Casualties unknown

2006-01-26: Eurocopter France AS-350-B2 (N911ES) — Frederick A. Rappleyea Jr. — Port Isabel, TX

Port Isabel, TX, US

On January 26, 2006, an Eurocopter France AS-350-B2 (registration N911ES) operated by Frederick A. Rappleyea Jr. was involved in an aviation accident near Port Isabel, TX. Investigators recorded the probable cause as: The pilot's failure to maintain rotor RPM and his improper touchdown during a simulated hovering autorotation. A contributing factor was the flight instructor's delayed remedial action. 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

During a training flight, a helicopter experienced a hard landing after the instructor initiated a hovering autorotation. The pilot's control inputs were considered excessive, causing a high sink rate. The instructor regained control but the helicopter descended and impacted terrain.

Incident Details

A helicopter flight instructor with 5,591 hours of experience was conducting the second day of training for a newly hired commercial helicopter rated pilot. The pilot had accumulated 10,000 flight hours. The incident occurred after the pilot completed the first landing on Runway 03, which measured 4,999 feet in length and 150 feet in width, with an asphalt-concrete surface.

Flight Profile

Following the landing, the flight instructor directed the pilot to perform an Emergency Medical Service (EMS) takeoff as described in the company's operations manual, followed by entry into the local traffic pattern. According to the instructor, the EMS takeoff procedure required the pilot to bring the helicopter to a hover at an altitude of three to five feet to conduct a power check before applying takeoff power.

Instructor's Account

While the helicopter was stationary in a hover, the flight instructor initiated a hovering autorotation. The pilot immediately responded by applying forward cyclic and then pulling up on the collective. The flight instructor assessed the pilot's control inputs as excessive, resulting in a high rate of descent and an undesirable helicopter attitude for touchdown. The instructor then took control of the aircraft, bringing it back to a level attitude in an attempt to cushion the landing.

The flight instructor reported that the main rotor RPM was low and that most of the collective had been used to prevent a nose-low impact. The helicopter subsequently descended approximately one to two feet, making contact with the terrain in a level attitude before bouncing forward about four feet.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060209X00183. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.