Annex 8. Издание 5. AMENDMENT No. 90

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Annex 8. Издание 5

AMENDMENT No. 90

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COVER SHEET TO AMENDMWT 90 INTERNATIONAL STANDARDS AIRWORTHINESS OF AIRCRAFT ANNEX 8 TO THE WNVJWTION ON INTERNATIONAL CIVIL AVIATION INTERNATIONAL CIVIL AVIATION ORGANIZATION

Check-List of Amendments to Annex 8 Fifth Edition Fifth Edition incorporating Amendments 1 to 86. Amendment 87 adopted by the Council on 12 November 1963. Amendment 88 adopted by the Council on 8 November 1967. Replacement pages 8, 9, 11 and 15. Amendment 89 approved by the Council on 2 April 1971. Replacement pages 7, 8 and 14. Amendment 90 adopted by the Council on 10 December 1971. Replacement pages 4, 5, 8, 9, 14, 15, '18, 20, 21, 23-39 and 41 Effective Date 1/4/62 1/4/64 8/3/68 - Date of Applicability 13/12/64 12/11/66 22/8/68 6/1/72 7/12/72

AMENDMENT 90 to the International Standards AIRWORTHINESS OF AIRCRAFT Annex 8 to the Convention on International Civil Aviation Amend Annex 8 Fifth Edition as follows to incorporate Amendment 90 which was adopted by the Council on 10 December 1971 and becomes applicable on 7 December 1972 1 Insert the following replacement pages a Pages 4 and 5 - Table of Contents b Pages 8 and 9 - Foreword c Pages 14, 15, 18, 20 and 21 - International Standards, Part I11 d Pages 23-39 and 41 - Acceptable Means of Compliance 2 Record entry of amendment on Page 2.

TABLE OF CONTENTS CHAPTER 3.-Structures ..................... .. ... .................................. 3.1.-General 3.1.1.-Weight and Weight Distribution ........ 3.1.2.-Limit Loads ........................... ............... 3.1.3.-Strength and Deformation 3.2.AAirspeeds ...................... ... .... , . 3.2.1.-Design Airspeeds .................... 3.2.2.-Limiting Airspeeds ..................... 3.3.-Flight Loads .............................. 3.3.1.-Manmuvring Loads .................... ........................ 3.3.2.-Gust Loads .................. 3.4.-Ground and Water Loads .................... 3.4.1.-Landing Conditions 3.5.-Miscellaneous Loads ..................... 3.6.-Flutter, Divergence and Vibration ........... .......................... 3.7.-Fatigue Strength International Standards ................... 1.-Certificate of Airworthiness 3.-Proof of Compliance with Appropriate Airworthi- ............................ ness Requirements ........... 4.-Continuing Airworthiness of Aircraft 4.1.-Determination of Continuing Airworthiness . . 4.2.-Infornation Related to Continuing Airworthi- ............................ ness of Aircraft ......... 5.-Validity of Certificate of Airworthiness 5.2.-Method of Rendering a Certificate of Air- .......................... u. orthiness Valid CHAPTER 4.-Design and Construction ...... .............. 6.-Temporary Loss of Airworthiness .................................. 4.1.-General 4.1.1.-Substantiating Tests .................... 4.1.2.-Materials .................... , ......... 4.1.3.-Fabrication Methods ................... ... 4.1.4.-Protection ........................ , , ................... 4.1.5.-Inspection Provisions ....................... 4.1.6.-Design Features 4.1.7.-Emergency Landing Provisions .......... ...................... 4.1.8.-Ground Handling ................................... 6.1.-Geleral ........................ 6.2.-Damage to Aircraft 7.-Standard Form of Certificate of Airworthiness .. ............ 8.-Aircraft Limitations and Information .............................. 1.1.-Applicability ..................... 1.2.-Number of Power.units 1.3.-Limitations ................................ 1.4.-Unsafe Features and Characteristics ......... ....................... 1.5.-Proof of Compliance CHAPTER 5.--Engines ............................ 5.1.-Scope ..................................... 5.2.-Design, Construction and Funct' .An g ....... 5.3.-Declared Ratings, Conditions and Limitations 5.4.-Tests ..................................... CHAPTER 2.-Flight ............................... 2.1.-General ................................... 2.2.-Performance ............................. 2.2.1.-General .............................. 2.2.2.-Minimum Performance ................. 2.2.2.1.-Takeoff ........................... 2.2.2.2.-Landing ........................... 2.2.3.-Scheduling of Performance .............. 2.2.3.1.-Take.off ........................... 2.2.3.2.-En Route .......................... 2.2.3.3.-Landing ............................ 2.3.-Flying Qualities ........................... 2.3.1.-Controllability ........................ 2.3.2.-Trim .................................. 2.3.3.-Stability .............................. 2.3.4.-Stalling .................... .. .... .. .. 2.3.5.-Flutter and Vibration ................. 6.1.-Scope ..................................... ....... 6.2.-Design, Construction and Functioning 6.3.-Declared Ratings, Conditions and Limitations 6.4.-Tests ..................................... ................ CHAPTER 7.-Powerplant InstaUation 7.1.-General .............................. .... . ................... 7.1.1.-Applicable Standards 7.1.2.-Compliance with Engine and Propeller ............................ Limitations .............. 7.1.3.-Control of Engine Rotation ...................... 7.1.4.-Engine Restart'.g 7.2.-Arrangement and Functioning .............. 7.2.1 .-Independence of Power-units ............ .................... 7.2.2.-Propeller Vibratioli

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