CESSNA 172N near Orange Beach, AL — 2011-07-04
- Date
- 2011-07-04
- Location
- Orange Beach, AL, USA
- Aircraft
- CESSNA 172N
- Registration
- N109DP
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Climb
Probable cause
The operation of the airplane using unapproved fuels, which resulted in abnormal combustion and subsequent damage to the No. 3 cylinder. Contributing to the accident was the inadequate 100-hour inspection because the mechanic failed to note the lack of placards by either fuel filler cap specifying the minimum automotive fuel grade and no alcohol allowed as specified by the installed STC’s.
NTSB narrative
The airplane had been modified by several Supplemental Type Certificates (STCs) allowing the use of 91 minimum octane alcohol-free fuel, or a combination of 100LL and 91 minimum octane ethanol-free fuel. After takeoff while operating the engine on a mixture of 100LL and 87 octane automotive fuels with 10 percent ethanol additive, the engine experienced abnormal combustion in the No. 3 cylinder, which burned a hole through the cylinder near the lower spark plug hole. The resulting loss of engine power necessitated a forced landing in water. Postaccident examination of the engine revealed no discrepancies with the power train, ignition, lubrication, or air induction systems that would have led to the event. Metallurgical examination of the No. 3 cylinder revealed no manufacturing defects that would have damaged to the cylinder. No placards were noted by either fuel cap; these were required by the installed STCs specifying minimum octane rating of 91 without alcohol; however, on the day of the accident, the airplane underwent a 100-hour inspection by the pilot-in-command who held a mechanic certificate with airframe and powerplant ratings and inspection authorization; he had also performed the modification allowing the airplane to use automotive fuel. Although no fuel samples were retained for testing, the damage to the cylinder was consistent with the usage of unapproved fuel with too low an octane rating.
Analysis
- Primary failure mode
- Fuel management
- First missed decision gate
- Properly managing fuel type and ensuring no automotive fuel was used.
NTSB coding
Evidence available
- Photos
- 17 docket documents
Docket documents17
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- FAA Inspector Statementsinterview
- Engine Type Certificate Data Sheet for Lycoming O-320-E2Dother
- Engine Type Certificate Data Sheet for Lycoming O-360-A4Mother
- Excerpts from Airframe Maintenance Recordsother
- Excerpts from Engine Maintenance Recordsother
- NTSB Record of Conversationother
- Supplemental Type Certificate (STC) SA2600CEother
- Supplemental Type Certificate (STC) SE2563CEother
- Photo 1: Digital Photograph Provided by FAA. View depicting the Nos. 1 and 3 Cylinder Pistons After Cylinder Removal.photos
- Photo 2: Digital Photograph Provided by FAA. View Depicting the Fuel Quantity Gauges and Placard Beneathphotos
- Photo 3: Digital Photograph Provided by FAA. View Depicting a Portion of the Engine Data Plate Associated with the Lycoming O-320-E2Dphotos
- Photo 4: Digital Photograph Provided by FAA. View Depicting a Portion of the Engine Data Plate Associated with the Lycoming O-360-A4Mphotos
- Photo 5: Digital Photograph Provided by FAA. View Depicting Both Engine Data Platesphotos
- Materials Laboratory 15 - Factual Report of Group Chairmanreport
- Weather Reports and Recordsreport
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