A Great Slave Helicopter Bell 206L-4 (C-GSHX) rolled over when pilot exited helicopter to unhook sling load. The pilot contacted Ektaki, NT (CYOA) radio.
A Great Slave Helicopter Bell 206L-4 (C-GSHX) rolled over when pilot exited helicopter to unhook sling load. The pilot contacted Ektaki, NT (CYOA) radio.
The privately owned Rotorway 162F, C-FLRQ, was enroute from the manufacturer’s facility in Red Deer, AB (CYQF), to a private strip near Big Valley, AB. In the vicinity of Delburne, AB, the FADEC controlled engine (RI162) began to lose power, and then came back on. The pilot decided to conduct an autorotation in a field. During touchdown, the helicopter flipped onto its right side. The helicopter was substantially damaged; the pilot, who was the lone occupant, was not injured.
C-GOPK, a Highland Helicopters Bell 206 B departed Williams Lake (CYWL) and was carrying out scanning operations over a logged area about 112 nm NW of Prince George when the helicopter spun to the left and descended into the ground. The helicopter was destroyed, the pilot was injured, but the 2 passengers appeared to have no injuries. All 3 were taken to hospital in Fort St. James, BC. There was no post impact fire. The 406 Emergency Locator Transmitter activated
on a local pleasure flight from a private facility at Redfern Lake, BC. As the pilot attempted a landing at approximately 7800 feet ASL near the edge of a cirque, the aircraft encountered descending air on final. The pilot elected to continue the approach and increased the collective to maintain the sight picture. The pilot then noticed the low rotor warning with the rotor RPM decreasing rapidly toward 70%. The aircraft landed hard and rolled over several times down the slope. The pilot and the two passengers evacuated the aircraft with no injuries. There was no post impact fire; however the aircraft sustained substantial damage.
C-GGQL, a Far West Helicopters Bell 206B, was departing with two passengers on board off a helipad at an elevation of about 2500 feet ASL, 4 nautical miles north of Port Renfrew, BC. During the vertical ascent to rise above tree height, the torque gauge was indicating about 90-95%. Upon reaching an estimated 100-150 feet, the rotor RPM (Nr) was down to about 97%. The pilot reduced the collective slightly in an attempt to recover to 100% Nr. When the RPM did not recover, the ascent was stopped (at tree top height, approximately 200-250 feet) and the pilot immediately initiated a descent back towards the helipad. Almost immediately, the rotor RPM had decreased to 90% Nr and the low rotor RPM caution light and horn activated. The landing was hard, the left skid wedged under a helipad log and tilted backward. The main rotor blades struck the ground as the throttle was being rolled off and the helicopter came to rest on its right side. The occupants were not injured and evacuated unassisted.
C-FBLW, a TRK Helicopters Aerospatiale AS350 BA helicopter, was operated under contract to SKEENA Heli-Ski from the Bear Creek Lodge, BC, about 82 nautical miles north west of Smithers, BC. The flight was returning to base camp in the late afternoon with a pilot and 6 passengers on board. As the pilot was maneuvering the helicopter close to the steepening terrain, the cyclic control was moved forward. The nose of the helicopter pitched down and the speed increased to Vne (+/-). The pilot then moved the cyclic back and left, however the helicopter rolled right and pitched up. The cyclic stick was difficult to move, and the helicopter collided with terrain on a steep snow covered slope. The main rotor blades cut a swath through the deep snowpack on the left side, and continued to turn until the pilot shut down the engine (Honeywell LTS 101-700D-2) and applied the rotor brake. All occupants appeared uninjured and expedited egress to the left side due to the steep, downhill slope on the right side. The helicopter was substantially damaged, but the ELT was not triggered to send out an emergency signal.
The privately-registered Eurocopter EC-120B helicopter was on a local VFR flight from Toronto Billy Bishop/Toronto City Centre Airport, ON (CYTZ). The helicopter was being flown in circuits at Brampton Airport, ON (CNC3) when it experienced a loss of power. The helicopter crashed near the southern end of the airport property. Two (2) souls on board — no reported injuries. The helicopter was substantially damaged. Transportation Safety Board (TSB) advised.
