Accident Overview
An aircraft was destroyed when it impacted trees in mountainous terrain at an elevation of approximately 7,850 feet mean sea level (msl). The density altitude at the time was calculated to be about 8,400 feet. Examination of the tree strike pattern and aircraft wreckage indicated that the aircraft was in near level flight at the moment of initial tree contact.
Aircraft Weight and Modifications
The aircraft's gross weight at impact was calculated to be approximately 3,900 pounds. The maximum certificated takeoff weight for the aircraft was 3,500 pounds. The owner had personally installed a set of amphibious floats and a three-blade propeller. This installation was not inspected or signed off for return to service, and no evidence was found that the weight and balance had been recomputed following these modifications.
Mechanical Examination
Examination of the airframe and engine revealed no mechanical malfunction. No pre-impact anomalies were identified in the structure or powerplant.
Conclusion
The aircraft impacted trees in mountainous terrain. No probable cause was stated in the investigation findings.