N750R

Substantial
Serious

Piper PA32RS/N: 32R-7780067

Accident Details

Date
Tuesday, March 12, 2019
NTSB Number
CEN19LA098
Location
Waterloo, IL
Event ID
20190312X02726
Coordinates
38.362777, -90.100280
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
1
Total Aboard
3

Probable Cause and Findings

The loss of engine power due to a connecting rod failure for reasons that could not be determined due to secondary mechanical damage, which resulted in a subsequent forced landing.

Aircraft Information

Registration
N750R
Make
PIPER
Serial Number
32R-7780067
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
PA32RP32R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
STODARD MICHAEL O
Address
205 NICHOLS AVE
Status
Deregistered
City
FAIRHOPE
State / Zip Code
AL 36532-1558
Country
United States

Analysis

On March 12, 2019, at 1442 central daylight time, a Piper PA32R-300 airplane, N750R, was substantially damaged during a forced landing following a loss of engine power near Waterloo, Illinois. The pilot sustained serious injuries, one passenger sustained minor injuries, and the second passenger, a child restrained in a car seat, was not injured. The airplane operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot reported hearing a "horrible noise" and the engine "immediately seized" about 10 minutes from the destination airport. Oil covered the windshield, obstructing his forward field of view. He executed a forced landing to a road by holding the airplane in a right crab to see out of the left side window. The airplane came to rest inverted in a grass area adjacent to the road with damage to the fuselage and both wings.

A postrecovery engine examination revealed the No. 4 and No. 6 connecting rods had separated from the crankshaft. The no. 4 connecting rod was fractured through the upper rod yoke. The corresponding rod cap and bearing fragments were deformed. The no. 6 connecting rod was fractured across one side of the rod yoke; the opposite side was intact but deformed. The corresponding rod cap was deformed. The connecting rods remained attached to the pistons. The pistons were wedged within the cylinders. The pistons, lower cylinder flanges and connecting rods exhibited secondary mechanical damage. The crankshaft was intact. The crankcase was fractured above the No. 4 and No. 6 cylinders exposing a hole in the upper surface of the crankcase.

Metallurgical examination was unable to determine source of the initial failure due to secondary mechanical damage. The intact fracture surfaces that were available for examination exhibited features 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# CEN19LA098