14 CFR 23.2100
§ 23.2100 Weight and center of gravity.
United States · 14 CFR — Aeronautics and Space · Status: effective
Cite this
- Citation
- 14 CFR 23.2100, § 23.2100 Weight and center of gravity, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/53889
- Permanent ID
ys:prov:53889@1- SHA-256
89010a3b73f56a9d36b8b470402ebaef1a7d07a2bbdb4c847384ed1f17db90e4
The hash is SHA-256 of this version's text, with every run of whitespace collapsed to a single space and the ends trimmed. The ID always leads back here, and checking it says whether the text you cited is still the current version.
Full text
(a) The applicant must determine limits for weights and centers of gravity that provide for the safe operation of the airplane.
(b) The applicant must comply with each requirement of this subpart at critical combinations of weight and center of gravity within the airplane's range of loading conditions using tolerances acceptable to the Administrator.
(c) The condition of the airplane at the time of determining its empty weight and center of gravity must be well defined and easily repeatable.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.