Aviation Crash Map

Luters Arnis V LEGEND N3YZ

27 June 2012 · Glenwood, Florida, United States · No injuries

Summary

On 27 June 2012 at about 14:28 local time, a Luters Arnis V LEGEND registered N3YZ was involved in an accident near Glenwood, Florida, 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 14:28
Classification
Accident
Location
Glenwood, Florida, United States
Coordinates
29.0864, -81.3542
Aircraft
Luters Arnis V LEGEND
Registration
N3YZ
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Deland → Norfolk
Aircraft damage
Substantial
Weather
IMC
Light
Day
NTSB number
ERA12LA417

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

The total loss of engine power due to the airplane builder’s improper installation of the fuel control unit condition lever cables, which resulted in the airplane’s subsequent forced landing.

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

Read the full NTSB narrative

The amateur-built airplane was in cruise flight at 3,000 feet above ground level when it experienced a total loss of engine power. The pilot performed a forced landing to a field, and the airplane sustained substantial damage during the landing. Postaccident examination revealed that the fuel control unit (FCU) condition lever was 20 degrees out of its run position. Further examination of the condition lever revealed that the condition lever’s outer cable had been improperly installed, which allowed the uncommanded aft movement of the condition lever, which could result in a loss of engine power. A broken engine mount, which was likely the result of impact-related forces, was also found. This broken engine mount resulted in a slight turbine misalignment. When the turbine was realigned, the FCU condition lever settings were normal. The engine was subsequently started and operated normally with no irregular noises or hesitation. According to the engine manufacturer’s representative, if the condition lever had been installed properly, there should have been no such movement of the condition lever.

Quoted verbatim from the NTSB record.

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