The pilot was attempting to land on a marked heliski landing site on a ski run called “Nicole”. This was the second landing of the day at this location; the helicopter was carrying 10 guests, 2 guides and the pilot. The first approach was abandoned due to skiers from a previous group waiting on the landing site. On the second approach, visibility was reduced in fog and blown-up snow. The pilot still had the site markers and skiers in sight when it became apparent that the helicopter could not come to a complete hover and touch down would result in a run-on landing. The helicopter touched down on the pilot’s right-hand side due to skiers near the left side of the site. With some forward momentum and sloping ground to the right, the helicopter’s right-side skid dug into the soft snow, resulting in the helicopter rolling over to the right side. The pilot pulled both fire T-handles and exited the aircraft while the guides were assisting guests out from the back seats. There were no injuries or fire.
The Custom Helicopters Bell 206L-1, C-GOFH, was hovering prior to touchdown at a remote camp in north eastern Manitoba when an unsecured canvas portion of a Quonset hut was blown into the rotor disc. The aircraft landed without further incident. The helicopter sustained damage to one rotor blade and will remain on location pending inspection and repair.
A 55-year-old male pilot from Campbell River, B.C., and a 35-year-old male passenger from Prince Albert, Sask., were the only 2 POB when it crashed. They were pronounced dead at the scene. Helicopter was contracted by electric utility SaskPower to access and repair power poles and struck a powerline causing the aircraft to crash. Post crash fire completely consumed the aircraft.
Cougar Flight 232 was shut down upon arrival at the Hibernia Gravity Based Structure (GBS) after experiencing engine fuel bypass indications on both engines. The aircrew awaited the arrival of maintenance crew. Overnight the Aircraft Maintenance Engineers, in consultation with the engine manufacturer, conducted all required maintenance procedures. The helicopter was subsequently flight tested and certified serviceable on the morning of October 7. Cougar aircrew then returned the aircraft to St. John’s without further incident.
Helicopter was landing at a gravel pit near a hunting camp. While manoeuvring to land to refuel the helicopter, the tail rotor struck a fuel drum. The rotor blade was destroyed, the tail rotor drive train was damaged and one main rotor blade was damaged by debris. The helicopter landed safely and the pilot, the sole occupant, was not injured.
Helicopter was hovering approximately 40 feet AGL to assess the landing area. The helicopter moved laterally to the right in order to increase the visibility of the landing area. During this time, the helicopter rotated to the right and started to spin about the vertical axis. An attempt to control the rotational spin was made, however, there was little to no tail rotor effectiveness. CGNET was put down after the second rotation while striking the tail rotor on the ground and damaging the landing skids. There were no injuries
Helicopter crashed into trees, dropping vertically nose-first between the trees down to the ground, killing both on board – named as 24-year-old Jeremie Belanger and 41-year-old Ken Mielke – both were pilots were pilots for Apex Helicopters, which was performing aerial spraying for a forestry company in the area.
Heilcopter with 5 POB went down on a wide rock adjacent to a river, with the tail boom detached. Two fatalities, three seriously injured
Press report of Cougar Helicopters flight CGR151 outbound to a rig when it turned back to base as a result of an “intermittent fire warning,” the operator was quoted as saying. Uneventful and safe landing back at St John’s, it’s departure point. According to a company spokeswoman, Cougar Helicopters maintenance staff have since inspected the aircraft and determined it was a false warning.
while approximately 100 nm from St. John’s and en route to the GSF Grand Banks drilling rig, Cougar Flight CGR151 experienced an intermittent Fire Warning Light on the #2 engine. There were no secondary indications of fire
The helicopter landed on a gravel bar about 15 nm west of Nanaimo Airport, BC (CYCD). Shortly after landing the pilot engaged the cyclic control lock and exited the helicopter to take a photograph with the engine running and rotors turning. After re-entering the helicopter, it was lifted off into a hover with the cyclic control lock still engaged. The aircraft rolled over and was substantially damaged.
Helicopter was operating VFR from CYFB Iqaluit, NU to BGGH Nuuk, Greenland as part of a solo circumnavigation attempt. The pilot (Sergey Ananov from Russia) autorotated and ditched the aircraft in the Davis Strait, 204 nm east of CYFB, reportedly due to a broken drive belt. He was wearing an immersion suit and managed to take the life raft while exiting the aircraft. The aircraft sank. There was no ELT signal captured. Although there were several alerting devices on board the aircraft, the pilot only had time to retrieve the life raft before the aircraft sank. He managed to swim to a nearby ice floe. The pilot was being tracked by a responsible person. When the target had not moved for a period of 30 minutes, authorities were advised and search & rescue efforts commenced. Rescue efforts were affected by dense fog. The pilot floated on the ice floe until noticing the lights of the Coast Guard vessel 3 miles away. He fired a flare to attract attention and was rescued by helicopter approximately 32 hours after ditching. He was not injured.
Transporting 6 workers from the Bobbie Burns lodge when the engine lost power. The pilot carried out an emergency landing to an area of new growth trees. The landing with low rotor rpm was hard, but the helicopter stayed upright. The tail section of the helicopter was struck by a main rotor blade and severed. The pilot and 2 passengers had no injuries, 3 passengers had minor injuries and 1 incurred a serious injury. CADORS 2015P1390
Helicopter was being used to spray fungicide on fields of corn. The pilot approached and overflew one field checking for hazards and wind conditions, and then began a spray swath across the field. Midway through the first swath, the pilot heard the low rotor horn sound. Manually rolling the throttle up did not prevent the rotor RPM from continuing to drop. The pilot then attempted a quick stop and a controlled autorotation into the corn. The helicopter was substantially damaged by the impact but the pilot who was wearing a four point shoulder harness and a helmet was not injured.
There were no reported injuries among the 4 souls on board. Search and rescue located the site via emergency locator transmitter (ELT) signal and extracted the occupants. Unknown damage to the aircraft. CADORS 2015C2524
helicopter en route to the West Hercules drilling rig returned to base due to a low oil pressure indication in one of its two engines. The incident occurred on Tuesday, June 30 when the helicopter was 20 km outside St. John’s. The helicopter returned to St. John’s without incident and the seven passengers on board were briefed by the pilots.
conducting forest fire fighting operations in the area of Fort Simpson, NT. Prior to landing in CYFS, the pilot maneuvered to set down the water bucket. While preparing to set down on the landing pad beside the bucket, the tail rotor blades contacted a fuel drum. The helicopter touched down shortly thereafter and remained upright. There was significant damage to the tail rotor, tail rotor gear box, tail boom, ventral fin and collateral damage to the horizontal stabilizer from tail rotor blade fragments. The pilot, who was the sole occupant, was uninjured. CADORS 2015C2436
The helicopter was landing on an unprepared, deeply cultivated field. During the vertical landing, the left skid settled into the soft ground and the helicopter entered into a dynamic rollover. There was substantial damage to the helicopter. There were no injuries to the pilot or passenger. CADORS 2015C2439
A private Schweitzer 269C helicopter took off from a sandy beach at Lac Central for Lac Kénogami with a pilot and a passenger on board. During the initial climb, the aircraft (Lycoming HIO-360-D1A engine) experienced a loss of lift for an undetermined reason and crashed in the lake. The occupants were not injured in the accident. CADORS 2015Q1046
The privately owned Enstrom 280FX helicopter, was being flown from Bralorne to Langley. The pilot/owner ditched the aircraft in the Harrison River. The pilot was not injured but the aircraft was significantly damaged. CADORS 2015P0926
The Safari 400 homebuilt helicopter was being operated on the owner’s property. The engine was being tested to ensure the governor was correctly installed. The helicopter became airborne by 2-3 feet and the operator lost control. The helicopter went sideways and struck the ground rolling on its side. The helicopter was destroyed but the pilot was not seriously injured. CADORS 2015A0434
The Expedition Helicopters Bell 206B (C-GJID) was flying with a pilot and three passengers. The passengers were checking land claims and were dropped off before the helicopter proceeded to an area where it landed and waited for the passengers. The ground was soft and the pilot landed with caution to ensure the skid gear would not sink into the soft ground. When the pilot received the call to pick up the passengers, the helicopter was started and as the pilot applied collective to lift off, he turned back to look at his skid gear to verify they weren’t stuck. The pilot felt the helicopter rolling to the right and applied opposite cyclic control. The recovered attempt was unsuccessful and the aircraft came to rest on its right side. The pilot secured the aircraft by selecting; the fuel valve to the off position, battery off, and pulled the boost pump circuit breakers. The pilot evacuated the aircraft and after waiting a few minutes to make sure there was no fire, returned to the aircraft and removed the first aid kit and satellite phone. The pilot contacted the company which dispatched a helicopter to the accident site to pick up the pilot.
R22 piloted by a student on a solo flight from Kelowna (CYLW) to Salmon Arm (CZAM) crashed beside the runway at CZAM. The pilot first approached the airport and crossed mid-field to assess the wind direction; however, it was determined that the aircraft was not into wind. On the second approach from the opposite direction, at about 30 feet above ground elevation, the helicopter was observed to rotate right about three revolutions before falling rapidly, and impacting the ground with little forward momentum. The left main landing skid gear fractured forward of the forward cross-tube and the R22B came to rest after rolling to the left. The pilot was uninjured but the helicopter sustained substantial damage. The pilot reported losing tail rotor authority just before the helicopter yawed right. The main rotor blades showed damage consistent with low rpm. CADORS 2015P0662
While in the hover and conducting preflight checks, Cougar flight CGR181 experienced a #2 engine power loss. The aircraft was in a 10 foot hover when the incident occurred. With the remaining engine the aircraft landed safely without further incident. All 8 passengers were briefed by the two crew members onboard the helicopter as well as upon their arrival in the terminal
After landing, the pilot exited the helicopter with the engine running to attach a longline. The force trim was not set, and the aircraft started to spin and rotated off the helipad with nobody onboard. The aircraft collided with a metal container that was located by the helipad causing substantial damage to the boom, left skid and to the left side of the airframe. There were no injuries.
The Pilot was repositioning 12 passengers from the bottom to the top of the Ghosts Drimie ski run. Upon departure, the Pilot elected to take-off downhill and downwind due to the terrain. The aircraft started to settle as it transited across a field and entered a ‘snowball’ at which time the pilot lost visual reference. The main rotor blades struck a tree and the helicopter touched down in the snow, remaining upright. There was substantial damage to the helicopter but there were no injuries.
Cougar Flight 231 was shut down on arrival at the Hibernia Gravity Based Structure (GBS) on February 18 due to an issue related to anti-vibration control and a chip light indication. Two Aircraft Maintenance Engineers deployed by Cougar to investigate determined that replacement parts are necessary. The parts are being shipped to Hibernia by vessel for installation. The helicopter remained on site until 27th February – weather played a part in this too
Heliski operation landing atop Sprout Mountain with 2 pax in an area cleared of snow accumulation, when the main rotor struck a nearby cabin. The helicopter tail section was severed but the helicopter remained upright and all occupants exited uninjured. The area which had been prepared for the arrival of the helicopter was located beside the helipad where the pilot expected to land; it resulted in a confined space for landing.
conducting heliski operations with one pilot and five passengers aboard. During a run-on downwind landing, the main rotor contacted the helicopters tail boom. The tail rotor driveshaft cover was damaged and the tail rotor driveshaft was creased. The aircraft’s vertical winglets were also struck by the main rotor blades. The helicopter’s occupants were not injured. CADORS 2015P0188
Helicopter was involved with long line operations on a power-line construction project 11 nm SE of Key Lake, SK. After a power-line cable was moved, the long line did not release. The helicopter descended and struck the ground. The pilot was injured and was transferred to La Ronge Hospital for medical attention. The helicopter sustained substantial damage but there was no fire.
On take off, main rotor blade(s) contacted the wind sock mast. A vibration was felt and the pilot landed immediately at the same site. An inspection of the main rotor revealed damage to one of the blades. CADORS 2014C5006
During the landing approach at a height of about 20-30 feet above the ground, a quick right yaw occurs. Pilot lost control resulting in a hard landing and the helicopter rolled to the side and suffered significant damage, but the pilot was not injured.
The helicopter was slinging a hydro tower into position. After positioning the tower, the ground crew secured two of the support cables to their foundations. The pole was then shifted to accommodate securing of the remaining two support cables. As the two secured cables became taut, the pilot felt a bump and the helicopter became unstable. The pilot then released the load and was able to regain control of the helicopter. The helicopter then landed safely. There were no injuries and there was no damage to the helicopter.
On a local flight 32 NM northwest of Matagami, QC, when the engine (Honeywell LTS-101-700-D2) failed on final for the helipad. The aircraft was not damaged and the pilot, alone on board, was not injured. The TSB will implement a plan to examine some of the components
Crashed west of Whitecourt, AB after experiencing tail rotor problems. Four occupants suffered minor injuries, two were taken to hospital. The aircraft had significant damage. Helicopter was contracted to Alberta Environment and Sustainable Resource Development and carrying out a pine beetle survey
Shortly after liftoff, in the climb through 3000 feet ASL (800 feet above ground), the pilot experienced an uncommanded yaw and complete loss of engine power. The pilot performed an autorotation into a wheat field. The helicopter sustained substantial damage to tail boom and tail rotor driveshaft from main rotor blade contact. There were no injuries to the pilot, who was the sole occupant. CADORS 2014C3154
During the run-up before takeoff at night, the aircraft rapidly rotated about 180 degrees to the left. The pilot initiated a takeoff and the helicopter rolled onto its left side. The pilot and passenger suffered minor injuries and the aircraft sustained substantial damage.
In visibility of 1 mile in smoke, the helicopter overflew a lake with a glassy surface. The pilot lost visual reference and the helicopter collided with the water surface, pitched inverted, and sank. The pilot and both passengers egressed from the helicopter with only minor injuries.
In the initial climb at less than 20ft agl and engine lost power and the pilot observed illumination of the overtorque warning light and heard the low rotor RPM warning tone. A forced landing was completed. There were no injuries to the pilot or passenger; the helicopter sustained substantial damage to the tail boom. After landing the pilot shut down the engine that was operating at idle.
During the descent for landing, the pilot was not able to stop the descent and yaw. The pilot pushed the cyclic to exit the vortex and pick up speed, but the main rotor collided with the ground and the aircraft rolled to a stop on the ground. CADORS 2014Q1246
Dynamic roll over on take-off after catching a fuel drum with a skid. The pilot, the sole occupant, sustained minor injuries. The 406 ELT activated and was shut off immediately. CADORS 2014P0717
Helicopter hit wire in flight followed by a hard landing, which activated the ELT. Both persons on board were reported as being okay (pilot with no injuries and passenger with only sore ribs). CADORS 2014Q0857
Departed from a private residence in Queensville, Ontario for a local flight with the pilot and two passengers on board. During a landing in a marshy area of the Holland Marsh near Cooks Bay, a skid cut in the soft earth and the helicopter dynamically rolled over. There were no injuries and the helicopter was substantially damaged. CADORS ref 2014O0834
departed from a private residence in Queensville, Ontario for a local flight with the pilot and two passengers on board. During a landing in a marshy area of the Holland Marsh near Cooks Bay, a skid cut in the soft earth and the helicopter dynamically rolled over. There were no injuries and the helicopter was substantially damaged. CADORS 2014O0834
AS350-B2 with a pilot and three passengers on board, took off while it was near a communication tower. During takeoff, the pilot wanted to bypass the tower and conduct a takeoff facing the wind away from the guy wires. Nevertheless, the main rotor came into contact with a guy wire and the aircraft crashed into the ground. The aircraft was substantially damaged. The pilot and one passenger were seriously injured while the two other passengers were not injured.. CADORS 2014Q0581
The helicopter set down right side low on the chosen sloping landing site and remained partially supported by the rotor. The pilot attempted to move to a different site nearby, but a skid dug into the snow and the helicopter entered a dynamic rollover condition and fell to the ground on its right-hand side. There was no fire nor were there injuries. The helicopter was substantially damaged.
During a hydraulics off landing exercise, control of the helicopter was lost and the helicopter collided with the ground resulting in substantial damage. The two flight crew sustained minor injuries. The engine continued to run after the impact; however, there was no post impact fire. CADORS 2014C0677
The helicopter had just been started with an ground power unit (GPU). The pilot exited the aircraft in order to disconnect the GPU, when a gust of wind pushed the helicopter into the trees next to the helipad. The pilot was not injured. CADORS 2014C0375