14 CFR 23.2210
§ 23.2210 Structural design loads.
United States · 14 CFR — Aeronautics and Space · Status: effective
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- Citation
- 14 CFR 23.2210, § 23.2210 Structural design loads, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/53906
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Full text
(a) The applicant must:
(1) Determine the applicable structural design loads resulting from likely externally or internally applied pressures, forces, or moments that may occur in flight, ground and water operations, ground and water handling, and while the airplane is parked or moored.
(2) Determine the loads required by paragraph (a)(1) of this section at all critical combinations of parameters, on and within the boundaries of the structural design envelope.
(b) The magnitude and distribution of the applicable structural design loads required by this section must be based on physical principles.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.