Aircraft Operations. Volume II - Construction of Visual and Instrument ...

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III-2-3-6 Procedures — Aircraft Operations — Volume II 23/11/06 Direct entry IAF Procedure turn required 70° 70° Direct entry Figure III-2-3-3. Reversal procedures where offset initial not provided IAF ___________________ 70° IF FAF 70° Procedure turn required Capture region adjustment
Chapter 4 TERMINAL ARRIVAL ALTITUDE (TAA) 4.1 GENERAL 4.1.1 Terminal Arrival Altitudes (TAAs) are associated with an RNAV procedure based upon the T or Y arrangement described in Chapter 3. 4.1.2 TAAs shall be established for each aerodrome where RNAV instrument approach procedures have been established. 4.1.3 The TAA reference points are the initial approach and/or intermediate fixes. 4.1.4 Each TAA shall be calculated by taking the highest elevation in the area concerned, adding a clearance of at least 300 m (1 000 ft) and rounding the resulting value up to the next higher 50-m or 100-ft increment, as appropriate. If the difference between adjacent TAAs is insignificant (i.e. in the order of 100 m or 300 ft as appropriate) a minimum altitude applicable to all TAAs may be established. 4.1.5 A minimum altitude shall apply within a radius of 46 km (25 NM) of the RNAV waypoints on which the instrument approach is based. The minimum obstacle clearance when flying over mountainous areas should be increased by as much as 300 m (1 000 ft). 4.2 CONSTRUCTION 4.2.1 The standard arrangement consists of three TAAs: straight-in, right and left base. 4.2.2 TAA lateral boundaries are defined by the extension of the left and right base initial segments. The outer area boundaries are determined by arcs of 46 km (25 NM) radius centered on each of the three IAFs or on the two base area IAFs and the IF where the central initial segment is not provided. (See Figure III-2-4-1 and Figure III-2-4-2). 4.3 BUFFER AREA Each TAA is surrounded by a buffer area of 9 km (5 NM). If obstacles within the buffer area are higher than the highest obstacle within the TAA area, then the minimum altitude shall be calculated by taking the highest elevation in the buffer area, adding a clearance of at least 300 m (1 000 ft) and rounding the resulting value to the nearest 50 m or 100 ft. 4.4 TAA STEP-DOWN ARCS AND SUBSECTORS 4.4.1 To accommodate terrain diversity, operational constraints or excessive descent gradients, an additional circular boundary or “step-down arc” may be defined dividing a terminal arrival altitude (TAA) into two areas with III-2-4-1 23/11/06
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Doc 8168 OPS/611 Procedures for Air
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TABLE OF CONTENTS FOREWORD ........
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Table of Contents (v) Chapter 5. Pu
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Table of Contents (vii) Chapter 9.
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Table of Contents (ix) 4.3 Intermed
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Table of Contents (xi) Chapter 5. S
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Table of Contents (xiii) Appendix t
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(xvi) Procedures — Aircraft Opera
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(xviii) Procedures — Aircraft Ope
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(xx) Procedures — Aircraft Operat
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(xxii) Procedures — Aircraft Oper
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(xxiv) Procedures — Aircraft Oper
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Section 1 DEFINITIONS, ABBREVIATION
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I-1-1-2 Procedures — Aircraft Ope
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Chapter 2 ABBREVIATIONS (used in th
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Part I — Section 1, Chapter 2 I-1
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Section 2 GENERAL PRINCIPLES I-2-(i
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Appendix to Chapter 1 CONVERSION TA
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Part I — Section 2, Chapter 1, Ap
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I-2-2-10 Procedures — Aircraft Op
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Chapter 1 INTRODUCTION TO DEPARTURE
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Chapter 2 GENERAL CONCEPTS FOR DEPA
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I-3-3-App-2 Procedures — Aircraft
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Section 4 ARRIVAL AND APPROACH PROC
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Chapter 3 INITIAL APPROACH SEGMENT
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I-4-3-App A-2 Procedures — Aircra
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I-4-3-App A-10 Procedures — Aircr
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Appendix B to Chapter 3 REDUCTION O
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Appendix C to Chapter 3 CONSTRUCTIO
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Chapter 4 INTERMEDIATE APPROACH SEG
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Chapter 6 MISSED APPROACH SEGMENT 6
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Chapter 7 VISUAL MANOEUVRING (CIRCL
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Chapter 8 MINIMUM SECTOR ALTITUDES
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Procedures for Air Navigation Servi
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Chapter 1 INSTRUMENT LANDING SYSTEM
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Part II — Section 1, Chapter 1 II
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Appendix A to Chapter 1 ILS: TURNIN
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Part II — Section 1, Chapter 1, A
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Appendix B to Chapter 1 STEEP GLIDE
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II-1-1-App C-2 Procedures — Aircr
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II-1-1-App D-2 Procedures — Aircr
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II-1-1-App D-4 Procedures — Aircr
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Chapter 2 OFFSET ILS 2.1 USE OF ILS
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II-1-3-2 Procedures — Aircraft Op
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II-1-3-10 Procedures — Aircraft O
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Chapter 4 OFFSET MLS 4.1 USE OF MLS
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Chapter 5 PAR Note.— Only PAR app
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Section 2 NON-PRECISION APPROACHES
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Chapter 2 MLS AZIMUTH ONLY 2.1 GENE
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Chapter 5 DF 5.1 GENERAL This chapt
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Section 3 EN-ROUTE CRITERIA II-3-(i
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Appendix A to Chapter 1 VOR AND NDB
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II-3-1-App B-2 Procedures — Aircr
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Chapter 1 HOLDING CRITERIA Note 1.
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Appendix A to Chapter 1 PARAMETERS
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II-4-1-App B-2 Procedures — Aircr
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II-Att-2 Procedures — Aircraft Op
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II-Att-4 Procedures — Aircraft Op
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Chapter 1 FIXES 1.1 FIX IDENTIFICAT
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III-1-2-2 Procedures — Aircraft O
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Part III — Section 3, Chapter 4 I
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III-3-4-App A-2 Procedures — Airc
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Chapter 6 PRECISION APPROACH PROCED
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III-3-7-App-2 Procedures — Aircra
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Section 4 QUALITY ASSURANCE (To be
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Chapter 1 RNAV DATABASE PATH TERMIN
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Chapter 3 PROCEDURE NAMING 3.1 GENE
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IV-1-2 Procedures — Aircraft Oper
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IV-1-10 Procedures — Aircraft Ope
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IV-1-12 Procedures — Aircraft Ope
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© ICAO 2006 10/06 Published by ICA
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