14 CFR Part 36 - NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION
- SUBPART A — General (§§ 36.1 - 36.11)
- SUBPART B — Transport Category Large Airplanes and Jet Airplanes (§§ 36.101 - 36.105)
- SUBPART C — [Reserved]
- SUBPART D — Noise Limits for Supersonic Transport Category Airplanes (§§ 36.301 - 36.301)
- SUBPART E — [Reserved]
- SUBPART F — Propeller Driven Small Airplanes and Propeller-Driven, Commuter Category Airplanes (§§ 36.501 - 36.501)
- SUBPART G — [Reserved]
- SUBPART H — Helicopters (§§ 36.801 - 36.805)
- SUBPART I — N [Reserved]
- SUBPART O — Documentation, Operating Limitations and Information (§§ 36.1501 - 36.1583)
- Appendix A to Part 36 - Aircraft Noise Measurement and Evaluation Under § 36.101
- Appendix B to Part 36 - Noise Levels for Transport Category and Jet Airplanes Under § 36.103
- Appendixes C-E to Part 36 [Reserved]
- Appendix F to Part 36 - Flyover Noise Requirements for Propeller-Driven Small Airplane and Propeller-Driven, Commuter Category Airplane Certification Tests Prior to December 22, 1988
- Appendix G to Part 36 - Takeoff Noise Requirements for Propeller-Driven Small Airplane and Propeller-Driven, Commuter Category Airplane Certification Tests on or After December 22, 1988
- Appendix H to Part 36 - Noise Requirements For Helicopters Under Subpart H
- Appendix I to Part 36 [Reserved]
- Appendix J to Part 36 - Alternative Noise Certification Procedure for Helicopters Under Subpart H Having a Maximum Certificated Takeoff Weight of Not More Than 7,000 Pounds
Title 14 published on 2012-01-01
The following are only the Rules published in the Federal Register after the published date of Title 14.
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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 2012-01-01
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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2012-22714 RIN 2120-AJ96 Docket No. FAA-2012-0948 Notice No. 12-06 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed rulemaking (NPRM). Send comments on or before November 19, 2012. 14 CFR Part 36 This rulemaking proposes to adopt more stringent noise certification standards for helicopters that are certificated in the United States (U.S.). This rule would apply to applications for a new helicopter type design and for a supplemental type certificate for those new type designs. A helicopter type certificated under this standard would be designated as a Stage 3 helicopter. This rule proposes to adopt the same noise certification standards for helicopters that exist in the standards of the International Civil Aviation Organization (ICAO). The proposal of these more stringent noise certification standards into U.S. regulations is consistent with the FAA's goal of harmonizing U.S. regulations with international standards.
- Appendix A to Part 36 - Aircraft Noise Measurement and Evaluation Under § 36.101
- Appendix B to Part 36 - Noise Levels for Transport Category and Jet Airplanes Under § 36.103
- Appendixes C-E to Part 36 [Reserved]
- Appendix F to Part 36 - Flyover Noise Requirements for Propeller-Driven Small Airplane and Propeller-Driven, Commuter Category Airplane Certification Tests Prior to December 22, 1988
- Appendix G to Part 36 - Takeoff Noise Requirements for Propeller-Driven Small Airplane and Propeller-Driven, Commuter Category Airplane Certification Tests on or After December 22, 1988
- Appendix H to Part 36 - Noise Requirements For Helicopters Under Subpart H
- Appendix I to Part 36 [Reserved]
- Appendix J to Part 36 - Alternative Noise Certification Procedure for Helicopters Under Subpart H Having a Maximum Certificated Takeoff Weight of Not More Than 7,000 Pounds