14 C.F.R. · Aeronautics and Space
14 C.F.R. § 27.723

Shock absorption tests.

Title 14 C.F.R. ● ACTIVE Primary Source
Regulatory Text

14 C.F.R. § 27.723 — Shock absorption tests.

§ 27.723 Shock absorption tests. 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.

Source: ecfr.gov · govinfo.gov — public domain Official Source ↗
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14 C.F.R. § 27.723
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The regulatory text of 14 C.F.R. § 27.723 is reproduced from the official Code of Federal Regulations as published by the Office of the Federal Register and the National Archives and Records Administration.
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boisestandard.org United States Law CFR Title 14 14 C.F.R. § 27.723