West Columbia

The airplane used about 1/2 of the 8,602 feet runway for the t/o roll. After t/o it pitched nose-down briefly over the runway during initial climb. The pilot radioed that he was having a problem with the elevator which required 'full back pressure' to keep the nose up, and that he was returning to land. After maneuvering around the airport, the aircraft pitched 70-80° nose down and dove into terrain off the approach end of the runway. The wreckage examination revealed that the bolt securing the elevator trim tab pushrod to the actuator was missing. The rod had become wedged inside the elevator which resulted in an extreme tab up (nose down) condition. The aircraft underwent an annual inspection two days/5 flight hours earlier. The ia mechanic reported that no maintenance was performed on the tab system, and that he was certain the bolt was properly safetied. Another pilot who flew the aircraft the day of the accident reported that he found the pushrod to be secure during his preflight inspection. The 402B poh indicated that the aircraft should have request about 1,200 feet for the t/o ground roll. The pilot, sole on board, was killed.

During final approach the pilot noticed aircraft flying 'unusual' and elected go-around. During power-up, the aircraft lost power and a forced landing was made on a residential street near the airport. The pilot stated that he had inadvertently placed the fuel selector in crossfeed and had exhausted the fuel supply in the right wing by feeding both engines. There were no reported mechanical problems prior to the accident.