Casualties unknown

Helicopter Damaged During Landing Following Engine Power Loss (N1020Q)

Omaha, NE, US

On November 5, 2005, a Hughes 269A (registration N1020Q) was involved in an aviation accident near Omaha, NE. Investigators recorded the probable cause as: The loss of engine power for an undetermined reason and the pilot's improper execution of the emergency procedure which resulted in an excessive descent rate and subsequent hard landing. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A helicopter was damaged during landing after the pilot reported a loss of engine power on approach. Attempted autorotation was complicated by a sudden power recovery and adverse yaw, resulting in ground impact. Postaccident examination found no pre-impact anomalies.

Incident Overview

A helicopter sustained damage during a landing after the pilot reported a loss of engine power. The incident occurred as the aircraft was on approach to a hover. The pilot described the sequence of events in a statement following the event.

Pilot's Account

The pilot reported that while passing through 60 feet above ground level during the approach, the engine lost power. He stated that he pulled back on the cyclic to slow down and initiate autorotation, and began to roll off the throttle and lower the collective. According to the pilot, almost immediately after these actions, engine power returned and the rotor rpm needles joined, accompanied by a yawing motion of the aircraft. He attempted to apply power and recover from the situation, but reported that his rate of descent, low altitude, and adverse yaw complicated the recovery. Subsequently, the helicopter impacted the ground and slid to a stop.

Postaccident Examination

Following the incident, a postaccident examination of the helicopter was conducted. The examination failed to reveal any pre-impact anomalies. No mechanical or system malfunctions were identified that could explain the reported loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20051219X01991. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.