N5351C

Substantial
None

CESSNA 140AS/N: 15482

Accident Details

Date
Saturday, February 26, 2011
NTSB Number
WPR11LA150
Location
Newark, CA
Event ID
20110228X73238
Coordinates
37.499721, -122.101669
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A loss of engine power due to water contamination in the fuel system as a result of the pilot’s inadequate preflight inspection to identify and remove the water.

Aircraft Information

Registration
Make
CESSNA
Serial Number
15482
Engine Type
Reciprocating
Year Built
1950
Model / ICAO
140AC140
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
140A

Registered Owner (Current)

Name
LC AVIATION CONSULTING LLC
Address
PO BOX 1556
City
MONTAUK
State / Zip Code
NY 11954-0892
Country
United States

Analysis

HISTORY OF FLIGHT

On February 26, 2011, about 1245 Pacific standard time (PST), a Cessna 140A, N5351C, nosed over during a forced landing following a loss of engine power near Newark, California. The owner/pilot was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The airline transport pilot was not injured; the airplane sustained substantial damage. The cross-country personal flight departed Palo Alto Airport, Palo Alto, California, about 1240, with a planned destination of Victorville, California. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot had just purchased the airplane on February 26, 2011, and it was being flown to his home in Illinois.

After takeoff, the pilot reported that the engine lost power. During the forced landing the airplane flipped over. The airplane sustained substantial damage to the main landing gear box. The airplane was recovered for further investigation.

The pilot submitted a Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), and reported that he had drained the sump points after filling the airplane with fuel; however, he did not lift the tail prior to sumping the tanks. He opined that since the airplane was a tailwheeled airplane, the water might have been trapped.

On March 2, 2011, the airplane and engine were examined at Plain Parts Enterprises, Pleasant Grove, California. During the examination, water was found in the carburetor bowl. The estimated quantity of water was about 3/4 ounce. Evidence of water was also found in the gascolator. A copy of the wreckage examination is attached to the accident docket.

At the conclusion of the engine examination, no evidence of preimpact mechanical malfunctions or failures were found that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR11LA150