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[A1]
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Electronic Code of Federal Regulations
| e-CFR data is current as of October 21, 2019
TITLE 14—Aeronautics and Space
CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C—AIRCRAFT PART 36—NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION
Subpart A—GENERAL
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| Applicability and definitions. |
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| Requirements as of date of application. |
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| Compatibility with airworthiness requirements. |
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| Incorporation by reference. |
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| Acoustical change: Transport category large airplanes and jet airplanes. |
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| Acoustical change: Propeller-driven small airplanes and propeller-driven commuter category airplanes. |
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| Acoustical change: Helicopters. |
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| Acoustical change: Tiltrotor aircraft. |
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Subpart B—TRANSPORT CATEGORY LARGE AIRPLANES AND JET AIRPLANES
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| Noise measurement and evaluation. |
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| Flight Manual Statement of Chapter 4 equivalency. |
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| Flight Manual statement of Chapter 14 noise level equivalency. |
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Subpart C—[RESERVED]
Subpart D—NOISE LIMITS FOR SUPERSONIC TRANSPORT CATEGORY AIRPLANES
Subpart E—[RESERVED]
Subpart F—PROPELLER DRIVEN SMALL AIRPLANES AND PROPELLER-DRIVEN, COMMUTER CATEGORY AIRPLANES
Subpart G—[RESERVED]
Subpart H—HELICOPTERS
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| Noise evaluation and calculation. |
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Subparts I-J [Reserved]
Subpart K—TILTROTORS
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| Noise measurement and evaluation. |
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Subparts L-N [Reserved]
Subpart O—DOCUMENTATION, OPERATING LIMITATIONS AND INFORMATION
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| Procedures, noise levels and other information. |
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| Manuals, markings, and placards. |
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| Noncomplying agricultural and fire fighting airplanes. |
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| Appendixes C-E to Part 36 [Reserved] |
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| 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 |
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| 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 |
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| Appendix I to Part 36 [Reserved] |
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| 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 |
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