N150ER

Unknown
None

PIPER PA-28-161 S/N: 2841146

Accident Details

Date
Sunday, September 10, 1995
NTSB Number
MIA95IA243
Location
NEW SMYRNA BCH, FL
Event ID
20001207X04544
Coordinates
29.019193, -80.920715
Aircraft Damage
Unknown
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

fatigue failure of the piston assembly (piston and piston pin).

Aircraft Information

Registration
N150ER
Make
PIPER
Serial Number
2841146
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
PA-28-161 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RICHARDS ROBERT
Address
3578 MODOC #7
Status
Deregistered
City
SANTA BARBARA
State / Zip Code
CA 93105
Country
United States

Analysis

On September 10, 1995, about 1700 eastern daylight time, a Piper PA-28-161, N150ER, registered to and operated by Embry- Riddle Aeronautical University, was not damaged during a forced landing at the New Smyrna Beach Municipal Airport, New Smyrna Beach, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 141 instructional flight. The certified flight instructor (CFI), pilot-rated student, and observer were not injured. The flight originated about 1 hour 12 minutes earlier from the Daytona Beach International Airport, Daytona Beach, Florida.

The CFI stated that he reduced the throttle to idle to simulate a loss of engine power. The maneuver was discontinued about 500 feet mean sea level with application of power. While climbing through 1,100 feet, the engine suddenly began operating "rough" and the tachometer indicated 2,000 rpm. Attempts to restore engine power were unsuccessful. The CFI then took the controls and landed uneventfully at the New Smyrna Beach Municipal Airport.

Disassembly of the engine by the operator revealed that a piston and piston pin both manufactured by Superior Air Parts, Inc., were failed in the No. 2 cylinder. The failed components and an intact piston pin from the same engine were sent to the NTSB Materials Laboratory, Washington, D.C., for metallurgical examination.

Metallurgical examination of the failed piston and piston pin revealed that both failed due to fatigue. The surface and core hardness of the failed and intact piston pins were determined to be within the engineering specification.

Review of the maintenance records revealed that the failed components had been installed when the engine was last overhauled on March 22, 1995. The components had accumulated 316.9 hours since manufacture.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA95IA243