N2061D

Substantial
None

Schweizer 269DS/N: 0034A

Accident Details

Date
Thursday, May 3, 2001
NTSB Number
SEA01LA082
Location
Nampa, ID
Event ID
20010507X00894
Coordinates
43.600444, -116.609977
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's inadequate compensation for strong, gusty, shifting winds while hovering in ground effect. Factors include a sudden directional change and increase in velocity of the gusty wind conditions.

Aircraft Information

Registration
N2061D
Make
SCHWEIZER
Serial Number
0034A
Engine Type
Reciprocating
Year Built
2001
Model / ICAO
269DH269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BEELER DIANE
Address
440 CLAIRE DR NE
Status
Deregistered
City
ATLANTA
State / Zip Code
GA 30307-1828
Country
United States

Analysis

On May 3, 2001, approximately 1715 mountain daylight time, a Schweizer 269D, N2061D, collided with a gas island light pole while hovering at Nampa Municipal Airport, Nampa, Idaho. The private pilot, who was the sole occupant, was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. At the time of the accident, the aircraft was hovering over its parking location near the fuel island just prior to initiating taxi for a CFR Part 91 personal pleasure flight to Twin Falls, Idaho. The accident occurred in visual meteorological conditions. No flight plan had been filed.

According to the pilot, he lifted off and was hovering about one foot above the ground while visually clearing the area prior to initiating his taxi to the runway. As he looked out to his right he noticed a "twirl" of dust and small trees that were "laying over." He also noticed that the wind sock seemed to be standing straight out. Soon thereafter the helicopter encountered a "severe wind" that, according to the pilot, lifted the aircraft six feet in the air, and required him to reverse his slightly left anti-torque pedal input to a full right input. His initial reaction was to transition to forward flight, but after initially starting to do so, he "dropped" the collective in an attempt to put the helicopter back on the ground. While he was trying to land, the aircraft weathervaned into the wind and started to drift backwards toward the fuel pump island. At that time, the pilot applied forward cyclic in order to stop the helicopter from moving backwards, but he was unable to arrest the drift prior to the tail boom impacting the fuel island light pole.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA01LA082