N469SAHAEUSSLER RAY SONEX2010-11-29 NTSB Accident Report

Substantial
None

HAEUSSLER RAY SONEXS/N: 0206

Summary

On November 29, 2010, a Haeussler Ray SONEX (N469SA) was involved in an incident near Buffalo, NY. 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's failure to maintain directional control during takeoff due to his abrupt advancing of the throttle.

The pilot stated that, when starting to takeoff in the tailwheel-equipped airplane he immediately applied full throttle and lost control of the airplane. The airplane departed the runway to the left and impacted a visual approach slope indicator control box, resulting in substantial damage to the right wing spar. The pilot reported that there were no mechanical malfunctions or anomalies with the airplane, and said that the accident may have been prevented if he had applied the throttle gradually.

This incident is documented in NTSB report ERA11CA092. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N469SA.

Accident Details

Date
Monday, November 29, 2010
NTSB Number
ERA11CA092
Location
Buffalo, NY
Event ID
20101216X10638
Coordinates
42.861946, -78.716392
Nearest Airport
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 failure to maintain directional control during takeoff due to his abrupt advancing of the throttle.

Aircraft Information

Registration
Make
HAEUSSLER RAY
Serial Number
0206
Engine Type
None
Year Built
2002
Model / ICAO
SONEXFEST
No. of Engines
0

Registered Owner (Historical)

Name
FLY LITE INC
Address
248 WOOD ACRES DR
Status
Deregistered
City
EAST AMHERST
State / Zip Code
NY 14051-1759
Country
United States

Analysis

The pilot stated that, when starting to takeoff in the tailwheel-equipped airplane he immediately applied full throttle and lost control of the airplane. The airplane departed the runway to the left and impacted a visual approach slope indicator control box, resulting in substantial damage to the right wing spar. The pilot reported that there were no mechanical malfunctions or anomalies with the airplane, and said that the accident may have been prevented if he had applied the throttle gradually.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA11CA092