N439MMQUICKSILVER SPORT 2S2010-04-09 NTSB Accident Report

Substantial
None

QUICKSILVER SPORT 2SS/N: 0189

Summary

On April 09, 2010, a Quicksilver SPORT 2S (N439MM) was involved in an incident near Canton, TX. 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 airplane builder’s improper installation of the left rear wing strut eyebolt.

While in a turn at low altitude, the pilot of the open cockpit experimental airplane heard a “loud pop,” followed by a change in the feel of the flight controls. The pilot elected to reduce the engine power to idle and activate the ballistic recovery system (BRS). Seconds later the airplane impacted into an area of trees and came to rest in the trees near the ground. The pilot was able to exit the airplane unassisted. An examination of the wreckage revealed that the left wing rear strut threaded eyebolt had pulled free from the threaded barrel of the wing strut. The thread-to-barrel engagement was measured at 5/32 of an inch with approximately 16 threads exposed.

This incident is documented in NTSB report CEN10CA200. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N439MM.

Accident Details

Date
Friday, April 9, 2010
NTSB Number
CEN10CA200
Location
Canton, TX
Event ID
20100412X71830
Coordinates
32.578056, -95.871391
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The airplane builder’s improper installation of the left rear wing strut eyebolt.

Aircraft Information

Registration
Make
QUICKSILVER
Serial Number
0189
Engine Type
Reciprocating
Model / ICAO
SPORT 2SSA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
444 E RENFRO ST APT 2106
Status
Deregistered
City
BURLESON
State / Zip Code
TX 76028-4353
Country
United States

Analysis

While in a turn at low altitude, the pilot of the open cockpit experimental airplane heard a “loud pop,” followed by a change in the feel of the flight controls. The pilot elected to reduce the engine power to idle and activate the ballistic recovery system (BRS). Seconds later the airplane impacted into an area of trees and came to rest in the trees near the ground. The pilot was able to exit the airplane unassisted. An examination of the wreckage revealed that the left wing rear strut threaded eyebolt had pulled free from the threaded barrel of the wing strut. The thread-to-barrel engagement was measured at 5/32 of an inch with approximately 16 threads exposed. Per the manufacturer’s assembly manual, the eyebolt was to have a minimum of 5/8 of an inch thread-to-barrel engagement with approximately three-and-a-half threads exposed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10CA200