PART II. AIRCRAFT NOISE CERTIFICATION
CHAPTER 1. ADMINISTRATION
CHAPTER 2. SUBSONIC JET AEROPLANES — Applicationfor Type Certificate submitted before 6 October 1977
2.2 Noise evaluation measure
2.3 Noise measurement points
CHAPTER 3.1.— SUBSONIC JET AEROPLANES — Application for Type Certificate submitted on or after 6 October 1977 and before 1 January 20062.— PROPELLER-DRIVEN AEROPLANES OVER 8 618 kg — Application for TypeCertificate submitted on or after 1 January 1985 and before 1 January 2006
3.3 Noise measurement points
3.6 Noise certification reference procedures
CHAPTER 4.1.— SUBSONIC JET AEROPLANES AND PROPELLER-DRIVEN AEROPLANESWITH MAXIMUM CERTIFICATED TAKE-OFF MASS 55 000 kg AND OVER— Application for Type Certificate submitted on or after 1 January 2006 andbefore 31 December 20172.— SUBSONIC JET AEROPLANES WITH MAXIMUM CERTIFICATEDTAKE-OFF MASS LESS THAN 55 000 kg — Application for Type Certificatesubmitted on or after 1 January 2006 and before 31 December 20203.— PROPELLER-DRIVEN AEROPLANES WITH MAXIMUM CERTIFICATEDTAKE-OFF MASS OVER 8 618 kg AND LESS THAN 55
4.3 Reference noise measurement points
4.5 Noise certification reference procedures
CHAPTER 5. PROPELLER-DRIVEN AEROPLANES OVER8 618 kg — Application for Type Certificate submittedbefore 1 January 1985
5.3 Noise measurement points
5.6 Noise certification reference procedures
CHAPTER 6. PROPELLER-DRIVEN AEROPLANESNOT EXCEEDING 8 618 kg — Application forType Certificate submitted before 17 November 1988
6.2 Noise evaluation measure
6.4 Noise certification reference procedures
CHAPTER 7. PROPELLER-DRIVEN STOL AEROPLANES
8.2 Noise evaluation measure
8.3 Reference noise measurement points
8.6 Noise certification reference procedures
CHAPTER 9. INSTALLED AUXILIARY POWER UNITS (APU) AND ASSOCIATED AIRCRAFT SYSTEMS DURING GROUND OPERATIONS
CHAPTER 10. PROPELLER-DRIVEN AEROPLANES NOT EXCEEDING 8 618 kg — Application for Type Certificateor Certification of Derived Version submitted onor after 17 November 1988
10.2 Noise evaluation measure
10.3 Reference noise measurement points
10.4 Maximum noise levels
10.5 Noise certification reference procedures
CHAPTER 11. HELICOPTERS NOT EXCEEDING 3 175 kg MAXIMUM CERTIFICATED TAKE-OFF MASS
11.2 Noise evaluation measure
11.3 Reference noise measurement points
11.5 Noise certification reference procedures
CHAPTER 12. SUPERSONIC AEROPLANES
12.1 Supersonic aeroplanes — Application for Type Certificate submitted before 1 January 1975
12.2 Supersonic aeroplanes — Application for Type Certificate submitted on or after 1 January 1975
13.2 Noise evaluation measure
13.3 Noise measurement reference points
13.4 Maximum noise levels
13.6 Noise certification reference procedures
CHAPTER 14.1.— SUBSONIC JET AEROPLANES AND PROPELLER-DRIVEN AEROPLANESWITH MAXIMUM CERTIFICATED TAKE-OFF MASS 55 000 kg AND OVER— Application for Type Certificate submitted on or after 31 December 20172.— SUBSONIC JET AEROPLANES WITH MAXIMUM CERTIFICATEDTAKE-OFF MASS LESS THAN 55 000 kg — Application for Type Certificatesubmitted on or after 31 December 20203.— PROPELLER-DRIVEN AEROPLANES WITH MAXIMUM CERTIFICATEDTAKE-OFF MASS OVER 8 618 kg AND LESS THAN 55 000 kg — Applicationfor Type Certificate submitted on or after 31 December 2020
