Volume: 1Date: 2021-01-01Original Date: 2021-01-01Title: Section § 25.523 - Design weights and center of gravity positions.Context:
Title 14 - Aeronautics and Space. CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION. SUBCHAPTER C - AIRCRAFT. PART 25 - AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES. Subpart C - Structure. - Water Loads.
§ 25.523Design weights and center of gravity positions.
(a)
Design weights.
The water load requirements must be met at each operating weight up to the design landing weight except that, for the takeoff condition prescribed in § 25.531, the design water takeoff weight (the maximum weight for water taxi and takeoff run) must be used.
(b)
Center of gravity positions.
The critical centers of gravity within the limits for which certification is requested must be considered to reach
maximum design loads for each part of the seaplane structure.
Code of Federal Regulations /
Title 14 - Aeronautics and Space /
Vol. 1 / 2021-01-01256
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-23, 35 FR 5673, Apr. 8, 1970]