What happened
On August 21, 2011, at approximately 12:26 UTC, a GY 80-160 aircraft departed from Mauterndorf airfield on runway 25. The flight was a VFR operation with a pilot and one passenger on board. After taking off approximately 460 meters into the takeoff roll, the aircraft reached an altitude of about 15 meters above the ground. During this early climb phase, the pilot began retracting the landing gear and the flaps.
As the aircraft continued its climb, the left wing collided with the treetops of a group of trees approximately 1,124 meters from the start of the runway. Following this impact, the aircraft entered a steep left turn and struck a rising meadow about 100 meters beyond the collision point. The impact triggered a post-crash fire that caused extensive damage to the airframe.
The investigation
The Austrian Federal Safety Investigation Board (SUB) examined the aircraft, the flight conditions, and video footage of the event. The investigation confirmed that the aircraft's maintenance was up to date and all required documentation was valid. The aircraft's weight and center of gravity were within permissible limits.
Investigators analyzed the engine and fuel system, finding that the fuel was a 1:1 mixture of AVGAS and regular gasoline, though this was not considered a cause of the accident. While the spark plugs showed signs of wear and a lean burn pattern, no mechanical failures or engine malfunctions were identified as contributing to the crash. The investigation also reviewed the takeoff performance calculations, noting that while the calculated distance to clear a 15-meter obstacle was sufficient under the prevailing weather, the actual flight path deviated due to aerodynamic changes.
Findings
- The pilot retracted the flaps and landing gear prematurely before clearing obstacles.
- The retraction of the gear and flaps increased the aircraft's angle of attack to maintain altitude, which subsequently increased drag.
- This increased drag led to a significant loss of airspeed, causing the aircraft to enter a sink condition (stall/sink rate increase).
- The pilot was unable to recover the lost airspeed due to the low altitude and proximity to obstacles.