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September 16, 2022 · Cessna 172L · N7917G

Ventura, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 16, 2022
Injury Outcomes
2 injuries (2 minor injuries), 1 uninjured
Location
Ventura, CA
Aircraft
Cessna 172L (1970)
Tail Number
N7917G
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
WPR22LA351

According to the pilot, while conducting a local flight, 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, which resulted in substantial damage to the fuselage and left horizontal stabilizer. Examination of the engine revealed that the No. 4 exhaust valve was fractured. Metallurgical examination of the fracture surfaces on the exhaust valve revealed that it had fractured due to fatigue. The fatigue fracture of the No. 4 exhaust valve likely led to the partial loss of engine power.

NTSB Probable Cause

Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng cyl section-Fatigue/wear/corrosion

Full Narrative

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.

Flight

Event TypeAccident
Event Time16:30 PDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 172L
Tail NumberN7917G
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-E2D · Reciprocating · 150
Seats4

People & Injuries

Injury Summary2 injuries (2 minor injuries), 1 uninjured
Fatal0
Serious0
Minor2
Uninjured1
Total3
Crew 1Age 46 · Third Class · None
Crew 2Minor
Crew 3Minor

Conditions

ConditionsVMC
LightDaylight
Wind260° @ 12 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F
Altimeter29.86 inHg
Observation Time16:51
Weather SourceWFAC

Appendix: Source Data