Regulatory Text
14 C.F.R. § 29.723 — Shock absorption tests.
§ 29.723 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 §§ 29.725 and 29.727, 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
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Root-LD v1.0 · boisestandard.org
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BS-CFR14-SEC-3BEDF1
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REGULATION / FEDERAL-CFR-SECTION
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boisestandard.org
Citation
14 C.F.R. § 29.723
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CFR — Code of Federal Regulations
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PRIMARY-SOURCE
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3626f165c8b7da11...
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The regulatory text of 14 C.F.R. § 29.723 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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Title 14 — Aeronautics and Space
14 C.F.R. § 1.114 C.F.R. § 1.214 C.F.R. § 1.314 C.F.R. § 3.114 C.F.R. § 3.514 C.F.R. § 3.20014 C.F.R. § 3.20514 C.F.R. § 5.114 C.F.R. § 5.314 C.F.R. § 5.514 C.F.R. § 5.2114 C.F.R. § 5.2314 C.F.R. § 5.2514 C.F.R. § 5.2714 C.F.R. § 5.5114 C.F.R. § 5.5314 C.F.R. § 5.5514 C.F.R. § 5.7114 C.F.R. § 5.7314 C.F.R. § 5.7514 C.F.R. § 5.9114 C.F.R. § 5.9314 C.F.R. § 5.9514 C.F.R. § 5.9714 C.F.R. § 11.114 C.F.R. § 11.314 C.F.R. § 11.514 C.F.R. § 11.714 C.F.R. § 11.914 C.F.R. § 11.11
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