N5178DPreceptor Aircraft Ultra pup2002-12-22 NTSB Accident Report

Substantial
None

Preceptor Aircraft Ultra pupS/N: 1223

Summary

On December 22, 2002, a Preceptor Aircraft Ultra pup (N5178D) was involved in an incident near Smithville, TN. All 1 person aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's inadequate preflight fuel planning of fuel resulted in fuel starvation, the total loss of engine power and the subsequent forced landing.

On December 22, 2002, at 1450 eastern standard time, an experimental Preceptor Ultra Pup, N5178D, registered to and operated by a private owner, experienced a loss of engine power and collided with the ground near Smithville, Tennessee. The personal flight was operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of accident. The airplane sustained substantial damage, and the private pilot received minor injuries. The flight departed Evansville Regional Airport, Evansville, Indiana on December 22, 2002 at 1255 central standard time.

According to the pilot, he had just purchased the airplane and was returning to his home base.

This incident is documented in NTSB report ATL03LA026. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N5178D.

Accident Details

Date
Sunday, December 22, 2002
NTSB Number
ATL03LA026
Location
Smithville, TN
Event ID
20030103X00006
Coordinates
35.985279, -85.809165
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 fuel planning of fuel resulted in fuel starvation, the total loss of engine power and the subsequent forced landing.

Aircraft Information

Registration
Make
PRECEPTOR AIRCRAFT
Serial Number
1223
Engine Type
Reciprocating
Year Built
2002
Model / ICAO
Ultra pupAT2P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
2335 LINDEN AVE
Status
Deregistered
City
BOULDER
State / Zip Code
CO 80304-1618
Country
United States

Analysis

On December 22, 2002, at 1450 eastern standard time, an experimental Preceptor Ultra Pup, N5178D, registered to and operated by a private owner, experienced a loss of engine power and collided with the ground near Smithville, Tennessee. The personal flight was operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of accident. The airplane sustained substantial damage, and the private pilot received minor injuries. The flight departed Evansville Regional Airport, Evansville, Indiana on December 22, 2002 at 1255 central standard time.

According to the pilot, he had just purchased the airplane and was returning to his home base. Approximately 14 miles from the Smithville Municipal Airport, Smithville, Tennessee, the engine began to run rough. The pilot applied carburetor heat, and the engine stopped. The pilot executed an emergency landing in a rough and uneven field; the airplane collided with a fence during the landing roll.

Examination of the airplane revealed that the main landing gear separated from the airframe, and the right wing was partially separated from the fuselage. No fuel was found in the left or right wing tanks. Three gallons of fuel was drained from the header tank, and no blockages were observed. The fuel gascolator under the header tank was empty. The pilot did not report any mechanical or flight control malfunctions prior to the flight.

The pilot stated that he preflight planned for 2.5 hours, a fuel capacity of 12 gallons. The pilot had been flying for approximately 2 hours. Additionally, the airplane did not have an electrical system installed or an engine driven fuel pump, but there was an electric power fuel pump installed. The examination of the electric fuel pump system revealed that the battery power pack was discharged. According to the builder, the electrical fuel pump was used to supply additional pressure to the fuel system.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL03LA026