Aviation Crash Map

Chevrier Armand J-3K N43432

7 July 2006 · Charlotte, Vermont, United States · No injuries

Summary

On 7 July 2006 at about 14:45 local time, a Chevrier Armand J-3K registered N43432 was involved in an accident near Charlotte, Vermont, United States. One person was on board and nobody was 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 14:45
Classification
Accident
Location
Charlotte, Vermont, United States
Nearest airport
Private (NONE)
Coordinates
44.2689, -73.2506
Aircraft
Chevrier Armand J-3K
Registration
N43432
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Charlotte → Charlotte
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
NYC06LA129

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

A complete loss of engine power on takeoff for undetermined reasons, which resulted in a forced landing.

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

Read the full NTSB narrative

According to the pilot of an amateur built J-3K airplane, the engine was producing maximum power during takeoff, when only a few seconds later, the engine stopped without warning. The pilot performed an emergency landing during which the airplane impacted a tree and was substantially damaged. According to maintenance records the engine had experienced an engine seizure approximately 47 hours prior to the accident and the engine had received a "top end overhaul," during which one piston, its piston rings, and piston needles had been replaced. On the day of the accident, the pilot performed "minor" engine and fuel system maintenance, and a fuel primer bulb was installed. During a postaccident examination of the engine and airplane, no preimpact malfunctions were discovered. The engine was manufactured in 1994. At the time of the accident the engine had accumulated 272 total hours of operation. According to the Rotax Aircraft Engines Maintenance Manual, a complete general overhaul was to be carried out every 5 years or every 300 hours which ever comes first. No record of the engine ever having received a complete general overhaul was discovered during the investigation.

Quoted verbatim from the NTSB record.

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