No fatalities

13 Jun 2009: SCHWEIZER 269C-1 — BRISTOW ACADEMY INC — Titusville, FL

Titusville, FL, United States

On 13 Jun 2009, a SCHWEIZER 269C-1 operated by BRISTOW ACADEMY INC was involved in an aviation accident near Titusville, FL. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain control of the helicopter during hover, resulting in a rollover. This summary draws on records from NTSB; 17 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A certificated private rotorcraft pilot practicing flight maneuvers experienced an accident when the helicopter's right rear skid contacted the ground during a hover, causing the helicopter to roll onto its right side and sustain substantial damage to the tail rotor gearbox.

Accident Overview

A certificated private rotorcraft pilot was conducting a flight with the stated purpose of practicing flight maneuvers. According to the pilot's account, the accident occurred while the helicopter was at a hover approximately 3 feet above the ground. During this hover, the right rear skid made contact with the ground surface.

Sequence of Events

Upon the right rear skid contacting the ground, the helicopter suddenly rolled onto its right side. The impact resulted in substantial damage to the tail rotor gearbox. The pilot reported no mechanical or flight control anomalies that could have contributed to the accident.

Environmental Conditions

At the time of the accident, wind conditions were recorded from 250 degrees at a speed of 5 knots. The pilot did not specify the time of day, weather characterization, or other environmental details.

Aircraft and Pilot Information

The pilot held a private rotorcraft certificate. The specific type and registration of the aircraft were not disclosed in the accident report. The pilot was the sole occupant and no injuries were reported as per the available information.

Damage Assessment

The helicopter sustained substantial damage, particularly to the tail rotor gearbox. The extent of damage to other components was not detailed in the report.

Contributing factors

PilotLateral/bank control — Not attained/maintained