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The USA Federal Aviation Regulations, Part 21, §21.183(d) has a procedural definition of airworthy: "other aircraft An applicant for a standard airworthiness certificate for aircraft not covered by paragraphs (a) through (c) (a:"New aircraft manufactured under a production certificate." b:"New aircraft manufactured under type certificate only."
A standard airworthiness certificate ceases to be valid when the aircraft ceases to be registered. Change of ownership of an aircraft does not require re-issue or re-validation of that aircraft's standard airworthiness certificate. In contrast to a standard airworthiness certificate, an aircraft may be issued with a special airworthiness ...
Part 21 is certification procedures for products and parts. Part 39 are airworthiness directives. Part 43 is maintenance, preventive maintenance, rebuilding, and alteration. Part 145 contains the rules a certificated repair station must follow as well as any person who holds, or is required to hold, a repair station certificate issued under ...
DO-178B, Software Considerations in Airborne Systems and Equipment Certification is a guideline dealing with the safety of safety-critical software used in certain airborne systems. It was jointly developed by the safety-critical working group RTCA SC-167 of the Radio Technical Commission for Aeronautics (RTCA) and WG-12 of the European ...
Where DERs find compliance, they certify that compliance by completing FAA Form 8110-3, Statement of Compliance with Airworthiness Standards for the specific configuration of the technical data they reviewed. [7] Form 8110-3 is the only FAA form that any DER may sign under their designated authority. [14]
The FAA's FAQ on Part 21 stated that PMA quality systems would be evaluated for compliance by the FAA during certificate management activity after the compliance date of the rule. [23] Today, all FAA production approvals – whether for complete aircraft or for piece parts – rely on a common set of quality assurance system elements.
A type certificate (TC) is issued to signify the airworthiness of the approved design or "type" of an aircraft to be manufactured. The TC is issued by a regulatory authority, and once issued, the design cannot be changed unless at least part of the process for certification is repeated to cover the changes.
FAA Order 8130.34D, Airworthiness Certification of Unmanned Aircraft Systems, establishes procedures for issuing either special airworthiness certificates in the experimental category or special flight permits to unmanned aircraft systems (UAS), optionally piloted aircraft (OPA), and aircraft intended to be flown as either a UAS or an OPA.