CESSNA 172S near Daytona Beach, FL — 2012-04-09
- Date
- 2012-04-09
- Location
- Daytona Beach, FL, USA
- Aircraft
- CESSNA 172S
- Registration
- N375LP
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Climb
Probable cause
A total loss of engine power due to a catastrophic engine failure, the origin of which could not be determined during postaccident examination.
NTSB narrative
Upon reaching a cruise altitude of 3,000 feet, the engine began to run rough and make loud noises. The flight instructor assumed control of the airplane, and the engine subsequently lost all power. Oil was present on the windscreen. The instructor performed a forced landing in a nearby field where the nose gear contacted a ditch, resulting in a nose over and substantial damage to the airframe. Initial examination of the engine revealed a hole on the lower case and the camshaft partially protruding from the upper case. Suspecting a failure of the No. 4 piston, it and cylinder were subsequently examined; all fracture surfaces showed signs of overstress; however, there was no indication of preexisting mechanical damage that would have led to progressive failure, including fatigue. No corrosion or chemical degradation was found on the piston fracture surfaces. Accordingly, the initiating event that led to the catastrophic failure of the engine could not be determined.
Analysis
- Primary failure mode
- Engine power loss
NTSB coding
Evidence available
- Photos
- 10 docket documents
Docket documents10
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Excerpt from Maintenance Logbooksother
- NTSB Record of Conversation - FAA Inspectorother
- NTSB Record of Conversation - Insurance Adjusterother
- Photo 1: Failed No. 4 Piston Fragments Inside Cylinder (FAA Digital Photo)photos
- Photo 2: Failed No. 4 Piston Fragments Inside Cylinder (FAA Digital Photo)photos
- Photo 3: No. 4 Connecting Rod Bearing (FAA Digital Photo)photos
- Photo 4: No. 4 Cylinder Position in Engine Case (FAA Digital Photo)photos
- Photo 5: Hole in Upper Engine Case (FAA Digital Photo)photos
- Materials Laboratory 15 - Factual Report of Group Chairmanreport
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