N407SHBell 4072006-08-19 NTSB Accident Report

Substantial
None

Bell 407S/N: 53045

Summary

On August 19, 2006, a Bell 407 (N407SH) was involved in an incident near Havre, MT. All 1 person aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot inadvertently allowing the helicopter to enter into a vortex ring state (settling with power) condition while he was lowering a long-line load to the ground, resulting in the helicopter settling to the ground and its tail rotor impacting part of the rigging used to haul the load. Factors include the long-line load and its rigging sitting on the ground at the point where the helicopter settled to the terrain.

The pilot, who was approaching an area where he was going to place a long-line load onto the terrain, inadvertently allowed the helicopter to enter into a vortex ring state (settling with power) condition, resulting in his inability to keep the helicopter from descending at a rate that resulted in it hitting the ground and bouncing back into the air. At the point in time when it contacted the ground with its skids, the helicopter's tail rotor impacted a portion of the rigging for the load that it had been hauling, which resulted in substantial damage to the tail rotor and the tail rotor drive shaft.

This incident is documented in NTSB report SEA06CA165. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N407SH.

Accident Details

Date
Saturday, August 19, 2006
NTSB Number
SEA06CA165
Location
Havre, MT
Event ID
20060913X01334
Coordinates
48.190261, -114.379692
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot inadvertently allowing the helicopter to enter into a vortex ring state (settling with power) condition while he was lowering a long-line load to the ground, resulting in the helicopter settling to the ground and its tail rotor impacting part of the rigging used to haul the load. Factors include the long-line load and its rigging sitting on the ground at the point where the helicopter settled to the terrain.

Aircraft Information

Registration
Make
BELL
Serial Number
53045
Engine Type
Turbo-shaft
Year Built
2014
Model / ICAO
407B407
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
8
FAA Model
407

Registered Owner (Current)

Name
STANISLAUS COUNTY
Address
250 E HACKETT RD
City
MODESTO
State / Zip Code
CA 95358-9415
Country
United States

Analysis

The pilot, who was approaching an area where he was going to place a long-line load onto the terrain, inadvertently allowed the helicopter to enter into a vortex ring state (settling with power) condition, resulting in his inability to keep the helicopter from descending at a rate that resulted in it hitting the ground and bouncing back into the air. At the point in time when it contacted the ground with its skids, the helicopter's tail rotor impacted a portion of the rigging for the load that it had been hauling, which resulted in substantial damage to the tail rotor and the tail rotor drive shaft.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA06CA165