No fatalities

30 May 2010: BELL 206B (N6401X) — CITY OF MEMPHIS — Memphis, TN

Memphis, TN, United States

On 30 May 2010, a BELL 206B (registration N6401X) operated by CITY OF MEMPHIS was involved in an aviation accident near Memphis, TN. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain adequate rotor rpm and the certificated flight instructor’s delayed remedial action, which resulted in a hard landing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Bell 206B helicopter, operated by the Memphis Police Department, sustained substantial damage during a practice autorotation at the Memphis Police Department Heliport. The flight instructor and commercial pilot were not injured.

Accident Overview

On May 30, 2010, at approximately 1245 central daylight time, a Bell 206B helicopter, registration N6401X, operated by the City of Memphis Police Department, was substantially damaged during a practice autorotation at the Memphis Police Department Heliport (27TN) in Memphis, Tennessee. The certificated flight instructor and certificated commercial pilot were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The public use training flight was conducted under the provisions of 14 Code of Federal Regulations Part 91.

Maneuver Sequence

According to the flight instructor, after takeoff, the helicopter remained in the traffic pattern to conduct flight maneuvers. After about 20 minutes, as the commercial pilot was climbing the helicopter through approximately 450 feet, the flight instructor rolled the throttle back to flight idle to simulate an engine failure. He then advised the commercial pilot to terminate the maneuver with a power recovery.

The commercial pilot immediately lowered the collective and entered an autorotation. Approximately 100 feet above ground level, the flight instructor advised the commercial pilot to increase the throttle to full power. Shortly thereafter, the flight instructor heard the low rotor warning signal and "got on the controls with the pilot." The flight instructor advanced the throttle to 100 percent power, as both pilots remained on the controls.

Impact and Damage

During the flare, the tail stinger struck the ground, and the helicopter landed hard. The main rotor came into contact with the tail boom aft of the horizontal stabilizer and severed it. Examination by a Federal Aviation Administration inspector revealed that the helicopter came to rest on the helipad, with the tail boom severed aft of the horizontal stabilizer. Examination of the airframe and flight control system components revealed no evidence of preimpact mechanical malfunctions, and neither pilot reported any flight control or engine anomalies.

Contributing factors

CopilotProp/rotor parameters — Not attained/maintainedInstructor/check pilot