Elements and Performance Criteria
- Design an aerobatic sequence
- Performance parameters are identified based on physical limitations of the pilot and structural limitations of the aircraft
- A sequence of aerobatic manoeuvres is designed that meets a specified requirement
- Practical transitions are included between aerobatic manoeuvres
- Performance parameters are identified based on a combination of aircraft attitude, power setting, altitude and speed that provide go-no-go guidance for safe completion of all manoeuvres above safety height
- Perform aerobatic sequences above specified safety height
- Specified sequences of manoeuvres are completed in accordance with aerobatics design
- Performance parameters required for safe completion of the manoeuvre are achieved prior to commencement
- Orientation with display axis is maintained
- Energy potential of the aircraft is managed to ensure completion of manoeuvres and sequences of manoeuvres within aircraft structure and minimum height limits
- Failure to achieve performance parameters (energy requirement) to complete a manoeuvre is recognised and aircraft is managed to regain control above safety height
- Height at or above a specified altitude is maintained