§ 22.110 Structural integrity.
Part 22 — DESIGN, PRODUCTION, AND AIRWORTHINESS REQUIREMENTS FOR NON-TYPE CERTIFICATED AIRCRAFT · Subpart B — Light-Sport Category Aircraft · Amended 2026-09-15
(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.