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

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Part I — Section 4, Chapter 1 I-4-1-3 1.8.2 The criteria taken into consideration for the classification of aeroplanes by categories is the indicated airspeed at threshold (Vat) which is equal to the stall speed Vso multiplied by 1.3 or stall speed Vs1g multiplied by 1.23 in the landing configuration at the maximum certificated landing mass. If both Vso and Vs1g are available, the higher resulting Vat shall be used. 1.8.3 The landing configuration which is to be taken into consideration shall be defined by the operator or by the aeroplane manufacturer. 1.8.4 Aircraft categories will be referred to throughout this document by their letter designations as follows: Category A — less than 169 km/h (91 kt) indicated airspeed (IAS) Category B — 169 km/h (91 kt) or more but less than 224 km/h (121 kt) IAS Category C — 224 km/h (121 kt) or more but less than 261 km/h (141 kt) IAS Category D — 261 km/h (141 kt) or more but less than 307 km/h (166 kt) IAS Category E — 307 km/h (166 kt) or more but less than 391 km/h (211 kt) IAS Category H — see 1.8.8, “Helicopters”. 1.8.5 The ranges of speeds (IAS) in Tables I-4-1-1 and I-4-1-2 are to be used in calculating procedures. For conversion of these speeds to TAS, see Part I, Section 1, Appendix to Chapter 1. 1.8.6 Permanent change of category (maximum landing mass). An operator may impose a permanent, lower, landing mass, and use of this mass for determining Vat if approved by the State of the Operator. The category defined for a given aeroplane shall be a permanent value and thus independent of changing day-to-day operations. 1.8.7 Restrictions on category and IAS. Where airspace requirements are critical for a specific category of aircraft, procedures may be based on lower speed category aircraft, provided use of the procedure is restricted to those categories. Alternatively the procedure may be designated as limited to a specific maximum IAS for a particular segment without reference to category. 1.8.8 Helicopters a) The stall speed method of calculating aircraft category does not apply to helicopters. Where helicopters are operated as aeroplanes, the procedure may be classified as Category A. However, specific procedures may be developed for helicopters and these shall be clearly designated “H”. Category H procedures shall not be promulgated on the same instrument approach chart (IAC) as joint helicopter/aeroplane procedures. b) Helicopter-only procedures should be designed using the same conventional techniques and practices as those pertaining to Category A aeroplanes. Some criteria such as minimum airspeeds and descent gradients may be different, but the principles are the same. c) The specifications for Category A aeroplane procedure design apply equally to helicopters, except as specifically modified herein. The criteria that are changed for helicopter-only procedures are appropriately indicated throughout the text. 1.8.9 For precision approach procedures, the dimensions of the aircraft are also a factor for the calculation of the OCH. For Category DL aircraft, additional OCA/H is provided, when necessary, to take into account the specific dimensions of these aircraft (see Part II, Section 1, Chapters 1 and 3 and Part III, Section 3, Chapter 6 (GBAS Cat I)). 23/11/06
I-4-1-4 Procedures — Aircraft Operations — Volume II 23/11/06 1.9 DESCENT GRADIENTS Throughout the document, optimum and maximum descent gradients are specified. The optimum is the operationally preferred descent gradient. This should only be exceeded where alternative means of satisfying obstacle clearance requirements are impracticable. The maximum gradient shall not be exceeded. (See also Section 4, Chapter 9.) Table I-4-1-1. Speeds (IAS) for procedure calculations in kilometres per hour (km/h) Aircraft category Vat Range of speeds for initial approach Range of final approach speeds Max speeds for visual manoeuvring (circling) Max speeds for missed approach Intermediate Final A
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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 4 INTERMEDIATE APPROACH SEG
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Chapter 6 MISSED APPROACH SEGMENT 6
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I-4-6-App-2 Procedures — Aircraft
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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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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 3 NON-PRECISION APPROACH PR
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Chapter 4 APV/BAROMETRIC VERTICAL N
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Chapter 6 PRECISION APPROACH PROCED
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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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© ICAO 2006 10/06 Published by ICA
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