Is it envisaged an EASA generic CRI to deal with this new technology?
Does EASA has a Group/Team who we can work to develop the processes to qualify additive manufacturing parts.
Isn’t there a difference between monolithic materials Vs sandwiched Composite materials?
Do you consider Rapid Prototyping as Additive Manufacturing?
Regarding EASA/FAA TIP rev 6: Is additive manufacturing still considered „new technology“?