- Date
- August 12, 1993, 11:25 local (17:25 UTC)
- Place
- Nephi, UT
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N123EKEkins Protech PT2C Prostar
- Weather
- Visual (VMC) · Day
- Status
- Completed · report August 1, 1994
- Report
- Approved by Office Director
- FAA report
- 19930812029169A
- Case key
- 41748
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
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.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
A total loss of power occurred following a touch and go landing. The pilot executed a forced landing, reporting poor braking on the wet terrain. The main landing gear separated and the aircraft nosed over when it rolled through a concrete drainage culvert. Post accident examination by an FAA inspector revealed fuel contamination.
Factual narrative
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).
Aircraft
- Registration
- N123EK
- Reported as
- Ekins Protech PT2C Prostar (PROTECH PT)
- Category
- Airplane, amateur-built
- Serial number
- PT1213
- Airframe hours
- 7
- Engine
- Lycoming O-360-A2G, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Operator
- Ekins & Larsen
- Registered owner
- Ekins & Larsen
- Airworthiness certificate
- Special, Experimental (Special)
- Last inspection
- Unknown · June 25, 1993 · 7 hours before
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 61
- Certificates
- Flight instructor, Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Left
- Flight hours
- 22,605 total · 5 in this make and model · 22,476 as pilot in command · 105 in the last 90 days · 40 in the last 30 days · 1 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 140° at 4 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 79 °F, dew point 46 °F
- Altimeter
- 30.00 inHg
- Observed at
- PVU, 30 nm away
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.