CMA-9000.pdf

OPERATOR'S MANUAL FLIGHT MANAGEMENT SYSTEM

CMA-9000 OPERATIONAL PROGRAM S/W 169-614876-056

Esterline CMC Electronics 600 Dr. Frederik Philips Boulevard Ville Saint-Laurent, Quebec, Canada H4M 2S9

This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.

OPERATOR'S MANUAL FLIGHT MANAGEMENT SYSTEM

CMA-9000 OPERATIONAL PROGRAM S/W 169-614876-056

Esterline CMC Electronics 600 Dr. Frederik Philips Boulevard Ville Saint-Laurent, Quebec, Canada H4M 2S9 Item No.: 930-600166-000

July 17, 2013

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

LIST OF EFFECTIVE PAGES NOTE The portion of the text affected by the latest change is indicated by a vertical line in the margin of the page. Changes to illustrations are indicated by miniature pointing hands or black vertical lines. Original ...................0 ..................July 17, 2013

SUBJECT

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Record of Revisions

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Table of Contents

TC-1 TC-2

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Purpose of Operator's Manual Operational Approval and Limitations

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

LIST OF EFFECTIVE PAGES SUBJECT 1 - Introduction

PAGE 1-i 1-ii 1-1 1-2 1-3 1-4 1-5 1-6 1-7 1-8 1-9 1-10 1-11 1-12 1-13 1-14

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2 - Control and Display

2-i 2-ii 2-1 2-2 2-3 2-4 2-5 2-6 2-7 2-8 2-9 2-10 2-11 2-12 2-13 2-14 2-15 2-16 2-17 2-18 2-19 2-20

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3 - Preflight

3-i 3-ii 3-1 3-2 3-3 3-4 3-5 3-6 3-7 3-8

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PAGE 3-9 3-10 3-11 3-12 3-13 3-14 3-15 3-16 3-17 3-18 3-19 3-20 3-21 3-22 3-23 3-24 3-25 3-26 3-27 3-28 3-29 3-30

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4 - Departures

4-i 4-ii 4-1 4-2 4-3 4-4 4-5 4-6

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5 - Enroute

5-i 5-ii 5-1 5-2 5-3 5-4 5-5 5-6 5-7 5-8 5-9 5-10 5-11 5-12 5-13 5-14 5-15 5-16 5-17

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PAGE 5-18 5-19 5-20 5-21 5-22 5-23 5-24 5-25 5-26 5-27 5-28 5-29 5-30 5-31 5-32 5-33 5-34 5-35 5-36

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

6 - Arrivals

6-i 6-ii 6-1 6-2 6-3 6-4 6-5 6-6

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7 - Approach

7-i 7-ii 7-1 7-2 7-3 7-4 7-5 7-6 7-7 7-8 7-9 7-10 7-11 7-12 7-13 7-14 7-15 7-16 7-17 7-18 7-19 7-20

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PAGE 7-21 7-22 7-23 7-24 7-25 7-26 7-27 7-28

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8 - Post-Flight Procedures

8-i 8-ii 8-1 8-2

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9 - Direct-To/Intercept

9-i 9-ii 9-1 9-2 9-3 9-4 9-5 9-6

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10 - Holding Pattern Navigation

10-i 10-ii 10-1 10-2 10-3 10-4 10-5 10-6 10-7 10-8 10-9 10-10 10-11 10-12

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11 - Tactical Functions

11-i 11-ii 11-1 11-2 11-3 11-4 11-5 11-6 11-7 11-8 11-9 11-10 11-11

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PAGE 11-12 11-13 11-14 11-15 11-16 11-17 11-18 11-19 11-20 11-21 11-22 11-23 11-24 11-25 11-26 11-27 11-28

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12 -Navigation Sensors

12-i 12-ii 12-1 12-2 12-3 12-4 12-5 12-6 12-7 12-8 12-9 12-10 12-11 12-12 12-13 12-14

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13 - Radio Tuning Pages

13-i 13-ii 13-1 13-2 13-3 13-4 13-5 13-6 13-7 13-8 13-9 13-10 13-11 13-12 13-13 13-14

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PAGE 13-15 13-16 13-17 13-18 13-19 13-20 13-21 13-22 13-23 13-24 13-25 13-26 13-27 13-28 13-29 13-30 13-31 13-32 13-33 13-34 13-35 13-36 13-37 13-38 13-39 13-40 13-41 13-42 13-43 13-44 13-45 13-46 13-47 13-48

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

14 -Performance Functions

14-i 14-ii 14-1 14-2 14-3 14-4 14-5 14-6

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15 - RNP Capability

15-i 15-ii 15-1 15-2 15-3

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16 –MCDU Functions

16-i 16-ii 16-1 16-2 16-3 16-4

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17 - Abnormal Procedures

17-i 17-ii 17-1 17-2 17-3 17-4 17-5 17-6

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18A - Performance VNAV For A300/310

18A-i 18A-ii 18A-1 18A-2 18A-3 18A-4 18A-5 18A-6 18A-7 18A-8 18A-9 18A-10 18A-11 18A-12 18A-13 18A-14 18A-15 18A-16 18A-17 18A-18 18A-19 18A-20 18A-21 18A-22 18A-23 18A-24 18A-25 18A-26 18A-27 18A-28 18A-29

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PAGE 18A-30 18A-31 18A-32 18A-33 18A-34 18A-35 18A-36 18A-37 18A-38 18A-39 18A-40 18A-41 18A-42 18A-43 18A-44 18A-45 18A-46 18A-47 18A-48 18A-49 18A-50 18A-51 18A-52 18A-53 18A-54 18A-55 18A-56

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

18B - Performance VNAV For SUPERJET 100

18B-i 18B-ii 18B-1 18B-2 18B-3 18B-4 18B-5 18B-6 18B-7 18B-8 18B-9 18B-10 18B-11 18B-12 18B-13 18B-14 18B-15 18B-16 18B-17 18B-18 18B-19 18B-20 18B-21

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PAGE 18B-22 18B-23 18B-24 18B-25 18B-26 18B-27 18B-28 18B-29 18B-30 18B-31 18B-32 18B-33 18B-34 18B-35 18B-36 18B-37 18B-38 18B-39 18B-40 18B-41 18B-42 18B-43 18B-44 18B-45 18B-46 18B-47 18B-48 18B-49 18B-50 18B-51 18B-52

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

19 - Datalink Functions

19-i 19-ii 19-1 19-2 19-3 19-4 19-5 19-6 19-7 19-8 19-9 19-10 19-11 19-12 19-13 19-14 19-15 19-16 19-17

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LIST OF EFFECTIVE PAGES SUBJECT

PAGE 19-18 19-19 19-20 19-21 19-22 19-23 19-24 19-25 19-26 19-27 19-28 19-29 19-30 19-31 19-32 19-33 19-34 19-35 19-36 19-37 19-38 19-39 19-40 19-41 19-42 19-43 19-44

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13

Appendix A - FMS Pages - Detailed Descriptions

A-i A-ii A-1 A-2 A-3 A-4 A-5 A-6 A-7 A-8 A-9 A-10 A-11 A-12 A-13 A-14 A-15 A-16 A-17 A-18 A-19 A-20 A-21

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PAGE A-22 A-23 A-24 A-25 A-26 A-27 A-28 A-29 A-30 A-31 A-32 A-33 A-34 A-35 A-36 A-37 A-38 A-39 A-40 A-41 A-42 A-43 A-44 A-45 A-46 A-47 A-48 A-49 A-50 A-51 A-52 A-53 A-54 A-55 A-56 A-57 A-58 A-59 A-60 A-61 A-62 A-63 A-64 A-65 A-66 A-67 A-68 A-69 A-70 A-71 A-72

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13

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PAGE A-73 A-74 A-75 A-76 A-77 A-78 A-79 A-80 A-81 A-82 A-83 A-84 A-85 A-86 A-87 A-88 A-89 A-90 A-91 A-92 A-93 A-94 A-95 A-96 A-97 A-98 A-99 A-100 A-101 A-102 A-103 A-104 A-105 A-106 A-107 A-108 A-109 A-110 A-111 A-112 A-113 A-114 A-115 A-116 A-117 A-118 A-119 A-120 A-121 A-122 A-123

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13

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LIST OF EFFECTIVE PAGES SUBJECT

Appendix A300-A - CMA-9000 VNAV A300/310 Display Pages Detailed Descriptions

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PAGE A-124 A-125 A-126 A-127 A-128 A-129 A-130 A-131 A-132 A-133 A-134 A-135 A-136 A-137 A-138 A-139 A-140 A-141 A-142 A-143 A-144

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

A300-A-i A300-A-ii A300-A-1 A300-A-2 A300-A-3 A300-A-4 A300-A-5 A300-A-6 A300-A-7 A300-A-8 A300-A-9 A300-A-10 A300-A-11 A300-A-12 A300-A-13 A300-A-14 A300-A-15 A300-A-16 A300-A-17 A300-A-18 A300-A-19 A300-A-20 A300-A-21 A300-A-22 A300-A-23 A300-A-24 A300-A-25 A300-A-26

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PAGE A300-A-27 A300-A-28 A300-A-29 A300-A-30 A300-A-31 A300-A-32 A300-A-33 A300-A-34 A300-A-35 A300-A-36 A300-A-37 A300-A-38 A300-A-39 A300-A-40 A300-A-41 A300-A-42 A300-A-43 A300-A-44 A300-A-45 A300-A-46 A300-A-47 A300-A-48 A300-A-49 A300-A-50 A300-A-51 A300-A-52 A300-A-53 A300-A-54 A300-A-55 A300-A-56 A300-A-57 A300-A-58 A300-A-59 A300-A-60 A300-A-61 A300-A-62 A300-A-63 A300-A-64 A300-A-65 A300-A-66 A300-A-67 A300-A-68 A300-A-69 A300-A-70 A300-A-71 A300-A-72 A300-A-73 A300-A-74

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

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LIST OF EFFECTIVE PAGES SUBJECT Appendix SSJ 100-A - CMA-9000 VNAV SUPERJET 100 Display Pages - Detailed Descriptions

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PAGE

DATE

SSJ 100-A-i SSJ 100-A-ii SSJ 100-A-1 SSJ 100-A-2 SSJ 100-A-3 SSJ 100-A-4 SSJ 100-A-5 SSJ 100-A-6 SSJ 100-A-7 SSJ 100-A-8 SSJ 100-A-9 SSJ 100-A-10 SSJ 100-A-11 SSJ 100-A-12 SSJ 100-A-13 SSJ 100-A-14 SSJ 100-A-15 SSJ 100-A-16 SSJ 100-A-17 SSJ 100-A-18 SSJ 100-A-19 SSJ 100-A-20 SSJ 100-A-21 SSJ 100-A-22 SSJ 100-A-23 SSJ 100-A-24 SSJ 100-A-25 SSJ 100-A-26 SSJ 100-A-27 SSJ 100-A-28 SSJ 100-A-29 SSJ 100-A-30 SSJ 100-A-31 SSJ 100-A-32 SSJ 100-A-33 SSJ 100-A-34 SSJ 100-A-35 SSJ 100-A-36 SSJ 100-A-37 SSJ 100-A-38 SSJ 100-A-39 SSJ 100-A-40 SSJ 100-A-41 SSJ 100-A-42 SSJ 100-A-43 SSJ 100-A-44 SSJ 100-A-45 SSJ 100-A-46 SSJ 100-A-47 SSJ 100-A-48

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LIST OF EFFECTIVE PAGES SUBJECT

PAGE SSJ 100-A-49 SSJ 100-A-50 SSJ 100-A-51 SSJ 100-A-52 SSJ 100-A-53 SSJ 100-A-54 SSJ 100-A-55 SSJ 100-A-56 SSJ 100-A-57 SSJ 100-A-58 SSJ 100-A-59 SSJ 100-A-60 SSJ 100-A-61 SSJ 100-A-62 SSJ 100-A-63 SSJ 100-A-64 SSJ 100-A-65 SSJ 100-A-66

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 Blank

Appendix FANS-A – FMS FANS Pages - Detailed Descriptions

FANS-A-i FANS-A-ii FANS-A-1 FANS-A-2 FANS-A-3 FANS-A-4 FANS-A-5 FANS-A-6 FANS-A-7 FANS-A-8 FANS-A-9 FANS-A-10 FANS-A-11 FANS-A-12 FANS-A-13 FANS-A-14 FANS-A-15 FANS-A-16 FANS-A-17 FANS-A-18 FANS-A-19 FANS-A-20 FANS-A-21 FANS-A-22 FANS-A-23 FANS-A-24 FANS-A-25 FANS-A-26 FANS-A-27 FANS-A-28 FANS-A-29 FANS-A-30

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This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.

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LIST OF EFFECTIVE PAGES SUBJECT

PAGE FANS-A-31 FANS-A-32 FANS-A-33 FANS-A-34 FANS-A-35 FANS-A-36 FANS-A-37 FANS-A-38 FANS-A-39 FANS-A-40

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13

Appendix B - Navigation Leg Type Definitions

B-i B-ii B-1 B-2 B-3 B-4 B-5 B-6 B-7 B-8 B-9 B-10 B-11 B-12 B-13 B-14 B-15 B-16 B-17 B-18 B-19 B-20

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Appendix C - Navigation Displays

C-i C-ii C-1 C-2 C-3 C-4 C-5 C-6 C-7 C-8 C-9 C-10

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Appendix D - CMA-9000 FMS Display Pages Flow Diagrams

D-i D-ii D-1 D-2

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LIST OF EFFECTIVE PAGES SUBJECT

PAGE D-3 D-4 D-5 D-6 D-7 D-8 D-9 D-10 D-11 D-12 D-13 D-14 D-15 D-16 D-17 D-18 D-19 D-20

DATE July 17/13 Blank July 17/13 Blank July 17/13 Blank July 17/13 Blank July 17/13 Blank July 17/13 Blank July 17/13 Blank July 17/13 Blank July 17/13 Blank

Appendix E - System Messages and Remote Annunciators

E-i E-ii E-1 E-2 E-3 E-4 E-5 E-6 E-7 E-8 E-9 E-10 E-11 E-12 E-13 E-14 E-15 E-16 E-17 E-18 E-19 E-20 E-21 E-22 E-23 E-24 E-25 E-26 E-27 E-28 E-29 E-30

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LIST OF EFFECTIVE PAGES SUBJECT

PAGE E-31 E-32 E-33 E-34 E-35 E-36 E-37 E-38 E-39 E-40 E-41 E-42 E-43 E-44 E-45 E-46 E-47 E-48 E-49 E-50

DATE July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13

Index

IND-1 IND-2 IND-3 IND-4 IND-5 IND-6

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RECORD OF REVISIONS ASSIGNED TO (JOB TITLE)

REV. NO.

