N41BB

Destroyed
Serious

Wallace SkyboltS/N: 1

Accident Details

Date
Wednesday, March 17, 2004
NTSB Number
LAX04LA163
Location
Reno, NV
Event ID
20040324X00366
Coordinates
39.692779, -119.961944
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Failure of the left wing spar during an aerobatic maneuver.

Aircraft Information

Registration
N41BB
Make
WALLACE
Serial Number
1
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
SkyboltSBM3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LOUDON ROSS W TRUSTEE
Address
1577 BELFORD RD
Status
Deregistered
City
RENO
State / Zip Code
NV 89509-3907
Country
United States

Analysis

On March 17, 2004, about 0720 Pacific standard time, an experimental Wallace Skybolt, N41BB, experienced an in-flight breakup while executing an aerobatic maneuver near Reno/Stead Airport (4SD), Reno, Nevada. The owner/pilot was operating the airplane under the provisions of 14 CFR Part 91. The private pilot, the sole occupant, sustained serious injuries; the airplane was destroyed. The personal local flight departed Stead about 0645. Visual meteorological conditions prevailed, and no flight plan had been filed. The primary wreckage was at 39 degrees 41.34 minutes north latitude and 119 degrees 57.43 minutes west longitude.

The Federal Aviation Administration (FAA) accident coordinator responded to the accident scene. He interviewed the pilot on March 25, 2004.

The pilot reported that he was executing an aerobatic outside loop maneuver. During the bottom of the loop, while inverted, his airspeed was about 160 mph, and he was about 8,000 feet mean sea level (msl). While pushing forward on the stick to about -2.5G to start the ascending part of the maneuver, the airplane began to vibrate violently. The pilot felt the vibration in the airframe, not in the stick or the rudder. He felt the vibration for 1 to 2 seconds, followed by the left wing of the airplane detaching from the airplane's structure.

During the airplane's continued disintegration, the pilot was able to release his seat belt and exit the airplane. The pilot deployed his parachute, which opened just prior to his impacting the ground.

The airplane received its original experimental certification in January 1975. Subsequently, the airplane received annual condition inspections. In January 1979, at 307 hours total time, the airplane was disassembled, inspected/repaired, and reassembled/recovered. In March 2000, a larger engine/prop combination was installed. In January 2001, at 733 hours total time, the airframe only was disassembled, inspected, and repaired as necessary, and reassembled/recovered. The wings were not disassembled, inspected, repaired or recovered.

According to the accident airplane's records and the pilot's statement, it had been more than 20 years since the wings had undergone any extensive inspection, repair, or rebuild with the fabric removed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX04LA163