ICAO 7300 ANNEX 16 VOL.1 : 2011

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