REVISION DATE

0

July 17/13

INSERTION DATE

On receipt of revisions, insert pages and record date inserted and initial. LOCATION

BY

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REV. NO.

REVISION DATE

INSERTION DATE

BY

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

TABLE OF CONTENTS Subject

Section/Appendix

Introduction

Section 1

Control and Display

Section 2

Preflight

Section 3

Departures

Section 4

Enroute

Section 5

Arrivals

Section 6

Approach

Section 7

Post-Flight Procedures

Section 8

Direct-To/Intercept

Section 9

Holding Pattern Navigation

Section 10

Tactical Functions

Section 11

Navigation Sensors

Section 12

Radio Tuning Pages

Section 13

Performance Functions

Section 14

RNP Capability

Section 15

MCDU Functions

Section 16

Abnormal Procedures

Section 17

Performance VNAV For A300/310

Section 18A

Performance VNAV For SUPERJET 100

Section 18B

Datalink Functions

Section 19

FMS Pages - Detailed Descriptions

Appendix A

CMA-9000 VNAV A300/310 Display Pages - Detailed Descriptions

Appendix A300-A

CMA-9000 VNAV SUPERJET 100 Display Pages - Detailed Descriptions

Appendix SSJ 100-A

APPENDIX FANS FMS- A – FMS FANS Pages - Detailed Descriptions

Appendix FANS FMS-A

Navigation Leg Type Definitions

Appendix B

Navigation Displays

Appendix C

CMA-9000 FMS Display Pages Flow Diagrams

Appendix D

System Messages and Remote Annunciations

Appendix E

Index

Index

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

PURPOSE OF OPERATOR'S MANUAL This Operator's Manual applies only to CMA-9000 Flight Management Systems (FMS) which incorporate the specific operational program(s) indicated on the cover page. This manual describes the capabilities, components, typical flight applications, and operating procedures for the CMA-9000 family of the Flight Management Systems (FMS). THIS MANUAL IS INTENDED TO BE A GENERIC MANUAL FOR ALL FMS APPLICATIONS. THE PROCEDURES DESCRIBED HEREIN INCLUDE ALL THE AVAILABLE DISPLAYS AND CONTROLS. When the CMA-9000 FMS is set up through the configuration procedures, as described in the installation manual, some of the features described herein may be disabled and not displayed. CAUTION THE INFORMATION CONTAINED IN NAVIGATION DATABASES IS NOT CERTIFIED BY A REGULATORY AUTHORITY; THEREFORE, THE USER IS ULTIMATELY RESPONSIBLE FOR ENSURING THAT DATA IS CORRECT PRIOR TO USE. ALL FMSs ARE CERTIFIED FOR IFR NAVIGATION UNDER THE CONDITION THAT ANY INFORMATION TAKEN FROM THE DATABASE BE VERIFIED AGAINST AN INDEPENDENT SOURCE PRIOR TO USE. IT IS ESSENTIAL THAT PILOTS COMPLY WITH THIS REQUIREMENT BY USING APPROACH, TERMINAL AND ENROUTE CHARTS TO CHECK FOR DISCREPANCIES IN FMS GENERATED NAVIGATION DATA. IF THERE ARE ANY DISCREPANCIES BETWEEN THE INFORMATION FROM THE FMS DATABASE AND THE OFFICIAL PUBLISHED HARD COPY, THE PILOTS MUST FOLLOW THE HARD COPY PROCEDURE, AND ADVISE THE FMS DATABASE SUPPLIER OF THE DISCREPANCY.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

OPERATIONAL APPROVAL AND LIMITATIONS OPERATIONAL APPROVAL Approval of the CMA-9000 FMS for VFR/IFR operation must be obtained from the Civil Aviation Authority of the country of registration of the aircraft. When operated with any of the external GPS equipment listed in Figure 5B Approved Installation Configurations with GPS Equipment of the Installation Flight Line Manual, the CMA-9000 FMS has been approved for VFR/IFR GPS supplemental navigation in en-route, terminal and non-precision approach. LIMITATIONS Limitations on the operation of the system and its particular installation, are outlined in the Airplane Flight Manual Supplement (AFMS). In particular the operational manual is affected by the way the equipment has been configured with respect to its installation. Instructions for installation and configuration are provided in the Installation Manual. It is expected that the installer takes into account the “Installation Considerations and Limitations” provided in Section 1.L. of the Installation Manual to plan the installation and operation of the aircraft and to obtain TC or STC approval.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 1 - INTRODUCTION

CONTENTS Subject

Page

SYSTEM OVERVIEW ........................................................................................................................................1-1 COMPONENT DESCRIPTION ..........................................................................................................................1-2 A. Flight Management System (FMS) with Embedded Display Unit..........................................................1-2 B. External Global Positioning System (GPS) Receiver .............................................................................1-2 NAVIGATION MODES ......................................................................................................................................1-3 A. GPS..............................................................................................................................................................1-3 B. DME/DME ....................................................................................................................................................1-4 C. VOR/DME ....................................................................................................................................................1-4 D. Inertial .........................................................................................................................................................1-4 E. Dead Reckoning (DR) ................................................................................................................................1-4 WAYPOINT NAVIGATION ................................................................................................................................1-5 TERMINAL AREA OPERATIONS AND GPS INSTRUMENT APPROACHES................................................1-7 NAVIGATION DATABASE................................................................................................................................1-7 PHASES OF FLIGHT ........................................................................................................................................1-7 ACRONYMS AND ABBREVIATIONS ..............................................................................................................1-8

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 1 INTRODUCTION SYSTEM OVERVIEW The CMA-9000 Flight Management System (FMS) provides a complete Global Navigation System (GNS) and area navigation (RNAV) solution for world-wide four-dimensional aircraft navigation in the oceanic/remote, enroute, terminal and non-precision approach. It includes extensive flight management capabilities and a full range of navigation and flight planning features, together with simple route and flight plan creation and modification procedures. A world-wide subscription navigation database, stored in a non-volatile memory, provides the FMS with information on waypoints, navaids, airports, terminal area procedures, airways... In addition the database is capable of storing customer defined routes and waypoints. The CMA-9000 also integrates the functionality of Radio Management System (RMS) and Multi-Function Control Display Unit (MCDU) into a standalone, cockpit mounted enclosure. In dual/triple FMS installations, the synchronization is established automatically on power-up. Flight management capabilities include: • Multi-sensor navigation modes • Navigation performance monitoring and alerting • Flight planning • Standard Instrument Departure (SID) • Standard Terminal Arrival Routes (STAR) • Instrument approaches (RNAV, GPS, ILS, VOR, NDB, …) • LP/LPV approaches are supported when the FMS is used with the CMA-4024 GLSSU • Direct-to/intercept navigation, holding patterns, procedure turns, arcs and offset tracks • Lateral guidance along flight plan • Automatic waypoint sequencing, with and without turn anticipation • Navigation and communications radio tuning functions •

For some aircraft models: • Vertical flight planning and performance initialization • Performance predictions and vertical profile generation • Vertical guidance along computed profile

The FMS accepts data from the following navigation sensors, if installed: • Global Positioning System (GPS) • Distance Measuring Equipment (DME) • •

• • •

VHF Omni-directional Range (VOR) TACAN Inertial Reference System (IRS) Heading Source (AHRS) Air Data Computer

Information from these sensors is combined to determine aircraft position. This position is then used for navigating along a programmed flight plan created by selecting procedures/waypoints from the navigation database.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

COMPONENT DESCRIPTION A. Flight Management System (FMS) with Embedded Display Unit The CMA-9000 provides a color display of alphanumeric data. An alphanumeric keyboard allows data entry, data editing and system control of the flight management functions. The display is a sunlight readable color Active Matrix Liquid Crystal Display (AMLCD). Dedicated function keys and line select keys allow easy operator control of flight management functions. The keyboard panel is integrally lit from a panel light dimming bus. The front panel is illustrated in Section 2 along with an explanation of the keys and their function. For the control of the display brightness, two options are proposed. The first option consists in the combination of light sensors and manual brightness setting. Two light sensors on the FMS front panel sense any change in the cockpit ambient light level. This results in an increase or decrease in display brightness relative to a manual brightness setting. The second option consists in an external dimming bus. The Flight Management Unit (FMU) accepts data from external navigation sensors and performs all the signal processing and computations required to generate high performance navigation data. The FMU accepts operator’s commands from the alphanumeric keyboard, provides navigation, steering and status data on its own display and to the primary navigation flight displays. The FMU also provides suitably formatted outputs for the flight guidance system. B. External Global Positioning System (GPS) Receiver The external GPS Receiver receives signals transmitted by US DoD Global Positioning System satellites. It provides all the signal processing and computational capability required to determine aircraft position, velocity and time. The GPS sensor continuously monitors the integrity of the satellites using a SBAS satellite source (for TSO-C145a/C146 receivers) or an embedded high performance Receiver Autonomous Integrity Monitor (RAIM) (for TSO-C129a receivers).

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

NAVIGATION MODES The FMS follows a hierarchical navigation mode system using TSO-approved sensors characterized by the following decreasing priority order: Navigation modes

Sensor

Inertial

TSO-C129a B1/C1 GPS sensor (or TSOC145/C146) TSO-C66c DME receiver TSO-C66c DME receiver; TSO-C40c VOR receiver TSO-C4c, TSO-C6d IRS

Dead Reckoning

Heading + TAS inputs

GPS DME/DME VOR/DME

The FMS will use GPS data for navigation provided the GPS Horizontal Integrity Limit (HIL) meets the phase of flight requirement. Otherwise, the FMS will select the next best navigation mode meeting the TSO-C115b accuracy requirement (95% confidence factor) for the phase of flight, following the above priority order. This complies with TSO-C129a and TSO-C115b. The following navigation modes are supported: A. GPS GPS is the highest priority navigation mode of the FMS, and will be used when sufficient satellite coverage exists in the phases of flight for which it is approved. The GPS mode is selected for navigation by the FMS when the GPS receiver computes an Integrity value(HIL or HPL) which is less than the Required Accuracy or Error Limit for the current phase of flight being either approach, terminal or En-Route. The GPS receivers may derive the integrity(HPL) using SBAS uplink or will use RAIM (HIL) when there is no SBAS source available. GPS receivers approved for TSOC145/C146 are capable of using the SBAS signal. When the HIL or HPL exceeds the alert limit, or if the GPS loses its integrity capability, then: •

If GPS is the only sensor available for navigation: GPS will remain selected for navigation, but the GPS Integrity annunciator will illuminate and the “GPS POS UNCERTAIN” alert message will be displayed. If at any time GPS becomes unavailable for navigation, the FMS will revert to the Dead Reckoning (DR) mode of navigation, the GPS integrity annunciator will illuminate, and the “GPS NAV LOST” alert message will be displayed.

•

If additional sensors are available and approved for the phase of flight (DME/DME or VOR/DME): The FMS will continuously compute an ANP based on the difference of two positions (GPS and other sensor) and the accuracy of the other sensor. If this ANP exceeds the required accuracy, or if at any time the GPS sensor becomes unavailable for navigation, the FMS will revert to the next best IFR-approved navigation mode, the GPS Integrity annunciator will illuminate, and the “GPS NAV LOST” alert message will be displayed.

