Federal Aviation Regulations

Part 36: Noise standards: Aircraft type and airworthiness certification

Federal Aviation Regulations

Subpart A - General


• Sec. 36.1 - Applicability and definitions.
• Sec. 36.2 - Requirements as of date of application.
• Sec. 36.3 - Compatibility with airworthiness requirements.
• Sec. 36.5 - Limitation of part.
• Sec. 36.6 - Incorporation by reference.
• Sec. 36.7 - Acoustical change: Transport category large airplanes and jet airplanes.
• Sec. 36.9 - Acoustical change: Propeller-driven small airplanes and propeller-driven commuter category airplanes.
• Sec. 36.11 - Acoustical change: Helicopters.

Subpart B - Transport Category Large Airplanes and Jet Airplanes



• Sec. 36.101 - Noise measurement and evaluation.
• Sec. 36.103 - Noise limits.

Subpart D - Noise Limits for Supersonic Transport Category Airplanes



• Sec. 36.301 - Noise limits: Concorde.

Subpart F - Propeller Driven Small Airplanes and Propeller-Driven, Commuter Category Airplanes



• Sec. 36.501 - Noise limits.

Subpart H - Helicopters



• Sec. 36.801 - Noise measurement.
• Sec. 36.803 - Noise evaluation and calculation.
• Sec. 36.805 - Noise limits.

Subpart O - Operating Limitations and Information



• Sec. 36.1501 - Procedures, noise levels and other information.
• Sec. 36.1581 - Manuals, markings, and placards.
• Sec. 36.1583 - Noncomplying agricultural and fire fighting airplanes.

Appendices

• 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 6,000 Pounds