PART 36—NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION

• § 36.1 Applicability and definitions
• § 36.2 Requirements as of date of application
• § 36.3 Compatibility with airworthiness requirements
• § 36.5 Limitation of part
• § 36.6 Incorporation by reference
• § 36.7 Acoustical change: Transport category large airplanes and jet airplanes
• § 36.9 Acoustical change: Propeller-driven small airplanes and propeller-driven commuter category airplanes
• § 36.11 Acoustical change: Helicopters
• § 36.13 Acoustical change: Tiltrotor aircraft
• § 36.101 Noise measurement and evaluation
• § 36.103 Noise limits
• § 36.105 Flight Manual Statement of Chapter 4 equivalency
• § 36.106 Flight Manual statement of Chapter 14 noise level equivalency
• § 36.301 Noise limits: Concorde
• § 36.501 Noise limits
• § 36.801 Noise measurement
• § 36.803 Noise evaluation and calculation
• § 36.805 Noise limits
• § 36.1101 Noise measurement and evaluation
• § 36.1103 Noise limits
• § 36.1501 Procedures, noise levels and other information
• § 36.1581 Manuals, markings, and placards
• § 36.1583 Noncomplying agricultural and fire fighting airplanes
• 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
• 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 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
• Appendix K to Part 36—Noise Requirements for Tiltrotors Under Subpart K