Aviation Crash Map

Griff CHALLENGER N582L

11 June 2019 · Switz City, Indiana, United States · Serious injuries

Summary

On 11 June 2019 at about 01:00 local time, a Griff CHALLENGER registered N582L was involved in an accident near Switz City, Indiana, United States. One person was on board and one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 01:00
Classification
Accident
Location
Switz City, Indiana, United States
Coordinates
39.0647, -87.0533
Aircraft
Griff CHALLENGER
Registration
N582L
Category
Airplane
Year built
2010
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Bloomfield → Bloomfield
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN19LA163

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
1 0 1 0 0

Probable cause

A total loss of engine power due to failure of a connecting rod bearing. Contributing to the engine failure was the lack of an engine overhaul within the prescribed interval.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot of the experimental, amateur-built airplane reported that, while returning to the airport after a local flight, the engine speed "suddenly" decreased from about 5,000 rpm to 2,500 rpm. He trimmed the airplane for its best glide airspeed and began looking for a forced landing site. About 30 seconds later, the engine seized and lost power completely. The airplane touched down short of the pilot's intended landing point and nosed over resulting in substantial damage to the fuselage and empennage. An engine examination revealed that a lower connecting rod bearing had failed, resulting in the total loss of engine power. Maintenance records indicated that an engine overhaul was completed slightly more than 5 years before the accident flight. The engine manufacturer's maintenance schedule specified that an engine overhaul be completed every 5 years or 300 hours, whichever comes first. It is likely that, had the engine been overhauled in accordance with manufacturer guidance, the worn connecting rod bearing would have been detected during the overhaul and resulted in its replacement.

Quoted verbatim from the NTSB record.

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