WebAug 4, 2016 · 14 CFR 23.561 : Aeronautics And Space (§ 1.1 To Parts 1311-1399) — (§ 1.1 To Parts 50-59) — Federal Aviation Administration, Department Of Transportation (§ 1.1 … http://federal.elaws.us/cfr/title14.part23.section23.562
Federal Aviation Regulation Sec. 23.562 - RisingUp.com
Web(a) Each seat/restraint system and the supporting structure must be designed to support occupants weighing at least 215 pounds when subjected to the maximum load factors corresponding to the specified flight and ground load conditions, as defined in the approved operating envelope of the airplane. Web§23.967 14 CFR Ch. I (1–1–10 Edition) (d) Each tank with a nonmetallic liner must be subjected to the sloshing test outlined in paragraph (b)(5) of this section, with the fuel at room tempera-ture. In addition, a specimen liner of the same basic construction as that to be used in the airplane must, when in- hidrat 40 crema
Federal Aviation Regulation Sec. 23.561 - General. - RisingUp.com
WebTitle 14 Code of Federal Regulations (14 CFR) Title 14 Code of Federal Regulations (14. CFR. ) Part 23, Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes. Part 34, Fuel Venting and Exhaust Emission Requirements for Turbine Engine Powered Airplanes. Webwith Title 14 of the Code of Federal Regulations (14 CFR) part 23, Subpart C, and portions of Subpart D. However, if you use the means described in the AC, you must follow it in all important respects. This AC consolidates the substance of existing Civil Aeronautics Administration (CAA) and Federal Aviation Administration (FAA) letters into a ... Web§23.537 14 CFR Ch. I (1–1–13 Edition) K=0.8, except that lower values may be used if it is shown that the floats are incapa-ble of submerging at a speed of 0.8 V so in normal operations; V so=seaplane stalling speed (knots) with landing flaps extended in the appropriate position and with no slipstream effect; and how far can a blimp travel