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Page 1-3 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) B. DME/DME DME/DME is used in areas with sufficient DME and TACAN coverage, provided the appropriate navigation database is configured. In this mode the FMS automatically tunes the DME transceiver, acquiring distance information from up to six DME and TACAN (DME capable) ground stations. The DME distance is corrected for slant range error. Information on the DME facilities in use is displayed on the DME STATUS page, and individual stations can be inhibited from the navigation solution from the VHF NAV DESELECT page. C. VOR/DME VOR/DME navigation is used in areas with sparse DME coverage where there are less than three DME stations available. This mode combines co-located DME distance and VOR bearing to determine position. Tuned facility information is displayed on the VOR/DME STATUS page. Individual stations can be inhibited from the navigation solution from the VHF NAV DESELECT page. D. Inertial The FMS inertial navigation mode is based on the following parameters: • Present Position Latitude and Longitude; • North-South velocity; • East-West velocity. The FMS uses the raw Inertial position and velocities provided by the IRS. When the FMS is interfaced with 3 IRS, the resulting inertial navigation mode position will be a weighted average of the 3 IRS raw inertial positions. E. Dead Reckoning (DR) When the external sensor data inputs become insufficient to maintain the normal navigation modes, the FMS reverts to the dead reckoning mode of navigation. The FMS must then rely on the last known aircraft position, combined with heading and TAS inputs, and the last valid computed wind, for its aircraft position calculation. Prolonged DR operation will result in decreased position accuracy. Alerts are provided when the estimated position accuracy exceeds the requirements for each phase of flight. Refer to Section 12 for additional information on the various FMS navigation modes.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

WAYPOINT NAVIGATION The FMS navigates from waypoint to waypoint sequentially, automatically changing the legs, and displays all required navigation parameters, computed according to the relationships and direction sense illustrated in Figure 1-1. The FMS steering function anticipates the next leg prior to reaching the active waypoint so that the aircraft turns are smooth without any overshoot. Waypoints may be defined as either fly-by (with turn anticipation) or fly-over (no turn anticipation). For fly-over transition the aircraft is considered to have passed a given point when it has crossed the perpendicular to the desired track at that point (wayline). Thus, for leg sequencing to occur, the aircraft needs only to pass abeam the waypoint. For fly-by leg transition, leg switching, in most cases, occurs when the aircraft passes the bisector of the active leg and the next leg. After the last defined waypoint is overflown, or when a route discontinuity is active, the FMS will invalidate its roll steering to the autopilot/flight director (AP/FD) system, thus forcing the AP/FD to revert to a basic lateral mode. Angular inputs to the FMS may be referenced to either magnetic or true north. The input mode is installation dependent as defined in the Airplane Flight Manual Supplement. The reference used for the FMS angular displays and outputs to the flight instruments, can also be selected by the operator. NOTE: On certain installations only magnetic angular reference is supported, due to Display System limitations.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

NORTH

WIND DIRECTION (WD)

BEARING TO WAYPOINT (BRG)

WINDSPEED (WS)

A HE

DESIRED TRACK (DTK)

DRIFT ANGLE (DA) RIGHT

GROUND TRACK ANGLE (TK)

R HEADING AI (HDG) RUE T

SP

D EE

S) (TA

O GR

P DS UN

EE

D(

GS

S OS CR IND W

DW

D IN

ND WI E D E SP S) (W

TRACK ANGLE ERROR (TKE) LEFT

)

"TO" WAYPOINT

CROSS-TRACK DISTANCE (XTK) LEFT

INE S. SE L YPOINT A OUR E D C WE E N W IR S T DE E BE IRCL AT C GRE

0012033

Figure 1-1 Navigation Relationships

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

TERMINAL AREA OPERATIONS AND RNAV INSTRUMENT APPROACHES Standard Instrument Departures (SID), Airways, Standard Terminal Arrival Routes (STAR), STAR transitions, GPS and GPS overlay instrument approaches, and approach transitions, can be selected for the departure/arrival airports. These procedures may be modified on the LEGS pages. The implementation of the RNAV ( LPV, LNAV/VNAV and LNAV minima) instrument approach procedures is primarly based on TSO-C129a, TSO-C145a and TSO-C146.The transition from en-route through terminal to non-precision approach is effectively a seamless series of waypoints/legs with progressive increases in HSI lateral deviation display sensitivity (to reduce flight technical error), and reductions in Error Limit value for each phase of flight, and appropriately-timed alert or advisory messages

NAVIGATION DATABASE The navigation database includes most of the information that the operator would normally determine by referring to the navigation charts. The database may be tailored to specific customer needs and contains such data as en-route and terminal VHF, NDB navigation facilities, airports, waypoints, named intersections, and terminal area procedures. All ARINC 424 procedural legs are implemented. These leg types and their corresponding graphical representation are illustrated in Appendix B.

PHASES OF FLIGHT The phases of flight are defined as follows: Approach:

When below 15,000 feet AGL and within 2 nm of the FAF, with all GPS instrument approach conditions satisfied.

Terminal:

For arrivals, when below 15,000 feet AGL and within 30 nm radial distance of the arrival airport, but not in approach phase of flight. For departures, when below 16,000 feet AGL and less than 33 nm radial distance from the departure airport.

En-route:

When in neither approach nor terminal phases of flight.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

ACRONYMS AND ABBREVIATIONS A AA AAIM AAR AC ACARS ACCUR ACID ACT ACMS ACQ ADC ADF ADIRS ADS ADx AF AFCS AFMS AFN AG AGC AGL AHRS ALT AMLCD ANP ANT AOC AP/FD APPR APU ARC ARINC ARPT ARR ATA ATC ATK ATT ATS

-

Above (altitude) Air-To-Air Aircraft Autonomous Integrity Monitoring Air-To-Air Refuelling Aircraft Aircraft Communications Addressing and Reporting System Accuracy Aircraft Identifier Active Aircraft Conditioning Monitoring System Acquisition mode Air Data Computer Automatic Direction Finder Air Data Inertial Reference System Automatic Dependent Surveillance Primary (AD1) or Secondary (AD2) ADF radio Initial Approach Fix Automatic Flight Control System Airplane Flight Manual Supplement ATS Facilities Notification Air-To-Ground Automatic Gain Control Above Ground Level Attitude Heading Reference System Altitude Active Matrix Liquid Crystal Display Actual Navigation Performance Antenna Airline Operational Communications Autopilot/Flight Director Approach Auxiliary Power Unit Arc to Fix/Radius to Fix Aeronautical Radio Incorporated Airport Arrival Actual Time of Arrival Air Traffic Control Along Track Distance Attitude Air Traffic Services

BARO BRT BRG BW

-

Barometric Brightness Bearing Back Course Marker

Cx CAP CARP

-

COM radio (primary : C1, secondary : C2) Capable Calculated Air Release Point

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) CDI CDU CF CFG CHK CLR CMx CMA CMD CMU COM COMMS CON CONC COORD CPDLC CPS CRP CRS CRZ CTR

-

Course Deviation Indicator Control Display Unit Final Approach Course to fix Configuration Checker Clear Primary (CM1) or Secondary (CM2) COM radio Canadian Marconi (Avionics) Command Communications Management Unit Communication Communication Radios Connection Concentrator Coordinates Controller Pilot Datalink Communication Compass Computed Air Release Point Course (desired track) of route leg or to waypoint Cruise Center

DA DEL DEP DES DESEL DEST DF DGNSS DIFF DISCON DIS DIST DLU DME DOD DOP DR DTG DTK DTO DTRA DTW

-

Drift Angle Delete Departure Destination Deselected Destination Direct To Fix Differential Global Navigation Satellite System Differential Route Discontinuity Distance Distance Data Loader Unit Distance Measurement Equipment Department Of Defense Dilution of Precision Dead Reckoning Distance To Go Desired Track Direct To Transition Distance Distance To Waypoint

E E/W EDT EFA EFIS EHE EHSI ENRT EQUIP ESC

-

East East/West Edit Estimated Fuel at Arrival Electronic Flight Instrumentation System Estimated Horizontal Error Electronic Horizontal Situation Indicator En-Route Equipment Escape Point

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Page 1-9 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) EST ESS ETA ETE EW EXEC

-

Estimated External Sub-System Estimated Time of Arrival Estimated Time Enroute Electronic Warfare Execute

FAF FDE FF FFK FIR FL FLT FMS FMU F/O FOM FPU FR FREQ FSD FT FTE

-

Final Approach Fix Failure Detection and Exclusion Final Approach Fix Front panel Function Key Flight Information Region Flight Level Flight Flight Management System Flight Management Unit First Officer Figure of Merit Floating Point Unit From Frequency Full Scale Deflection Feet Flight Technical Error

GD GDOP GLNS GLONASS GMT GNS GNSSU GPIAL GPS GS GSM GWT

-

Guard Geometric Dilution of Precision GLONASS Global Navigation Satellite System (Russian) Greenwich Mean Time Global Navigation System Global Navigation System Sensor Unit GPS Position Integrity Alert Limit Global Positioning System Ground Speed Global Navigation System Sensor Module Gross Weight

/H HARP HAT HDG HDOP HF HFOM HIL HOR HR HSI HT HW HYB

-

Holding Pattern High Altitude Release Point Height Above Terrain Heading Horizontal Dilution of Precision High Frequency Horizontal Figure Of Merit Horizontal Integrity Limit Horizontal Hour Horizontal Situation Indicator Height Hardware Hybrid

IAF IAS

-

Initial Approach Fix Indicated Airspeed

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Page 1-10 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) IC ICAO ID IDENT IDT IF IFR in Hg ILS IM INBD INACT INIT INT INTC INS IP IRS ITU

-

Intercom International Civil Aviation Organization Identifier Identifier Identifier Intermediate Fix Instrument Flight Rules Inches of Mercury Instrument Landing System Innner Marker Inbound Inactive Initialize Integrity Intercept Course Inertial Navigation System Identification Point Inertial Reference System Telecommunication Union

KG KT

-

Kilogram Knot(s)

L LAT LB LDA LDR LIB LNAV LOC LOCB LONG LP LPV LRU LSK LVL

-

Left Latitude or Lateral Pound Landing distance available Light Detect Resistor Library Lateral Navigation mode of the autopilot/flight director system Localizer Localizer Backcourse approach Longitude Localizer Precision approach Localizer Precision with Vertical guidance approach Line Replaceable Unit Line Select Key Level

M MA MAG MAGVAR MAHP MAINT MAP MB MC MCDU MDA MDA-DA MEW MGRS MHz MID

-

Meter Missed Approach Point when not RW Magnetic Magnetic Variation Missed Approach Holding Point Maintenance Missed Approach Point Millibars (hectopascal) Mission Computer Multipurpose Control and Display Unit Minimum Descent Altitude Minimum Descent Altitude-Decision Altitude Mean Effective Wind Military Grid Reference System Mega Hertz Maritime Identification Digits

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Page 1-11 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) MIN MLS MM MOD MRK MSG MSLA MTBF

-

Minute Microwave Landing System Middle Marker Modified Mark Message Mean Sea Level Altitude Mean Time Between Failures

N Nx NAV NDB NDBD NM NOTAMS NP NPA NVx NVM VNAV NVIS

-

North NAV radio (primary : N1, secondary : N2) Navigation or Navaid Non-directional Beacon NDB approach with DME facility (GPS or NDB/(DME)) Nautical Mile Notices To Airmen Navigation Performance Non-Precision Approach Primary (NV1) or secondary (NV2) NAV radio Non-Volatile Memory Vertical Navigation Night Vision Imaging System

/O OAT OFST OM OP ORIG

-

Overfly Waypoint Outside Air Temperature Offset Outer Marker Operations (independent/synchronized) Origin

PBD PBPB PEE PERF PG PIT POF POS PPOS PREDEF PREV PRN PROG P-T PWR

-

Place/Bearing/Distance Place/Bearing-Place/Bearing Position Estimation Error Performance Page Programmable Interrupt Timer Phase of Flight Position Present Aircraft Position Predefined Previous Pseudo Range Number Progress Procedure Turn Power

QFE QNH

-

Field Elevation Pressure Sea Level Pressure

/R R RAD RADALT RAIM RALT

-

Radial-To Right Radial Radar Altitude Receiver Autonomous Integrity Monitor Radio Altimeter

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Page 1-12 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) RCU RCV REC REF REL RES RESEL RF RIB RMS RNAV RNG RNP RTA RTC RTE RW

-

Remote Control Unit Receive only Flight Recorder Reference Relative Reserve Reselect Radio Frequency Radio Interface Board Radio Management System Required Navigation Range Required Navigation Performance Required Time of Arrival Real Time Clock Route Runway Threshold

/S S/W S SAR SAT SATCOM SD SDF SEL SID SMS SP SPD SQK SSM SSR STAR STAT STBY STC STS SURF SYNC

-

Search Pattern Software South Search and Rescue Satellite Satellite Communication System Slowdown Point Simplified Directional Facility Selected Standard Instrument Departure Short Message Service Space Speed Squawk Sign Status Matrix Secondary Surveillance Radar Standard Terminal Arrival Routes Status Standby Supplemental Type Certificate Status Surface Synchronization

/T T TACAN TACT TAS TCN TD TE TEL TEMP TERM TF TGL

-

Tactical Direct-To Angle referenced to True North Tactical Air Navigation Tactical True Air Speed TACAN Touchdown Fix when not RW Trailing Edge Telephone Temperature Terminal Track To Fix Temporary Guidance Leaflet

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Page 1-13 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) TK TKE TOGA TP TPDR TR TRANS TRK TRG TSE TSO TTFF TTG TTS TX1 TX2

-

Track (Actual) Track Angle Error Take-Off/Go-Around Turn Point Transponder Transmit/Receive Transition Track Transmit on Guard Total System Error Technical Standard Order Time To First Fix Time To Go Time To Station V/UHF1 Transmitting V/UHF2 Transmitting

UF UHF UTC UTM

-

UHF radio Ultra High Frequency Universal Time Coordinates Universal Transverse Mercator

V VAL VDOP VECT VERT VFOM VFR VHF VNAV VUHF VIR VIS VOR VORD

-

Velocity (VX, VY, VZ) Value Vertical Dilution of Precision Vector Vertical Vertical Figure Of Merit Visual Flight Rules Very High (30-300 MHz) Frequency Vertical Navigation Very Ultra High Frequency VOR ILS Receiver Visible VHF Omni-directional Radio Range VOR/DME approach (GPS or VOR/DME)

W WD WPT WS WT WGS WGT WXR

-

West Wind Direction Waypoint Windspeed Weight World Geodetic System Weight Weather Radar

XFILL XPDR XMT XTE XTK

-

Cross FMS Fill Transponder Transmit Extended Trailing Edge Point Cross Track

Z

-

Zulu (UTC) time

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 2 - CONTROL AND DISPLAY

CONTENTS Subject

Page

GENERAL .......................................................................................................................................................2-1 FMCDU FRONT PANEL .................................................................................................................................2-1 GENERAL DISPLAY CONVENTIONS .........................................................................................................2-12 Standard Colour Convention......................................................................................................................2-13 Airbus Colour Convention ..........................................................................................................................2-14 Font Size .......................................................................................................................................................2-15 Special Symbols ..........................................................................................................................................2-15 SCRATCHPAD MESSAGES ........................................................................................................................2-17 WAYPOINT NAMES AND OTHER CONVENTIONS ...................................................................................2-19

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

This Page Intentionally Left Blank

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 2 CONTROL AND DISPLAY

GENERAL The CMA-9000 FMS is a Flight Management Computer (FMC) embedded within a Multipurpose Control Display Unit (MCDU), thus becoming an FMCDU. The MCDU function can be interfaced with up to seven other ARINC739 capable LRUs (ACARS, SATCOM, ACMS, etc.). The unit’s front panel presents a full alphanumeric keyboard, with special function keys. These special function keys are mostly dedicated to FMS operations (e.g. INIT/REF, RTE, DEP/ARR, etc.). There are six line select keys (LSK) on each side of the display area. The functions of the LSKs are specific to each screen page.

