US14 CFR14 CFR Part 22Secondary legislationIn force

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PART 22—XXX

Source

https://www.ecfr.gov/current/title-14/part-22

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Connexes dans United States

US14 CFR14 CFR Part 26Secondary legislationIn force

Continued Airworthiness and Safety Improvements for Transport Category Airplanes

14 CFR Part 26 establishes regulatory requirements for maintaining continued airworthiness and implementing safety improvements for transport category airplanes. The rule applies to type certificate holders, supplemental type certificate applicants, and airplane manufacturers, requiring development of design assessments, airworthiness directives, and Instructions for Continued Airworthiness (ICA). Key provisions address electrical wiring interconnection systems (EWIS) maintenance programs for turbine-powered transport aircraft with 30+ passenger capacity or 7,500+ pounds payload capacity, mandating comprehensive ICA development and review by FAA Aircraft Certification Service offices.

US14 CFR14 CFR Part 1Secondary legislationIn force

Definitions and Abbreviations

14 CFR Part 1 provides definitions and abbreviations for Federal Aviation Regulations. It defines key aviation terms including aircraft, air carriers, airports, air traffic control, airspace concepts, and related equipment. The regulation establishes standardized terminology for regulatory compliance and operational safety across US air transportation.

US14 CFR14 CFR Part 11Secondary legislationIn force

General Rulemaking Procedures

14 CFR Part 11 establishes general rulemaking procedures for FAA issuance, amendment, and repeal of regulations under the Administrative Procedure Act. It defines key procedural instruments including advance notices of proposed rulemaking (ANPRM), notices of proposed rulemaking (NPRM), supplemental notices (SNPRM), final rules, direct final rules, and petitions for exemption or rulemaking. The part outlines the FAA's framework for public notice and comment procedures, including circumstances for issuing final rules with request for comments without prior notice when impracticable or unnecessary.

US14 CFR14 CFR Part 21Secondary legislationIn force

Certification Procedures for Products and Articles

SFAR 88 establishes fuel tank system fault tolerance evaluation requirements for transport category turbine-powered airplanes with 30+ passenger capacity or 7,500+ pound payload capacity. Certificate holders must conduct safety reviews to ensure compliance with fuel tank design standards, develop necessary design changes, create maintenance and inspection instructions to prevent ignition sources, and submit reports for approval by the Aircraft Certification Service within specified compliance timeframes.

US14 CFR14 CFR Part 27Secondary legislationIn force

Airworthiness Standards: Normal Category Rotorcraft

14 CFR Part 27 establishes airworthiness standards for type certification of normal category rotorcraft weighing 7,000 pounds or less with up to nine passenger seats. It mandates safety requirements including combined safety belts and shoulder harnesses with single-point release for all occupants (effective post-September 1992), head injury protection, and compliance demonstration through testing or calculation across all loading conditions and weight/center-of-gravity combinations.