N3211NBell 206B · 1984

On February 5, 2014, about 1430 mountain standard time, a Bell 206B helicopter, N3211N, was substantially damaged when it rolled onto its right side during the initial phase of an attempted takeoff from a remote landing zone (LZ) near Bountiful, Utah. Neither the flight instructor nor the pilot under instruction was injured. The instructional flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. The helicopter was operated by the Salt Lake City Utah division of Upper Limit Aviation, which was a Part 141 certificated training facility. Visual meteorological conditions prevailed, and no Federal Aviation Administration (FAA) flight plan was filed for the flight.

According to both pilots, a portion of the flight was being used to practice operations from a snow-covered LZ, which was located in mountainous terrain at an elevation several thousand feet above that of the school's base airport. The pilots had already completed one landing and takeoff at the LZ. After the second landing, which was uneventful, the helicopter sat on the snow for a few minutes before the pilots initiated the next takeoff. Winds at the LZ were light, and the helicopter nose was pointed into the wind. Just after engine power application, the right forward skid sank into the snow, and the pilots were unable to prevent the ensuing rollover.

Flight Instructor

According to the flight instructor, he held commercial pilot and flight instructor certificates, with ratings for airplane single engine, helicopter, instrument helicopter, and helicopter instructor. He had approximately 1,550 total hours of flight experience, including about 750 hours in the accident helicopter make and model. His most recent flight review was completed in January 2014.

According to the operator's Chief Safety Officer, in order for an instructor to conduct instruction in operations on snow more than 6 inches deep, the operator's policy required that the helicopter must be appropriately equipped, and the instructor must have received specific training from the chief flight instructor. The instructor had not received the required training.

Pilot Under Instruction

According to the pilot under instruction, he held a private pilot certificate with ratings for helicopter and instrument helicopter. He had approximately 244 total hours of flight experience, including about 72 hours in the accident helicopter make and model. The pilot was enrolled in the operator's course for a commercial helicopter certificate, and the accident flight was in support of that course work.

FAA information indicated that the helicopter was manufactured in 1984, and was equipped with a Rolls-Royce (Allison) 250-C20 series turboshaft engine. The helicopter was equipped with "tundra pads" mounted near the rear landing skid crosstube. According to the operator, tundra pads are smaller than the "bear paws" intended for use in deep snow, but were suitable for operations on limited (less than about 6 inches) depths of snow.

Neither NTSB nor FAA personnel traveled to the accident site. According to information provided by the operator, the helicopter came to rest on its right side, on top of the snow. The two-blade main rotor assembly had separated from the helicopter, and both blades were extensively damaged. The right landing skid tube forward of the forward crosstube was bent about 45 degrees up and inboard. According to operator personnel, damage to the main rotor blades and the tail boom was consistent with one or both blades striking the tail boom at some point during the rollover.

Examination of site photographs provided by the operator showed that the overall LZ area within an approximate 100-foot diameter circle was snow-covered, and that the snow surface was essentially level. However, due to variations in the underlying terrain, the snow depth was not uniform. The area located about 15 feet forward and to the right of the helicopter was covered with snow less than 6 inches deep, and grass protruded through the snow. The snow beneath and to the right of the helicopter was about 2 feet deep. Site examination by company personnel indicated that the helicopter had landed on an area of snow that consisted of a soft layer of snow that was about 5 to 6 inches thick, which overlaid a crust of firmer snow that was on top of a base of about 12 to 18 inches of more soft snow.

The helicopter was recovered from the LZ the day after the accident, and was examined by FAA inspectors. The pilots did not report, and the FAA inspectors did not observe, any indications of any pre-existing mechanical deficiencies or failures.

The FAA Rotorcraft Flying Handbook contained the following information regarding dynamic rollover:

- A helicopter is susceptible to a lateral rolling tendency, called dynamic rollover, when lifting off the surface. For dynamic rollover to occur, some factor has to first cause the helicopter to roll or pivot around a skid, or landing gear wheel, until its critical rollover angle is reached. Then, beyond this point, main rotor thrust continues the roll and recovery is impossible. If the critical rollover angle is exceeded, the helicopter rolls on its side regardless of the cyclic corrections made.

- Dynamic rollover begins when the helicopter starts to pivot around its skid or wheel. This can occur for a variety of reasons, including….if the gear is stuck in ice, soft asphalt, or mud.

- Once started, dynamic rollover cannot be stopped by application of opposite cyclic control alone.

- The following conditions are most critical for helicopters with counter-clockwise rotor rotation:

1. right side skid/wheel down, since translating tendency adds to the rollover force.