N126DT

Substantial
None

Tillman Long EZS/N: 1264L

Accident Details

Date
Wednesday, March 13, 2002
NTSB Number
FTW02LA093
Location
Lockhart, TX
Event ID
20020327X00405
Coordinates
29.850555, -97.676391
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N126DT
Make
TILLMAN
Serial Number
1264L
Year Built
1989
Model / ICAO
Long EZ

Registered Owner (Historical)

Name
TILLMAN DONALD E
Address
625 SPERRY LOOP
Status
Deregistered
City
WAHIAWA
State / Zip Code
HI 96786
Country
United States

Analysis

On March 12, 2002, at 1800 central standard time, a Tillman Long EZ homebuilt experimental airplane, N126DT, was substantially damaged during a forced landing following a loss of engine power during initial takeoff climb near Lockhart, Texas. The commercial pilot, who was the sole occupant, was not injured. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight departed the Lockhart Municipal Airport, Lockhart, at 1757.

The pilot reported that he had not flown the airplane in approximately three weeks and planned to fly the airplane around the traffic pattern. The pilot performed a preflight inspection, taxied the airplane to runway 36, and then performed a "normal" engine run-up prior to takeoff. Shortly after takeoff, approximately 200 feet agl, the engine began to lose power. The pilot "switched tanks, checked the mixture, and jockeyed the throttle a couple of times," with no response from the engine. Unable to make the runway, the pilot initiated a forced landing to a field. During the landing, the airplane struck a fence separating the right wing and right main landing gear. The pilot stated that the airplane contained approximately 20 gallons of fuel prior to takeoff.

According to an FAA inspector, who responded to the accident site, he and the pilot performed a field inspection on the engine. Both the magnetos produced spark at the spark plugs, valve train continuity was established, and the engine cylinders produced compression. The carburetor contained fuel, which was clean and free of contaminants. No anomalies with the engine or airframe were noted during the examination. The reason for the loss of engine power was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA093