The S-1 scenario

(Replaced by Open Category)

Obligation for all non-captive aircraft:
– Altitude information based on a barometric sensor
– Maximum flight height can be programmed
– Ability to shut down engines in flight
– Fail-safe function in the event of loss of control link

– Electronic reporting for UAS weighing over 800gr

Maximum authorized weight according to operational scenarios :
Unless specifically authorized, only aircraft whose weight does not exceed the following limits, depending on the scenario, may be used:

Scenario S-1: no particular restrictions (*)

(*)Aircraft over 25 kg Aircraft over 25 kg are subject to additional technical design conditions, defined on a case-by-case basis. The DSAC should be contacted in advance of any project involving such an aircraft.