14 CFR 36, Subpart D - Noise Limits for Supersonic Transport Category Airplanes
Title 14 published on 2013-01-01
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§ 4321 - Congressional declaration of purpose
§ 106 - Federal Aviation Administration
§ 40113 - Administrative
§ 44701 - General requirements
§ 44702 - Issuance of certificates
§ 44704 - Type certificates, production certificates, airworthiness certificates, and design organization certificates
§ 44715 - Controlling aircraft noise and sonic boom
Executive Order ... 11514
Title 14 published on 2013-01-01
The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 36 after this date.
GPO FDSys XML | Text type regulations.gov FR Doc. 2013-00111 RIN 2120-AJ76 Docket No. FAA-2011-0629 Amdt. Nos. 21-97 36-29 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule. Effective March 11, 2013. 14 CFR Parts 21 and 36 This rule amends the regulations governing noise certification standards for issuing type and airworthiness certificates for a new civil, hybrid airplane-rotorcraft known as the tiltrotor. This noise standard establishes new noise limits and procedures as the basis to ensure consistent aviation noise reduction technology is incorporated in tiltrotors for environmental protection. It provides uniform noise certification standards for tiltrotors certificated in the United States and harmonizes the U.S. regulations with the standards of the International Civil Aviation Organization's (ICAO) Annex 16.