N514PT

Substantial
Minor

Kinnson Lancair IV-P TurbineS/N: LIV-498

Accident Details

Date
Tuesday, August 22, 2006
NTSB Number
SEA06LA167
Location
Helena, MT
Event ID
20060901X01280
Coordinates
46.606945, -111.982780
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The total loss of engine power as a result of turbine over temperature due to the pilot's failure to follow proper procedures for engine operation. A contributing factor was the lack of suitable terrain for the ensuing forced landing.

Aircraft Information

Registration
N514PT
Make
KINNSON
Serial Number
LIV-498
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
Lancair IV-P TurbineSA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SHUNKWILER NEILAN C
Address
640 COUNTY ROAD 1470
Status
Deregistered
City
NINNEKAH
State / Zip Code
OK 73067-3054
Country
United States

Analysis

On August 22, 2006, about 1715 mountain daylight time, a Kinnson Lancair IV-P Turbine amateur-built experimental airplane, N514PT, sustained substantial damage when it struck a fence and terrain during a forced landing following a loss of engine power about 2 miles north of the Helena Regional Airport, Helena, Montana. The private pilot, the sole occupant, received minor injuries. The airplane was being operated by the pilot under 14 CFR Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the local personal flight that departed the Helena Airport about 1623.

According to the pilot, after flying in the local area for about 40 minutes, he returned to the airport to practice some takeoffs and landings. After completing the first landing, he departed and was climbing out with the landing gear and flaps retracted when he "noticed flames coming out of the right side exhaust stack." The engine lost power, and the pilot executed a forced landing in a field. During the landing roll, the airplane impacted irrigation ditches and a fence.

An FAA inspector examined the airplane and reported that the right wing spar was broken. He further reported observing dents in the exhaust stacks that appeared to be from turbine blade material breaking off the turbine wheels and exiting the engine. The inspector oversaw a read out of engine parameters stored in avionics equipment installed in the airplane. According to the inspector, the data revealed "over temp and over torque of the engine for in excess of 60 seconds." The pilot stated that the accident could have been prevented by having equipment installed in the airplane that would prevent turbine over temperature by automatically limiting the fuel flow to the turbine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA06LA167