14 CFR 414.23: Technical criteria for reviewing a safety element approval application.
Where this section sits in the code
- Title 14—Aeronautics and Space
- CHAPTER III—COMMERCIAL SPACE TRANSPORTATION, FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
- SUBCHAPTER C—LICENSING
- PART 414—SAFETY ELEMENT APPROVALS
- Subpart C—Safety Element Approval Review and Issuance
The FAA will determine whether a safety element is eligible for and may be issued a safety element approval. The FAA will base its determination on performance-based criteria, against which it may assess the effect on public health and safety and on safety of property, in the following hierarchy:
(a) FAA or other appropriate Federal regulations.
(b) Government-developed or adopted standards.
(c) Industry consensus performance-based criteria or standard.
(d) Applicant-developed criteria. Applicant-developed criteria are performance standards customized by the manufacturer that intends to produce the system, system component, or part. The applicant-developed criteria must define—
(1) Design and minimum performance;
(2) Quality assurance system requirements;
(3) Production acceptance test specifications; and
(4) Continued operational safety monitoring system characteristics.
Collected 2026-08-27T02:24:20Z. Source file · JSON