N6636A

Substantial
Minor

CESSNA 172S/N: 28736

Accident Details

Date
Sunday, October 18, 2015
NTSB Number
ERA16LA018
Location
Campobello, SC
Event ID
20151019X04728
Coordinates
35.134723, -82.113609
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
2
Total Aboard
3

Probable Cause and Findings

The pilot's inadequate preflight inspection of the fuel system, which resulted in a total loss of engine power due to water contamination.

Aircraft Information

Registration
N6636A
Make
CESSNA
Serial Number
28736
Engine Type
Reciprocating
Year Built
1956
Model / ICAO
172C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MYALIK GENNADY
Address
1990 DICKSON RD
Status
Deregistered
City
INMAN
State / Zip Code
SC 29349-9226
Country
United States

Analysis

On October 18, 2015, about 1912 eastern daylight time, a Cessna 172, N6636A, nosed over in a field following a forced landing near Campobello, South Carolina. The private pilot had minor injuries, two passengers were not injured, and the airplane was substantially damaged. The airplane was operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. Dusk, visual meteorological conditions prevailed, and no flight plan was filed. The local flight originated from Fairview Airport (33A), Landrum, South Carolina, about 1845.The pilot reported the following. He was taking his son and a friend on a local, sightseeing flight to a nearby lake. During cruise flight, the engine lost all power. Attempts to regain power were unsuccessful. He elected to force land the airplane in a nearby farm field. During the landing roll, the airplane nosed over and came to a stop. He subsequently reported to an inspector with the Federal Aviation Administration (FAA) that he took off with 30 gallons of fuel on board. He also reported that he performed a thorough preflight inspection and the fuel was free of contaminants.

An inspector with the FAA responded to the accident site and examined the wreckage. The airplane came to rest on a northwesterly heading, inverted. Structural damage was confirmed to the wings, fuselage, and vertical stabilizer. Once the airplane was positioned upright, the fuel system was inspected. The firewall-mounted fuel strainer contained visible water. The cockpit fuel selector handle was found in the "BOTH OFF" position. The left wing was empty of fuel, and there was evidence of fuel leakage under the left wing. The right wing tank was sumped utilizing a standard six-inch tube-type fuel tester. The tester was filled two times and only water drained from the tank. On the third sumping attempt, the tester was filled and contained about three quarters water and one quarter fuel. The exact amount of fuel and water in the right tank was not determined.

The pilot completed a NTSB Form 6120.1 after the accident and reported that there were no mechanical malfunctions or failures that would have precluded normal operation the airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA018