Annex 16. Том 1. Издание 3. AMENDMENT 5

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Annex 16. Том 1. Издание 3

AMENDMENT 5

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COVER SHEET TO AMENDMENT 5 INTERNATIONAL STANDARDS AND RECOMMENDED PRACTICES ENVIRONMENTAL PROTECTION ANNEX 16 TO THE CONVENTION ON INTERNATIONAL CIVIL AVIATION VOLUME I AIRCRAFT NOISE THlRD EDITION - JULY 1993 INTERNATIONAL CIVIL AVIATION ORGANIZATION

Checklist of Amendments to Annex 16, Volume I Efiective date Date of applicability Third Edition incorporates Amendments 1 to 4 26 July 1993 11 November 1993 Amendment 5 adopted by the Council on 19 March 1997 Replacement pages iii, iv, vii to ix, 1, 5 tog, 13, 15 to 18,20,22, 23, 61, 79, 84, 88,97 to 100, 104 to 106, 108, 109, 111 and 112 21 July 1997 6 November 1997

Transmittal Note Amendment 5 to the International Standards and Recommended Practices ENVIRONMENTAL PROTECTION Annex 16 to the Convention on International Civil Aviation Volume I - Aircraft Noise To incorporate Amendment 5, which becomes applicable on 6 November 1997 1. Insert the following new and replacement pages dated 611 1/97 a iii and iv - b Pages vii to ix - c Page 1 - d Pages 5 to 8 - e Page 13 - f Pages 15 to 18 - g Page 20 - h Pages 22 and 23 - i Pages 61, 79, 84 and 88 - j Pages 97 to 100 - k Pages 104 to 106, 108 and 109 - 1 Pages 11 1 and 1 12 - Table of Contents Foreword Part I Part 11, Chapter 3 Part 11, Chapter 6 Part 11, Chapter 8 Part 11, Chapter 10 Part 11, Chapter 11 Appendix 2 Appendix 4 Appendix 6 Attachment A 2. Record the entry of this amendment on page ii.

TABLE OF CONTENTS Page Page ....... Foreword .................................. v 5.6 Noise certification reference procedures 11 ........................ 5.7 Test procedures 12 ........................ Part I . DEFINITIONS 1 CHAPTER 6 . Propeller-driven aeroplanes not exceeding 8 618 kg - application for certificate of airworthiness .... ..... . Part LI AIRCW NOISE CERTIFICATION 2 for the prototype accepted before 17 November 1988 13 .......................... 6.1 Applicability 13 .................... CHAPTER 1 . Administration 2 6.2 Noise evaluation measure ................. 13 ................... 6.3 Maximum noise levels 13 CHAFTER 2 . Subsonic Jet aeroplanes - application 6.4 Noise certification reference procedures ....... 13 for certificate of airworthiness for the prototype 6.5 Test procedures ........................ 13 accented before 6 October 1977 .................. 3 .......................... 2.1 Applicability 3 ................. 2.2 Noise evaluation measure 3 ................. 2.3 Noise measurement points 3 2.4 Maximum noise levels ................... 3 ............................ 2.5 Trade-offs 4 ........................ 2.6 Test procedures 4 CHAPTER 3 . 1 . Subsonic jet aeroplanes - application for certificate of airworthiness for the prototype accepted on or after 6 October 1977 2 . Propeller-driven aeroplanes over 5 700 kg - application for certificate of airworthiness for the prototype accepted on or after 1 January 1985 and before 17 November 1988 3 . Propeller-driven aeroplanes over 8 618 kg - application for certificate of airworthiness for the prototype accepted on or after ......................... 17November1988 5 .......................... 3.1 Applicability 5 ..................... 3.2 Noise measurements 5 3.3 Reference noise measurement points .......... 5 .................... 3.4 Maximum noise levels 6 ............................ 3.5 Trade-offs 6 3.6 Noise certification reference procedures ....... 7 ........................ 3.7 Test procedures 8 ............... CHAPTER 4 . Supersonic aeroplanes 9 4.1 Supersonic aeroplanes - application for certificate of airworthiness for the prototype ............. accepted before 1 January 1975 9 4.2 Supersonic aeroplanes . application for certificate of airworthiness for the prototype accepted on or after 1 January 1975 .......... 9 CHAPTER 5 . Propeller-driven aeroplanes over 5 700 kg . ....... . CHAPTER 7 Propeller-driven STOL aeroplanes 14 ....................... . CHAPTER 8 Helicopters 15 .......................... 8.1 Applicability 15 ................. 8.2 Noise evaluation measure 15 .......... 8.3 Reference noise measurement points 15 ................... 8.4 Maximum noise levels 15 ............................ 8.5 Trade-offs 16 ....... 8.6 Noise certification reference procedures 16 ........................ 8.7 Test procedures 17 CHAPTER 9 . Installed auxiliary power units APU and .... associated aircraft systems during ground operations I9 CHAPTER 10 . Propeller-driven aeroplanes not exceeding 8 618 kg - application for certificate of airworthiness for the prototype or derived version accepted on or ........................ after 17 November 1988 20 .......................... 10.1 Applicability 20 ................. 10.2 Noise evaluation measure 20 .......... 10.3 Reference noise measurement points 20 ................... 10.4 Maximum noise levels 20 ....... 10.5 Noise certification reference procedures 20 ........................ 10.6 Test procedures 21 CHAPTER 11 . Helicopters not exceeding 2 730 kg ................ maximum certificated take-off mass 22 .......................... 11.1 Applicability 22 ................. 1 1.2 Noise evaluation measure 22 .......... 11.3 Reference noise measurement point 22 .................... 11.4 Maximum noise level 22 ........ 11.5 Noise certification reference procedure 22 ........................ 1 1.6 Test procedures 23 application for certificate of airworthiness for . ......... the prototype accepted before 1 January 1985 10 Part rn NOISE MEASUREMENT FOR .................... MONITORING PURPOSES 24 .......................... 5.1 Avvlicability 10 ..................... 5.2 Noise measurements 10 part IV . ASSESSMENT OF . AIRPORT NOISE ... 25 5.3 Reference noise measurement points .......... 10 ................... 5.4 Mavimum noise levels 11 Part V . CRITERIA FOR THE APPLICATION OF ............................ 5.5 Trade-offs 1 1 NOISE ABATEMENT OPERATING PROCEDURES . 26 ANNEX 16 . VOLUME I iii

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