Foreword
Part I - DEFINITIONS
Part II - AIRCRAFT NOISE CERTIFICATION
CHAPTER 1 - Administration
CHAPTER 2 - Subsonic jet aeroplanes - Application for
Type Certificate submitted before 6 October
1977
CHAPTER 3
CHAPTER 4
CHAPTER 5 - Propeller-driven aeroplanes over 8618 kg -
Application for Type Certificate submitted
before 1 January 1985
CHAPTER 6 - Propeller-driven aeroplanes not exceeding 8618
kg - Application for Type Certificate submitted
before 17 November 1988
CHAPTER 7 - Propeller-driven STOL aeroplanes
CHAPTER 8 - Helicopters
CHAPTER 9 - Installed auxiliary power units (APU) and
associated aircraft systems during ground operations
CHAPTER 10 - Propeller-driven aeroplanes not exceeding 8618
kg - Application for Type Certificate or
certification of Derived Version submitted on or
after 17 November 1988
CHAPTER 11 - Helicopters not exceeding 3175 kg maximum
certificated take-off mass
CHAPTER 12 - Supersonic aeroplanes
CHAPTER 13 - Tilt-rotor aircraft
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
APPENDIX 2 - Evaluation method for noise certification
APPENDIX 3 - Evaluation method for noise certification of
propeller-driven aeroplanes not exceeding 8618
kg - Application for Type Certificate submitted
before 17 November 1988
APPENDIX 4 - Evaluation method for noise certification of
helicopters not exceeding 3175 kg maximum
certificated take-off mass
APPENDIX 5 - Monitoring aircraft noise on and in the vicinity
of aerodromes
APPENDIX 6 - Evaluation method for noise certification of
propeller-driven aeroplanes propeller-driven
aeroplanes not exceeding 8618 kg - Application for
Type Certificate or certification of Derived
Version submitted on or after 17 November 1988
ATTACHMENT A - Equations for the calculation of noise levels
as a function of 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-rotor
aircraft
ATTACHMENT G - Guidelines for the administration of noise
certification documentation
ATTACHMENT H - Guidelines for obtaining helicopter noise data
for land-use planning purposes