Casualties unknown

2019 Robinson R44 Raven II accident at Chessenaz (F-HNAF)

Chessenaz, FR

On May 26, 2019, a Robinson R44 Raven II (registration F-HNAF) was involved in an aviation accident near Chessenaz, FR. Investigators recorded the probable cause as: It is probable that the yaw rotation resulted from insufficient coordination by the student between the pedals and the collective pitch control. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA).

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Robinson R44 Raven II (F-HNAF) was destroyed on 26 May 2019 during a training flight at Chessenaz after losing control in yaw and colliding with the ground.

Flight details and accident sequence On 26 May 2019, at about 10:55 local time, a Robinson R44 Raven II helicopter, registration F-HNAF, operated by Société Alpes Hélicoptères, was destroyed during an instruction flight. The aircraft was carrying an instructor and a student. The flight began at Annecy Meythet aerodrome for local training. After about 35 minutes, the instructor landed in a field to allow the student to rest. During the subsequent takeoff for a hover exercise, the helicopter began rotating around its yaw axis, apparently to the right. The instructor took control but was unable to stop the rotation despite rudder input. The collective was lowered, and the helicopter struck the ground hard, rolling onto its left side. Both occupants evacuated as a post-crash fire started. ## Site, weather, and aircraft condition The accident occurred in a field with grass about 40 cm high and a slight slope. Estimated weather at the site included a 5 kt variable north wind, visibility over 10 km, cloud bases between 3,000 and 4,000 ft, and a temperature of 18 °C. The aircraft examination was partial due to fire, but the tail and anti-torque rotor were preserved. Observations indicated the engine was producing and transmitting power. Fuel likely flowed onto hot engine parts after the impact and rollover, initiating the fire. ## Personnel and training context The instructor held a CPL(H) obtained in October 2018 and an FI(H) qualification obtained in December 2018, with about 320 flight hours, including 44 as an instructor. The student had about 7 flight hours in six flights, all in dual command; the accident flight was the seventh. The instructor noted the student had difficulty controlling height and yaw precisely. The chosen field was not on the ATO’s approved list for such exercises, though nearby aerodromes were. The student’s progress record showed three different instructors over seven flights, with a note on excessive control amplitude during flight 3 that appeared corrected. The student had requested less instructor presence on the controls.

Probable cause

It is probable that the yaw rotation resulted from insufficient coordination by the student between the pedals and the collective pitch control. The freedom of action given by the instructor to the student on the controls, following the student’s request, probably led to a delayed reaction and prevented the instructor from regaining yaw control. Possible resistance by the student on the pedals may have reduced the effectiveness of the instructor’s rudder input to counter the rotation.