N5281R

Substantial
None

WOGENSTAHL WALLACE L WOGENSTAHL 281 MRS/N: 281MR

Accident Details

Date
Wednesday, July 14, 2010
NTSB Number
CEN10LA414
Location
Mount Cory, OH
Event ID
20100720X12606
Coordinates
40.936668, -83.822219
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The improper installation of the rivets at the aft fuselage bulkhead which resulted in the pilot not having full elevator control on landing.

Aircraft Information

Registration
N5281R
Make
WOGENSTAHL WALLACE L
Serial Number
281MR
Year Built
2008
Model / ICAO
WOGENSTAHL 281 MR

Registered Owner (Historical)

Name
WOGENSTAHL WALLACE L
Address
5742 REIGART RD
Status
Deregistered
City
HAMILTON
State / Zip Code
OH 45011-2160
Country
United States

Analysis

On July 14, 2010, at 1230 eastern daylight time, an amateur built experimental Wogenstahl 281 MR, N5281R, collided with concrete posts and nosed over during an off airport precautionary landing following an in-flight structural failure. The pilot and passenger were not injured. The airplane was substantially damaged. The Title 14 Code of Federal Regulations Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The flight departed from Middletown, Ohio, at 1030 with an intended destination of Bowling Green, Ohio.

The pilot reported that he heard what sounded like an explosion in the rear of the airplane during cruise flight at 3,000 feet. He stated the airplane then began to vibrate and it sounded as if something was banging on the airplane. The pilot reported he chose a street on which to make a precautionary landing and that the elevator was ineffective during the landing flare. The airplane touched down hard, bounced, and veered off the side of the road where it contacted two concrete posts prior to nosing over.

The pilot reported that the riveting had already been accomplished when he purchased the unfinished airplane from a previous owner. The post accident inspection by a Federal Aviation Administration Inspector and the pilot revealed that 26 of the Avex rivets on the aft bulkhead had failed/worked out allowing the several sections of the aft fuselage skin to pop up. The inspection also revealed that “smoking” was visible around some of the rivet holes indicating that the rivets were loose. The kit manufacturer does call for Avex rivets to be used. The inspector stated that the partial separation of the skin from the bulkhead allowed the empennage to flex which would have resulted in the lack of elevator control during the landing.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10LA414