FMCDU FRONT PANEL A typical front panel arrangement of the FMCDU is illustrated in Figure 2-1 on next page. The display screen is approximately 3 x 4 inch colour Active Matrix Liquid Crystal Display (AMLCD) providing fourteen lines of twentyfour characters. The page format is divided in four areas: page title, left side, right side, and scratchpad.

Page Title:

This area is the top line of the display (line 1 of 14). It identifies the page in view and indicates how many pages of the same set are available.

Left Side:

This area is comprised of six pair of lines, up to twelve characters per line. A line pair comprises a field title line and a data line. The operator has access to the data line of each pair through a Line Select Key aligned on the left side. This area extends from the left side of the screen to the center.

Right Side:

This area is similar to the Left Side area. The operator has access to the data line of each pair through a Line Select Key aligned on the right side. This area extends from the right side of the screen to the center. On some pages a field is placed in the middle of a line. For these fields the user cannot enter or delete data through the line select keys. Scratchpad: This area is the bottom line of the display (line 14 of 14). Typed characters and FMS-generated messages are displayed on this line.

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Page 2-1 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Figure 2-1 CMA-9000 FMS Front Panel, Hardware variation 045

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Page 2-2 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Figure 2-2 FMS Front Panel, Hardware variation 445

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

VAR 060

VAR 460

Figure 2-3 Front Panel, Hardware variation 060/460

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

VAR 070

VAR 470/471

Figure 2-4 Front Panel, Hardware variation 070/470/471

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Page 2-5 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Figure 2-5 Front Panel, Hardware variation 050

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Page 2-6 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

The item numbers 1 to 33 below refer to the front panel elements of Figure 2-1 and subsequent figures. Display Screen (Item 1): Provides 14 lines of 24 characters: • Line 1 displays the page title and page number; • Lines 2 to 13 are used for data display; • Line 14 (scratchpad) is for user data entry, and system display of alert/advisory messages. Alphanumeric Keyboard (Item 28) These keys allow typing alphanumeric characters into the scratchpad successively from left to right. Line Select Keys (LSK) (Item 10) There are twelve LSKs on the front panel, six on either side of the display, aligned with their corresponding data field. LSKs are identified by their location from top to bottom of the screen and as left or right (LSK1L, LSK2L, …LSK6R). Depending of the context of a given page, pressing a line select key may: • display a new page, • enter data from the scratchpad into the selected field, • copy data from the selected field to the scratchpad. Data Entry from Scratchpad Data entries are permitted only on lines adjacent to the LSKs. Entry of data from the scratchpad into the selected field is accomplished by pressing the adjacent LSK which moves the data from the scratchpad to the selected field. This action clears the scratchpad, unless an entry format error is made. Data Copy to Scratchpad When the scratchpad is empty, data can also be copied from a data field to the scratchpad by pressing the LSK adjacent to the desired data line. Slash (/) Key (Item 26) The slash key " / " is used to separate two items of data entered in the same data field (LSK) (such as wind direction and speed): • If a single entry is made without being preceded or followed by a slash, it will be entered into the field adjacent to the LSK (field closest to the edge of the screen). • Entering data into the field closest to the center of the screen always requires typing of a slash. Cancellation of Waypoint Attribute (/H, /O) – Some waypoints are displayed on the LEGS page with an attribute appended to the right of the identifier: • waypoint followed by a holding pattern (/H), • waypoint marked as a mandatory fly-over (/O), This waypoint attribute is identified using the slash symbol followed by a single letter. The attribute can be cancelled using the slash key alone without a letter and the appropriate LSK. NOTE:

Cancellation of the attribute does not delete the waypoint itself.

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Page 2-7 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) SP Key (Item 24) This key allows typing a blank space into the scratchpad. Plus-Minus [+/-] Key (Item 25) This key allows typing a "+" (plus) or "-" (minus) sign into the scratchpad. Pressing this key will first display a "-" (minus) sign in the scratchpad. Pressing it a second time will replace the minus sign with a "+" (plus) sign. Decimal (.) Key (Item 27) This key allows typing a decimal point into the scratchpad, for numeric data entries. CLR Key (Item 15) The CLR key is used to clear messages and data from the scratchpad or an individual data field. Clearing Data from Scratchpad One press clears the last entered character from the scratchpad. When pressed and held for more than 1 second, it clears the entire scratchpad. Acknowledging Alert and Advisory Messages The CLR key also acknowledges alert and advisory messages and clears them from the scratchpad. Delete Data from an Entry Field To delete an entry already made in a given data field: •

Pressing the CLR key with the scratchpad empty will display DELETE in the scratchpad.

•

This DELETE message can be cleared by another press of the CLR key if the latter was inadvertently pressed.

•

The deletion process is completed by pressing the LSK next to the data to be deleted.

Function Keys (qty 10) (Items 14, 16-23 & 33) Function keys are used for single-key access to certain FMS pages. The first row of function keys (INIT/REF, RTE, DEP/ARR, LEGS, PROG) is common to all hardware variations of the unit. •

INIT REF - provides access to pre-flight initialization pages and various reference data pages. NOTE : If the key is pressed for more than 1 second, the MESSAGE RECALL page will be displayed.

•

RTE - provides access to the ROUTE page for the definition of routes.

•

DEP ARR - provides access to the DEP/ARR page for the selection of departure and arrival procedures and runways.

•

LEGS - provides access to the LEGS pages containing detailed data concerning each leg of the route.

•

PROG - provides access to the PROGRESS pages for display of current flight and navigation status information.

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Page 2-8 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) For the second row, various variations of the unit support different combinations of function key labelling (see Figure 2-1 to 2-5 above, and Table 2-1 below). A given combination is selected by the operator depending of the type of operations of this aircraft. •

MSG - provides access to the MESSAGE RECALL page for display of System Alert messages.

•

HOLD - if no holding pattern exists in the route, brings LEGS page in view with “/H” in the scratchpad for line selection of the desired holding fix waypoint. If a holding pattern already exists in the route, accesses the HOLD page for the definition of holding pattern parameters at the designated waypoint or present position.

•

VNAV – o provides access to the VNAV Approach page when advisory (uncoupled) approach VNAV is enabled (see section 7). o provides access to the vertical navigation page associated to the current phase-of-flight when Performance VNAV is enabled (see section 18).

•

FMC COMM - provides access to company datalink (Airline Operational Communications) related pages.

•

RADIO - provides access to RADIO tuning functions.

•

ATC - provides access to ATC datalink related pages, or provides access to ATC Transponder control and display pages NOTE: On a given installation, the ATC key can be used only for one of these two purposes. If transponder control and display is required on an installation where ATC Datalink is also enabled, access to the transponder control pages is via the RADIO page.

•

FIX - provides access to FIX page for all fix and abeam waypoint functions.

•

TACT - provides access to tactical functions (not for airlines operations). See Section 11.

Front Panel Variation 045/445 050 060/460 070/470/471

Item 22

Item 20

Item 33

Item 17

Item 14

RADIO RADIO ATC RADIO

FMC COMM TACT FMC COMM ATC

VNAV VNAV VNAV VNAV

HOLD HOLD HOLD HOLD

FIX ATC FIX MSG

Table 2-1 Configurable Key layout per Front Panel Variation NEXT Key (Item 29) When multiple-page of a given set exist (as indicated in the page title line), pressing the NEXT key advances the display to the next page number, or wraps around to page 1 if presently on the last page. NOTE:

If the NEXT functionality is configured, additional press of the INIT/REF, RTE, DEP/ARR, LEGS, PROG, FREQ, FUEL and HOLD keys allow the access to the next page, as per the NEXT key.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

PREV Key (Item 30) When multiple-page of a given set exist (as indicated in the page title line), pressing the PREV key moves backs the display to the previous page number, or wraps around to the last page if presently on page 1. EXEC Annunciator (Item 11) Illuminates when the active route is being edited. A modified (temporary) route is thus being created to allow editing and reviewing without affecting the current guidance being performed with the active route. When the EXEC annunciator is lit, all flight planning pages display: • MOD in reverse video in the column 2 of the title line, and • the ERASE prompt in field LSK6L o Pressing the ERASE prompt LSK erases all modifications and restores the display of the active route. Even if a modified route exists, the FMS continues to use the (unmodified) active route for navigation and guidance. EXEC Key (Item 12) Allows crew to accept modifications to the active route. When data entries have been made active (by pressing the EXEC key), the title MOD status will revert to ACT (active). Any modification can be erased (cancelled) prior to EXECution by pressing the ERASE prompt (LSK6L). System Annunciators (Items 2-8) Various hardware variations of the unit support different annunciator labelling. Conditions for illumination vary with hardware variation and software configuration options. Front Panel Variation 045/445 050 060/460 070/470/471

Item 2

Item 3

Item 4

Item 5

Item 6

Item 7

Item 8

FAIL FAIL FAIL FAIL

MSG MSG MSG MSG

RNP RNP RNP RNP

OFST OFST OFST OFST

IND IND IND IND

None None None None

ATC ATC ATC ATC

Table 2-2 Annnunciator layout per Front Panel Variation FAIL (Item 2) -

illuminates at maximum brightness with the display blank upon detection of a major unit failure (e.g. system is halted).

MSG (Item 3) - illuminates when a new alert message appears in the scratchpad. The annunciator stays lit as long as the condition causing the alert message remains, or until the message is acknowledged by pressing the CLR key, or until the message is viewed on the MESSAGE RECALL page. RNP (Item 4) -

illuminates when the FMS ANP exceeds the RNP.

POS (Item 4) -

illuminates when the FMS is in dead reckoning navigation mode.

OFST (Item 5) - illuminates during offset (parallel track) navigation IND (Item 6) -

illuminates when the FMS operates on INDEPENDENT mode.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

BRT Key (Item 13) Controls the brightness of the screen and annunciators. After an elapsed time of 5 seconds, the first press of this key will always increase brightness, each depression of the BRT key alternately brightens or dims the display. NOTE1: When night and NVG mode selected and short power interruption occurs, the brightness of the display may require minor re-adjustments. NOTE2: When external dimming control is selected in the configuration, the brightness of the screen and annunciators can also be controlled by an external system providing a 0-5 VDC to the FMS. LDR Sensor (Item 9) Detects ambient light conditions in order to perform auto-brightness control of display screen and annunciators. MENU Key (Item 31) Provides access to the MCDU MENU 1/2 page, which allows access to other subsystems connected to the MCDU (e.g. ACARS, SATCOM, …). This key relates only to the ARINC 739 MCDU capabilities of the CMA9000. MENU Annunciator (Item 32) Illuminates when a sub-system, other than the one currently displaying pages, is requesting crew attention. • •

For example, if any of the installed subsystems that uses the FMCDU as control head (e.g. CMU, IFDMU, SATCOM, ACMS, DFDAU) is requesting crew attention while the MCDU function is connected to the FMS, the MENU light will be turned on. Conversely, if the MCDU function is connected to any of the above mentioned sub-systems and the FMS is requesting attention, the MENU annunciator will equally be turned on.

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

GENERAL DISPLAY CONVENTIONS

A typical screen page is illustrated below as an aid in describing the various page layouts, page prompts, and data entry rules.

ACT,MOD STATUS FIELD [CYAN] [LARGE]

MOD BOX DATA FIELD [GREEN] [LARGE]

PAGE NUMBER AND NUMBER OF PAGES [CYAN] [LARGE]

PAGE TITLE [CYAN] [LARGE]

RTE1 LEGS

299o

CAFTA

1/2 2.25N M

A

THEN †††††

COMPUTED AND RECEIVED DATA [WHITE] [SMALL]

-- ROUTE DISCONTINUITY -

YZP01 299o DASH DATA FIELD [GREEN] [LARGE]

ERASE PROMPT [GREEN] [LARGE]

10.6N M

YZP02 ----

PAGE PROMPT [BLUE [LARGE]

MESSAGES DISPLAYED IN THE SCRATCHPAD [AMBER] [LARGE]

Figure 2-6 Basic Display Format Page Title -

displayed in cyan on the top line of the screen.

Page Number -

when a display consists of several pages (as indicated in the upper right of the page), the additional pages may be displayed by pressing the NEXT or PREV keys. When the NEXT key configuration option is selected, the Front-panel Function Keys (FFKs) (elements 14 to 23 on Figure 2-1) can be used as a NEXT key as well.

Page Prompt -

pressing the LSK adjacent to a page prompt will bring in view the associated page.

Scratchpad -

This area is the bottom line of the display (line 14 of 14).

•

Keyboard entries are displayed in white large font in the scratchpad and then moved to the data field by pressing the appropriate Line Select Key (LSK). Error checking for invalid format or data type, or out of range values, is performed when the LSK is pressed.

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Page 2-12 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) •

Copying data from a data field into the scratchpad is accomplished by pressing the appropriate LSK when the scratchpad is empty. Data in the scratchpad remains there when a new page is selected, and can thus be carried over for entry into other pages.

Standard Colour Convention The colour convention used on the FMS pages is configurable in order to better blend with a given cockpit environment. The standard colour convention is as follows:

Figure 2-7 Standard Colour Convention Green

Fixed data fields, field titles and waypoint names (on LEGS page).

White

Computed (dynamic) data, data units, scratchpad data, data entry error, and advisory/maintenance messages.

Cyan

Page titles, page browsing prompts and inactive route related information.

Magenta

Depending on configuration, used in normal video, or reverse video, to identify the active waypoint on ACT RTE LEGS 1/X, and PROGRESS pages.

Amber

Used to display cautions and warnings, including alert conditions requesting immediate crew attention or action (e.g. alert scratchpad messages).

Red

Reserved for maintenance purposes only. Major change (e.g. confirmation of system reconfiguration).

Reverse Video Text can also be displayed in reverse video: Green

Temporary states prompting crew attention (such as CONFIRM and CANCEL). Navigation and guidance actions (e.g. missed approach initiation, manual waypoint sequence, hold exit initiation).

White

Pending active waypoint sequencing; activated mode/function; temperature compensated altitudes; waypoint attribute designators (e.g.: FAF, MAP).

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Page 2-13 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Cyan

Used for certain status advisories, such as modified route in title line.

Magenta

Depending on configuration, used in normal video, or reverse video, to identify the active waypoint on ACT RTE LEGS 1/X, and PROGRESS pages.

Amber

Unachievable temperature compensated altitudes constraints.

Red

Not used

Temperature Compensation All temperature compensated altitude constraints are displayed in reverse video. Thus altitude constraints can be displayed in reverse Green (constraints), or Amber (broken altitude constraints).

Airbus Colour Convention The Airbus colour convention diverts from the standard configuration as follows: •

the active waypoint is displayed in reverse video green on the LEGS/PROGRESS pages,

•

downpath waypoints are displayed in white on the LEGS/PROGRESS pages,

•

altitude, speed, and time constraints are displayed in magenta,

•

On LEGS pages, text in the title lines is displayed in green.

Figure 2-8 Airbus Colour Convention

NOTE:

In this document, the page examples will follow the standard convention. For page examples using the Airbus A300/310 standard, refer to section 18A Performance VNAV for A300/310 and appendix A300-A CMA-9000 VNAV A300/310 Display Pages – Detailed Descriptions.

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Page 2-14 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Font Size There are 2 types of fonts, small and large, on the pages. Each font supports upper and lower case alpha characters. Lower case alpha characters are used only for the display of units and unit acronyms. The data fields (line adjacent to LSK) are displayed in: • •

Large Small

Manual entries. Computed or system generated data.

Data on the field title line (above the data line) are displayed in small font. The page title line is displayed in large font.

Special Symbols The following special symbols are used to convey their respective meaning: Dash Data Field (-----) Box Data Field (

Optional data entry. ) Mandatory data entry.

Blank Fields

Data cannot be computed.

Triangle (>) Pointing inward

Toggle prompt or command prompt

Pointing outwards Page access prompt

Asterisk Fields (****)

Data exceeds the maximum value for that field, or the external source of data is failed.

Leading Zeros

Only required during data entry for: • angular data (bearing, course, wind direction, etc.) • latitude/longitude coordinates • runway identifiers

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Page 2-15 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Summary of conventions:

Page Title Active waypoint

Display Elements

Font Large Large

Page prompt (with outward triangle) Legs page waypoint

Large Large

Fix caption Units Tuning in progress Active waypoint being sequenced (fly-by transition) Entered data Computed data Temporary states pilot attention requested Toggle option (with inward triangle) Command prompt (with inward triangle)

Small Small Large Large Large Small Large Large Large

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Color Cyan Reverse video magenta Reverse video green (Airbus) Cyan Green White (Airbus) Green White Reverse video white Reverse video white White White Reverse video green Green triangle with White text Green triangle with Green text

Page 2-16 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SCRATCHPAD MESSAGES

The FMS can generate the following types of system messages: System Alerts

Require immediate pilot action or attention. Example:

Data Entry Advisories

Indicate that the user-entered data is incorrect. Example:

Status Advisories

Do not require immediate pilot action but require pilot awareness. Example:

Maintenance Advisories

Do not require immediate pilot action but indicate a particular external input failure condition. Example:

Maintenance Alerts

Indicate a particular FMCDU internal failure condition. Such messages never displayed in scratchpad.

Refer to Appendix E of this manual for additional information and the complete list of messages. Alert Messages A. System Alerts •

• • • •

Indicate: • a required pilot action, • a loss of functionality • or a degraded mode of operations. Displayed in amber in the scratchpad until acknowledged. Cause both the FMS front panel MSG annunciator and the remote MSG annunciator to illuminate until all new messages are cleared/acknowledged by the pilot. Displayed in amber in the MESSAGE RECALL page. Highest priority scratchpad messages: • cannot be typed over or overwritten by any other message type or data entry; • must be acknowledged by pressing the CLR key before data entry can take place.

B. Maintenance Alerts • • •

Indicate an internal FMCDU failure condition. Never displayed in the scratchpad as they are covered by the generic FMS FAILED (system alert) collector message. Displayed in amber on the MAINT MESSAGES page.

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Page 2-17 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Advisory Messages C. Data Entry Advisories • • • • • •

Immediate system response to data entries performed by the crew. Notifiy the crew that the entered data is incorrect. Identified in the scratchpad by a leading exclamation mark "!". Displayed in white in the scratchpad (until acknowledged) Never displayed on the MESSAGE RECALL or MAINT MESSAGES page Can be typed over and overwritten by system alerts only

D. Status Advisories • • • •

Do not require immediate pilot action but require pilot awareness Displayed in white in the scratchpad (until acknowledged). Never displayed on the MESSAGE RECALL or MAINT MESSAGES page. Second lowest scratchpad priority (can be typed over and overwritten by any message type except maintenance advisories).

E. Maintenance Advisories • Do not require immediate pilot action but indicate a particular external input failure condition, typically a loss of redundancy without loss of capability (e.g. DME 1 FAILED). • Displayed in white in the scratchpad unless an associated (system alert) collector message is active. • Displayed in white on the MAINT MESSAGES page, regardless of the presence of an associated (system alert) collector message. • Lowest priority scratchpad messages (can be typed over and overwritten by any other message type).

This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.

Page 2-18 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

WAYPOINT NAMES AND OTHER CONVENTIONS Terminal Area Waypoints - where specific identifiers have not been assigned, the following two-character prefix codes are added to the runway identifier (number) to create terminal area and approach-related waypoints in the navigation database: AF CF FF IF MA SD RW OM MM IM BM TD

-

Initial Approach Fix Final Approach Course Fix Final Approach Fix Intermediate Fix Missed Approach Point when not RW Step-down Fix Runway Threshold Outer Marker Middle Marker Inner Marker Back Course Marker Touchdown Fix when not RW

Unnamed Turnpoints and Intersections - where no name has been assigned to a turnpoint or intersection, the waypoint name in the navigation database is created by adding the distance of the point from the nearest applicable navigation facility to the facility identifier, e.g. SEA77. Temporary Waypoints - place/bearing/distance (PBD), place/bearing-place/bearing (PBPB) and along track waypoints are automatically named by adding a sequence number to the first three characters of the reference waypoint, e.g. ANC01. Similarly, the names of waypoints entered in latitude/longitude are created by adding a sequence number to the prefix WPT. Alternatively, depending of configuration option, waypoints entered in latitude/longitude can be automatically named per the entered coordinates (e.g. N45W123). DME ARC Waypoints - the waypoint name in the navigation database is created by adding the radial from the DME station in degrees followed by the radius of the arc in nautical miles (represented by a letter: A = 1 nm, B = 2 nm, J = 10 nm, etc) to the prefix D, e.g. D173J. Conditional Waypoints - a conditional waypoint is used in the navigation database when a route leg does not terminate at a defined latitude and longitude. Such legs include radar vectors, intercepts, and course or heading legs, or a leg with a manual or an altitude termination. Conditional waypoint names are displayed in parentheses as shown below. Conditional waypoints cannot be used for direct-to navigation, nor as references for temporary waypoint creation, and cannot be copied into the scratchpad. (INTC)

-

Leg terminates at the interception of the next leg.

(3000)

-

Leg terminates automatically when climbing through the displayed altitude.

(VECT)

-

Leg is a radar vector. Operator action is required to sequence to the next leg.

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Page 2-19 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Course Legends - courses may be displayed with the following legends depending on the leg type, as listed below: CRS

-

Indicates a course leg inbound to the next waypoint

FR FIX

-

Indicates a course outbound from the FIX

HDG

-

Indicates a heading leg

HOLD AT -

Replaces the active waypoint course on RTE LEGS 1/X and PROGRESS 1/4 pages when navigating a holding pattern

P-T

Appended to the courses of the outbound legs of the procedure turn

-

Course Prefixes - the required turn direction (L or R) is added as a prefix to the displayed course, and is most commonly used at the inbound turn of a procedure turn and in missed approaches.

This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.

Page 2-20 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 3 - PREFLIGHT

CONTENTS Subject

Page

SECTION 3 - PREFLIGHT.........................................................................................................................................3-i CONDENSED PREFLIGHT PROCESS..........................................................................................................3-1 PREFLIGHT.....................................................................................................................................................3-2 START-UP AND INITIALIZATION..................................................................................................................3-3 ACTIVE DATABASE SELECTION.................................................................................................................3-4 FMS DISPLAY SETUP....................................................................................................................................3-5 SYSTEM POSITION, DATE AND TIME UPDATE..........................................................................................3-6 ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY (POLAR AREA DEFINITION) ................3-7 ACTIVE ROUTE SELECTION USING THE COMPANY ROUTE NAME.......................................................3-8 ROUTE SELECTION FROM THE LIST OF COMPANY ROUTES ................................................................3-9 BUILDING A ROUTE BY WAYPOINT INSERTION .....................................................................................3-10 BUILDING A ROUTE BY AIRWAY INSERTION..........................................................................................3-11 VERIFYING ACTIVE ROUTE LEGS BY COURSE AND DISTANCE..........................................................3-12 INITIAL LEG ..................................................................................................................................................3-13 CANCELLING ANY PROCEDURE OR ROUTE MODIFICATION...............................................................3-13 ROUTE 2 OPTION ........................................................................................................................................3-13 ROUTES 2 & 3 OPTION ...............................................................................................................................3-17 ACCESSING INIT/REF INDEX PAGES........................................................................................................3-24 CRUISE PERFORMANCE PARAMETERS INITIALIZATION (if configured) ............................................3-25 FUEL PERFORMANCE PARAMETERS INITIALIZATION (if configured) ................................................3-26 FUEL AND WEIGHT PERFORMANCE PARAMETERS INITIALIZATION (if configured) ........................3-26 GPS SATELLITE DESELECTION (If configured).......................................................................................3-28 DUAL/TRIPLE FMS OPERATIONS .............................................................................................................3-28 SYNCHRONIZED OPERATIONS .................................................................................................................3-29 INDEPENDENT OPERATIONS ....................................................................................................................3-30 RADIO TUNING OPERATIONS – DUAL/TRIPLE FMS or FMS and RADIO HEAD ..................................3-30 EMBEDDED CALCULATOR/CONVERSION TOOL (if configured) ..........................................................3-30

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Page 3-i July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

This Page Intentionally Left Blank

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Page 3-ii July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 3 PREFLIGHT CONDENSED PREFLIGHT PROCESS This page sequence gives an overview of the Preflight operations of the FMS. The intent of each step is summarized on the next page.

FMS1 IDENT

1/2

NAV DATABASE ACTIVE K L M W W 0 6 9 7 OCT10-NOV06/03 S E C O N1/3 D POS INIT/REF -DEC04/96 K L MFWMWS0 6P9O7S NOV07 DR O P P R ON47 G R Ao26.28 M C F G o18.67 NO W122 ACT RTE 1 6 1 4R0E0F0 -W0A0Y5P O I N T 0 0 7 71/3 7 CKUBFI SOTROIMNG4ID7NAo 3 T1 A. B8 A0 SW E 1 2 2 oD1A8TD.EE0S0T E C -MKSEA ROTDEES T M A R 2 1 / 0PANC 2 UACT NDWAATYARTE O USSTA ERRNDBY B A S E1 LEGS DFALTTE N1/2 KL007 E C --U---D2T6E4SoT S E TM AIRN12S21./P80ON2SM CO ROUTE JOH /H

. . o 1D 1A 3T NE M 1/1 U T C2 6 2 FMS1 SETUP 280/1600A :04z OCT20/99 175D7173J DISPLAY o 6MAG 3ACT R ARTE R C A N1 C CO 1 0ROUTES> .6N M FUEL 1/2 1. GOR1600A T IMMAEX R A N G E FOFSSSE TW T 0>UTC 5736o0 NCMR S 1 0 . 0+5.0 N M9 7H 0 R0 SK G OFFSET ANC 2. RANCE FDUAETLU MW T C OEONRDDU/oFAF o 0>5LAT_ 5 .---.0 9 NWGS84< M1N4M0 0 K G 132 + 4CLONG 4R S RW06R F U E L/oFAF FLOW MILEAGE 3.

4.

100K G / N M 110K G / H R F U E LLEGS R E M A I N ILEGS N G A TETA> FIX ZCH 892K G UNIT



5.2 4 3 o / 3 0 K T 1 3 0 K T 34 CYUL TEMP TGT VS ---o C -1200F P M QNH VPA >2 9 . 9 2 i n H g -3.00o

1R 2R 3R 4R 5R 6R

When LNAV/VNAV is the active approach minima and the FMS baro-altitude input becomes invalid, the FMS will trigger the APPR DEGRADE TO LNAV alert message and will blank its vertical deviation. The active minima are thus downgraded to LNAV.

