Annex 16. Том 1. Издание 1. AMENDMENT 1

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Annex 16. Том 1. Издание 1

AMENDMENT 1

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COVER SHEET TO AMENDMINT 1 INTERNATIONAL STANDARDS AND RECOMMENDED PRACTICES ENVIRONMENTAL PROTECTION ANNEX 16 TO THE CONVENTION ON INTERNATIONAL CIVIL AVLATION VOLUME I AIRCRAFT NQISE

Check-list of Amendments to Annex 16, Vcilume I Date of Effective Date Applicability First Edition 11 September 1981 26 November 1981 Amendment 1 adopted by Council on 30 March 1983 Replacement pages 3, 4, 8 and 28 29 July 1983 24 November 1983

AMENDMENT 1 to the International Standards and Recommended Practices ENVIRONMENTAL PROTECTION Annex 16 to the Convention on International Civil Aviation VOLUME I - AIRCRAFT NOISE 1. Insert the following replacement pages in Annex 16, Volume I First Edition to incorporate Amendment l whicYbecomes applicable on 24 November 1983 a Pages 3 and 4 b Page 8 Table of Contents Foreword c Page 28 Part V Delete Attachment G pages 112 to 114. Record the entry of this Amendment on page 2.

TABLE OF CONTENTS ................................... FOREWORD PART I . Definitions ............................. PART I1 . Aircraft Noise Certification .............. CHAPTER 1 . Administration .................. CHAPTER 2 . Subsonic5et aeroplanes . application for certificate of airworthiness for the ..... prototype accepted before 6 October 1977 2.1 Applicability ........................... 2.2 Noise evaluation measure ............... 2.3 Noise measurement points .............. 2.4 Maximum noise levels .................. 2.5 Trade-offs ............................. 2.6 Test procedures ........................ CHAPTER 3 . Subsonic jet aeroplanes . application for certificate of airworthiness for the prototype accepted on or after 6 October 1977 . . 3.1 Applicability .......................... 3.2 Noise measurements .................. 3.3 Reference noise measurements paints ... 3.4 Maximum noise levels ................. 3.5 Trade-offs ............................ 3.6 Noise certification reference procedures . 3.7 Test procedures ....................... CHAPTER 4 . Supersonic aeroplanes ............ 4.1 Supersonic aeroplanes . application for certificate of airworthiness for the prototype accepted before 1 January 1975 . 4.2 Supersonic aeroplanes . application for certificate of airworthiness for the prototype accepted on or after 1 January 1975 ......................... CHAPTER 5 . Propeller-driven aeroplanes over 5 700 kg ................................... 5.1 Applicability ........................... 5.2 Noise measurements ................... ..... 5.3 Reference noise measurement points .................. 5.4 Maximum noise levels 5.5 Trade-offs ............................. 5.6 Noise certification reference procedures . . 5.7 Test procedures ........................ CHAPTER 6 . Propeller-driven aeroplanes not exceeding 5 700 kg .......................... ........................... 6.1 Applicability 6.2 Noise evaluation measure ............... 6.3 Maximum noise levels .................. 6.4 Noise certification reference procedures . . 6.5 Test procedures ........................ CHAPTER 7 . propeller-driven STOL aeroplanes . CHAPTER 8 . Helicopters ...................... ........................... 8.1 Applicability 8.2 Noise evaluation measure ............... 8.3 Reference noise measurement points ..... 8.4 Maximum noise levels .................. 8.5 Trade-offs ............................. 8.6 Noise certification reference procedures . . 8.7 Test procedures ........................ CHAPTER 9 . Installed auxiliary power units APU and associated aircraft systems during ground operations ........................... PART 111 . Noise measurement for monitoring purposes ..................................... PART IV . International noise exposure reference ...................... unit for land-use planning PART V . Criteria for the application of noise ................. abatement operating procedures .- .. APPENDICES TO ANNEX 16- VOLUME I APPENDIX 1 . Evaluation method for noise certifi- cation of subsonic jet aeroplanes . application for certificate of airworthiness for the prototype ................. accepted before 6 October 1977 1 . Introduction ............................ 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 ... authorities and correcting measured data 6 . Nomenclature ........................... .... . 7 Mathematical formulation of noy tables . .................. 8 Sound attenuation in air 9 . Detailed correction procedures ............ ANNEX 16 . VOLUME I

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