N55329

Substantial
None

PIPER PA-28R S/N: 28R-7385217

Accident Details

Date
Thursday, February 8, 1996
NTSB Number
MIA96LA075
Location
BOCA RATON, FL
Event ID
20001208X05296
Coordinates
26.379997, -80.169570
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the partial loss of engine power due to the fatigue failure of the number 3 cylinder hold down studs and nut. A factor was the pilot'e evasive maneuver to avoid golphers on a golf course.

Aircraft Information

Registration
N55329
Make
PIPER
Serial Number
28R-7385217
Engine Type
Reciprocating
Model / ICAO
PA-28R P28R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
THRUSH AIRCRAFT INC
Address
300 OLD PRETORIA RD
Status
Deregistered
City
ALBANY
State / Zip Code
GA 31721-5285
Country
United States

Analysis

On February 8, 1996, about 0845 eastern standard time, a Piper PA-28R, N55329, registered to Professional Flight Training Inc., operating as a 14 CFR Part 91 instructional flight, experienced a partial loss of engine power, and made a forced landing in the vicinity of Boca Raton, Florida. Visual meteorological conditions prevailed and an IFR flight plan was filed. The commercial pilot/certified flight instructor (CFI), and student pilot reported no injuries. The flight originated from Fort Lauderdale about 19 minutes before the accident.

The CFI stated they were climbing through 4,000 feet when they heard a noise similar to a "pop" and the engine started shaking. The CFI reversed course for Fort Lauderdale and informed Miami Approach Control of his intentions. The airplane would not maintain altitude so he started flying towards Boca Raton Airport. He realized he would not make the airport and made a forced landing to a golf course. On landing roll he had to turn to the left to avoid hitting some golfers who did not move. The right wing of the airplane collided with a tree sustaining substantial damage.

Examination of the engine assembly by the FAA revealed a failure of the hold down studs on the No. 3 cylinder and one hold down nut on the No. 1 cylinder.

Examination of the hold down studs and nut was performed by the NTSB materials laboratory. The examination revealed that all three studs separated as a result of fatigue fracture mechanism. The fracture face on the nut contained characteristic features of a high stress fatigue separation. (See NTSB Metallurgist's Factual Report No. 96-86.)

The hold down studs and nut were released to Mr. Tom Margagliano, Professional Flight Training Inc., on April 23, 1996.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96LA075