N5297E

Substantial
None

PARK WIZARD S/N: 0010

Accident Details

Date
Monday, August 14, 1995
NTSB Number
FTW95LA343
Location
MINERAL WELLS, TX
Event ID
20001207X04244
Coordinates
32.820606, -98.070236
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A SEIZED ENGINE FOLLOWING THE TOTAL LOSS OF ENGINE COOLANT FROM A LOOSE LINE DUE TO AN INADEQUATE MAINTENANCE INSTALLATION BY THE BUILDER. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

Aircraft Information

Registration
N5297E
Make
PARK
Serial Number
0010
Engine Type
Reciprocating
Model / ICAO
WIZARD BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Status
Deregistered
Country
United States

Analysis

On August 14, 1995, at 1520 central daylight time, a homebuilt Park Wizard, N5297E, collided with a ground structure during a forced landing near Mineral Wells, Texas. The commercial pilot and pilot rated passenger were not injured and the airplane sustained substantial damage. The airplane, operated by the S-TEC Corporation under Title 14 CFR Part 91, departed the Mineral Wells Airport approximately 1515. The purpose of the flight was to flight check several autopilot components manufactured by S-TEC. Visual meteorological conditions prevailed and a flight plan was not filed.

During cruise flight at 2,000 feet MSL, the engine RPM decreased from 7,000 to 5,500 and, subsequently degrading to a complete loss of engine power. A forced landing was made to a playground. During the landing roll, the left wing sustained structural damage when it struck a "baseball backstop."

The airplane was examined by the operator and the Federal Aviation Administration (FAA) inspector. The water cooled engine was "stiff and felt notchy when rotated by hand." An engine coolant line was found loose from the cylinder head fitting and no engine coolant (antifreeze) remained in the radiator. Disassembly of the engine by the operator revealed that the "front cylinder had overheated and the piston had bound up in the cylinder, leaving aluminum scuff marks on the cylinder wall."

An examination of the engine coolant fitting revealed a smooth mating surface with "no mechanical means to retain the rubber coolant hose." Technicians for the operator reported the "fitting appeared as a standard plumbing fitting." According to the engine manufacturer's representative, "all engine and radiator connections distributed by Rotax contain a mechanical means to retain the connections." The FAA experimental airworthiness certificate issued on March 30, 1994, states the airplane was built by Adrian Bloomfield.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA343