N817EV

Substantial
None

EVEKTOR-AEROTECHNIK AS SPORTSTARS/N: 20070817

Accident Details

Date
Thursday, March 20, 2014
NTSB Number
WPR14LA141
Location
Porterville, CA
Event ID
20140321X00837
Coordinates
36.030834, -119.059722
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The student pilot’s failure to maintain directional control during takeoff.

Aircraft Information

Registration
Make
EVEKTOR-AEROTECHNIK AS
Serial Number
20070817
Engine Type
4-cycle
Year Built
2007
Model / ICAO
SPORTSTAREVSS
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SPORTSTAR

Registered Owner (Current)

Name
SECOND ICARIAN CHURCH OF AVIATION LLC
Address
1623 DOROTHY LN
City
YUBA CITY
State / Zip Code
CA 95993-5256
Country
United States

Analysis

On March 20, 2014, about 1650 Pacific daylight time, an Evektor-Aerotechnik-AS Sportstar, N817EV, was substantially damaged during takeoff from the Porterville Municipal Airport, Porterville, California. The airplane was registered to and operated by Lighten Up Aviation LLC. under the provisions of Title 14 Code of Federal Regulations Part 91. The student pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local instructional flight. The flight was originating at the time of the accident.

In a written statement to the National Transportation Safety Board investigator-in-charge the student reported that during takeoff on runway 30, as the airplane accelerated past about 30 miles per hour, he felt it dip to the right. The pilot stated that when he reduced throttle and applied brakes, the airplane suddenly spun to the left and exited the runway.

A witness, located adjacent to the accident site, reported that he observed the airplane veer to the left and the right wing drop during the takeoff roll. The witness stated that he heard the engine reduce in power, and observed the right main landing gear begin to "flip around" as the airplane exited the left side of the runway. He added that the airplane came to rest adjacent to the runway opposite the direction of takeoff, and that the right main landing gear had separated.

Recorded weather information revealed that about 5 minutes after the accident, wind was from 290 degrees at 6 knots. About 20 minutes after the time of the accident, wind was from 270 degrees at 7 knots.

Postaccident examination of the airplane by a Federal Aviation Administration inspector revealed that the right main landing gear was separated and the right wing was bent up slightly about mid-span. The inspector stated that examination of the airplane did not reveal any preexisting mechanical anomalies that would have precluded normal operation. The inspector reported that skid marks, consistent with a left skidding turn, were observed on the runway surface.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR14LA141