N11280

Substantial
None

CESSNA 150LS/N: 15075294

Accident Details

Date
Wednesday, October 5, 2011
NTSB Number
ERA12LA009
Location
Punta Gorda, FL
Event ID
20111006X95405
Coordinates
26.918888, -81.990837
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power due to contamination of the fuel system that was not detected because of the pilot’s inadequate preflight inspection.

Aircraft Information

Registration
N11280
Make
CESSNA
Serial Number
15075294
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
150LC150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JOHNSON WILLIAM H
Address
2635 SLEEPY HOLLOW LN
Status
Deregistered
City
LAKELAND
State / Zip Code
FL 33810-6773
Country
United States

Analysis

On October 5, 2011, at 1055 eastern daylight time, a Cessna 150L, N11280, experienced a partial loss of engine power while approaching to land and collided with the airport perimeter fence at Punta Gorda Airport (PGD), Punta Gorda, Florida. The airplane sustained structural damage to the airframe and wings. The airplane was registered to a private owner and operating as a personal flight under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed. The private pilot was not injured. The flight originated from Winter Haven's Gilbert Airport (GIF), Winter Haven, Florida, at 1000.

According to the pilot, he departed GIF on cross country flight to PGD. Upon arrival he entered a downwind for runway 09. While turning on final approach the engine experienced a partial loss of engine power. The airplane landed short of the runway and on landing roll collided with airport perimeter fence.

Examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed the left and right main fuel caps did not match and the fuel cap seals were deteriorated. The fuel tanks were sumped; and a half jar of rust and water was recovered from the left tank. The pilot stated in the interview with the inspector that he found water in the fuel during his preflight.

A cursory examination was performed on the engine and an engine run-up was conducted. The engine ran successfully but could only be advanced to 1,500 rpm due to a bent propeller as result of the accident. No other anomalies were noted with the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA12LA009