N53ET

Substantial
Minor

Theis QUICKIE S/N: 007

Accident Details

Date
Wednesday, April 2, 1997
NTSB Number
IAD97LA061
Location
FOSTORIA, OH
Event ID
20001208X07727
Coordinates
41.150325, -83.410232
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

a disconnect of electrical wires to the engine ignition, which resulted in loss of engine power and a forced landing. Factors relating to the accident were: the lack of suitable terrain for a forced landing, and the wheat (crop) that was encountered during the landing.

Aircraft Information

Registration
N53ET
Make
THEIS
Serial Number
007
Engine Type
Reciprocating
Model / ICAO
QUICKIE SBM3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
THEIS ROBERT A
Address
2473 US 23 NORTH
Status
Deregistered
City
FOSTORIA
State / Zip Code
OH 44830
Country
United States

Analysis

On April 2, 1997, at 1700 eastern standard time, N53ET, a Theis Quickie, a homebuilt airplane, was substantially damaged after it impacted terrain near Fostoria, Ohio. The certificated airline transport pilot received minor injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the local, personal flight conducted under 14 CFR Part 91. The flight originated in Fostoria, Ohio.

According to the pilot, shortly after takeoff from runway 27, at 100 feet AGL, the engine lost power. During the forced landing in a wheat field, the airplane nosed over.

The airplane was examined at the accident site by a Federal Aviation Administration (FAA) Inspector. The examination revealed fuel in the fuel line, and in the carburetor. Engine continuity was confirmed; however, there was no spark when the engine was rotated by hand.

Examination of the cockpit ignition switch revealed that the two wires that provide battery power to the engine ignition unit were separated from the switch. When the two wires were re-connected, the ignition system operated satisfactory.

The ignition switch was located in the instrument panel, which was a part of the canopy that rotated approximately 90 degrees when it opened. The wire routing, from the switch to the engine ignition unit ran along the right side of the cockpit, the same side the canopy was hinged. There was impact damage in this area, and it was not determined if the wires separated during the impact.

According to the FAA, the wire routing was observed to be tight, without much slack to accommodate the travel of the switch when the canopy was opened. When the canopy was opened, there was stress on the ignition wires, and on the switch.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# IAD97LA061