*The exception I'm aware of: The Cirrus SR-20, by FAA Special Condition 23-ACE-88, which in small part reads [the "system" being CAPs]:
No: when the SR series received EASA approval a full program of spin testing was conducted. The earlier FAA certification allowed CAPS as an alternative, I think probably to save cost, and this has led to the myth that a Cirrus can not be recovered from a spin.