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Aviation safety reports, made easier to study

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NTSB Report

April 2, 1997 · Theis Quickie · N53ET

Fostoria, OH

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 2, 1997
Injury Outcomes
1 injury (1 minor injury)
Location
Fostoria, OH
Aircraft
Theis Quickie
Tail Number
N53ET
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
IAD97LA061

According to the pilot, shortly after takeoff at about 100 feet AGL, the engine lost power. During a subsequent forced landing, the airplane nosed over in a wheat field. Examination of the airplane revealed that the two wires that provide battery power to the engine ignition had separated. When the wires were reconnected, the ignition system functioned normally. The ignition switch was located on the instrument panel, which was part of the canopy that rotated approximately 90 degrees, when it was opened.

NTSB Probable Cause

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time17:00 EST
Nearest AirportFostoria Metro (0nm)
Runway27
Runway Length4199 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftTheis Quickie
Tail NumberN53ET
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsOnan · 22 HP · Reciprocating · 22
Seats1

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 43 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind270° @ 7 kt
Visibility12 sm
CeilingOvercast 25000 ft
Temperature / Dew Point63 F / 27 C
Altimeter30.00 inHg
Observation Time22:15
Weather SourceWFAC

Appendix: Source Data