N131DL

Destroyed
Minor

LAVIGNA LANCAIR IV PS/N: LIV-131

Accident Details

Date
Wednesday, January 7, 2009
NTSB Number
CEN09LA124
Location
Iola, KS
Event ID
20090108X01714
Coordinates
37.868057, -95.386947
Aircraft Damage
Destroyed
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 for undetermined reasons.

Aircraft Information

Registration
N131DL
Make
LAVIGNA
Serial Number
LIV-131
Year Built
1996
Model / ICAO
LANCAIR IV P

Registered Owner (Historical)

Name
FLOATRON INC
Address
PO BOX 51000
Status
Deregistered
City
PHOENIX
State / Zip Code
AZ 85076-1000
Country
United States

Analysis

On January 7, 2009, about 1330 central standard time, a single-engine Lavigna Lancair IV P experimental airplane, N131DL, was destroyed following a loss of engine power and subsequent hard landing at the Allen County Airport (K88) near Iola, Kansas. The commercial pilot, sole occupant, sustained minor injuries. The airplane was registered to and operated by Floatron Incorprorated of Phoenix, Arizona. Visual meteorological conditions prevailed and no flight plan was filed for the 14 Code of Federal Regulations Part 91 personal flight. The 235-nautical mile cross-country flight originated from the Creve Coeur Airport (1H0), near St Louis, Missouri, with a planned fuel stop at K88. The pilot's final destination was to be the Chandler Municipal Airport (CHD), in Chandler, Arizona.

According to the pilot, while in the landing flare, he observed an airplane on short final landing in the opposite direction. The pilot elected to abort the landing and applied full engine power. As the airplane began to climb, the engine experienced a complete loss of power. Following the pilot's unsuccessful attempt to re-start the engine, the airplane experienced a hard landing in a grassy area north of the runway. The pilot was able to exit the airplane unassisted. Moments later the airplane was engulfed in flames.

An inspector from the Federal Aviation Administration (FAA) responded to the accident site. The inspector reported that the airplane's aft fuselage and empennage were mostly consumed in the post crash fire. Flight control continuity was confirmed. No anomalies were found with the engine or other airplane systems.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA124