N16HA

Substantial
Serious

BELL 206BS/N: 3229

Accident Details

Date
Monday, November 14, 2011
NTSB Number
WPR12LA036
Location
Woodburn, OR
Event ID
20111115X85553
Coordinates
45.136112, -122.823333
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s failure to maintain ground clearance while maneuvering with an external load line.

Aircraft Information

Registration
N16HA
Make
BELL
Serial Number
3229
Engine Type
Turbo-shaft
Year Built
1981
Model / ICAO
206BB06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
APPLEBEE AVIATION INC
Address
PO BOX 309
Status
Deregistered
City
BANKS
State / Zip Code
OR 97106-0309
Country
United States

Analysis

On November 14, 2011, about 1430 Pacific standard time a Bell 206B, N16HA, collided with terrain during an external load operation near Woodburn, Oregon. Applebee Aviation was operating the helicopter under the provisions of 14 Code of Federal Regulations (CFR) Part 133. The commercial pilot was seriously injured. The helicopter sustained substantial damage to the forward fuselage and tail boom during the accident sequence. The local flight departed from a road in Oregon City, Oregon, about 2 hours prior to the accident. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot reported that he was lifting bundles of Christmas trees from a field to a loading zone, utilizing a 25-foot-long steel line. Shortly after lifting a load, the bundle came apart and fell from the line. The pilot then lowered the helicopter so ground personable could reattach the bundle, but they had already moved to the next bundle of trees. The pilot then raised the helicopter, and as he did, the line became snagged on an obstacle on the ground. The pilot immediately reached for the line release switch, but the line did not detach. The helicopter pitched down, descended, and collided with terrain. The pilot could not definitively confirm that the release system failed, stating it was possible that he did not make positive contact with the release switch. He further stated that he did not have enough time to engage the manual backup release system.

An inspector from the Federal Aviation Administration (FAA) examined the helicopter at the accident site. He inspected both the electrically operated release mechanism, and the manual backup release system. No anomalies were found that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12LA036