This DOARI is intended to address competences of flight test crew involved in flight test activities on aircraft that meet the applicability criteria of SC-VTOL-01 i.e.:
- a person-carrying vertical take-off and landing (VTOL) heavier-than-air aircraft in the small category, with lift/thrust units used to generate powered lift and control;
- distinct from conventional aeroplanes by its VTOL capability or;
- distinct from conventional rotorcraft by the use of distributed propulsion;
- with a passenger seating configuration of 9 or less and;
- a maximum certified take-off mass of 3 175 kg (7 000 lbs) or less
