§22.110. Structural integrity.
14 C.F.R. § 22.110
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
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.
Notes, amendments, and revision history
Authority
Authority: 42 U.S.C. 7572; 49 U.S.C. 106(f), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303.
Source
Source: Amdt. No. 22-1, 90 FR 35208, July 24, 2025, unless otherwise noted.