Volume: 1Date: 2023-01-01Original Date: 2023-01-01Title: Section 23.2230 - Limit and ultimate loads.Context:
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. - Structural Loads.
Code of Federal Regulations /
Title 14 - Aeronautics and Space /
Vol. 1 / 2023-01-01184
§ 23.2230Limit and ultimate loads.The applicant must determine—(a) The limit loads, which are equal to the structural design loads unless otherwise specified elsewhere in this part; and(b) The ultimate loads, which are equal to the limit loads multiplied by a 1.5 factor of safety unless otherwise specified elsewhere in this part.Structural Performance