14 CFR 27.723

§ 27.723 Shock absorption tests.

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

Cite this

Citation: 14 CFR 27.723, § 27.723 Shock absorption tests, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54512
Permanent ID: ys:prov:54512@1
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Full text

The landing inertia load factor and the reserve energy absorption capacity of the landing gear must be substantiated by the tests prescribed in §§ 27.725 and 27.727, respectively. These tests must be conducted on the complete rotorcraft or on units consisting of wheel, tire, and shock absorber in their proper relation.

Legislative history

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