N526DLBell 206B2008-04-27 NTSB Accident Report

Substantial
None

Bell 206BS/N: 3215

Summary

On April 27, 2008, a Bell 206B (N526DL) was involved in an incident near Murietta, CA. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The flight instructor's inadequate supervision and delayed remedial action. A contributing factor to the accident was the dual student's improper flare.

The commercial pilot receiving instruction reported that during the seventh practice autorotation to landing that day, the helicopter touched down on the aft part of the landing skids and started to roll forward. The pilot stated he applied aft cyclic to prevent the helicopter from rolling forward and one of the main rotor blades subsequently struck the tail boom. The flight instructor stated that he was unable to react in time to level the helicopter prior to touchdown. Examination of the helicopter revealed structural damage to the tail boom and tail rotor drive shaft. No mechanical anomalies were reported with the flight control system.

This incident is documented in NTSB report SEA08CA124. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N526DL.

Accident Details

Date
Sunday, April 27, 2008
NTSB Number
SEA08CA124
Location
Murietta, CA
Event ID
20080528X00741
Coordinates
33.571109, -117.128334
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The flight instructor's inadequate supervision and delayed remedial action. A contributing factor to the accident was the dual student's improper flare.

Aircraft Information

Registration
Make
BELL
Serial Number
3215
Engine Type
Turbo-shaft
Model / ICAO
206BB06
Aircraft Type
Rotorcraft
No. of Engines
1

Analysis

The commercial pilot receiving instruction reported that during the seventh practice autorotation to landing that day, the helicopter touched down on the aft part of the landing skids and started to roll forward. The pilot stated he applied aft cyclic to prevent the helicopter from rolling forward and one of the main rotor blades subsequently struck the tail boom. The flight instructor stated that he was unable to react in time to level the helicopter prior to touchdown. Examination of the helicopter revealed structural damage to the tail boom and tail rotor drive shaft. No mechanical anomalies were reported with the flight control system. The pilot stated in the "how could this accident/incident have been prevented" section of the Pilot/Operator Aircraft Accident Report form, "proper execution of a full down autorotation by fully leveling the aircraft before touchdown."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08CA124