N1LM

Substantial
None

Abernathy STREAKER S/N: 1

Accident Details

Date
Tuesday, September 5, 2000
NTSB Number
FTW00LA254
Location
SHERMAN, TX
Event ID
20001212X21975
Coordinates
33.610576, -96.600715
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the wing skin and the rear spar while performing aerobatics, which resulted in the restricted movement of the aileron.

Aircraft Information

Registration
Make
ABERNATHY
Serial Number
1
Engine Type
Reciprocating
Year Built
1983
Model / ICAO
STREAKER FK9
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
STREAKER

Registered Owner (Current)

Name
ARMSTRONG ROBERT B
Address
PO BOX 239
City
BISHOP
State / Zip Code
GA 30621-0239
Country
United States

Analysis

On September 5, 2000, approximately 1130 central daylight time, an Abernathy Streaker aerobatic experimental biplane, N1LM, was substantially damaged while maneuvering near Sherman, Texas. The commercial pilot, sole occupant of the airplane, was not injured. The airplane was registered to a private individual and operated by the pilot. Visual meteorological conditions prevailed and no flight plan was filed for the 14 Code of Federal Regulation Part 91 personal flight. The local flight originated from the Grayson County Airport, Sherman, Texas, at 1123.

According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), and a telephone interview conducted by the NTSB investigator-in-charge, the pilot departed Grayson County Airport for the first of three aerobatic contest flights. At 4,300 feet agl, the pilot began a 45 degree nose down dive into the "aerobatic box". After the "second wing wag (used to signify the start of aerobatic performance)," the airplane experience a "high rate" roll to the right. The pilot reported that the right aileron "jammed," however, he eventually regained control of the airplane, and landed it on runway 17L without further incident.

Examination of the airplane by the pilot revealed that the skin on the top of the right wing failed and separated from the rear spar. The rear spar was buckled and the aileron's leading edge was "jammed," in the full up position, under the wing's trailing edge.

The airplane had accumulated 1,123 hours of total flight time at the time of the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW00LA254