Crash of a Swearingen SA226T Merlin IIIB in Arnprior

Date & Time: May 26, 2017
Operator:
Registration:
C-GFPX
Flight Type:
Survivors:
Yes
Schedule:
North Bay - Arnprior
MSN:
T-310
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane departed North Bay on an ambulance flight to Arnprior, carrying two pilots and a doctor. Following an uneventful flight, the crew was cleared for a VOR/DME approach to runway 28 under VFR conditions. On short final, the aircraft descended too low and impacted ground 50 metres short of runway. Upon impact, the nose gear collapsed and the airplane slid for about 600 metres before coming to rest. All three occupants evacuated safely and the aircraft was damaged beyond repair.

Crash of a Cessna 208B Grand Caravan near Pickle Lake: 1 killed

Date & Time: Dec 11, 2015 at 0909 LT
Type of aircraft:
Operator:
Registration:
C-FKDL
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Pickle Lake – Angling Lake
MSN:
208B-0240
YOM:
1990
Flight number:
WSG127
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2990
Captain / Total hours on type:
245.00
Aircraft flight hours:
36073
Aircraft flight cycles:
58324
Circumstances:
On 11 December 2015, the pilot of Wasaya Airways Limited Partnership (Wasaya) flight 127 (WSG127) reported for duty at the Wasaya hangar at Pickle Lake Airport (CYPL), Ontario, at about 0815. The air taxi flight was to be the first of 3 cargo trips in the Cessna 208B Caravan (registration C-FKDL, serial number 208B0240) planned from CYPL to Angling Lake / Wapekeka Airport (CKB6), Ontario. The first flight was planned to depart at 0900. The pilot went to the Wasaya apron and conducted a pre-flight inspection of C-FKDL while a ground crew was loading cargo. A Wasaya aircraft fuel-handling technician confirmed with the pilot that the planned fuel load was 600 pounds per wing of Jet A fuel. After completing the fueling, the technician used the cockpit fuel-quantity indicators to verify that the distribution was 600 pounds per wing. The pilot returned to the hangar and received a briefing from the station manager regarding the planned flights. The pilot was advised that the first officer assigned to the flight had been reassigned to other duties in order to increase the aircraft’s available payload and load a snowmobile on board. The pilot completed and signed a Wasaya flight dispatch clearance (FDC) form for WSG127, and filed a copy of it, along with the flight cargo manifests, in the designated location in the company operations room. The FDC for WSG127 showed that the flight was planned to be conducted under visual flight rules (VFR), under company flight-following, at an altitude of 5500 feet above sea level (ASL). Time en route was calculated to be 66 minutes, with fuel consumption of 413 pounds. The pilot returned to the aircraft on the apron. Loading and fueling were complete, and the pilot conducted a final walk-around inspection of C-FKDL. Before entering the cockpit, the pilot conducted an inspection of the upper wing surface. At 0854, the pilot started the engine of C-FKDL and conducted ground checks for several minutes. At 0858, the pilot advised on the mandatory frequency (MF), 122.2 megahertz (MHz), that WSG127 was taxiing for departure from Runway 09 at CYPL. WSG127 departed from Runway 09 at 0900, and, at 0901, the pilot reported on the MF that the flight was airborne. The flight climbed eastward for several miles and then turned left toward the track to CKB6. At about 3000 feet ASL, WSG127 briefly descended about 100 feet over 10 seconds, and then resumed climbing. At 0905, the pilot reported on the MF that WSG127 was clear of the MF zone. WSG127 intercepted the track to CKB6 and climbed northward until the flight reached a peak altitude of about 4600 feet ASL at 0908:41, and then began descending at 0908:46. At 0909:16, the flight made a sharp right turn of about 120° as it descended through about 4000 feet ASL. At 0909:39, the descent ended at about 2800 feet and the aircraft climbed to about 3000 feet ASL before again beginning to descend. At approximately 0910, WSG127 collided with trees and terrain at an elevation of 1460 feet ASL during daylight hours.
Probable cause:
Findings as to causes and contributing factors:
1. Although the aircraft was prohibited from flying in known or forecast icing conditions, Wasaya Airways Limited Partnership (Wasaya) flight 127 (WSG127) was dispatched into forecast icing conditions.
2. The high take-off weight of WSG127 increased the severity of degraded performance when the flight encountered icing conditions.
3. The pilot of WSG127 continued the flight in icing conditions for about 6 minutes, resulting in progressively degraded performance.
4. WSG127 experienced substantially degraded aircraft performance as a result of ice accumulation, resulting in aerodynamic stall, loss of control, and collision with terrain.
5. The Type C pilot self-dispatch procedures and practices in use at Wasaya at the time of the occurrence did not ensure that operational risk was managed to an acceptable level.
6. Wasaya had not implemented all of the mitigation strategies from its January 2015 risk assessment of Cessna 208B operations in known or forecast icing conditions, and the company remained exposed to some unmitigated hazards that had been identified in the risk assessment.
7. There was a company norm of dispatching Cessna 208B flights into forecast icing conditions, although 4 of Wasaya’s 5 Cessna 208B aircraft were prohibited from operating in these conditions.

Findings as to risk:
1. Without effective risk-management processes, aircraft may continue to be dispatched into forecast or known icing conditions that exceed the operating capabilities of the aircraft, increasing the risk of degraded aircraft performance or loss of control.
2. If pilots operating under self-dispatch do not have adequate tools to complete an operational risk assessment before releasing a flight, there is an increased likelihood that hazards will not be identified or adequately mitigated.
3. If aircraft that are not certified for flight in known or forecast icing conditions are dispatched into, and encounter, such conditions, there is an increased risk of degraded performance or loss of control.
4. If aircraft that are certified for flight in known or forecast icing conditions are dispatched into, and encounter, such conditions, at weights exceeding limitations, there is an increased risk of loss of control.
5. If flights are continued in known icing conditions in aircraft that are not certified to do so, there is an increased risk of degraded aircraft performance and loss of control.
6. If operators exceed aircraft manufacturers’ recommended ICEX II servicing intervals, there is an increased risk of degraded aircraft performance or loss of control resulting from greater accretion of ice on the leading-edge de-icing and propeller blade anti-icing boots.
7. If pilots do not receive the minimum required training, there is an increased risk that they will lack the necessary technical knowledge to operate aircraft safely.
8. If pilots are not provided with the information they need to calculate the aircraft’s centre of gravity accurately, they risk departing with their aircraft’s centre of gravity outside the limits, which can lead to loss of control.
9. If emergency locator transmitter antennas and cable connections are not robust enough to survive impact forces, potentially life-saving search-and-rescue operations may be impaired by the absence of a usable signal.

Other findings:
1. Wasaya’s use of a satellite aircraft flight-following system provided early warning of WSG127’s abnormal status and an accurate last known position for search-and-rescue operations.
2. The investigation could not determine whether the autopilot had been used by the pilot of WSG127 at any time during the flight.
Final Report:

Crash of a Beechcraft A100 King Air in Timmins

Date & Time: Sep 26, 2014 at 1740 LT
Type of aircraft:
Operator:
Registration:
C-FEYT
Survivors:
Yes
Schedule:
Moosonee – Timmins
MSN:
B-210
YOM:
1975
Flight number:
CRQ140
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2400
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
580
Copilot / Total hours on type:
300
Aircraft flight hours:
14985
Aircraft flight cycles:
15570
Circumstances:
The aircraft was operating as Air Creebec flight 140 on a scheduled flight from Moosonee, Ontario, to Timmins, Ontario, with 2 crew members and 7 passengers on board. While on approach to Timmins, the crew selected “landing gear down,” but did not get an indication in the handle that the landing gear was down and locked. A fly-by at the airport provided visual confirmation that the landing gear was not fully extended. The crew followed the Quick Reference Handbook procedures and selected the alternate landing-gear extension system, but they were unable to lower the landing gear manually. An emergency was declared, and the aircraft landed with only the nose gear partially extended. The aircraft came to rest beyond the end of Runway 28. All occupants evacuated the aircraft through the main entrance door. No fire occurred, and there were no injuries to the occupants. Emergency services were on scene for the evacuation. The accident occurred during daylight hours, at 1740 Eastern Daylight Time.
Probable cause:
Findings as to causes and contributing factors:
1. During the extension of the landing gear, a wire bundle became entangled around the landing-gear rotating torque shaft, preventing full extension of the landing gear.
2. The entanglement by the wire bundle also prevented the alternate landing-gear extension system from working. The crew was required to conduct a landing with only the nose gear partially extended.
Other findings:
1. The wire bundle consisted of wiring for the generator control circuits, and when damaged, disabled both generators. The battery became the only source of electrical power until the aircraft landed.
Final Report:

Crash of a De Havilland DHC-2 Beaver near Kennedy Lake

Date & Time: Jun 25, 2014 at 1425 LT
Type of aircraft:
Operator:
Registration:
C-FHVT
Survivors:
Yes
Schedule:
Sudbury - Kennedy Lake
MSN:
284
YOM:
1952
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3500
Captain / Total hours on type:
1000.00
Circumstances:
The Sudbury Aviation Limited float-equipped de Havilland DHC-2 Beaver aircraft (registration C-FHVT, serial number 284) was on approach to Kennedy Lake, Ontario, with the pilot and 2 passengers on board, when the aircraft rolled to the left prior to the flare. The pilot attempted to regain control of the aircraft by applying full right rudder and right aileron. The attempt was unsuccessful and the aircraft struck rising tree-covered terrain above the shoreline. The aircraft came to a stop on its right side and on a slope. The pilot and the passenger in the rear seat received minor injuries. The passenger in the right front seat was not injured. All were able to walk to the company fishing camp on the lake. There was no fire and the 406 megahertz emergency locator transmitter (ELT) was manually activated by one of the passengers. One of the operator's other aircraft, a Cessna 185, flew to the lake after C-FHVT became overdue. A search and rescue aircraft, responding to the ELT, also located the accident site. Radio contact between the Cessna 185 and the search and rescue aircraft confirmed that their assistance would not be required. The accident occurred at 1425 Eastern Daylight Time.
Probable cause:
Prior to touchdown in a northerly direction, the aircraft encountered a gusty westerly crosswind and the associated turbulence. This initiated an un-commanded yaw and left wing drop indicating an aerodynamic stall. The pilot was unsuccessful in recovering full control of the aircraft and it impacted rising terrain on the shore approximately 30 feet above the water surface.
Final Report:

Crash of a Swearingen SA227AC Metro III in Red Lake: 5 killed

Date & Time: Nov 10, 2013 at 1829 LT
Type of aircraft:
Operator:
Registration:
C-FFZN
Survivors:
Yes
Schedule:
Sioux Lookout - Red Lake
MSN:
AC-785B
YOM:
1991
Flight number:
BLS311
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
5150
Captain / Total hours on type:
3550.00
Copilot / Total flying hours:
2200
Copilot / Total hours on type:
1060
Aircraft flight hours:
35474
Circumstances:
Flight from Sioux Lookout was uneventful till the final descent to Red Lake completed by night and in light snow with a ceiling at 2,000 feet and visibility 8 SM. On final approach to runway 26, crew reported south of the airport and declared an emergency. Shortly after this mayday message, aircraft hit power cables and crashed in flames in a dense wooded area located 800 meters south of the airport. Two passengers seating in the rear were seriously injured while all five other occupants including both pilots were killed.
Probable cause:
A first-stage turbine wheel blade in the left engine failed due to a combination of metallurgical issues and stator vane burn-through. As a result of the blade failure, the left engine continued to operate but experienced a near-total loss of power at approximately 500 feet above ground level, on final approach to Runway 26 at the Red Lake Airport. The crew were unable to identify the nature of the engine malfunction, which prevented them from taking timely and appropriate action to control the aircraft. The nature of the engine malfunction resulted in the left propeller being at a very low blade angle, which, together with the landing configuration of the aircraft, resulted in the aircraft being in an increasingly high drag and asymmetric state. When the aircraft’s speed reduced below minimum control speed (VMC), the crew lost control at an altitude from which a recovery was not possible.
Final Report:

Crash of a Beechcraft D18S off Red Lake: 2 killed

Date & Time: May 30, 2013 at 1727 LT
Type of aircraft:
Registration:
C-FWWV
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Red Lake - Red Lake
MSN:
A-618
YOM:
1951
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The pilot and his wife, a couple from Phoenix, were performing a flight from the Red Lake Seaplane base to a tourist Camp located north of Red Lake. The twin engine aircraft took off at 1727LT in marginal weather conditions consisting of wind and rain showers. Shortly after departure, the aircraft crashed into the Bruce Channel located between Cochenour and McKenzie Island. The aircraft sank and both occupants were killed.

