NC247E

Substantial
None

WACO SRES/N: 5081

Accident Details

Date
Sunday, November 4, 2012
NTSB Number
CEN13LA050
Location
Lafayette, LA
Event ID
20121106X72042
Coordinates
30.208889, -91.990554
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot’s inability to maintain directional control of the airplane during the landing roll.

Aircraft Information

Registration
Make
WACO
Serial Number
5081
Engine Type
Reciprocating
Model / ICAO
SREWACE
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
5
FAA Model
SRE

Registered Owner (Current)

Name
FOSTER MATTHEW R
Address
2932 HOWARD ST
City
POPLAR GROVE
State / Zip Code
IL 61065-8247
Country
United States

Analysis

On November 4, 2012, at 1700 central standard time, a WACO SRE, NC247E, nosed over following a loss of control during landing roll at the Lafayette Regional Airport (LFT), Lafayette, Louisiana. The pilot and two passengers on board were not injured. The airplane was substantially damaged. The airplane was owned and operated by the pilot. The local personal flight was being conducted under 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated from LFT at 1630.

The pilot reported he made an uneventful landing and during the landing roll, the airplane veered to the right. He applied left rudder and little power in an attempt to straighten the airplane heading with no response. The airplane then nosed over.

A postaccident inspection of the airplane revealed that the right main landing gear collapsed, the vertical stabilizer was crushed, and the right lower wing was substantially damaged as was the fuselage. An inspection of the brakes and tires did not reveal any anomalies that would have resulted in the loss of directional control. The right gear brace strut was bent and cracked. The strut remained secured at its gear and fuselage attach points.

The right main landing gear brace strut was sent to the National Transportation Safety Board’s materials laboratory for examination. The examination revealed that the crack faces and bending patterns were consistent with overstress.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA050