A VTOL example is needed to show how aircraft-level Failure Conditions and their associated requirements can be flown down to system level, specifically for the highly-integrated functions of a VTOL aircraft and the new flight phases / operational aspects that they introduce. The purpose of this task is to review existing materials to identify what is suitable to be adopted, what needs to be adapted and create a partial example of a VTOL-AFHA as a EUROCAE Guidance Document, in accordance with ED-135 and ED-79.