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Crash of a Piper PA-31-310 Navajo in Schefferville: 2 killed

Date & Time: Apr 30, 2017 at 1756 LT
Type of aircraft:
Operator:
Registration:
C-FQQB
Survivors:
No
Schedule:
Schefferville - Schefferville
MSN:
31-310
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
461
Captain / Total hours on type:
110.00
Copilot / Total flying hours:
1693
Copilot / Total hours on type:
650
Aircraft flight hours:
20180
Circumstances:
The Piper PA-31 (registration C-FQQB, serial number 31-310) operated by Exact Air Inc., with 2 pilots on board, was conducting its 2nd magnetometric survey flight of the day, from Schefferville Airport, Quebec, under visual flight rules. At 1336 Eastern Daylight Time, the aircraft took off and began flying toward the survey area located 90 nautical miles northwest of the airport. After completing the magnetometric survey work at 300 feet above ground level, the aircraft began the return flight segment to Schefferville Airport. At that time, the aircraft descended and flew over the terrain at an altitude varying between 100 and 40 feet above ground level. At 1756, while the aircraft was flying over railway tracks, it struck power transmission line conductor cables and crashed on top of a mine tailings deposit about 3.5 nautical miles northwest of Schefferville Airport. Both occupants were fatally injured. The accident occurred during daylight hours. Following the impact, there was no fire, and no emergency locator transmitter signal was captured.
Probable cause:
Findings:
Findings as to causes and contributing factors:
- Sensation seeking, mental fatigue, and an altered risk perception very likely contributed to the fact that, immediately after completing the magnetometric survey work, the pilot flying descended to an altitude varying between 100 and 40 feet above ground level and maintained this altitude until the aircraft collided with the wires.
- It is highly likely that the pilots were unaware that there was a power transmission line in their path.
- The pilot flying did not detect the power transmission line in time to avoid it, and the aircraft collided with the wires, which were 70 feet above the ground.
- Despite the warning regarding low-altitude flying in the Transport Canada Aeronautical Information Manua, and in the absence of minimum-altitude restrictions imposed by the company, the pilot chose to descend to a very low altitude on the return flight; as a result, this flight segment carried an unacceptable level of risk.

Findings as to risk:
- If pilots fly at low altitude, there is a risk that they will collide with wires, given that these are extremely difficult to see in flight.
- If lightweight flight data recording systems are not used to closely monitor flight operations, there is a risk that pilots will deviate from established procedures and limits, thereby reducing safety margins.
- If Transport Canada does not take concrete measures to facilitate the use of lightweight flight data recording systems and flight data monitoring, there is a risk that operators will be unable to proactively identify safety deficiencies before they cause an accident.
- If safety management systems are not required, assessed, and monitored by Transport Canada in order to ensure continual improvement, there is an increased risk that companies will be unable to effectively identify and mitigate the hazards involved in their operations.
- Not wearing a safety belt increases the risk of injury or death in an accident.
- The current emergency locator transmitter system design standards do not include a requirement for a crashworthy antenna system. As a result, there is a risk that potentially life-saving search‑and‑rescue services will be delayed if an emergency locator transmitter antenna is damaged during an occurrence.
Final Report:

Crash of a Beechcraft A100 King Air in Chicoutimi: 2 killed

Date & Time: Dec 9, 2009 at 2250 LT
Type of aircraft:
Operator:
Registration:
C-GPBA
Survivors:
Yes
Schedule:
Val d'Or - Chicoutimi
MSN:
B-215
YOM:
1975
Flight number:
ET822
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3500
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
1000
Copilot / Total hours on type:
150
Circumstances:
The Beechcraft was on an instrument flight rules flight between Val-d’Or and Chicoutimi/Saint-Honoré, Quebec, with 2 pilots and 2 passengers on board. At 2240 Eastern Standard Time, the aircraft was cleared for an RNAV (GNSS) Runway 12 approach and switched to the aerodrome traffic frequency. At 2250, the International satellite system for search and rescue detected the aircraft’s emergency locator transmitter signal. The aircraft was located at 0224 in a wooded area approximately 3 nautical miles from the threshold of Runway 12, on the approach centreline. Rescuers arrived on the scene at 0415. The 2 pilots were fatally injured, and the 2 passengers were seriously injured. The aircraft was destroyed on impact; there was no post-crash fire.
Probable cause:
Findings as to Causes and Contributing Factors:
For undetermined reasons, the crew continued its descent prematurely below the published approach minima, leading to a controlled flight into terrain (CFIT).
Findings as to Risk:
1. The use of the step-down descent technique rather than the stabilized constant descent angle (SCDA) technique for non-precision instrument approaches increases the risk of an approach and landing accident (ALA).
2. The depiction of the RNAV (GNSS) Runway 12 approach published in the Canada Air Pilot (CAP) does not incorporate recognized visual elements for reducing ALAs, as recommended in Annex 4 to the Convention, thereby reducing awareness of the terrain.
3. The installation of a terrain awareness warning system (TAWS) is not yet a requirement under the Canadian Aviation Regulations (CARs) for air taxi operators. Until the changes to regulations are put into effect, an important defense against ALAs is not available.
4. Most air taxi operators are unaware of and have not implemented the FSF ALAR task force recommendations, which increases the risk of a CFIT accident.
5. Approach design based primarily on obstacle clearance instead of the 3° optimum angle increases the risk of ALAs.
6. The lack of information on the SCDA technique in Transport Canada reference manuals means that crews are unfamiliar with this technique, thereby increasing the risk of ALAs.
7. Use of the step-down descent technique prolongs the time spent at minimum altitude, thereby increasing the risk of ALAs.
8. Pilots are not sufficiently educated on instrument approach procedure design criteria. Consequently, they tend to use the CAP published altitudes as targets, and place the aircraft at low altitude prematurely, thereby increasing the risk of an ALA.
9. Where pilots do not have up-to-date information on runway conditions needed to check runway contamination and landing distance performance, there is an increased risk of landing accidents.
10. Non-compliance with instrument flight rules (IFR) reporting procedures at uncontrolled airports increases the risk of collision with other aircraft or vehicles.
11. If altimeter corrections for low temperature and remote altimeter settings are not accurately applied, obstacle clearance will be reduced, thereby increasing the CFIT risk.
12. When cockpit recordings are not available to an investigation, this may preclude the identification and communication of safety deficiencies to advance transportation safety.
13. Task-induced fatigue has a negative effect on visual and cognitive performance which can diminish the ability to concentrate, operational memory, perception and visual acuity.
14. Where an emergency locator transmitter (ELT) is not registered with the Canadian Beacon Registry, the time needed to contact the owner or operator is increased which could affect occupant rescue and survival.
15. If the tracking of a call to 911 emergency services from a cell phone is not accurate, search and rescue efforts may be misdirected or delayed which could affect occupant rescue and survival.
Other Findings:
1. Weather conditions at the alternate airport did not meet CARs requirements, thereby reducing the probability of a successful approach and landing at the alternate airport if a diversion became necessary.
2. Following the accident, none of the aircraft exits were usable.
Final Report: