Incident Sequence
During the return leg of an air ambulance flight, the helicopter was approximately one mile from the airport when it yawed to the left and the N2 (gas generator speed) dropped to about 92%. As the aircraft descended to an altitude of 30-50 feet and an airspeed of approximately 20 knots, it yawed violently to the left, accompanied by corresponding drops in N2 to 55-60%, followed by surges back to 102-105%.
Pilot Response and Landing
The pilot initiated an autorotation and touched down hard approximately 300 yards short of the intended landing point.
Maintenance Background
Detroit Diesel Allison Commercial Engine Bulletin (CEB) A-73-2020, dated September 7, 1981, and revised October 5, 1981, recommends disarming the N2 (electronic) overspeed control system due to reported intermittent and spurious activations. Compliance with Bell Alert Service Bulletin (ASB) 206L-81-24, dated September 11, 1981, resulted in only partial deactivation of the system, as the operator's maintenance personnel reported that they had not received the referenced CEB as of the date of the accident.