N234JD

Substantial
Minor

Jackie SNS-7-Hiperbipe 3S/N: 234

Accident Details

Date
Saturday, July 6, 2002
NTSB Number
FTW02LA202
Location
Lancaster, TX
Event ID
20020710X01080
Coordinates
32.712501, -96.718887
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain adequate airspeed which resulted in an inadvertent stall. A contributing factor was the pilot's failure to maintain directional control during takeoff roll.

Aircraft Information

Registration
N234JD
Make
JACKIE
Serial Number
234
Year Built
1982
Model / ICAO
SNS-7-Hiperbipe 3

Registered Owner (Historical)

Name
CLEMENTS LLOYD G
Address
900 SOUTHWOOD DR
Status
Deregistered
City
DE SOTO
State / Zip Code
TX 75115
Country
United States

Analysis

On July 6, 2002, approximately 0845 central daylight time, a Jackie SNS-7-Hiperbipe 3 experimental single-engine airplane, N234JD, sustained substantial damage after impacting terrain following a loss of control during takeoff/initial climb at the Lancaster Airport, Lancaster, Texas. The airplane was owned and operated by the pilot. The private pilot, sole occupant of the airplane, sustained minor injuries. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 91 personal flight, and no flight plan was filed. The flight was originating at the time of the accident.

In a telephone interview with the NTSB investigator-in-charge, the pilot reported that on takeoff roll from runway 13, the airplane swerved "for some reason" to the left. The pilot further stated that he must have over corrected by applying right brake or rudder. The airplane then swerved to the right across the runway and became airborne. Approximately 15 feet agl, due to "lack of airspeed," the airplane stalled and impacted the ground with its left wing. Subsequently, the airplane's right wing hit the ground, separating it from the fuselage. The pilot stated that the airplane came to rest upright approximately 100 yards to the right side and perpendicular to the runway.

An FAA inspector, who traveled to the accident site, reported the right wing had separated, the propeller was bent and twisted, and both main gear were folded up underneath the fuselage.

At 0853, the Redbird Automatic Surface Observing System, located 10 nautical miles northwest of the accident site, reported wind calm, visibility 8 statute miles, sky clear, temperature 25 degrees Centigrade, dew point 22 degrees Centigrade, with an altimeter setting of 30.09 inches of mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA202