Aviation Crash Map

Huebbe SONEX HB N244HB

26 October 2014 · Plainview, Illinois, United States · Fatal

Summary

On 26 October 2014 at about 20:50 local time, a Huebbe SONEX HB registered N244HB was involved in an accident near Plainview, Illinois, United States. 2 people were on board and one died, one had minor injuries. 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 20:50
Classification
Accident
Location
Plainview, Illinois, United States
Coordinates
39.1201, -90.0395
Aircraft
Huebbe SONEX HB
Registration
N244HB
Category
Airplane
Year built
2010
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Taylorville → St. Charles
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN15LA028

People

1 person died.

On board Died Serious Minor Uninjured
2 1 0 1 0

Probable cause

The loss of engine power during cruise flight due to a fatigue fracture of the crankshaft, which resulted in a forced landing on unsuitable terrain.

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

Read the full NTSB narrative

The private pilot and a sport pilot-rated passenger were conducting a personal cross-country flight in the experimental amateur-built airplane, which was powered by an uncertified automotive engine. The airplane was in cruise flight when it experienced a total loss of engine power. The pilot(s) attempted a forced landing on a field, during which the airplane nosed over. The wreckage path through the field was about 200 ft long, which was consistent with excessive energy/speed upon touchdown. A review of maintenance logbook entries revealed that the engine had been assembled by the owner and that the camshaft and crankshaft had been removed when work was performed on the engine about 3 years before the accident. Postaccident examination of the engine indicated that the crankshaft had fractured due to a fatigue crack that had initiated at a fillet radius at the forward end of the No. 2 main bearing journal where the journal transitioned to the forward cheek. The cause of the fatigue crack could not be determined.

Quoted verbatim from the NTSB record.

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