquise in Le Havre-aux-Maisons: 7 killed

Date & Time: Mar 29, 2016 at 1230 LT
Type of aircraft:
Operator:
Registration:
N246W
Survivors:
No
Schedule:
Montreal - Le Havre-aux-Maisons
MSN:
1552
YOM:
1982
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
2500
Captain / Total hours on type:
125.00
Aircraft flight hours:
11758
Circumstances:
The twin engine aircraft left Montreal-Saint-Hubert Airport at 0930LT for a two hours flight to Le Havre-aux-Maisons, on Magdalen Islands. Upon arrival, weather conditions were marginal with low ceiling, visibility up to two miles, rain and wind gusting to 30 knots. During the final approach to Runway 07, when the aircraft was 1.4 nautical miles west-southwest of the airport, it deviated south of the approach path. At approximately 1230 Atlantic Daylight Time, aircraft control was lost, resulting in the aircraft striking the ground in a near-level attitude. The aircraft was destroyed and all seven occupants were killed, among them Jean Lapierre, political commentator and former Liberal federal cabinet minister of Transport. All passengers were flying to Magdalen Islands to the funeral of Lapierre's father, who died last Friday. The captain, Pascal Gosselin, was the founder and owner of Aéro Teknic.
Crew:
Pascal Gosselin, pilot.
Passengers:
Fabrice Labourel, acting as a copilot,
Jean Lapierre,
Nicole Beaulieu, Jean Lapierre's wife,
Martine Lapierre, Jean Lapierre's sister,
Marc Lapierre, Jean Lapierre's brother,
Louis Lapierre, Jean Lapierre's brother.
Probable cause:
Findings as to causes and contributing factors:
1. The pilot’s inability to effectively manage the aircraft’s energy condition led to an unstable approach.
2. The pilot “got behind” the aircraft by allowing events to control his actions, and cognitive biases led him to continue the unstable approach.
3. A loss of control occurred when the pilot rapidly added full power at low airspeed while at low altitude, which caused a power-induced upset and resulted in the aircraft rolling sharply to the right and descending rapidly.
4. It is likely that the pilot was not prepared for the resulting power-induced upset and, although he managed to level the wings, the aircraft was too low to recover before striking the ground.
5. The pilot’s high workload and reduced time available resulted in a task-saturated condition, which decreased his situational awareness and impaired his decision making.
6. It is unlikely that the pilot’s flight skills and procedures were sufficiently practised to ensure his proficiency as the pilot-in-command for single-pilot operation on the MU2B for the conditions experienced during the occurrence flight.

Findings as to risk:
1. If the weight of an aircraft exceeds the certified maximum take-off weight, there is a risk of aircraft performance being degraded, which may jeopardize the safety of the flight.
2. If pilots engage in non-essential communication during critical phases of flight, there is an increased risk that they will be distracted, which reduces the time available to complete cockpit activities and increases their workload.
3. If flight, cockpit, or image/video data recordings are not available to an investigation, the identification and communication of safety deficiencies to advance transportation safety may be precluded.
4. If pilots do not recognize that changing circumstances require a new plan, then plan continuation bias may lead them to continue with their original plan even though it may not be safe to do so.
5. If pilots do not apply stable-approach criteria, there is a risk that they will continue an unstable approach to a landing, which can lead to an approach-and-landing accident.
6. If pilots are not prepared to conduct a go-around on every approach, they risk not responding appropriately to situations that require one.
7. If a flight plan does not contain search-and-rescue supplementary information, and if that information is not transmitted or readily available, there is a risk that first responders will not have the information they need to respond adequately.

