N123SDBell 206A2007-11-21 NTSB Accident Report

Substantial
None

Bell 206AS/N: MB-1

Summary

On November 21, 2007, a Bell 206A (N123SD) was involved in an incident near Twin Falls, ID. 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 pilot misjudged the flare which resulted in a hard landing.

The pilot indicated that the purpose of the flight was to finish the post annual flight check and to check the autorotational rpm during a simulated engine out condition. The pilot was flying in the left seat and there was an observer in the right seat. He entered a 180-degree autorotation and at 70 feet above ground level, began a gradual flare. During the flare, the helicopter contacted the asphalt surface of the taxiway. The helicopter hopped and then came to a stop. The pilot initiated another pattern and power recovery autorotation. He then hover taxied to the maintenance hangar ramp area and performed a normal shutdown. Post flight inspection revealed a wrinkle in the tail boom.

This incident is documented in NTSB report SEA08CA037. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N123SD.

Accident Details

Date
Wednesday, November 21, 2007
NTSB Number
SEA08CA037
Location
Twin Falls, ID
Event ID
20071203X01890
Coordinates
42.481945, -114.471107
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot misjudged the flare which resulted in a hard landing.

Aircraft Information

Registration
Make
BELL
Serial Number
MB-1
Engine Type
Turbo-shaft
Year Built
2013
Model / ICAO
206AB06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
IVES TYLER M
Address
1206 S 1680 W
Status
Deregistered
City
OREM
State / Zip Code
UT 84058-4938
Country
United States

Analysis

The pilot indicated that the purpose of the flight was to finish the post annual flight check and to check the autorotational rpm during a simulated engine out condition. The pilot was flying in the left seat and there was an observer in the right seat. He entered a 180-degree autorotation and at 70 feet above ground level, began a gradual flare. During the flare, the helicopter contacted the asphalt surface of the taxiway. The helicopter hopped and then came to a stop. The pilot initiated another pattern and power recovery autorotation. He then hover taxied to the maintenance hangar ramp area and performed a normal shutdown. Post flight inspection revealed a wrinkle in the tail boom.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08CA037