ACT 1L 2L 3L 4L 5L 6L

VNAV NDB24L

1/1

MINIMA LNAV 2.5N M

MDA-DA 660 105o -3.00o ZUL FAF 1500A 259o 7.2N M -3.00o RW24L / o M A P 2167 MAG W I N D GS VDEV >2 4 3 o / 3 0 K T 1 3 0 K T 34 CYUL TEMP TGT VS ---o C -1200F P M QNH VPA >2 9 . 9 2 i n H g -3.00o

1R 2R 3R 4R 5R 6R

Conducting a missed approach: The FMS must be selected as the source of guidance (LNAV) to fly the missed approach procedure.

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Page 7-20 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 7-3 MISCELLANEOUS CONSIDERATIONS FOR TERMINAL AREA OPERATIONS

MANUAL WAYPOINT SEQUENCING Some terminal area procedures involve radar vectors and thus require crew intervention (following ATC instructions) to manually sequence to the next leg of the active flight plan. To manually sequence these types of legs, a direct-to is required.

VECTORING TO FINAL APPROACH FIX ATC (Air Traffic Control) clearance to the FAF can be handled by converting the loaded approach into a straight-in approach. This is accomplished by direct-to navigation to intercept the inbound course to the final approach fix (FAF). With the ACT or MOD RTE LEGS 1/X page displayed:

ACT

RTE 1 LEGS

042o 1L 2L 3L 4L

ANC

1/3

36.8N M

/

240o P-T ANCPTL 195o P-T ANCPTR R060o CRS

ANC

3.00N M

1R 2R

2.25N M 3R 4.86N M

FAF

060o CRS 5L

RW06R

6L



6R

1. Copy to the scratchpad, the FAF identifier, and move it to the active waypoint location by pressing LSK 1L. 2. Key-in the desired inbound course to the FAF and press (LSK 6R). The intercept course changes to LARGE font and is copied to the active waypoint course. 3. Verify the course and distance of the leg to the active waypoint, and make the direct-to intercept active by pressing EXEC. Navigation and guidance to intercept the inbound course to the FAF on the current heading is provided. A straight-in approach can also be created in advance by inserting a temporary waypoint into the route as an initial approach fix (IAF) created as a place/bearing/distance waypoint based on, the FAF. On receipt of the ATC clearance, direct-to navigation to this temporary IAF, or to intercept the new leg inbound to the FAF, can then be performed.

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Page 7-21 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

CIRCLING APPROACHES Navigation and guidance to the landing runway during a circling approach procedure can be obtained, while retaining the correct missed approach procedure waypoints, by using direct-to intercept navigation to the landing runway threshold waypoint at the appropriate time. With the primary GPS or GPS overlay instrument approach procedure loaded into the route and made active: 1. At a convenient time, prepare for the circling manoeuvre by entering the landing runway number in the scratchpad. NOTE: The prefix "RW" is not required, but a leading zero must be used (e.g. 14 or RW14, 06L or RW06L). 2. Display the ACT RTE x LEGS 1/X page by pressing [LEGS], and move the landing runway number identifier to the active waypoint field by pressing LSK 1L. The “INTC CRS" prompt is displayed at LSK 6R with dashes ("---") as the default inbound course. A route discontinuity is inserted after the landing runway threshold waypoint. 3. Key in the landing runway heading as the intercept course, and select the direct-to intercept mode by pressing (LSK 6R). The inbound course is moved to the INTC CRS prompt field in LARGE font and is also copied to the to waypoint course.

MOD

RTE 1 LEGS

290o CRS 1L

RW29

1/2

22.2N M

/o

178

THEN 2L

†††††

1R 2R

-- ROUTE DISCONTINUITY 3L

YJN

FAF

051o CRS 4L

RW06

/oMAP

050o CRS 5L

( 536)

900

3R

2.66N M

183

4R

0.71N M

536A

5R

INTC CRS 6L

< S E L > TRANS ODK

1R 2R

3L

3R

4L

4R

5L

5R

6L



6R

1. If an approach is already selected, delete it by pressing LSK 1R. All approaches and runways are listed. 2. Display the desired runway by pressing [PREV] or [NEXT] as required and select it by pressing the appropriate right hand LSK. The APPROACHES field title is replaced by RUNWAYS with the selected runway displayed below it with the legend "". 3. Display the MOD RTE x LEGS 1/X page by pressing [LEGS]. The runway threshold waypoint is inserted into the route preceded by a route discontinuity. 4. Create an initial approach fix at a suitable distance from the runway threshold on the backwards extension of the runway heading using a place/bearing/distance temporary waypoint. NOTE: The temporary IAF is optional since direct-to navigation to the runway threshold intercepting the inbound course will accomplish the same result. 5. Make the modified route active by pressing [EXEC]. Direct-to navigation to the temporary IAF, or to intercept the inbound leg to the runway threshold will provide the necessary navigation and guidance.

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Page 7-23 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

AUTO-TUNING OF PRECISION APPROACHES When configured accordingly, auto-tuning of the ILS/MLS receiver is possible if an ILS/(MLS) or LOC or LOC Back-Course approach procedure is part of the active flight plan. The FMS will automatically tune the ILS/MLS receiver to the ILS/LOC/(MLS) navaid corresponding to the approach runway when airborne and within 150 nm (direct distance) of the runway threshold. MODIFYING APPROACH PROCEDURES To accommodate changes in approach clearances, new procedures can be selected at any time. Display the ARRIVALS 1/1 page for the desired airport by pressing [DEP/ARR]. NOTE: The ARRIVALS 1/1 page for the destination airport will be displayed by default if the aircraft is more than halfway to its destination. Otherwise, if the DEP/ARR INDEX 1/1 page is displayed, select the desired arrival airport by pressing the appropriate prompt (LSK 1R or LSK 2R). 1. Press the appropriate right LSK. Pressing LSK toggles the selection status between selected and not selected. The selected approach procedure (or portion thereof) is deleted. Repeat this process as required. NOTE: Deleting the approach will re-display all approaches and runways. Deleting only the approach transition results in display of only the transitions appropriate to the selected approach. 2. Select the new procedure(s) as described in previous sections. 3. Display the MOD RTE x LEGS 1/X page by pressing [LEGS], and verify the course and distance of the legs of the modified approach procedure, pressing [PREV] or [NEXT] as required. 4. Make the modified route active by pressing [EXEC]. NOTE: Special care is required when verifying the legs of a modified approach procedure, particularly when only a partial reselection has been made. Route discontinuities may exist, and certain waypoints of the retained segment(s), which may have been deleted automatically as part of the loading of the original approach procedure, may have to be re-inserted individually into the route by manual entry. NOTE: Modifications to the approach procedure are only allowed on the missed approach section.

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Page 7-24 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

DME ARC INTERCEPTION

ACT

RTE 1 LEGS

264o 1L 2L 3L

JOH 262o

113N M

D173J 270oRARCANC

ANC

1R 2R

10.6N M

D233J

3R

059o CRS 4L

1/2

12.8N M

10.0N M

FAF

060o CRS 5L

RW06R

6L



6R

The FMS provides automatic, autopilot-coupled interception of a DME arc at the arc's starting point. Interception of the arc at an intermediate point on the arc must be accomplished manually, as follows: 1. Disengage LNAV. 2. Perform a Direct to the arc's starting waypoint. 3. Manually fly the intercept. NOTE: When the arc capture criteria* are met, leg sequencing to arc navigation occurs automatically, indicated by an automatic waypoint sequence to the waypoint terminating the arc, and rotation of the (E)HSI course pointer to the arc's tangential course at the aircraft position. * For manual arc captures, arc capture criteria include a combination of XTK and TKE as well as being within +/- 90 degrees of the tangent to the starting point of the arc. NOTE: The display must be set to MAG (refer to Section 3, Angular References For Navigation And Display). 4. Re-engage LNAV. or: Autopilot-coupled interception of the arc at an intermediate point on the arc may be accomplished by moving the arc's starting point along the arc to the desired radial from the DME station as follows: With the arc's starting waypoint identifier in scratchpad: 1. Key in /, radial of the desired intermediate point on the arc from the DME station e.g. D173J/220. 2. Display the arc's starting waypoint location in the route by pressing [LEGS] and [NEXT] or [PREV] as required.

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Page 7-25 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 3. Line selects the scratchpad entry to the arc's starting waypoint location.

ACT

RTE 1 LEGS

264o 1L 2L

JOH

A

264o

120N M

D220J 310oRARCANC

3L

ANC

1R 2R

2.45N M

D233J

3R

059o CRS 4L

1/2

12.8N M

10.0N M

FAF

060o CRS 5L

RW06R

6L



6R

NOTE: The display must be set to MAG (refer to Section 3, Angular References For Navigation And Display). The new arc's starting waypoint is displayed with a new identifier derived from the entered radial e.g. D220J. 4. Make the modified route active by pressing [EXEC]. Once established on the arc, the (E)HSI course pointer displays the tangential course along the arc path. Lateral deviation is measured from this tangential course. Near the end of the arc, sequencing to the next waypoint occurs automatically, with the turn anticipation point computed such that no overshoot of the next navigation leg will occur up to maximum ground speed of 315 knots. At any time on the arc, the message HIGH ARC EXIT SPEED may be generated to indicate that the combination of true air speed and wind will cause an overshoot of the next navigation leg.

PROCEDURE TURNS When the approach transition includes a procedure turn, the FMS creates two outbound legs based on the procedure turn reference fix, followed by a turn in the correct direction to intercept the inbound course to the final approach fix. The still-air lengths of the procedure turn outbound legs are computed based on a time of 1 minute and 45 seconds respectively at a speed of 180 knots. The two outbound waypoints are named using the first three characters of the procedure turn reference fix, with the suffix PT added. The last character (L or R) indicates the direction of the turn at that waypoint. In addition, the courses of the two outbound legs have the legend P-T. The FMS provides navigation and guidance in the normal fashion for the two outbound legs of the procedure turn, followed by a turn to intercept the final approach course inbound to the final approach fix. When the maximum allowable procedure turn distance is less than 10 nm, the length of the first outbound leg may be reduced. As a result, navigation and guidance may sequence to the second outbound leg almost immediately after crossing the procedure turn reference fix.

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Page 7-26 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) CAUTION: During the procedure turn, it is the responsibility of the crew to ensure that the maximum distance from the procedure turn reference fix is not exceeded and that the aircraft remains within protected airspace at all times. The distance-to-go shown on the PROGRESS 1/3 or 1/4 page cannot be used for this purpose, except when the FAF is the active waypoint. The distance from the procedure turn reference fix can be monitored using the FIX page, as described in Section 5. NOTE: The FMS assumes a speed of 180 knots when building the size of the procedure turn. If the procedure is to be flown at a significantly different speed, then the crew should enter a speed constraint accordingly at the procedure turn reference point. Deletion of the procedure turn reference fix or the first outbound waypoint results in the deletion of the entire procedure turn. The two outbound waypoints cannot be copied to the scratchpad, and cannot be used as reference waypoints.

DELETION OF PROCEDURE TURNS If an approach transition including a procedure turn has been loaded into the route, it can be readily deleted and converted into a straight-in approach. With the ACT or MOD RTE x LEGS 1/X page displayed: 1. Line select to the scratchpad (do not key in), the procedure turn reference fix LSK 4L.

ACT

RTE 1 LEGS

042o 1L 2L 3L 4L

ANC

1/3

36.8N M

/

240o P-T ANCPTL 195o P-T ANCPTR R060o CRS

ANC

3.00N M

1R 2R

2.25N M 3R 4.86N M

FAF

060o CRS 5L

RW06R

6L



6R

2. Move the procedure turn reference fix to the active waypoint location by pressing LSK 1L. The procedure turn reference fix and the two outbound waypoints are deleted from the MOD route, and the FAF waypoint becomes the active waypoint, with the correct inbound course to the FAF displayed as the default intercept course. NOTE: The procedure turn also can be deleted by deleting the reference fix by means of the [CLR] functional key. However, depending on the order of the deletion and direct-to navigation actions, the intercept inbound course may have to be entered manually since the default value will be that of the original leg inbound to the reference fix.

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Page 7-27 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

This Page Intentionally Left Blank

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Page 7-28 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 8 - POST FLIGHT PROCEDURES

CONTENTS Subject

Page

SECTION 8 - POST FLIGHT PROCEDURES..........................................................................................................8-i POSITION ACCURACY CHECK - FLIGHT TERMINATION..........................................................................8-1 TAKE-OFF AND LANDING TIMES (if configured) .......................................................................................8-2

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Page 8-i July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

This Page Intentionally Left Blank

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Page 8-ii July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 8 POST-FLIGHT PROCEDURES

POSITION ACCURACY CHECK - FLIGHT TERMINATION

At the end of the flight, each IRS position can be compared against a reference position (e.g. GPS, or gate coordinates entered by the crew).

There are up to three identical pages, one for each IRS.

IRS2 ACCURACY 1L 2L

2/3

FMS POS GPS N47o32.44 E122o18.52 ENTER REF POS N47o32.44 E122o18.52

3L

2R 3R

5L

IRS POS ERR 2.5N M RESID GS 5.2K T

6L



4L

1R

NAV TIME 02H16 IRS DRIFT 1.1N M / H R

4R 5R 6R

FMS POS (1L or 1R): Displays FMS present position. ENTER REF POS [2L or 2R]: Valid latitude and longitude entry will enable accuracy test to be performed and results displayed on following lines. Default value is FMS POS, as displayed in LSK 1R. The page displays the IRS position error (with respect to the reference position), the IRS residual ground speed, the IRS Time in Nav and the IRS drift rate (only when IRS Time in NAV > 10 minutes).

