N123EK

Substantial
None

EKINS PROTECH PT2C PROSTARS/N: PT1213

Accident Details

Date
Thursday, August 12, 1993
NTSB Number
SEA93LA175
Location
NEPHI, UT
Event ID
20001211X13267
Coordinates
39.679973, -111.829177
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE PILOT'S INADEQUATE PREFLIGHT INSPECTION WHICH RESULTED IN LOSS OF ENGINE POWER DUE TO FUEL CONTAMINATION. FACTORS CONTRIBUTING TO THE ACCIDENT WAS THE WET LANDING SURFACE AND TERRAIN CONDITION - DITCH.

Aircraft Information

Registration
N123EK
Make
EKINS
Serial Number
PT1213
Engine Type
Reciprocating
Model / ICAO
PROTECH PT2C PROSTARSA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
EKINS SHIRLEY L
Address
RT 1 BOX 67A GENOLA
Status
Deregistered
City
SANTAQUIN
State / Zip Code
UT 84655
Country
United States

Analysis

On August 12, 1993, at approximately 1125 hours mountain daylight time (MDT), an Ekins & Larsen Protech PT2C Prostar, N123EK, registered to and operated by the owners, and being flown by John D. Brown, a commercially certificated pilot, was substantially damaged during a forced landing and subsequent collision with a fence following a total loss of power immediately after takeoff from runway 16 at the Nephi Municipal Airport, Nephi, Utah. The pilot was uninjured. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was a personal early stage test flight, was to have been operated in accordance with the requirements set forth in 14CFR91, and originated from the Nephi Airport at approximately 1005 hours with approximately 30 gallons of 100 low lead fuel.

The pilot reported that at approximately 300 feet above ground, following a touch and go landing, the engine abruptly stopped operating. The pilot executed a 90 degree right turn to execute a forced landing onto plowed farmland. The pilot reported that "the field had recently been irrigated and the clay soil was extremely slippery" and that "braking was very poor." During the landing roll the aircraft impacted a wood fence and associated log posts, nosing over when the main landing gear separated as it rolled through a concrete drainage culvert.

FAA Inspector Douglas Hanson examined the aircraft subsequent to the accident and reported "extensive fuel contamination in the fuel tank, fuel lines and filters." Additionally, he reported "plastic shavings from the plastic fuel tank in the fuel" and "water and other contaminants in the fuel" (refer to attached FAA Accident Investigation Record).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA93LA175