Cfr 23.561
WebMar 29, 2024 · § 23.561 General. § 23.562 Emergency landing dynamic conditions. § 23.571 Metallic pressurized cabin structures. § 23.572 Metallic wing, empennage, and associated structures. § 23.573 Damage tolerance and fatigue evaluation of structure. § 23.574 Metallic damage tolerance and fatigue evaluation of commuter category airplanes. Webdefined by 49 CFR part 572, subpart B, or an FAA-approved equivalent, with a nominal weight of 170 pounds and seat-ed in the normal upright position. (1) For the first test, the change in velocity may not be less than 31 feet per second. The seat/restraint system must be oriented in its nominal posi-tion with respect to the airplane and
Cfr 23.561
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Web23.562-1 Initiated By: ACE-100 Change: AND OCCUPANT PROTECTION 1. PURPOSE. This advisory circular (AC) provides information and guidance rega rding … 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
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 … WebPart 23, Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes Part 34, Fuel Venting and Exhaust Emission Requirements for Turbine Engine Powered Airplanes Part 36, Noise Standards: Aircraft Type and Airworthiness Certification Part 43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration Policy
Web§ 23.2005 Certification of normal category airplanes. ( a) Certification in the normal category applies to airplanes with a passenger-seating configuration of 19 or less and a … Webdefined by 49 CFR Part 572, Subpart B, or an FAA-approved equivalent, with a nominal weight of 170 pounds and seat-ed in the normal upright position. (1) For the first test, the change in velocity may not be less than 31 feet per second. The seat/restraint system must be oriented in its nominal posi-tion with respect to the airplane and
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-
WebCFR Title 14 Section of the Electronic Code of Federal Regulations CFR Title 14 Section of the Electronic Code of Federal Regulations Toggle navigationeCFR Home Title 14 … safir creative communicationWebAug 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 To Parts 50-59) — Aircraft (§ 21.1 To Parts 50-59) — Airworthiness Standards: Normal, Utility, Acrobatic, And Commuter Category Airplanes (§ 23.1 To Appendix J To Part 23) — … safir consultingWebOfficial Publications from the U.S. Government Publishing Office. safir beach houseWebJan 3, 2010 · Authority: 49 U.S.C. 106(g), 40113, 44701–44702, 44704. Source: Docket No. 4080, 29 FR 17955, Dec. 18. 1964; 30 FR 258, Jan. 9, 1965, unless otherwise noted. Special Federal Aviation Regulation No. 23 top. 1. Applicability. An applicant is entitled to a type certificate in the normal category for a reciprocating or turbopropeller multiengine … safir cateringWebdefined by 49 CFR part 572, subpart B, or an FAA-approved equivalent, with a nominal weight of 170 pounds and seat-ed in the normal upright position. (1) For the first test, the change in velocity may not be less than 31 feet per second. The seat/restraint system must be oriented in its nominal posi-tion with respect to the airplane and safir check inWebOct 8, 2024 · Normal-Category Aeroplanes (CS-23) Certification Specifications group CS-23 Normal, Utility, Aerobatic and Commuter Aeroplanes Regulation group Initial Airworthiness 01 Jul 2024 Certification Specification (CS) CS-23 Amendment 5 and AMC & GM to CS-23 Issue 3 Aircraft cybersecurity Certification Specifications group safir beachWebSec. 23.562 — Emergency landing dynamic conditions. (a) Each seat/restraint system for use in a normal, utility, or acrobatic category airplane must be designed to protect each occupant during an emergency landing when— (1) Proper use is made of seats, safety belts, and shoulder harnesses provided for in the design; and they\\u0027re vh