N6983B

Substantial
None

Piper PA18S/N: 18-5105

Accident Details

Date
Sunday, July 14, 2019
NTSB Number
CEN19LA224
Location
Osceola, WI
Event ID
20190715X05519
Coordinates
45.310001, -92.690002
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the right horizontal stabilizer during takeoff, resulting in a loss of control and forced landing. Contributing to the accident was the installation of an unapproved stabilizer frame and failure of maintenance personnel to identify deterioration of the stabilizer during routine maintenance.

Aircraft Information

Registration
Make
PIPER
Serial Number
18-5105
Engine Type
Reciprocating
Model / ICAO
PA18PA18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
PA-18A 150

Registered Owner (Current)

Name
WILTZ PAUL E
Address
388 FLOSSIE LN
City
OPELOUSAS
State / Zip Code
LA 70570-8103
Country
United States

Analysis

On July 14, 2019, about 1315 central daylight time, a Piper PA18-150, N6963B, was substantially damaged when it was involved in an accident near Osceola, Wisconsin. The commercial pilot was not injured. The glider towing flight was conducted under the provisions Title 14 Code of Federal Regulations Part 91.

The pilot reported that he had three non-eventful glider tows prior to the accident flight. On the fourth glider tow of the day, the pilot added full power for takeoff and became airborne at 55 mph indicated airspeed. About 5 to 15 feet off the ground, the pilot heard a sudden '"bang," and the nose of the airplane pitched up about 40ºand rolled right about 45º. The aircraft seemed uncontrollable with rudder. The pilot was able to get the wings level before the airplane hit the ground hard. The pilot reduced the power to idle and applied brakes. The airplane skidded between two electric poles, bounced onto a road, went through a ditch, and came to rest inverted. The empennage sustained substantial damage. The glider being towed had released the tow rope and landed uneventfully nearby.

Examination of the airplane revealed a broken attachment fitting of the right horizontal stabilizer. The Ceconite fabric covering was removed from the right and left stabilizers. The attachment corner of the right stabilizer frame was fractured. Pitting, multiple broken welds, and corrosion were found around the fracture. The right stabilizer frame had been fabricated and was not a Federal Aviation Adminstration/parts manufacturer approval-approved part.

Review of maintenance records revealed that the stabilizer assembly had been removed for inspection, refurbished, and replaced multiple times. The most recent maintenance was performed on March 1, 2019, when an annual inspection was completed and new sleeves for the forward attachment points were fabricated and installed on the stabilizer assembly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN19LA224