Dramatic Loss of Control During AS350 Landing Practice
Two people died in a horrific accident when a private pilot practised landing his newly acquired Airbus Helicopters AS350B3 helicopter N711BE on a wheeled landing platform (or tow dolly) at McClellan-Palomar Airport, Carlsbad, CA on 18 November 2015.
The US National Transportation Board (NTSB) report that the pilot had practised several landings in a field before returning to the airport, “where the approach and hover taxi to the ramp were uneventful”. However:
In the weeks preceding the accident, the pilot had expressed concern to multiple flight instructors that he was having difficulty adjusting to the flight characteristics of the helicopter. In particular, he found dolly-landings challenging.
Although the pilot had many years of experience flying a Bell 407 helicopter, there were two significant differences between the Bell 407 and the accident helicopter.
First, their main rotor systems rotated in opposite directions; therefore, the foot pedal inputs required to counteract changes in torque during takeoff and landing were opposite. (The pilot’s difficulty adapting to this difference was evidenced during most of the previous takeoffs captured by the onboard video when the helicopter yawed significantly after lifting off.)
Second, the tips of the landing skids, which were used as a visual reference during landing, were forward of the pilot in the Bell 407 but just aft of the pilot in the accident helicopter.
This change in visual reference would have been particularly significant during dolly landings, which require landing on a specific point directly below the pilot’s field of view.
The pilot had received about 11 hours of flight instruction in the helicopter, and, despite the fact that his instructors advised him not to fly without an instructor, he opted to fly with a passenger…on the accident flight. Although the passenger held a helicopter rating, he was not an instructor or professional helicopter pilot and had about 180 hours total in helicopters. Furthermore, it was likely that he had little or no experience in the accident helicopter make and model.
The NSTB say:
The pilot made a landing attempt on a dolly but landed only partially on the dolly, which caused the helicopter to pitch nose up and strike the ground with its tail.
The helicopter hit the dolly with such force that the dolly broke free from the chocks securing it and spun around. The helicopter climbed and spun upwards aggressively but stabilized after rotating 270° to the right. Ground crew personnel re-secured the dolly with chocks, and, after about 2 1/2 minutes, the pilot again attempted to land on the dolly, this time from the opposite direction. He made two unsuccessful attempts but was unable to maintain a stabilized approach each time.
The pilot persisted:
On his third attempt, he again landed partially on the dolly…
…and the helicopter rocked back and forth striking the ground with its tailskid…
…before violently climbing and pitching nose down, while rolling right.
The helicopter spun 180° to the left and pitched up steeply…
…and the tail rotor and vertical stabilizer struck the ground and separated.
The helicopter hit the ground left side low, bounced, and rotated another 360° before landing hard on its belly. The main rotor blades continued to spin and the engine continued to operate; the helicopter spun on its belly at a rate of about one revolution per second for more than 5 minutes, while gradually sliding about 530 ft along the ramp.
The tailboom and horizontal stabilizer then separated, and the helicopter violently rolled onto its side, shed its main rotor blades, and came to rest.
The helicopter was equipped with an Appareo Vision 1000 flight data monitor. The unit was capable of recording video, audio, GPS coordinates, and pitch, roll, yaw and acceleration data. Onboard video showed that the pilot became incapacitated during the final ground collision. The passenger remained conscious after the impact…but he eventually became incapacitated after about 2 minutes due to his injuries, the forces imposed by the spinning helicopter, or both.
The pilot was using two Central Nervous System (CNS) depressants simultaneously, which the NTSB comment…
…typically results in cognitive impairment which is magnified well beyond the simple addition of the effects, even when the amount of one of them may be low. Therefore, the pilot’s decision-making, judgment, and psychomotor performance were most likely impaired by the combination of CNS depressants, diphenhydramine and alprazolam.
NTSB Probable Cause
The pilot’s loss of control during landing on a dolly.
Contributing to the accident were:
- the pilot’s decision to conduct the flight without an instructor despite multiple flight instructors’ recommendations to the contrary,
- his failure to land on the ramp when he experienced difficulty landing on the dolly, and
- his impaired decision-making, judgment, and psychomotor performance, due to his use of a combination of two psychoactive drugs.