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Page 8-1 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

TAKE-OFF AND LANDING TIMES (if configured)

FLIGHT LOG 1L 2L

TAKEOFF 1235Z INFLIGHT 01+00

3L

1/1

LANDING 1335Z AIR MILES 560N M LANDINGS 1

1R 2R 3R

4L

4R

5L

5R

6L

RIGHT

1/1

SPD/ALT 2 3 0 / 5000A ICAO SPD 230K T

1R 2R

INBD CRS 3L

050

4L

LEG TIME/DIS 1.0M I N / - - . - N M EXIT TYPE

5L 6L

o

3R FIX ETA

STATUS MANUAL INACTIVE *FIX CSTR:210/6000*

RIGHT

1/1

SPD/ALT 2 3 0 / 5000A ICAO SPD 230K T

1R 2R

INBD CRS 3L

282

4L

LEG TIME/DIS 1.0M I N / - - . - N M EXIT TYPE

5L 6L

o

MANUAL

3R FIX ETA

1425Z

4R

STATUS INACTIVE

5R

RIGHT

1/1

SPD/ALT 2 3 0 / 5000A ICAO SPD 230K T

1R 2R

INBD CRS 3L

050 o

4L

LEG TIME/DIS 1.0M I N / - - . - N M EXIT TYPE

5L 6L

MANUAL

4R 5R 6R

2. Arm the exit hold procedure by pressing (LSK 6R). The "EXIT HOLD" prompt disappears, the status changes to EXITING HOLD and the prompt displays in green reverse video. "ACT" status in the title line changes to "MOD", and the EXEC annunciator illuminates. NOTE: The hold exit can be cancelled at this point by pressing (LSK 6L). The prompt reverts to "NEW HOLD", the prompt is displayed in green reverse video, the status changes to IN PROGRESS, "MOD" status reverts to "ACT", and the EXEC annunciator extinguishes. 3. Initiate exit from the hold by pressing [EXEC]. The FMS commands an immediate turn towards the holding fix to exit the holding pattern over the fix, followed by continuation of the active route. If the hold exit is initiated on the outbound leg, a shortened racetrack holding pattern is displayed on the EFIS. If a parallel or teardrop is still being performed when the exit hold is initiated, the entry procedure is completed normally prior to exiting the hold. Sequencing of the holding fix is done without turn anticipation (Fly-over). B. EXIT BY DIRECT-TO NAVIGATION TO THE HOLDING FIX Perform a standard direct-to procedure to the holding fix. When the direct-to is executed, navigation and guidance is provided for an immediate turn towards the inbound holding course. Sequencing of the holding fix is done with turn anticipation (Fly-by). NOTE: This procedure is only valid if the holding fix is a navigation database waypoint, therefore this procedure could not be used for holding fix at present position (PPOS).

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Page 10-10 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

C. EXIT BY DIRECT-TO NAVIGATION TO ANY WAYPOINT Perform a standard direct-to procedure to any waypoint. When the direct-to is EXECuted, navigation and guidance is provided to turn in the shortest direction to the direct-to course.

CONTINUE TO HOLD When a procedure is defined with an exit type equals to “ONCE” or “AT TGT ALT”, and it is required to remain in the hold, the following procedure should be executed: 1. Display the ACT HOLD 1/X page by pressing [HOLD]. Refer to HOLD 1/1 page in Appendix A for details.

ACT

RTE 1 HOLD

FIX 1L

KILLA TURN DIR

2L

1/1

SPD/ALT 2 3 0 / 5000A ICAO SPD 230K T

>RIGHT

1R 2R

INBD CRS 3L

050o

4L

LEG TIME/DIS 1.0M I N / - - . - N M EXIT TYPE

5L 6L

MANUAL

4R 5R 6R

2. Resume the exit hold procedure by pressing (LSK 5L). The "RESUME HOLD" prompt disappears, the status changes to RESUMING HOLD, the exit type changes to MANUAL and the prompt is displayed in green reverse video. "ACT" status in the title line changes to "MOD", and the EXEC annunciator illuminates. NOTE: The resuming hold can be cancelled at this point by pressing (LSK 6L). The prompt reverts to "NEW HOLD", the prompt is displayed in green reverse video, the status changes to EXIT ARMED, "MOD" status reverts to "ACT", and the EXEC annunciator extinguishes. NOTE: After the ONCE or AT TGT ALT procedure has been changed to a manual hold, it is impossible to return to the hold procedure defined in the navigation database. 3. Confirm the resume hold procedure by pressing (LSK 6R). The "RESUME HOLD" prompt is changed to EXIT HOLD, the status changes to IN PROGRESS, and the prompt is displayed. "MOD" status in the title line changes to "ACT", and the EXEC annunciator extinguishes.

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Page 10-11 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

HOLDING PATTERN DELETION A. PRIOR TO ENTRY 1. Display the desired holding waypoint by pressing [LEGS], [NEXT] or [PREV] as required. 2. Key in /. 3. Cancel the hold by pressing the appropriate LSK. The "/H" legend at the selected waypoint is deleted. The waypoint is NOT deleted from route. 4. Accept the modified route by pressing [EXEC]. B. AFTER HOLD ENTRY INITIATED Perform any exit hold procedure.

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Page 10-12 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 11 - TACTICAL FUNCTIONS

CONTENTS Subject

Page

INTRODUCTION (additions to Section 1) ..................................................................................................11-1 NAVIGATION MODES...........................................................................................................................11-1 PREFLIGHT (additions to Section 3) .........................................................................................................11-2 FMS DISPLAY SETUP ..........................................................................................................................11-2 ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY ..........................................................11-2 USER DATABASE.................................................................................................................................11-4 A. MANUAL ENTRY OF A FIXED USER WAYPOINT IN THE DATABASE ...............................11-4 B. MANUAL ENTRY OF A MOVING USER WAYPOINT IN THE DATABASE ...........................11-6 C. MANUAL ENTRY OF AN AIRPORT TYPE USER WAYPOINT IN THE DATABASE ............11-7 D. DELETE A USER WAYPOINT FROM THE USER DATABASE .............................................11-8 E. DELETE ALL THE USER WAYPOINTS FROM THE USER DATABASE ............................11-10 F. VIEW ALL THE USER WAYPOINTS IN THE DATABASE ...................................................11-11 G. SAVING THE DATABASE FOR USE BY ANOTHER AIRCRAFT ........................................11-11 ACTIVE ROUTE SELECTION USING THE USER ROUTE NAME ....................................................11-13 ROUTE SELECTION FROM THE LIST OF USER ROUTES .............................................................11-14 ENROUTE (additions to Section 5) ..........................................................................................................11-15 INSERTING A RADIAL-TO SEGMENT...............................................................................................11-15 DIRECT-TO/INTERCEPT (additions to Section 9)...................................................................................11-17 INTRODUCTION ..................................................................................................................................11-17 NAVIGATION OF DIRECT-TO A WAYPOINT WHEN FMS IS CONFIGURED FOR A "MOVING DTK" DIRECT-TO ..........................................................................................................................................11-17 NAVIGATION OF TACTICAL DIRECT-TO A WAYPOINT .................................................................11-18 TACTICAL DIRECT-TO A WAYPOINT PROCEDURE.......................................................................11-18 BACKTRACK ROUTE .........................................................................................................................11-20 RENDEZ-VOUS WITH A MOVING WAYPOINT .................................................................................11-22 MARK ON TOP (If configured)...........................................................................................................11-23 POSITION UPDATE.............................................................................................................................11-25

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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

This Page Intentionally Left Blank

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Page 11-ii July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SECTION 11 TACTICAL FUNCTIONS This section covers tactical functions that are not normally enabled when the FMS is configured for Air Transport Operations. The sub-sections of this current section amend previous sections of the manual, in the context of tactical operations (non air-transport).

INTRODUCTION (additions to Section 1)

NAVIGATION MODES Current sub-section is introduced to document input from TACAN receiver. The FMS follows a hierarchical navigation mode system using TSO-approved sensors characterized by the following decreasing priority order: NAVIGATION MODES GPS DME/DME VOR/DME/TACAN Inertial Dead Reckoning

SENSOR

TSO-C129a B1/C1 GPS sensor TSO-C66c DME receiver TSO-C66c DME receiver; TSO-C40c VOR receiver TSO-C4c, TSO-C6d IRS Heading + TAS inputs

VOR/DME/TACAN VOR/DME navigation is used in areas with sparse DME coverage where there are less than three DME stations available. This mode combines co-located DME or TACAN distance and VOR or TACAN bearing to determine position. Tuned facility information is displayed on the VOR/DME/TACAN STATUS page and individual stations can be inhibited from the navigation solution from the VHF NAV DESELECT page.

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Page 11-1 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

PREFLIGHT (additions to Section 3)

FMS DISPLAY SETUP Color/Monochrome display setup: NOTE: COLOR/MONOCHROME selection prompt is unavailable when the Air Transport configuration option is enabled.

DISPLAY 1L

1/1

COLOR

3R

4L

4R

5L

5R

6L

6R

1.Press (LSK 3L) and select color or monochrome for this test. Re-select color thereafter. 2.Press [INIT/REF]. 3.Press to return to the IDENT 1/2 page.

ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY

FMS1 SETUP

1/1

DISPLAY 1L

>MAG TIME

2L

>UTC COORD

3L

>LAT_LONG

OFFSET

+5.0H R S

1R 2R

DATUM

WGS84<

4L

3R 4R

5L

FMS OPERATION >SYNCHRONIZED

6L



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Page 11-2 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Select time reference to LOCAL or UTC by pressing LSK 2L. If UTC time is selected enter the local time offset from the UTC time by pressing LSK 2R. (Validity checking ensures entry is between +/-12.0 hours and steps are 0.5 hours). Press (LSK 3L) and select coordinates. SWISS_GRID.

Possible values are LAT_LONG, UTM, MGRS and

NOTE: The TIME, OFFSET, COORD and DATUM prompts are not available when the Air Transport configuration option is enabled. Only one coordinate system is active for both entry and display of positional information at any given time. Swiss Grid position is defined as Northing and Easting coordinates up to 999 km, locating a position to within 10 meter square. The FMS is able to display to full range of the Swiss Grid coordinate system. However, the FMS will only accept manual entries within the following limits: 062 - 302 (Northing) 480 - 865 (Easting) Press (LSK 3R) and select appropriate datum. Fifty-one possible values can be configured (e.g.: WGS84, ARC 1960, AUSSIE 84). NOTE:

If the SWISS_GRID coordinates are chosen, the DATUM is set to CH1903 and cannot be changed.

NOTE:

WGS84 is the certified datum for commercial use.

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Page 11-3 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

USER DATABASE The FMS contains a User database which is used to store user waypoints and user routes. User waypoints can be: • entered from the scratchpad or • received from the digital map or • loaded from or saved to the DLU. It is also possible to associate the existing route (MOD/ACT) with a user route created by the user and stored in the User database. User waypoints can be defined as different types: • Waypoint (fixed or moving); • Airport; • VHF NAV (TACAN only). A new user waypoint can be created on the USER WPT pages either by directly entering the coordinates of the new waypoint or by using a known position as reference and a radial/distance from the reference position to the desired user waypoint position. Moving waypoints may be created if the Moving Waypoint configuration option is selected. The FMS can be configured to automatically delete the entire content of the user database on every cold start when aircraft is on the ground. A. MANUAL ENTRY OF A FIXED USER WAYPOINT IN THE DATABASE Display the NAV DATA 1/1 page by pressing [INIT REF], (LSK 1R).

NAV DATA

1/1

ID 1L

-----

1R

2L

2R

3L

3R

4L

4R

5L

5R

6L



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Page 11-4 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

1. Press the prompt at LSK 6R.

USER WPT

1/2

††††† I D / P O S o

1L

FREE= 459 o ††† ††.†††††† ††.†† BRG/DIS

1R

T

2L

--- /---N M

2R

TYPE 3L

>FIXED

3R

REF WPT ID 4L

RAD/DIS o

-----

/

NM

4R

REF WPT POS 5L

---o--.-- ----o--.--

5R

6L



2. Enter the waypoint identifier in the ID field at LSK 1L. 3. Enter the position at LSK 1R or enter the Bearing/Distance at position LSK 2L. By entering a Bearing/Distance, the FMS computes a position using as reference the present position and displays the coordinates of the user waypoint to be displayed on LSK 1R. The number of available waypoints are displayed in the “FREE=“field (a maximum of 460 user waypoints can be defined).

1L

USER WPT 1/2 ADFF I D / P O S ACT RTE N45o12.23 W043o32.12 BRG/DIS

TRK/GS

T

2L

1R

T

223 /115N M

111 /222K T

2R

TYPE 3L

MOVING

3R

REF WPT ID 4L

RAD/DIS o

ADED

000 /0.00N M

4R

REF WPT POS 5L

N45o12.23 W043o32.12

5R

6L



4. When the mandatory fields are filled (e.g. name and position of the new user waypoint), a CANCEL/CONFIRM prompt is displayed. Press to accept (LSK 6R) or (LSK 6L).

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Page 11-5 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

B. MANUAL ENTRY OF A MOVING USER WAYPOINT IN THE DATABASE Access the USER WPT 1/2 page by pressing [INIT REF], (LSK 1R), and (LSK 6L).

USER WPT

1/2

††††† I D / P O S o

1L

FREE= 459 o ††† ††.†††††† ††.†† BRG/DIS TRK/GS T

2L

T

--- /---N M

/

KT

1R 2R

TYPE 3L

>FIXED

3R

REF WPT ID 4L

RAD/DIS o

-----

/

NM

4R

REF WPT POS 5L

---o--.-- ----o--.--

5R

6L



1. To create a moving waypoint, toggle the “Type” prompt (LSK 3L) from Fixed to Moving. 2. Enter the waypoint identifier in the ID field at LSK 1L. 3. Enter the position at LSK 1R or the Bearing/Distance at position LSK 2L. 4. Enter the Track and Ground Speed of the moving waypoint at LSK 2R. 5. When the mandatory fields are filled, a CANCEL/CONFIRM prompt is displayed. Press (LSK 6R) to accept or (LSK 6L).

