No fatalities

28 Mar 2015: GIACKINO DONALD W ROTORWAY 162F (N556DG) — Marquette, MI

Marquette, MI, United States

On 28 Mar 2015, a GIACKINO DONALD W ROTORWAY 162F (registration N556DG) was involved in an aviation accident near Marquette, MI. No fatalities were reported. Investigators recorded the probable cause as: The loss of helicopter control for reasons that could not be determined based on the available evidence. This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On March 28, 2015, a Rotorway 162F helicopter (N556DG) impacted terrain after losing tail rotor effectiveness during a hover at a private helipad in Marquette, Michigan. The pilot was uninjured.

Accident Details

At about 1400 eastern daylight time on March 28, 2015, a Rotorway 162F helicopter, registration N556DG, impacted terrain shortly after lifting off from a private helipad in Marquette, Michigan. The helicopter, operated by a private individual under 14 CFR Part 91 for personal use, sustained substantial damage to its main rotor blades, fuselage, and tailboom. The commercial-rated pilot reported no injuries. Visual meteorological conditions, including light winds with no gusts, prevailed at the time of the accident.

Pilot Account

According to the pilot, he was operating in a confined area and intended to hover to take measurements from a vibration computer. Shortly after transitioning to a hover, the helicopter began to yaw left. Despite the pilot applying right pedal input, the yaw persisted. The pilot then attempted to maneuver the helicopter away from nearby buildings, but the helicopter entered a spin. The pilot recounted that the helicopter completed at least six to eight rotations before a main rotor blade struck a tree, causing the helicopter to fall to the ground.

Inspection Findings

The Federal Aviation Administration (FAA) inspector did not conduct an on-site examination of the helicopter. The pilot subsequently examined the tail rotor drive belts and determined that at least two of the three belts were undamaged. However, the pilot was unable to determine the reason for the loss of tail rotor effectiveness.