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14 CFR 27.21

§ 27.21 Proof of compliance.

United States · 14 CFR — Aeronautics and Space · Status: effective

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14 CFR 27.21, § 27.21 Proof of compliance, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54416
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Each requirement of this subpart must be met at each appropriate combination of weight and center of gravity within the range of loading conditions for which certification is requested. This must be shown— (a) By tests upon a rotorcraft of the type for which certification is requested, or by calculations based on, and equal in accuracy to, the results of testing; and (b) By systematic investigation of each required combination of weight and center of gravity if compliance cannot be reasonably inferred from combinations investigated.

Legislative history

This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.