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Initial Airworthiness

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Can "Field Loadable Software" be delivered with an EASA Form 1 and is an EASA Form 1 required for installation?

What is the definition of "Critical parts"?

What is the mandate of the Agency for Environmental issues? What does the Agency concretely do?

Design Approval: FAA Supplementary Type Certificates (STC) approved by National Aviation Authorities (NAAs) before 28-09-03 are deemed to be approved by EASA. If the NAA has limited the approval in scope compared to the original FAA STC such that it does not cover all the models, how can we apply for an extension of the scope?

Why and how must Parts and Appliances be marked, when are the letters EPA required, and which exceptions are acceptable?

Can manufacturers of raw materials obtain a Production Organisation Approval (POA) under Part 21 Subpart G?

Should parts fabricated under a maintenance approval (Part 145) be marked with an EPA (European Part Approval) marking in accordance with Part 21A.804(a)(3)?

EASA STC’s being presented for approval when the pre-mod configuration is not EASA approved. What are EASA changes embedded in Non-EASA approved design?

How can I find one particular AMC-20 in the published AMC-20 amendments?

According to point 21.A.95(c), minor changes to a type-certificate can be approved using Certifications Specifications which became applicable after those incorporated by reference in the type-certificate, provided that they do not affect the demonstration of compliance. Could you please clarify under which conditions the demonstration of compliance is not affected?

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