Aviation Accident Summaries

Aviation Accident Summary CHI90LA267

TROY, MI, USA

Aircraft #1

N6873M

CESSNA 182

Analysis

SHORTLY AFTER TAKEOFF, DURING INITIAL CLIMB, THE PLT SAID THAT THE ENGINE BEGAN TO SPUTTER AND RUN ROUGH. HE MADE A TURN TO RETURN FOR LANDING, BUT WAS TOO HIGH AND FAST, AND OVERSHOT THE AIRPORT. AN EMERGENCY LDG WAS ATTEMPTED IN A NEARBY FIELD WHICH RESULTED IN SUBSTANTIAL DAMAGE TO THE ACFT. POST-ACCIDENT INVESTIGATION REVEALED THE ROCKER ARM BOSSES ON # 2 CYLINDER HAD FAILED, WHICH CAUSED THE PARTIAL POWER LOSS AND ENGINE ROUGHNESS.

Probable Cause and Findings

A LOSS OF ENGINE POWER DUE TO FAILURE OF THE ROCKER ARM BOSSES ON THE #2 CYLINDER.

 

Source: NTSB Aviation Accident Database

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