Other findings:
1. Transport Canada does not monitor or track the number of days foreign-registered aircraft are in Canada during a given 12-month period.
2. Turbulence and icing were not considered factors in this occurrence.
3. Transport Canada considers that the discretionary installation of an angle-of-attack system on normal-category, type-certificated, Canadian-registered aircraft is a major modification that requires a supplemental type certificate approval.
4. Although the aircraft was not in compliance with Airworthiness Directive 2006-17-05 at the time of the occurrence, there was no indication that it was operating outside of the directive’s specifications.
5. Although not required by regulation, the installation and use of a lightweight flight recording system during the occurrence flight, as well as the successful retrieval of its data during the investigation, permitted a greater understanding of this accident.
Final Report:

Crash of a Beechcraft A100 King Air in Saint-Mathieu-de-Beloeil

Date & Time: Jun 10, 2013 at 1725 LT
Type of aircraft:
Operator:
Registration:
C-GJSU
Flight Type:
Survivors:
Yes
Schedule:
Montreal - Montreal
MSN:
B-88
YOM:
1971
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4301
Captain / Total hours on type:
1500.00
Aircraft flight hours:
13616
Aircraft flight cycles:
10999
Circumstances:
The aircraft took off from the Montréal/St-Hubert Airport, Quebec, on a local flight under visual flight rules with 1 pilot and 3 passengers on board. The purpose of the flight was to check the rudder trim indicator and to confirm a potential synchronization problem between the autopilot and the global positioning system (GPS). As the aircraft approached Runway 24R at the Montréal/St-Hubert Airport, both engines (Pratt & Whitney Canada, PT6A-28) stopped due to fuel exhaustion. The pilot diverted to the St-Mathieu-de-Beloeil Airport, Quebec, and then attempted a forced landing in a field 0.5 nautical mile west of the St-Mathieu-de-Beloeil Airport. The aircraft struck the ground 30 feet short of the selected field, at 1725 Eastern Daylight Time. The aircraft was extensively damaged, and the 4 occupants sustained minor injuries. The emergency locator transmitter activated during the occurrence. The flight took place during daylight hours, and there was no fire.
Probable cause:
Findings as to causes and contributing factors:
- The pilot relied exclusively on the gauge readings to determine the quantity of fuel on board, without cross-checking the fuel consumption since the last fueling to validate those gauge readings.
- The pilot misread the fuel gauges and assumed that the aircraft had enough fuel on board to meet the minimum fuel requirements of the Canadian Aviation Regulations for this visual flight rules flight, rather than adding more fuel to meet the greater reserves required by the company operations manual.
- The pilot did not monitor the fuel gauges while in flight and decided to extend the flight to carry out a practice instrument approach with insufficient fuel to complete the approach.
- The right engine stopped due to fuel exhaustion.
- The pilot did not carry out the approved engine failure procedure when the first engine stopped, and the propeller was not feathered, resulting in significant drag which reduced the aircraft's gliding range after the second engine stopped.
- The pilot continued flying toward Montréal/St-Hubert Airport (CYHU), Quebec, despite having advised air traffic control of the intention to divert to the St-Mathieu-de-Beloeil Airport (CSB3), Quebec, and without communicating the emergency. The priority given to communications resulted in the aircraft moving farther away from the intended diversion airport.
- The left engine stopped due to fuel exhaustion 36 seconds after the right engine stopped, when the aircraft was 7.4 nautical miles from Runway 24R at Montréal/St-Hubert Airport (CYHU), Quebec, and 2400 feet above sea level.
- The pilot's decision to lower the landing gear while the aircraft was still at 1600 feet above sea level further increased the drag, reducing the aircraft's gliding range. As a result, the aircraft was not able to reach the runway at St-Mathieu-de-Beloeil Airport (CSB3), Quebec.
- The operations manager was unable to perform the duties and responsibilities of the position related to monitoring and supervision of flight operations. As a result, the safety of more than half of the flights was compromised.
Findings as to risk:
- If the total fuel quantity required for a flight is not calculated and clearly displayed on the operational flight plan, there is an increased risk that aircraft will depart without the fuel reserves required by the Canadian Aviation Regulations.
- If flights are planned and carried out without the fuel reserves required by the Canadian Aviation Regulations, there is an increased risk of fuel exhaustion resulting from unanticipated situations that extend the duration of the flight.
- If pilots elect to extend flight without first determining whether sufficient fuel reserves are available to do so, there is an increased risk of fuel exhaustion.
- If pilots do not regularly check the quantity of fuel on board, there is an increased risk of fuel exhaustion.
- If pilots do not rule out a fuel leak before opening the crossfeed valve, they risk losing all of the remaining fuel on board.
- If a pilot does not maintain control of an aircraft until landing, the force of an impact following an aerodynamic stall is likely to be far greater, increasing the risk of injury or death during a forced landing.
- If a pilot does not declare an emergency to air traffic control in a timely manner, the pilot may be deprived of assistance and resources that could help deal with the emergency, increasing the risk of an accident.
- If pilots do not receive training in dealing with complex emergencies that require prioritizing tasks, there is a risk that they will not react effectively to emergencies, increasing the risk of an accident.
- If companies do not establish a process to monitor the performance of their pilots during training and testing, there is a risk that those companies will inadvertently assign pilots to carry out flights for which they are not proficient.
- If a flight is planned and authorized solely by the pilot, with no cross-check for compliance with existing regulations, there is a risk that deviations will continue undetected, reducing the safety of the flight.
- If pilots operate without regular supervision to ensure compliance with regulations and company procedures, coupled with effective training, there is a risk of procedural adaptations that result in reduced safety margins.
- If companies assign inexperienced personnel to key flight operations management positions, there is a risk that deviations in performance or from regulations will not be detected, reducing the safety of flight operations.
- If the pilot proficiency check requirements for a chief pilot are not more stringent than those for other pilots, there is a risk that the chief pilot will be unable to perform the duties required to ensure the safety of company training and operations.
- If the approval process for appointment of operations management personnel by companies is reduced to a compliance checklist based on the minimum standards in the Commercial Air Service Standards and on pilot proficiency checks that may be repeated an unlimited number of times, there is a risk that candidates who are unfit to perform the duties and responsibilities of their positions will be appointed.
- If Transport Canada does not take into consideration the combined knowledge and experience of a new operator's management team, there is a risk that the operator will lack the skills necessary to ensure the safety of flight operations.
- If process inspections carried out by Transport Canada do not examine factors related to a recent occurrence, there is a risk that those hazardous conditions will go undetected and will persist.
If process inspections carried by TC on newly certificated operators do not closely examine the outcomes of company processes, there is a risk that hazardous conditions will not be identified and will persist.
- If the inability of appointed individuals to perform their duties and responsibilities does not constitute grounds for suspending or revoking the ministerial approval of such appointments, there is a risk that operations management personnel who are not competent will remain in their positions, increasing the risk to flight safety.
Other findings:
- The chief pilot did not meet the requirements of the Canadian Aviation Regulations at the time of appointment.
- There was no indication that the aircraft's fuel gauges were not functioning properly at the time of the occurrence flight, and it is unlikely that a deviation of the fuel gauge indicator was a factor in the pilot's decision to take off.
- C-GJSU had approximately 260 pounds of fuel on board when it took off from Montréal/St-Hubert Airport (CYHU), Quebec, and did not experience a fuel leak during the occurrence flight.
Final Report:

