CESSNA R182 near McCall, ID — 2023-06-12
- Date
- 2023-06-12
- Location
- McCall, ID, USA
- Airport
- MYL
- Aircraft
- CESSNA R182
- Registration
- N3138C
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Takeoff roll
Probable cause
Maintenance personnel's failure to properly torque and inspect the magneto hardware, which resulted in a partial loss of engine power.
NTSB narrative
The passenger recalled that on the morning of the accident, the pilot had performed a preflight inspection and did not point out any mechanical issues with the airplane. The start-up and run-up were normal. As the airplane rotated for takeoff, the pilot reported that they had a power problem. The passenger stated that the pilot wanted to return to the airport, but the airplane had not gained enough altitude to clear the obstacles near the departure end of the runway. Witnesses near the accident site reported that the departure roll appeared to be unusually long and the engine did not seem to be developing full power. From their vantage point they saw the airplane's nose pitch up and begin to climb, but it did not gain enough altitude to clear the trees near the departure end of the runway where the airplane impacted the top of a pine tree. Postaccident examination of the engine revealed that the single-drive dual magneto remained attached to the engine accessory case, but not secured to the mounting pad. Both the upper and lower retaining hardware were loose, which allowed the magneto to be rotated with minimal resistance. The engine manufacturer issued a service instruction letter that cautioned that the magneto and/or its attaching hardware can become loose or unfastened following maintenance work. A review of the airplane’s maintenance records revealed that the magneto had been replaced about 15 hours before the accident flight. It is likely that the magneto’s hardware was not properly installed, torqued, or inspected, resulting in loose hardware and a subsequent loss of engine power.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have aborted takeoff after noting power problem.
NTSB coding
Evidence available
- 17 docket documents
Docket documents17
- AIRPLANE OWNER STATEMENTform
- RELEASE OF AIRCRAFT WRECKAGE, NTSB FORM 6120.15form
- STATEMENT OF PARTY REPRESENTATIVES TO NTSB INVESTIGATIONform
- A&P STATEMENTSinterview
- PASSENGER STATEMENTinterview
- WITNESS STATEMENTSinterview
- ACCIDENT SITE EXAMINATIONother
- AIRFRAME AND ENGINE EXAMINATIONother
- AIRPLANE LOGBOOK ENTRYother
- AUTOPSY MEMO FOR RECORDother
- LA GRANDE FBO FUEL RECEIPTother
- LYCOMING SERVICE INSTRUCTIONother
- PILOT LOGBOOKother
- EVIDENCE CONTROL FORMradar
- ATTACHMENT 1 TO ENGINE DATA MONITOR - SPECIALIST'S FACTUAL REPORTreport
- ENGINE DATA MONITOR - SPECIALIST'S FACTUAL REPORTreport
- TOXICOLOGICAL REPORTreport
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