14 CFR § 22.110

14 CFR · Aeronautics and Space

§ 22.110 — Structural integrity.

eCFR · current through Jul 31, 2026

§ 22.110 Structural integrity.

(a)The design and construction of the aircraft must provide sufficient structural integrity to enable safe operations within the aircraft's flight envelope throughout the aircraft's intended life cycle; and

(b)The aircraft must be able to withstand all likely flight and ground loads, including towing and any aerial work operation, when operated within its operational limits.

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§ 22.110 Structural integrity.

(a) The design and construction of the aircraft must provide sufficient structural integrity to enable safe operations within the aircraft's flight envelope throughout the aircraft's intended life cycle; and

(b) The aircraft must be able to withstand all likely flight and ground loads, including towing and any aerial work operation, when operated within its operational limits.

14 C.F.R. § 22.110 (Structural integrity.) — published by Counsel Stack Legal Research, free access to 12M+ legal documents.