GroundRules
← Search the law
Federal regulations · Through 2026-08-25 · Newer source version available

14 CFR 414.23: Technical criteria for reviewing a safety element approval application.

Read at publisher ↗
Where this section sits in the code
  1. Title 14—Aeronautics and Space
  2. CHAPTER III—COMMERCIAL SPACE TRANSPORTATION, FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
  3. SUBCHAPTER C—LICENSING
  4. PART 414—SAFETY ELEMENT APPROVALS
  5. 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

Browse this collection