Casualties unknown

1993-06-09: Enstrom 280C (N51739) — Horizon Helicopters, Inc. — Glen Mills, PA

Glen Mills, PA, US

On June 9, 1993, an Enstrom 280C (registration N51739) operated by Horizon Helicopters, Inc. was involved in an aviation accident near Glen Mills, PA. Investigators recorded the probable cause as: The pilot's inability to arrest the descent rate during the flare, resulting in a hard landing that caused the main rotor blades to sever the tail boom. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A helicopter sustained substantial damage after a hard landing on a grass field during approach. The main rotor blades severed the tail boom, though post-accident inspection revealed no mechanical failure.

What happened

The pilot initiated an approach to a grass field for landing. As he applied power to flare the aircraft for touchdown, he was unable to arrest the descent rate effectively. This resulted in a hard landing impact with the ground.

During the impact, the main rotor blades struck the rear section of the aircraft, cutting the tail boom off from the helicopter fuselage.

The investigation

Following the accident, the Federal Aviation Administration (FAA) conducted an examination of the helicopter to determine if mechanical issues contributed to the event. The post-accident inspection failed to find any evidence of a mechanical failure or malfunction in the aircraft systems prior to the impact.

Findings

The primary factor leading to the damage was the hard landing caused by the pilot's inability to stop the descent during the flare phase. The structural failure of the tail boom was a direct result of the rotor blades contacting it upon impact with the ground, not due to pre-existing mechanical defects.

Probable cause

The pilot's inability to arrest the descent rate during the flare, resulting in a hard landing that caused the main rotor blades to sever the tail boom.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X12695. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.