No fatalities

4 Apr 2010: SCHWEIZER 269C — Front Range Helicopters — Idledale, CO

Idledale, CO, United States

On 4 Apr 2010, a SCHWEIZER 269C operated by Front Range Helicopters was involved in an aviation accident near Idledale, CO. No fatalities were reported. Investigators recorded the probable cause as: The flight instructor's delayed remedial actions to regain rotor rpm, resulting in a rapid descent and hard landing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

During a pinnacle landing approach, a helicopter experienced low rotor rpm and descended rapidly. The instructor took control but the helicopter landed hard, bounced, and rolled before coming to rest on its side, sustaining substantial damage.

Event Details

A flight instructor and a private pilot were conducting an approach to a pinnacle landing pad. Before the accident, two previous passes were made, and both pilots estimated the winds to be from the northeast at 8 knots. While approaching the landing pad from the southwest, the flight instructor noticed that the helicopter's rotor rpm were slightly low. He reminded the private pilot to increase power until the rpm were in the green arc of the rpm gauge.

Pilot Actions

The private pilot did not increase power sufficiently to place the rotor rpm in the green arc, and the helicopter began to descend rapidly. The flight instructor then took control of the helicopter, increased power, and attempted to reverse course and travel downhill. Despite these efforts, the helicopter landed hard, bounced, and rolled approximately 1 1/4 times before coming to rest on its right side.

Damage and Inspection

The accident resulted in substantial damage to the fuselage and tail boom. An examination of the airframe by a Federal Aviation Administration inspector did not reveal any pre-impact anomalies. Additionally, neither pilot reported a malfunction of the airframe or engine.

Contributing factors

Prop/rotor parameters — Not attained/maintainedInstructor/check pilot