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FAR/AIM
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Federal Aviation Regulations
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PART 23—AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES
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Subpart C—Structures
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§ 23.2230 Limit and ultimate loads.
§ 23.2230 Limit 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.