14 CFR 25.681
§ 25.681 Limit load static tests.
United States · 14 CFR — Aeronautics and Space · Status: effective
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- Citation
- 14 CFR 25.681, § 25.681 Limit load static tests, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54100
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Full text
(a) Compliance with the limit load requirements of this Part must be shown by tests in which—
(1) The direction of the test loads produces the most severe loading in the control system; and
(2) Each fitting, pulley, and bracket used in attaching the system to the main structure is included.
(b) Compliance must be shown (by analyses or individual load tests) with the special factor requirements for control system joints subject to angular motion.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.