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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:

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

Date & Time: Oct 25, 2007 at 0859 LT
Type of aircraft:
Operator:
Registration:
C-FNIF
Flight Type:
Survivors:
No
Schedule:
Val d’Or – Chibougamau
MSN:
B-178
YOM:
1973
Flight number:
CRQ501
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1800
Captain / Total hours on type:
122.00
Copilot / Total flying hours:
1022
Copilot / Total hours on type:
71
Circumstances:
The Beechcraft A100 (registration C-FNIF, serial number B-178), operated by Air Creebec Inc. on flight CRQ 501, was on a flight following instrument flight rules between Val-d’Or, Quebec, and Chibougamau/Chapais, Quebec, with two pilots on board. The aircraft flew a non-precision approach on Runway 05 of the Chibougamau/Chapais Airport, followed by a go-around. On the second approach, the aircraft descended below the cloud cover to the left of the runway centreline. A right turn was made to direct the aircraft towards the runway, followed by a steep left turn to line up with the runway centreline. Following this last turn, the aircraft struck the runway at about 500 feet from the threshold. A fire broke out when the impact occurred and the aircraft continued for almost 400 feet before stopping about 50 feet north of the runway. The first responders tried to control the fire using portable fire extinguishers but were not successful. The Chibougamau and Chapais fire departments arrived on the scene at about 0926 eastern daylight time, which was about 26 minutes after the crash. The aircraft was destroyed by the fire. The two pilots suffered fatal injuries.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The aircraft was configured late for the approach, resulting in an unstable approach condition.
2. The pilot flying carried out a steep turn at a low altitude, thereby increasing the load factor. Consequently, the aircraft stalled at an altitude that was too low to allow the pilot to carry out a stall recovery procedure.
Findings as to Risk:
1. The time spent programming the global positioning system reduced the time available to manage the flight. Consequently, the crew did not make the required radio communications on the mandatory frequency, did not activate the aircraft radio control of aerodrome lighting (ARCAL), did not make the verbal calls specified in the standard operating procedures (SOPs), and configured the aircraft for the approach and landing too late.
2. During the second approach, the aircraft did a race-track pattern and descended below the safe obstacle clearance altitude, thereby increasing the risk of a controlled flight into terrain. The crew’s limited instrument flight rules (IFR) experience could have contributed to poor interpretation of the IFR procedures.
3. Non-compliance with communications procedures in a mandatory frequency area created a situation in which the pilots of both aircraft had poor knowledge of their respective positions, thereby increasing the risk of collision.
4. The pilot-in-command monitored approach (PICMA) procedure requires calls by the pilot not flying when the aircraft deviates from pre-established acceptable tolerances. However, no call is required to warn the pilot flying of an approaching steep bank.
5. The transfer of controls was not carried out as required by the PICMA procedure described in the SOPs. The transfer of controls at the co-pilot’s request could have taken the pilot-in-command by surprise, leaving little time to choose the best option.
6. Despite their limited amount of IFR experience in a multiple crew working environment, the two pilots were paired. Nothing prohibited this. Although the crew had received crew resource management (CRM) training, it still had little multiple crew experience and consequently little experience in applying the basic principles of CRM.
Other Findings:
1. The emergency locator transmitter (ELT) had activated after the impact but due to circuit board damage its transmission power was severely limited. This situation could have had serious consequences had there been any survivors.
2. The Chibougamau/Chapais airport does not have an aircraft rescue and firefighting service. Because the fire station is 23 kilometres from the airport, the firefighters arrived at the scene 26 minutes after the accident.
3. Although this accident does not meet the criteria of a controlled flight into terrain (CFIT), it nonetheless remains that a stabilized constant descent angle (SCDA) non-precision approach (NPA) would have provided an added defence tool to supplement the SOPs.
4. After the late call within the mandatory frequency (MF) area, the specialist at the Québec flight information centre asked the crew about its familiarity with the MF area while the aircraft was in a critical phase of the first approach, which was approaching the minimum descent altitude (MDA). This situation could have distracted the flight crew while they completed important tasks.
5. The standard checklist used by the flight crew made no reference to the enhanced ground proximity warning system (EGPWS). Therefore, the crew was not prompted to check it to ensure that it was properly activated before departure.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Val d'Or

Date & Time: Feb 20, 2001 at 1900 LT
Operator:
Registration:
C-GNIE
Flight Type:
Survivors:
Yes
Schedule:
Rouyn – Val d’Or – Saint-Hubert
MSN:
31-7552047
YOM:
1975
Flight number:
APO1023
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
900
Captain / Total hours on type:
30.00
Circumstances:
A Piper PA-31-350, registration C-GNIE, serial number 31-7552047, was on a scheduled (APO1023) instrument flight rules mail service flight between Rouyn Airport, Quebec, and Val-d'Or Airport, Quebec, at approximately 1845 . After checking for prevailing weather conditions at the destination airport, the pilot decided to make a visual approach on runway 36. The pilot reported by radio at two miles on final approach for runway 36 and then stated that he was going to begin his approach again after momentarily losing visual contact with the runway. This was the last radio contact with the aircraft. No emergency locator transmitter signal was received by the flight service station specialist. Emergency procedures were initiated, and searches were conducted. The aircraft was found by a search and rescue team about three hours after the crash. The aircraft was lying about two miles southeast of the end of runway 36; it was substantially damaged. The pilot suffered serious injuries.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The environmental conditions and loss of visual ground references near Val-d'Or Airport were conducive to spatial disorientation. Because of a lack of instrument flight experience, the pilot probably became disoriented during the overshoot and was unable to regain control of the situation.
2. During the approach, the pilot did not plan to and did not pull up towards the centre of the airport, thereby contributing to spatial disorientation.
3. Although the pilot-in-command received training required by Transport Canada, Aéropro did not ensure that the pilot-in-command completed the required Pilot Proficiency Check (PPC) and was adequately supervised and experienced to conduct a night IFR flight safely as pilot-in-command.
Final Report:

Crash of a Douglas C-47A-30-DK Dakota IIIR in Val d'Or

Date & Time: Jun 19, 1970 at 1601 LT
Operator:
Registration:
CF-AAC
Flight Phase:
Survivors:
Yes
MSN:
13924/25369
YOM:
1944
Location:
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon takeoff runway 36, AAC lifted off with 18 souls on board transporting 14 Indigenous children home for the Summer holidays accompanied by a chaperone. The crew consisted of a pilot, co-pilot and a flight engineer. The runway 18/36 was 10,000 ft long and 150 ft wide. As the aircraft lifted off and came abeam of the control tower, I observed a fire in the left engine. My transmission to the pilot was, quote “AAC Val d’Or Tower, fireball left engine”. Response was “Roger Tower”. Engine fire was immediately extinguished and shut down and aircraft continued to climb. Pilot was cleared for unrestricted landing and given winds. No further transmissions heard from pilot. Emergency crash bells were rung at this instance and emergency response stations were of an airborne emergency. I anticipated the aircraft would continue to climb, turn right into live engine and effect a landing on Rwy 18. However, the aircraft started to descend, commenced a left turn into the shutdown engine and was disappeared behind the hill just North West of the button of Rwy 18. Once I lost sight of the aircraft behind the hill, known to Station personnel as “Lang’s Hill”, the crash bells were again sounded indicating a Major Disaster which now required all Station personnel to respond. The Major Disaster alarm was sounded at exactly 4:01 p.m. on a Friday night. — Friday nights at CFS Val d’Or was a traditional beer call time when most of the 350 personnel of the Station were present at the various Messes which commenced at 1600 hrs. All 18 souls on aircraft AAC were rescued within 15 minutes of impact. Both the pilots were found still strapped to their seats upside down outside near their respective wings. The flight engineer was also still strapped to his seat and was found upside down in the nose of the aircraft which was split open and jagged. The aircraft had been guided into very high trees and had basically slid down the trees and came to approximately a 45-degree angle. The most serious injury, as I understand, was an injured vertebra sustained to one of the pilots which resulted in no permanent damage. All others sustained minor cuts and bruises. I was later told that this was precisely the manoeuvre the pilot said he would make if such an incident was encountered; it obviously worked. The efficiency of the Station Major Disaster Team in quickly locating and extracting the crew and passengers of AAC was amazing. All souls were housed in a Station Barrick Block, attended to medically and shortly after transferred to the St-Sauveur Hospital in Val d’Or for further care.
Thanks to Lou Travis, ATC on duty at the time of the accident, for his testimony.

Crash of a Lockheed L-414-56-11 Hudson III near Waskaganish: 4 killed

Date & Time: Jul 3, 1957 at 1200 LT
Type of aircraft:
Operator:
Registration:
CF-CRL
Flight Phase:
Survivors:
No
Schedule:
Great Whale River – Val-d’Or
MSN:
414-7546
YOM:
1943
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3000
Captain / Total hours on type:
150.00
Circumstances:
The aircraft, owned by the Photographic Survey Corporation Limited, departed Great Whale River at approximately 0915 hours eastern standard time on a non-scheduled flight to Val d'Or, with the pilot, a maintenance engineer and two passengers aboard. An instrument flight plan was filed prior to departure, and the aircraft was to fly at 7 000 ft direct to Val d'Or, the estimated time of arrival being 1200 hours. Following take-off CF-CRL climbed on a magnetic heading of 185° on instruments, and the pilot was requested to report passing through 7 000 ft and to continue the climb to 9 000 ft. After passing routine messages, in which the freezing level of 10 000 ft was included, the pilot reported at 0928 hours that he was visual at 10 000 ft and that he would maintain this altitude to Val d'Or. At 0930 he stated he would maintain 1 000 ft on top of the overcast, i.e. 11 000 ft. At 0957 the pilot requested a radio check, and Great Whale River informed him that his transmission was weak. The pilot acknowledged this message which was the last transmission received from him. At 1600 hours the RCAF Search and Rescue Co-ordination Centre at Trenton, Ontario was notified that the aircraft was overdue, and a search was begun. The wreckage was found on 25 July, 36 miles from Rupert House, P. Q., on a bearing of 153° True. All four occupants had been killed in the crash, and the aircraft was destroyed.
Probable cause:
The cause of the accident was not conclusively determined. It should be noted, however, that the pilot took off in weather conditions below permissible limits, in an area sparsely served with aids to navigation, in an aircraft not equipped with de- icing equipment.
Final Report:

Crash of a De Havilland DH.60X Moth in Val d'Or

Date & Time: Sep 19, 1948
Type of aircraft:
Registration:
G-CAPB
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
507
YOM:
1928
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Stalled shortly after takeoff from Val d'Or Airport. The pilot, sole on board, was injured and the aircraft was written off.