N707WHRobinson R222007-07-17 NTSB Accident Report

Substantial
None

Robinson R22S/N: 2814

Summary

On July 17, 2007, a Robinson R22 (N707WH) was involved in an incident near Bend, OR. 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: An excessive descent rate during a simulated power-off autorotation, and the pilot's failure to initiate corrective action in time to keep the helicopter from impacting the terrain.

After completing five or six successful simulated power-off autorotations, the pilot entered an autorotation in which he allowed the helicopter's descent rate to become excessive. Although he attempted to take corrective action, he did not do so in time to keep the aircraft from contacting an asphalt surface with sufficient force to result in substantial damage to the helicopter's airframe.

This incident is documented in NTSB report SEA07CA205. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N707WH.

Accident Details

Date
Tuesday, July 17, 2007
NTSB Number
SEA07CA205
Location
Bend, OR
Event ID
20070808X01143
Coordinates
44.094722, -121.200553
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

An excessive descent rate during a simulated power-off autorotation, and the pilot's failure to initiate corrective action in time to keep the helicopter from impacting the terrain.

Aircraft Information

Registration
Make
ROBINSON
Serial Number
2814
Engine Type
Reciprocating
Model / ICAO
R22R22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
HELICO LLC
Address
63048 POWELL BUTTE HWY
Status
Deregistered
City
BEND
State / Zip Code
OR 97701-9739
Country
United States

Analysis

After completing five or six successful simulated power-off autorotations, the pilot entered an autorotation in which he allowed the helicopter's descent rate to become excessive. Although he attempted to take corrective action, he did not do so in time to keep the aircraft from contacting an asphalt surface with sufficient force to result in substantial damage to the helicopter's airframe.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA07CA205