Accident Overview
The pilot reported that the rear engine failed shortly after takeoff. Examination revealed that the fuel selector was positioned on the right main tank, which was empty. The propeller was not feathered, and the landing gear was found in a transient position after the crash.
Performance Considerations
The aircraft's owner's manual cautions that landing gear in transit creates higher drag due to large gear doors and reduces single-engine capability, especially when relying on the front engine. The pilot began a turn back to the departure airport immediately after the engine failure.
Emergency Procedure Execution
The minimal single-engine capability was further degraded by the non-performance of the emergency procedure, premature maneuvering, and delayed gear retraction. The aircraft was unable to maintain altitude.
Forced Landing
After unsuccessfully attempting to restart the rear engine, the pilot selected a forced landing area. On final approach, power lines were observed. In an effort to avoid the power lines, the aircraft struck two utility poles.
Summary of Findings
The incident involved a rear engine failure after takeoff, improper fuel management, and incomplete execution of emergency procedures. The aircraft's performance was insufficient to sustain flight under the circumstances, leading to a forced landing and collision with obstacles.