---
kind: "section"
citation: "14 C.F.R. § 22.110"
title: "14"
number: "22.110"
heading: "Structural integrity."
url: "https://uscodex.org/cfr/14/22.110"
---

# §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.

## Notes

### 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.