Casualties unknown

2003-08-02: Enstrom F-28C (N15SA) — Spitfire Aerospace Technologies Inc. — Kankakee, IL

Kankakee, IL, US

On August 2, 2003, an Enstrom F-28C (registration N15SA) operated by Spitfire Aerospace Technologies Inc. was involved in an aviation accident near Kankakee, IL. Investigators recorded the probable cause as: The pilot misjudged flare which led to a hard landing. Contributing to the accident was the pilot's failure to follow procedures/directives when he exceeded the airplane's weight and balance. 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 1781061362Data APIEditorial standards
Aircraft registered N15SA
Aircraft registered N15SA. Photo: Unknown author Unknown author / Public domain, via Wikimedia Commons

A sightseeing helicopter sustained substantial damage when its main rotor struck the tail rotor drive shaft during landing in a fairground parking lot. Passengers reported minor injuries; the pilot was uninjured.

Accident Overview

A sightseeing observation helicopter was substantially damaged during a landing at a county fairground parking lot. The accident occurred when the main rotor contacted the tail rotor drive shaft, causing the latter to separate from the helicopter. The separated tail rotor drive shaft then struck the rear window of a parked vehicle. Three passengers reported minor injuries, while the pilot stated that he was uninjured.

Pilot Statement

The pilot described the approach as a stabilized steep descent to the landing area. He noted that upon detecting ground contact with the helicopter skids, he lowered the collective, at which point the helicopter dropped and lunged forward. The landing site was a nearly level area covered with 2-3 inch tall grass.

Environmental Conditions

The wind at the time of the accident was from 170 degrees at 7 knots.

Examination Findings

An on-scene examination of the helicopter revealed no pre-impact anomalies. The helicopter's flight manual specified that the cabin interior featured a full, three-place, side-by-side seating arrangement. The helicopter's center of gravity range was 92.0 to 100 inches, while the operator's calculated center of gravity was 91.74 inches.

Damage Assessment

The helicopter sustained substantial damage from the main rotor impact with the tail rotor drive shaft. The tail rotor drive shaft separated from the aircraft and damaged a parked vehicle's rear window.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030805X01267. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.