Crash of a Socata TBM-850 near Calabogie: 1 killed

Date & Time: Oct 8, 2012 at 1219 LT
Type of aircraft:
Registration:
C-FBKK
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Carp - Goderich
MSN:
621
YOM:
2012
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
19200
Captain / Total hours on type:
700.00
Aircraft flight hours:
64
Circumstances:
The privately owned SOCATA TBM 700N (registration C-FBKK, serial number 621) departed from Ottawa/Carp Airport, Ontario, on an instrument flight rules flight plan to Goderich, Ontario. Shortly after takeoff, the pilot and sole occupant altered the destination to Wiarton, Ontario. Air traffic control cleared the aircraft to climb to flight level 260 (FL260). The aircraft continued climb through FL260 and entered a right hand turn, which quickly developed into a spiral dive. At approximately 1219 Eastern Daylight Time, the aircraft struck the ground and was destroyed. Small fires broke out and consumed some sections of the aircraft. The pilot was fatally injured. The 406 MHz emergency locator transmitter on board the aircraft was damaged and its signal was not sensed by the search and rescue satellite-aided tracking (SARSAT) system.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The pilot lost control of the aircraft for undetermined reasons and the aircraft collided with terrain.
Findings as to Risk:
1. Operating an aircraft above 13 000 feet asl without an available emergency oxygen supply increases the risk of incapacitation due to hypoxia following depressurization.
Other Findings:
1. The avionics system had the capability to record data essential to the accident investigation but the recording medium was destroyed in the accident.
Final Report:

Ground fire of an Avro 748-264-2A in Sandy Lake

Date & Time: Jun 12, 2012 at 1343 LT
Type of aircraft:
Operator:
Registration:
C-FTTW
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Pickle Lake – Sandy Lake
MSN:
1681
YOM:
1970
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was parked on the ramp at Sandy Lake Airport. The flight crew had disembarked and were off-loading the cargo (JET A-1 jet fuel drums) from the aircraft to fuel tanks adjacent to the ramp. A fire broke out and the flight crew used the available fire extinguishers but the fire spread and consumed most of the aircraft that was totally destroyed. There were no injuries.
Probable cause:
A leak occurred in a hose downstream of the pumps (located on the ground beside the aircraft). The ambient wind blew vapors toward the pumps and a fire broke out. No official investigation was conducted by the TSB on this event.

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

Date & Time: May 25, 2012 at 1408 LT
Type of aircraft:
Operator:
Registration:
C-FGBF
Survivors:
Yes
Schedule:
Edgar Lake - Lillabelle Lake
MSN:
168
YOM:
1952
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1100
Captain / Total hours on type:
300.00
Aircraft flight hours:
22000
Circumstances:
The Cochrane Air Service de Havilland DHC-2 Mk.1 Beaver floatplane (registration C-FGBF, serial number 168) departed Edgar Lake, Ontario, with 2 passengers and 300 pounds of cargo on board. The aircraft was destined for the company’s main base located on Lillabelle Lake, Ontario, approximately 77 miles to the south. On arrival, a southwest-bound landing was attempted across the narrow width of the lake, as the winds favoured this direction. The pilot was unable to land the aircraft in the distance available and executed a go-around. At 1408, Eastern Daylight Time, shortly after full power application, the aircraft rolled quickly to the left and struck the water in a partially inverted attitude. The aircraft came to rest on the muddy lake bottom, partially suspended by the undamaged floats. The passenger in the front seat was able to exit the aircraft and was subsequently rescued. The pilot and rear-seat passenger were not able to exit and drowned. The emergency locator transmitter activated on impact.
Probable cause:
Findings as to Causes and Contributing Factors:
1. On the windward side of the landing surface, there was significant mechanical turbulence and associated wind shear caused by the passage of strong gusty winds over surface obstructions.
2. During the attempted overshoot, the rapid application of full power caused the aircraft to yaw to the left, and a left roll quickly developed. This movement, in combination with a high angle of attack and low airspeed, likely caused the aircraft to stall. The altitude available to regain control before striking the water was insufficient.
3. The pilot survived the impact, but was unable to exit the aircraft, possibly due to difficulties finding or opening an exit. The pilot subsequently drowned.
4. The rear-seat passenger did not have a shoulder harness and was critically injured. The passenger’s head struck the pilot’s seat in front; this passenger did not exit the aircraft and drowned.
Findings as to Risk:
1. Without a full passenger safety briefing, there is increased risk that passengers may not use the available safety equipment or be able to perform necessary emergency functions in a timely manner to avoid injury or death.
2. Not wearing a shoulder harness can increase the risk of injury or death in an accident.
3. Not having a stall warning system increases the risk that the pilot may not be aware of an impending aerodynamic stall.
4. Commercial seaplane pilots who do not receive underwater egress training are at increased risk of being unable to exit the aircraft following a survivable impact with water.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in North Spirit Lake: 4 killed