14.3 Reference noise measurement points
14.4 Maximum noise levels
14.5 Noise certification reference procedures
PART III. NOISE MEASUREMENT FOR MONITORING PURPOSES
PART IV. ASSESSMENT OF AIRPORT NOISE
PART V. BALANCED APPROACH TO NOISE MANAGEMENT
APPENDIX 1. EVALUATION METHOD FOR NOISE CERTIFICATION OF SUBSONIC JET AEROPLANES — Application for Type Certificate submitted before 6 October 1977
2. NOISE CERTIFICATION TEST AND MEASUREMENT CONDITIONS
3. MEASUREMENT OF AEROPLANE NOISE RECEIVED ON THE GROUND
4. CALCULATION OF EFFECTIVE PERCEIVED NOISE LEVEL FROM MEASURED NOISE DATA
5. REPORTING OF DATA TO THE CERTIFICATING AUTHORITY AND CORRECTING MEASURED DATA
7. MATHEMATICAL FORMULATION OF NOY TABLES
8. SOUND ATTENUATION IN AIR
9. DETAILED CORRECTION PROCEDURES
2. NOISE CERTIFICATION TEST AND MEASUREMENT CONDITIONS
3. MEASUREMENT OF AIRCRAFT NOISE RECEIVED ON THE GROUND
4. CALCULATION OF EFFECTIVE PERCEIVED NOISE LEVEL FROM MEASURED NOISE DATA
5. REPORTING OF DATA TO THE CERTIFICATING AUTHORITY
7. SOUND ATTENUATION IN AIR
8. ADJUSTMENT OF AIRCRAFT FLIGHT TEST RESULTS
APPENDIX 3. EVALUATION METHOD FOR NOISE CERTIFICATION OF PROPELLER-DRIVEN AEROPLANES NOT EXCEEDING8 618 kg — Application for Type Certificatesubmitted before 17 November 1988
2. NOISE CERTIFICATION TEST AND MEASUREMENT CONDITIONS
3. MEASUREMENT OF AEROPLANE NOISE RECEIVED ON THE GROUND
4. REPORTING OF DATA TO THE CERTIFICATING AUTHORITY AND CORRECTION OF MEASURED DATA
APPENDIX 4. EVALUATION METHOD FOR NOISE CERTIFICATION OF HELICOPTERS NOT EXCEEDING 3 175 kg MAXIMUMCERTIFICATED TAKE-OFF MASS
2. NOISE CERTIFICATION TEST AND MEASUREMENT CONDITIONS
4. MEASUREMENT OF HELICOPTER NOISE RECEIVED ON THE GROUND
5. ADJUSTMENT TO TEST RESULTS
6. REPORTING OF DATA TO THE CERTIFICATING AUTHORITYAND VALIDITY OF RESULTS
APPENDIX 5. MONITORING AIRCRAFT NOISE ON AND IN THE VICINITY OF AERODROMES
4. FIELD EQUIPMENT INSTALLATION
APPENDIX 6. EVALUATION METHOD FOR NOISE CERTIFICATION OF PROPELLER-DRIVEN AEROPLANES NOT EXCEEDING 8 618 kg — Application for Type Certificateor Certification of Derived Version submittedon or after 17 November 1988
2. NOISE CERTIFICATION TEST AND MEASUREMENT CONDITIONS
4. MEASUREMENT OF AEROPLANE NOISE RECEIVED ON THE GROUND
5. ADJUSTMENT TO TEST RESULTS
6. REPORTING OF DATA TO THE CERTIFICATING AUTHORITY AND VALIDITY OF RESULTS
ATTACHMENTS TO ANNEX 16, VOLUME I
ATTACHMENT A. EQUATIONS FOR THE CALCULATION OF MAXIMUM PERMITTED NOISE LEVELS AS A FUNCTIONOF TAKE-OFF MASS
ATTACHMENT B. GUIDELINES FOR NOISE CERTIFICATION OF PROPELLER-DRIVEN STOL AEROPLANES
ATTACHMENT C. GUIDELINES FOR NOISE CERTIFICATION OF INSTALLED AUXILIARY POWER UNITS (APU) AND ASSOCIATED AIRCRAFT SYSTEMS DURING GROUND OPERATION
ATTACHMENT D. GUIDELINES FOR EVALUATING AN ALTERNATIVE METHOD OF MEASURING HELICOPTER NOISE DURING APPROACH
ATTACHMENT E. APPLICABILITY OF ANNEX 16 NOISE CERTIFICATION STANDARDS FOR PROPELLER-DRIVEN AEROPLANES
ATTACHMENT F. GUIDELINES FOR NOISE CERTIFICATION OF TILT-ROTORS
ATTACHMENT G. GUIDELINES FOR THE ADMINISTRATION OF NOISE CERTIFICATION DOCUMENTATION
ATTACHMENT H. GUIDELINES FOR OBTAINING HELICOPTER NOISE DATA FOR LAND-USE PLANNING PURPOSES