N41765

Substantial
None

PIPER PA28-151S/N: 28-7415327

Accident Details

Date
Friday, November 20, 2009
NTSB Number
ERA10LA070
Location
Port Charlotte, FL
Event ID
20091121X05047
Coordinates
26.918333, -81.987777
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

A partial loss of engine power due to the separation of the spark plug hole helicoil from the bottom position of the No. 3 cylinder for undetermined reasons.

Aircraft Information

Registration
N41765
Make
PIPER
Serial Number
28-7415327
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
PA28-151P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
UNIVERSEL TECHNOLOGIES/UNITEC INC
Address
PO BOX 510637
Status
Deregistered
City
PUNTA GORDA
State / Zip Code
FL 33951-0637
Country
United States

Analysis

On November 20, 2009, about 1130 eastern standard time, a Piper PA-28-151, N41765, registered to Universel Technologies/Unitec, Inc., experienced partial loss of engine power and was substantially damaged during a forced landing in a wooded area near Port Charlotte, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 Code of Federal Regulations (CFR) Part 91 personal, local flight, from Charlotte County Airport (PGD), Punta Gorda, Florida. The certificated commercial pilot and two passengers were not injured. The flight originated from PGD about 1100.

The pilot stated that after takeoff, while flying over the Port Charlotte area, he heard a loud "pop" sound, followed by a substantial loss of engine power. Attempts to restore engine power were unsuccessful and the engine was not producing enough power to sustain flight. He announced on the PGD common traffic advisory frequency that he intended on performing a forced landing and also activated the emergency locater transmitter. While descending for the forced landing, the airplane collided with small trees short of a clearing and the right wing then contacted elevated terrain, causing the airplane to yaw 180 degrees to the right. The airplane came to rest upright and all occupants exited it.

Postaccident inspection of the engine by a Federal Aviation Administration airworthiness inspector revealed the bottom spark plug from the No. 3 cylinder was not secured to the cylinder, and had only remained secured to the engine by the ignition lead. A helicoil threaded insert remained attached to the threaded portion of the spark plug, but the insert was unwound.

Review of the maintenance records revealed the engine was overhauled in 1992. The entry pertaining to the overhaul indicates that two repaired cylinders were installed and the other two cylinders, which were reconditioned, were installed. A review of the serviceable tags for the two cylinders that were repaired revealed no indication that a helicoil was installed. No determination was made as to when the helicoil was installed in the bottom spark plug position of the No. 3 cylinder. The engine had accumulated approximately 2,142 hours since major overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA10LA070