Date & Time: Jan 10, 2012 at 0957 LT
Operator:
Registration:
C-GOSU
Survivors:
Yes
Schedule:
Winnipeg - North Spirit Lake
MSN:
31-7752148
YOM:
1977
Flight number:
KEE213
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
2400
Captain / Total hours on type:
95.00
Circumstances:
The Piper PA31-350 Navajo Chieftain (registration C-GOSU, serial number 31-7752148), operating as Keystone Air Service Limited Flight 213, departed Winnipeg/James Armstrong Richardson International Airport, Manitoba, enroute to North Spirit Lake, Ontario, with 1 pilot and 4 passengers on board. At 0957 Central Standard Time, on approach to Runway 13 at North Spirit Lake, the aircraft struck the frozen lake surface 1.1 nautical miles from the threshold of Runway 13. The pilot and 3 passengers sustained fatal injuries. One passenger sustained serious injuries. The aircraft was destroyed by impact forces and a post-impact fire. After a short period of operation, the emergency locator transmitter stopped transmitting when the antenna wire was consumed by the fire.
Probable cause:
Findings as to causes and contributing factors:
1. The pilot's decision to conduct an approach to an aerodrome not serviced by an instrument flight rules approach in adverse weather conditions was likely the result of the pilot's inexperience, and may have been influenced by the pilot's desire to successfully complete the flight.
2. The pilot's decision to descend into cloud and continue in icing conditions was likely the result of inadequate awareness of the Piper PA31-350 aircraft's performance in icing conditions and of its de-icing capabilities.
3. While waiting for the runway to be cleared of snow, the aircraft held near North Spirit Lake (CKQ3) in icing conditions. The resulting ice accumulation on the aircraft's critical surfaces would have led to an increase in the aircraft's aerodynamic drag and stall speed, causing the aircraft to stall during final approach at an altitude from which recovery was not possible.
Findings as to risk:
1. Terminology contained in aircraft flight manuals and regulatory material regarding “known icing conditions,” “light to moderate icing conditions,” “flight in,” and “flight into” is inconsistent, and this inconsistency increases the risk of confusion as to the aircraft’s certification and capability in icing conditions.
2. If confusion and uncertainty exist as to the aircraft’s certification and capability in icing conditions, then there is increased risk that flights will dispatch into icing conditions that exceed the capability of the aircraft.
3. The lack of procedures and tools to assist pilots in the decision to self-dispatch leaves them at increased risk of dispatching into conditions beyond the capability of the aircraft.
4. When management involvement in the dispatch process results in pilots feeling pressure to complete flights in challenging conditions, there is increased risk that pilots may attempt flights beyond their competence.
5. Under current regulations, Canadian Aviation Regulations (CARs) 703 and 704 operators are not required to provide training in crew resource management / pilot decision-making or threat- and error-management. A breakdown in crew resource management / pilot decision-making may result in an increased risk when pilots are faced with adverse weather conditions.
6. Descending below the area minimum altitude while in instrument meteorological conditions without a published approach procedure increases the risk of collision with terrain.
7. If onboard flight recorders are not available to an investigation, this unavailability may preclude the identification and communication of safety deficiencies to advance transportation safety.
Final Report: