GroundRules
14 CFR 23.2215: Flight load conditions.
Where this section sits in the code
- Title 14—Aeronautics and Space
- CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
- SUBCHAPTER C—AIRCRAFT
- PART 23—AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES
- Subpart C—Structures
The applicant must determine the structural design loads resulting from the following flight conditions:
(a) Atmospheric gusts where the magnitude and gradient of these gusts are based on measured gust statistics.
(b) Symmetric and asymmetric maneuvers.
(c) Asymmetric thrust resulting from the failure of a powerplant unit.
Collected 2026-08-27T02:24:20Z. Source file · JSON