N354MB

Substantial
Minor

Airborne Windsports PTY LTD Edge XS/N: 582-912

Accident Details

Date
Wednesday, June 2, 2010
NTSB Number
WPR10LA275
Location
Alturas, CA
Event ID
20100602X33637
Coordinates
41.483055, -120.565277
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

Fracture of a mast support cable due to corrosion, which resulted in a loss of control during the landing roll.

Aircraft Information

Registration
N354MB
Make
AIRBORNE WINDSPORTS PTY LTD
Serial Number
582-912
Engine Type
None
Year Built
2007
Model / ICAO
Edge XFK9
No. of Engines
0

Registered Owner (Historical)

Name
PARNOW THOMAS G
Address
33540 A HWY 299
Status
Deregistered
City
ALTURAS
State / Zip Code
CA 96101
Country
United States

Analysis

On June 1, 2010, about 1900 Pacific daylight time, an experimental Airborne Windsports PTY LTD Edge X, N354MB, collided with terrain during landing at Alturas, California. The student pilot/owner was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The student pilot sustained minor injuries, and the certified flight instructor (CFI) was not injured. The airplane sustained substantial damage to the wing and wire support bracing. The local instructional flight departed Alturas about 1800. Visual meteorological conditions prevailed, and no flight plan had been filed.

The CFI stated that the student had been practicing touch-and-go landings, and this was to be a final full stop landing. The airplane touched down safely, and was rolling straight at 30 miles per hour. Suddenly and without warning, the wing rolled severely to the left, and struck the ground. The wing crumpled, and dug into the surface. The airplane rolled onto its left side, and skidded to a stop on the runway. The CFI then shut off the ignition, magnetos, and fuel valve.

The CFI indicated that post flight examination revealed that the right rear mast support cable snapped about 3 inches above its lower attachment point. This was at a point where the cable enters a swedge. The cable is covered by the manufacturer with an opaque plastic cover, similar to shrink tubing. He stated that they observed no discrepancies on the cables, welds, engine, wing, suspension, or other components during preflight. They had completed about 12 landings during the day with no indications of a potential problem.

A Federal Aviation Administration (FAA) inspector examined the wreckage, and observed that the right mast to landing gear support cable was broken at the copper compression swedge. There appeared to be some bluish green corrosion on the swedge.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR10LA275