N7917G

Substantial
Minor

CESSNA 172LS/N: 17259617

Accident Details

Date
Friday, September 16, 2022
NTSB Number
WPR22LA351
Location
Ventura, CA
Event ID
20220919105963
Coordinates
34.254498, -119.269510
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
1
Total Aboard
3

Probable Cause and Findings

A partial loss of engine power due to the fatigue fracture of the No. 4 exhaust valve.

Aircraft Information

Registration
N7917G
Make
CESSNA
Serial Number
17259617
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
172LC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DELAHUNT STEVEN D
Address
2463 COLLEGE ST
Status
Deregistered
City
SIMI VALLEY
State / Zip Code
CA 93065
Country
United States

Analysis

On September 16, 2022, about 1630 Pacific daylight time, a Cessna 172L, N7917G, was substantially damaged when it was involved in an accident near Ventura, California. The pilot was not injured and both passengers sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that, while enroute about 2,000 ft mean sea level (msl), he heard a "pop" followed by a partial loss of engine power. The airframe started shaking badly, he pulled power to idle, established best glide, and contacted Air Traffic Control (ATC). ATC provided alternate airports and current weather information. Unable to maintain altitude, he initiated a forced landing to a clearing on the beach. During the landing roll, the airplane impacted a rock retaining wall.

Postaccident examination of the airplane revealed that the left wing and forward fuselage were substantially damaged. Subsequent lighted borescope examination of the airplane’s engine revealed mechanical damage to the No. 4 cylinder’s combustion dome and piston face. The Nos. 3 and 4 cylinders were removed. Metallic debris was observed obstructing the No. 3 cylinder intake valve. The No. 4 cylinder was removed, and remnants of the exhaust valve were observed within the cylinder.

The No. 4 cylinder and remnants of the No. 4 exhaust valve were sent to National Transportation Safety Board Materials Laboratory, Washington, DC, for examination. The examination of the fracture surface of the No. 4 exhaust valve revealed characteristics consistent with a fatigue fracture. Review of maintenance records did not reveal any recent maintenance performed on the cylinder.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR22LA351