N741WB

Substantial
Fatal

W.S. Bowers, Jr. RV-4 S/N: 262

Accident Details

Date
Saturday, October 10, 1998
NTSB Number
ATL99LA007
Location
APOPKA, FL
Event ID
20001211X11202
Coordinates
28.679763, -81.509925
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain airspeed while performing aerobatics which resulted in the lost of control and a stall/spin. A contributing factor was the low altitude at which the maneuver was performed.

Aircraft Information

Registration
N741WB
Make
W.S. BOWERS, JR.
Serial Number
262
Model / ICAO
RV-4

Registered Owner (Historical)

Name
XRAY78 INC
Address
551 N PARK AVE
Status
Deregistered
City
APOPKA
State / Zip Code
FL 32712-3525
Country
United States

Analysis

On October 10, 1998, at 1711 eastern daylight time, an experimental homebuilt RV-4 airplane, N741WB, collided with the ground near Apopka, Florida, while performing an aerobatics maneuver. The personal flight was operated by the pilot under the provisions of Title 14 CFR Part 91, with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. Examination of the airplane at the accident site revealed substantial airframe damage. The private pilot and passenger were fatally injured. The flight departed Bob White Field, in Zellwood, Florida, at 1515.

Witnesses located in the immediate vicinity of the accident site observed the airplane as it entered a loop at a low altitude. As the airplane entered the bottom of the maneuver, the airplane became erratic, partially spun, and collided with the ground in a nose down attitude. According to witnesses, the engine continued to operate throughout the maneuver. Strong fuel fumes existed at the accident site following the impact.

Examination of the accident site by a Federal Aviation Administration (FAA) inspector revealed the airplane fuselage, wing assembly, and empennage were attached to the airframe. Debris from the airplane was distributed evenly around the impact zone in a 360-degree pattern. The airplane was found in a flat attitude with the wing assembly leading edges bent upwards approximately 30 degrees. The fuselage was fractured on the left side aft of the main wing, all control cables were intact, the fuel selector was found in the on position, and the fuel tanks appeared to be ruptured from impact. Examination of the airframe and engine assembly failed to disclose a mechanical problem.

The toxicological examinations performed on the pilot were negative for carbon monoxide, cyanide, ethanol, or drugs.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL99LA007