Casualties unknown

2006-01-13: Bell 47-B3 (N1575) — Dennison, TX

Dennison, TX, US

On January 13, 2006, a Bell 47-B3 (registration N1575) was involved in an aviation accident near Dennison, TX. Investigators recorded the probable cause as: The in-flight separation of the stabilizer bar tube. 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

A 4,900-hour commercial pilot was maneuvering a single-engine helicopter on a photo mission when a loud bang and erratic cyclic movement occurred. The pilot landed in a football field via autorotation; no injuries.

Incident Overview

A commercial pilot with 4,900 hours of flight experience was operating a single-engine helicopter during a photographic mission. The aircraft was at an altitude of approximately 1,500 feet mean sea level (MSL) and an indicated airspeed of about 45 knots when the pilot heard a loud bang and simultaneously felt erratic movement in the cyclic control.

Pilot Actions

Immediately after the event, the pilot began searching for a suitable landing area. He increased airspeed and proceeded toward a vacant football field. As the helicopter approached the field on final, the airspeed decayed and the helicopter began to spin. The pilot then opted to execute an autorotation. The helicopter landed upright with no further damage.

Occupant Status

The pilot and his passenger were not injured.

Post-Inspection Findings

An FAA inspector who examined the accident site reported that one stabilizer tube from the mast control stabilizer bar assembly had separated from the main rotor system. After separation, the tube struck the tail rotor assembly. Approximately 3 inches of one tail rotor blade was found fractured, and the 90-degree tail rotor gear box had separated from the tail rotor drive shaft.

Weather Conditions

At the time of the incident, the wind was reported from 360 degrees at 22 knots, gusting to 29 knots.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060228X00254. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.