N58712

Substantial
None

Boeing A75N1 S/N: 75-341

Accident Details

Date
Sunday, July 21, 1996
NTSB Number
CHI96LA252
Location
EAST TROY, WI
Event ID
20001208X06189
Coordinates
42.779342, -88.389343
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

corrosion and fracture of the rudder control horn.

Aircraft Information

Registration
Make
BOEING
Serial Number
75-341
Engine Type
Reciprocating
Year Built
1941
Model / ICAO
A75N1 B752
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
A75N1(PT17)

Registered Owner (Current)

Name
HAMMERLE TYE F
Address
5324 38TH AVE
City
KENOSHA
State / Zip Code
WI 53144-2720
Country
United States

Analysis

On July 21, 1996, at 1011 central daylight time, a Boeing A75N1, N58712, sustained substantial damage when it nosed over during the landing roll at the East Troy Municipal Airport, East Troy, Wisconsin. The private pilot and one passenger reported no injuries. The personal, 14 CFR Part 91 flight originated in Staughton, Wisconsin, about 0940. Visual meteorological conditions prevailed and no flight plan was filed.

The pilot reported that he flew a "normal" approach to land on runway 08. During the landing roll, the airplane began to "drift" to the right. He "applied the brakes gently" and the airplane nosed over.

The airplane was inspected by a Federal Aviation Administration (FAA) inspector. He reported that the left rudder horn was fractured. No other evidence of mechanical malfunction was reported.

The rudder horn was examined by an engineering technician in the NTSB materials laboratory. In his factual report, the technician reported that the fracture "showed no evidence of progressive cracking, such as fatigue. The fracture was typical of an overstress separation. There was thinning of the wall and corrosion pits on the inside surface of the tube... ." Measurements of some of the corrosion pits revealed that the thickness of the .035 inch wall tubing was corroded to a thickness of .008 inches in some areas. "There was no indication that any of the corrosion pits had penetrated through the tube to the outside surface."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA252