We’re still collecting data for this aircraft. Routes appear once we’ve seen it fly enough times.
APPROX 10 MIN AFTER T/O, THE PILOT STATED HE WAS RETURNING TO LAND DUE TO A PROBLEM. ON FINAL THE ACFT ROLLED INVERTED AND DESCENDED NOSE DOWN INTO A RESIDENCE. ENGINE EXAM REVEALED A FAILED SUPERCHARGER INTERMEDIATE DRIVE SHAFT GEAR RESULTING IN LOSS OF SUPERCHARGER ON THE RT ENGINE. THE ACFT WAS APPROX 300 LBS OVER MAX GROSS WEIGHT. THE LNDG GEAR WAS DOWN AND THE FLAPS WERE EXTENDED APPROX 20 DEGREES. THE LEFT THROTTLE WAS FOUND IN THE FULL FORWARD (HIGH POWER) POSITION. THE RT PROP CONTROL W
Beech 65 · 2 fatalities