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

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I-4-3-App C-6 Procedures — Aircraft Operations — Volume II Note.— Units in following formulas: 23/11/06 SI units Non-SI units t s s v and w’ km/s NM/s Distances Km NM The values of v, w’ and h are given by Table I-4-3-App C-1 (lines 3, 8 and 6 respectively). D is the specified DME distance expressed in km (NM) and d1 is the tolerance of this DME indication: 3.2.4.2 Primary area d1 = 0.46 km (0.25 NM) + 0.0125 D a) Place the template point “a” on “Al”, with the template procedure axis parallel to the inbound track, and draw thecurve“l”(partoftheoutlineofthetemplate). b) In the same manner, place the template point “a” successively on “A2”, “A3” and “A4” to draw curves “2”, “3” and “4”. c) Draw the common tangents to curves “1” and “2”, “2” and “4”, “3” and “4” and the tangent from “0” to curve “l” and from “0” to curve “3”. 3.2.4.3 Secondary area. Draw the secondary area limit at a distance of 4.6 km (2.5 NM) from the boundary of the primary area. 3.2.5 Interface between initial segment area and base and procedure turn areas 3.2.5.1 General. The primary area of the initial segment, the boundaries of which are 4.6 km (2.5 NM) apart from the nominal path, shall be blended with the primary area of the turn procedure, which is described above in 3.1.2 (base turn) and 3.2.4 (procedure turn). The secondary areas of the two phases of the procedure shall be blended so that a constant width of 4.6 km (2.5 NM) is respected. 3.2.5.2 Construction of the secondary area outerboundary (see Figures I-4-3-App C-6 and I-4-3-App C-7). On one side of the initial segment path the outer boundaries of the two secondary areas will intersect. On the other side of the initial segment path, the outer boundary of the secondary area consists of an arc of circle, 9.2 km (5 NM) from the facility, and the tangent to that circle and the outer boundary of the secondary area of the turn. 3.2.5.3 Construction of the primary area boundary. The boundary of the primary area is drawn in 4.6 km (2.5 NM) from the outer boundary of the secondary area. 3.3.1 General 3.3 Protection area of racetrack and holding procedures Note.— The methods described in this paragraph are related to right turn procedures. For left turn procedures, the corresponding areas are symmetrical with respect to the inbound track.
Part I — Section 4, Chapter 3, Appendix C I-4-3-App C-7 3.3.1.1 The protection area of a racetrack procedure consists of a primary area and a secondary area; the protection area of a holding procedure consists of an area and a buffer area. Since the construction of the primary area of a racetrack and of the area of a holding is the same, they are referred to by the same term hereafter — the basic area of the procedure. 3.3.1.2 The construction of the basic area of the procedure is made in two steps. 3.3.1.2.1 The first step is to construct a template or to take a precalculated one from the Template Manual for Holding, Reversal and Racetrack Procedures (Doc 9371), for the appropriate time, speed and altitude. This template caters for all factors which can cause an aircraft to deviate from the nominal pattern except those related to the fix tolerance area. It is applicable to all types of procedures including VOR or NDB overhead, intersection of VOR radials, VOR/DME and their entries. 3.3.1.2.2 The second step is to draw the basic area of the procedure by moving the template-origin around the fix tolerance area for procedures overhead a facility or at the intersection of VOR radials, or by using it as described in 3.3.4 for VOR/DME procedures, and by adding areas to protect entries as required. 3.3.1.3 Finally, a secondary area of 4.6 km (2.5 NM) is added around the basic area for a racetrack, and a buffer area of 9.3 km (5.0 NM) is added around the basic area for a holding. 3.3.2 First step: construction of the template 3.3.2 (Reference Table I-4-3-App C-4 and Diagram I-4-3-App C-6) 3.3.2.1 The parameters used in the construction of the template are contained in Chapter 3, 3.6.2 for the racetrack and in Part II, Section 4, Chapter 1, 1.3, “Construction of holding areas”, for the holding procedures. 3.3.2.2 After completion of the calculations indicated in Table I-4-3-App C-4, the template is constructed as follows. 3.3.2.2.1 Draw a line representing the axis of the procedure and the nominal pattern. Locate point “a” at the procedure fix. (The radius of turn r is given at line 5 and the outbound length L is given at line 11 of Table I-4-3-App C-4.) 3.3.2.2.2 Influence of the navigation tolerances 3.3.2.2.2.1 Locate points “b” and “c” on the procedure axis (Table I-4-3-App C-4, lines 12 and 13); “b” and “c” represent the earliest (5 s after “a”) and the latest (11 s after “a”) still air positions of the beginning of the outbound turn. 3.3.2.2.2.2 Draw an arc of 180° with a radius r tangent to the procedure axis at “c”, which represents the latest still air outbound turn. Locate points “d”, “e”, “f” and “g” after 45, 90, 135 and 180° of turn from “c”. 3.3.2.2.2.3 Draw an arc of 270° with a radius r tangent to the procedure axis at “b”, which represents the earliest still air outbound turn. Locate points “h”, “o” and “p” after 180, 225 and 270° of turn from “b”. 3.3.2.2.2.4 From “g” draw two lines at 5° on each side of the nominal outbound leg. Locate points “il”, “i2”, “i3” and “i4’” on these lines (Table I-4-3-App C-4, lines 14 and 15). “i1” and “i3” are plotted (60T – 5) seconds after “g”; “i2” and “i4” should be (60T + 15) seconds after “h”, but for the sake of simplification they are plotted (60T + 21) seconds after “g”. il i2 i3 i4 determine the area containing the still air position of the beginning of the inbound turn. 23/11/06
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Doc 8168 OPS/611 Procedures for Air
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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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Section 4 ARRIVAL AND APPROACH PROC
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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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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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Appendix to Chapter 3 DERIVATION AN
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Part III — Section 1, Chapter 3,
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Part III — Section 1, Chapter 3,
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III-1-4-10 Procedures — Aircraft
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Chapter 5 SBAS RNAV 5.1.1 SBAS depa
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Chapter 7 RNP 7.1 EQUIPMENT REQUIRE
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Section 2 GENERAL CRITERIA III-2-(i
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Chapter 3 RNAV T- or Y-BAR PROCEDUR
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Part III — Section 2, Chapter 3 I
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Chapter 4 TERMINAL ARRIVAL ALTITUDE
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Chapter 1 DEPARTURE PROCEDURES 1.1
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Chapter 2 ARRIVAL AND APPROACH PROC
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Chapter 4 APV/BAROMETRIC VERTICAL N
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Chapter 6 PRECISION APPROACH PROCED
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Chapter 7 HOLDING PROCEDURES 7.1 GE
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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-1-10 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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