Accident Overview
The accident airplane sustained substantial damage when it struck a hill during an aborted takeoff from runway 27. The landing gear was sheared from the airframe, and the right main landing gear impacted the horizontal stabilizer.
Pilot Actions
The pilot reported using an informal short field takeoff procedure, employing 10 degrees of trailing edge flaps. He also stated that the aircraft was 80 pounds over its maximum gross weight limit. After observing a lower than expected climb rate, the pilot initiated an aborted takeoff on the remaining runway length to avoid a church located along the intended climb path.
Published Procedures
According to the Pilot's Operating Handbook (POH), the recommended flap setting for short field takeoff is 25 degrees. No takeoff performance data exists in the POH for a flap setting of 10 degrees.
Damage Assessment
The airplane's landing gear was torn off during the impact with the hill. The right main landing gear then struck the horizontal stabilizer, causing additional damage. The overall damage was classified as substantial.