Crash of a Beechcraft B100 King Air in Montmagny

Date & Time: Sep 22, 2010 at 1700 LT
Type of aircraft:
Operator:
Registration:
C-FSIK
Flight Phase:
Survivors:
Yes
Schedule:
Montmagny - Montreal
MSN:
BE-39
YOM:
1978
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4500
Captain / Total hours on type:
2500.00
Copilot / Total flying hours:
7800
Copilot / Total hours on type:
675
Circumstances:
The aircraft was operating as flight MAX100 on an instrument flight rules flight from Montmagny to Montreal/St-Hubert, Quebec, with 2 pilots and 4 passengers on board. At approximately 1700 Eastern Daylight Time, the aircraft moved into position on the threshold of 3010-foot-long runway 26 and initiated the take-off. On the rotation, at approximately 100 knots, the flight crew saw numerous birds in the last quarter of the runway. While getting airborne, the aircraft struck the birds and the left engine lost power, causing the aircraft to yaw and roll to the left. The aircraft lost altitude and touched the runway to the left of the centre line and less than 100 feet from the runway end. The take-off was aborted and the aircraft overran the runway, coming to rest in a field 885 feet from the runway end. All occupants evacuated the aircraft via the main door. There were no injuries. The aircraft was substantially damaged.
Probable cause:
Findings As To Causes and Contributing Factors:
The bird strike occurred on take-off at an altitude of less than 50 feet. Gulls were ingested in the left engine, which then lost power.
After the loss of engine power, the flight crew had difficulty controlling the aircraft. The aircraft touched the ground, forcing the pilot flying to abort the take-off when the runway remaining was insufficient to stop the aircraft, resulting in the runway overrun.
Findings As To Risks:
Although a cannon was in place, it was not working on the day of the accident, which increased the risk of a bird strike.
The presence of a goose and duck farm outside the airport perimeter but near a runway increases the risk of attracting gulls.
Operators subject to Canadian Aviation Regulations Subpart 703 are not prohibited from having an aircraft take off from a runway that is shorter than the accelerate-stop distance of that aircraft as determined from the performance diagrams. Consequently, travellers carried by these operators are exposed to the risks associated with a runway overrun when a take-off is aborted.
The absence of a CVR makes it harder to ascertain material facts. Consequently, investigations can take more time, resulting in delays which compromise public safety.
Final Report:

Crash of a De Havilland DHC-3 Otter near Lac des Chats: 3 killed

Date & Time: Sep 2, 1981 at 1600 LT
Type of aircraft:
Operator:
Registration:
9417
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Montreal - Montreal
MSN:
396
YOM:
1960
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew departed Montreal-Saint-Hubert Airport on a training mission. While cruising at low altitude, the airplane stalled and crashed in a wooded area, bursting into flames. The wreckage was found near Lac des Chats. All three occupants were killed.
Probable cause:
It was determined that the pilot-in-command failed to maintain sufficient airspeed while manoeuvring at low level, resulting in an aerodynamic stall.

Crash of a Douglas C-47B-20-DK Dakota 4P in Montreal

Date & Time: Jul 28, 1952
Operator:
Registration:
984
Flight Type:
MSN:
15690/27135
YOM:
1944
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances at Montreal-Saint-Hubert Airport. The crew fate remains unknown.

Crash of a Beechcraft CT-128 Expeditor in Montreal: 6 killed

Date & Time: Nov 23, 1951 at 1015 LT
Type of aircraft:
Operator:
Registration:
HB118
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
5858
YOM:
1943
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Shortly after takeoff from Montreal-Saint-Hubert Airport, while in initial climb, the crew did not realize his altitude was insufficient due to low visibility caused by mist and rain falls. The twin engine aircraft hit tree tops and crashed on the slope of Mt Saint-Bruno located about 8 km northeast of the airport. A passenger was injured while six other occupants were killed.
Crew:
F/O Vernon Clifford Murray,
F/O Frederick James Kane.

Crash of a Lockheed L-414 Hudson I in Montreal: 3 killed

Date & Time: Feb 19, 1941 at 1600 LT
Type of aircraft:
Operator:
Registration:
T9450
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Montreal - Gander
MSN:
414-2503
YOM:
1941
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The airplane was on a delivery flight from California to England via Canada, carrying three crew members. Shortly after takeoff from Montreal-Saint Hubert Airport, the airplane went out of control and crashed, bursting into flames. All three occupants were killed.
Crew:
Cpt L. A. Jackson, pilot,
S. H. McCaughan, radio operator +1.

Crash of a De Havillandf DH.80 Puss Moth in Matchi-Manitou

Date & Time: Mar 28, 1935
Operator:
Registration:
CF-CCI
Flight Type:
Survivors:
Yes
Schedule:
Montreal - Matchi-Manitou
MSN:
DHC.203
YOM:
1930
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, sole on board, departed Montreal-Saint-Hubert Airport on a control flight to Matchi-Manitou. Upon landing on a frozen lake in Matchi-Manitou, the airplane broke in two and came to rest. The pilot evacuated safely while the aircraft was abandoned on site and later sank when the ice melted. The pilot was conducting a mission on behalf of the Controller of Civil Aviation.

Crash of a De Havilland DH.60X Moth in Val-Morin

Date & Time: Mar 8, 1931
Type of aircraft:
Registration:
G-CATG
Flight Type:
Survivors:
Yes
Schedule:
Montreal - Val-Morin
MSN:
617
YOM:
1928
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing in Val-Morin, one of the skis hit a rock. The aircraft overturned and came to rest upside down. While both occupants were slightly injured, the aircraft was damaged beyond repair.