USER WPT ADFF

ID/POS

N45o12.23 043o32.12

1L

BRG/DIS

TRK/GS

T

2L

1/2

FREE= 459 1R

T

223 /115N M

111 / 22K T

2R

TYPE 3L

>MOVING

3R

REF WPT ID 4L

RAD/DIS

000o/0.00N M

ADED

4R

REF WPT POS 5L

N45o12.23 W043o32.12

5R

6L



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Page 11-6 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

6. After confirming, the moving waypoint is saved in the user database and can be viewed in the user waypoint list (user waypoints are displayed in alphabetical order on the USER WPT LIST 1/1 page). Access the USER WPT LIST 1/1 page by pressing [INIT REF], (LSK 2R), and (LSK 1L). The moving waypoints are identified by displaying the symbol MOV in reverse video besides and underneath the waypoint identifier. The distance from the present position to the user waypoints is also displayed in the USER WPT LIST 1/X page.

USER WPT LIST DIS NM 20.1

1R

82.7>

2R

32.6>

3R

24.1>

4R

1L



REGION 2L

---/--

1R 2R

3L

3R

4L

4R

5L

5R

6L



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Page 11-10 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

F. VIEW ALL THE USER WAYPOINTS IN THE DATABASE The complete list of the user waypoints can be viewed by pressing [INIT REF], , . Up to 10 user waypoints are displayed on a single page and a maximum of 460 waypoints can be defined. To view the other pages press [NEXT] or [PREV].

USER WPT LIST

1/2

1L

DIS NM

1R

2L



2R

3L



3R

4L



4R

5L



5R

6L

MOV

MOV

MOV

USER_DATA STATUS IDLE

1R 0000K B 2R

3L

3R

LOAD>

4L 5L 6L

4R 5R



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Page 11-11 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

2. Press SAVE (LSK 6R) to start data download from the FMS to the Data Loader Unit (only when aircraft on ground).

DATA LOAD

1/1

TYPE 1L

>USER_DATA

2L

STATUS SAVING TO DISK 0014KB 56%

3L 4L

2R 3R



5R

DEPARTURES>

6R

6L

DIRECT

6L



6R

User routes are displayed left to right, in the order of entry. 1. Display the desired route by pressing [NEXT] or [PREV] as often as required. 2. Select route identifier by pressing the appropriate LSK. 3. Select the direction in which the route is loaded by toggling DIRECT/INVERSE using LSK 5L. 4. The RTE 1/X page is re-displayed. Verify the ORIGIN and DEST identifiers. 5. Accept the new active route by pressing [EXEC]. When airborne, selecting a user route will replace the destination with the selected user route destination and will insert a discontinuity after the active waypoint followed by the selected user route waypoints. If a procedure (for e.g. STAR or Approach) is part of the flight plan, the whole procedure is replaced by the select user route.

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Page 11-14 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

ENROUTE (additions to Section 5)

INSERTING A RADIAL-TO SEGMENT A Radial-To segment is first defined in the RADIAL-TO, which is accessed in one of the following ways: • •

by pressing [INIT REF], (LSK 6R), entering the waypoint ident in the REF ID field at LSK 1L and then pressing (LSK 4R); by typing /R in the scratchpad and pressing the LSK corresponding to the waypoint on which the operator wants to define a Radial-To procedure.

NOTE:

A"RADIAL-TO" can also be inserted in the inactive route by pressing [INIT REF], (LSK 6R), [NEXT] (for the INACT DES+SAR 2/2), entering the waypoint ident in the REF ID field at LSK 1L and (LSK 4R).

RTE 1 RADIAL-TO

1/1

FIX 1L

YUL

1R

INBD CRS o

2L

016

2R

DISTANCE 3L

10.0N M

3R

4L

4R

5L

5R

6L

2 degrees intercept course is variable; deviation needle is centered

12

15

18

21

24

09

27

06

30

12

24

09

27

06

When TKE < 2 degrees intercept course is fixed; deviation needle is according to aircraft position

12

24

09

27

06

30

33

15

18

21

0703004

Figure 9-1 "Moving DTK" Direct-To a Waypoint Procedure

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Page 11-17 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

NAVIGATION OF TACTICAL DIRECT-TO A WAYPOINT When a Tactical Direct-To a waypoint procedure is executed, the FMS provides Roll steering, track angle error and lateral deviation guidance to the FD/AP based on the aircraft present position and track. The Tactical Direct-To behaves similarly as the “Moving DTK” Direct-To. The difference between the Tactical Direct-To and the “Moving DTK” Direct-To consists in the condition to freeze the direct track to the active waypoint. In the case of the Tactical Direct-To, this condition is the minimum turn distance (as opposed to the +/- 2 degrees track difference in the case of a “Moving DTK” Direct-To).

TACTICAL DIRECT-TO A WAYPOINT PROCEDURE A. TACTICAL DIRECT-TO A WAYPOINT IN THE ACTIVE ROUTE 1. Display the DES+SAR 1/2 page by pressing [INIT REF], . 2. Enter the waypoint identifier in the REF ID field. 3. Press (LSK 5R). 4. The waypoint identifier followed by the “/T” qualifier is displayed in the scratchpad and the ACT RTE x LEGS 1/X page is displayed. 5. Move the waypoint identifier to the active waypoint field by pressing LSK 1L. "ACT" status on the title line is replaced by "MOD". The direct course and distance from aircraft present position to the active waypoint is displayed. 6. Verify the inbound course and distance of the leg to the active waypoint. Information on any other page can be verified prior to making the tactical direct-to leg active. 7. Make the tactical direct-to leg active by pressing [EXEC]. Another method of initiating a Tactical Direct-To is using the “/T” qualifier directly: 1. Display ACT RTE x LEGS 1/X page by pressing [LEGS]. 2. Display the desired waypoint by pressing [NEXT] or [PREV] as required. 3. Key in, or copy the waypoint identifier into the scratchpad by pressing the appropriate LSK. 4. Key in the “/T” qualifier after the waypoint identifier. 5. Return to the first ACT RTE x LEGS 1/X page by pressing [LEGS] or [PREV] as required. 6. Move the waypoint identifier to the active waypoint field by pressing LSK 1L. "ACT" status on the title line is replaced by "MOD". The direct course and distance from aircraft present position to the active waypoint is displayed.

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Page 11-18 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 7. Verify the inbound course and distance of the leg to the active waypoint. Information on any other page can be verified prior to making the tactical direct-to leg active. 8. Make the tactical direct-to leg active by pressing [EXEC]. B. TACTICAL DIRECT-TO A WAYPOINT IN THE INACTIVE ROUTE 1. Display the INACT DES+SAR 2/2 page by pressing [INIT REF], , [NEXT]. 2. Enter the waypoint identifier in the REF ID field. 3. Press (LSK 5R). 4. The waypoint identifier followed by the “/T” qualifier is displayed in the scratchpad and the RTE x LEGS 1/X page is displayed. 5. Move the waypoint identifier to the active waypoint field by pressing LSK 1L. 6. Verify the inbound course and distance of the leg to the active waypoint. Information on any other page can be verified prior to making the tactical direct-to leg active. 7. Insert the tactical direct-to leg in the inactive route by pressing .

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Page 11-19 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

BACKTRACK ROUTE The FMS provides an backtrack route function which retraces the route flown allowing an aircraft to fly back, from the present position to the origin, following the same sequence of waypoints flown but excluding any waypoints associated to the following special procedures: • • • •

STAR; SID; APPROACH; HOLDING.

NOTE: The origin of a HOLDING procedure is included in the inverse route. When a manual Direct-To or a Direct-To with Intercept is performed in the active route, the FMS adds a temporary waypoint to the inverse route to mark the present position except when on ground or during the special procedures mentioned above. All legs in the backtrack route are flown as Track between two Fixes (ARINC 424 TF leg type), except for the first leg, which is flown as a Track between two Fixes (ARINC 424 TF leg type) only if the previously flown leg is preserved. Otherwise, the first leg is flown as a Direct To Fix (ARINC 424 DF leg type). Activation of the backtrack route while in-flight is configurable with two following options. The resulting modified route consists of: A. Configuration Option 1 (default) If a current active waypoint is defined: • the current active waypoint, starting at the Top waypoint location on the MOD LEGS page, followed by a discontinuity, then • a temporary waypoint to mark the present position and then • the waypoints of the backtrack route. Otherwise, • a temporary waypoint to mark the present position, starting at the Top waypoint location on the MOD LEGS page; then • the waypoints of the backtrack route. B. Configuration Option 2 • •

the first waypoint of the backtrack route, starting at the Top waypoint location on the MOD LEGS page, which is the last overflown waypoint with its course set in the opposite track direction (e.g. original track - 180º); then the remaining waypoints of the backtrack route.

Following activation of the backtrack route while on ground, the resulting modified route consist of the waypoints of the backtrack route, starting at the Top waypoint location on the MOD LEGS page, regardless of the selected configuration option. When the Inactive route is engaged, the FMS keeps the existent waypoints in the backtrack route and continues adding waypoints to the same backtrack route list as the new route is flown.

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Page 11-20 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

The backtrack route records the waypoint attribute (flyby or flyover). The backtrack route is available only from the active route page. The backtrack route is configurable. 1.

Display the ACT RTE 1 1/X page by pressing the RTE functional key:

ACT

RTE 1

ORIGIN 1L

KSEA RUNWAY

2L

-----

1/3 DEST

PANC FLT NO

KL007

1R 2R

ROUTE 3L 4L



5R

OFFSET 6L

+ 1 7 5 FT/MIN

6L



1R 2R 3R 4R 5R 6R

The crew can verify the individual IRS position and ground speed against the FMS system position and ground speed. It can also verify the individual IRS status, action code, and update mode. 1. Display the POS INIT/REF 3/3 page by pressing [INIT REF], , [NEXT], [NEXT]. A. LTN_92 installation:

POS INIT/REF 1L

3/3

FMS POS GPS GSK T N47o32.04 E122o18.50 250

2L

2R

5L

IRS1 N47o32.03 IRS2 N47o32.04 IRS3 N47o32.03

6L

AUTOMATIC NAV1 TEST

>READY

DME1 TEST

5L

>READY

6L

A C T I V E

6L

AUTOMATIC

2/2

MLS MODE

MANUAL<

1R

2L

2R

3L

3R

4L

4R

5L

5R

6L

ADF

4L

>OFF

ANT< ON<

MAG-BRG

5L

REL-BRG >2 3 1 o

6L



<

1R 2R 3R 4R 5R 6R

NOTE: The ADF ident suffix "x" (e.g. ADF, ADF1...) and the side (left or right) where the ADF units appear are depending on the installation configuration. The tables below provide examples. ADF1 [1L]: Display and modify active/standby frequency of the ADF1 radio. Selecting LSK_1L when the scratchpad is empty will toggle the standby and the active frequency. ADF2 [1R]: Display and modify active/standby frequency of the ADF2 radio. Selecting LSK_1R when the scratchpad is empty will toggle the standby and the active frequency. MODE [3L,3R]: Displays mode status for the ADF radio. Pressing this softkey selects the next option. The possible values are ADF and ANT if the ADF mode is configured for ADF and ANT operation. Otherwise, only ADF mode is available. BFO [4L,4R]: Displays mode status for the ADF radio. Pressing this softkey selects the next option. The possible values are ON and OFF. REL-BRG/MAG BRG/TRUE BRG [5L,5R]: Set and display of the ADF Bearing display mode and Bearing data. At power on, the FMS will display the last ADF Bearing display mode setting prior to the last FMS power interruption.

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Page 13-18 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) NOTE: The ADF does not provide bearing data while its mode of operation is set to "ANT". RADIO [6L]: Access to the RADIO top level page where ADF is located. LIBRARY [6R]: Access to the ADF Library page.

NAVIGATION RADIOS (ADF Page 2/2) This page allows the pilot to control the operation of up to 2 ADF units. NOTE: This page is only displayed if radio test is configured. NOTE: This page may no longer be displayed once airborne if configured accordingly. Display the second ADF RADIO page from the horizontal configuration by pressing [RADIO], , [NEXT] or [RADIO], [NEXT], , [NEXT] or [RADIO], [RADIO], , [NEXT]. Display the second ADF RADIO page from the vertical configuration by pressing [RADIO], [NEXT], , [NEXT] or [RADIO], , , [NEXT] or [RADIO], [RADIO], , [NEXT].

ADF 1L

1R

2L

2R

3L

3R

4L

NOTE:

2/2

ADF1 TEST

5L

>READY

6L

OFF

4L

-- 151.000b -- 124.650 SQUELCH

ON<

VOICE/DATA

5L 6L

1/2 VHF2



6R

NOTE: The COM VHF radio equipment name can also be configured as “COM" or "VHF". The VHF ident suffix "x" (e.g. VHF, VHF1...) and the side (left or right) where the COM units appear is depending on the installation configuration. The tables below provide examples. VHF1 [1L]: Display and modify active/standby frequency of the VHF1 radio. Selecting LSK 1L when the scratchpad is empty will toggle the standby and the active frequency. VHF2 [1R]: Same as above, but referencing VHF2 instead of VHF1 and LSK 2R instead of LSK 1L. NOTE: It is possible to have "-" in one or both of the active and standby fields after FMS maintenance. Toggling is not allowed when "-" are present in the standby field. Then, a frequency needs to be entered in the standby field first before the active/standby field toggling is allowed, otherwise a warning message will be displayed in the scratchpad. SQUELCH [3L]: When configured and for VHF-422 and VHF-4000 VHF radios only, toggles COM1 radio squelch status ON or OFF. SQUELCH [3R]: Same as above, but referencing COM2 instead of COM1.

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Page 13-20 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) VOICE/DATA [5R]: When voice/data control is configured and for the VHF-422 and VHF-4000 VHF radios only, allows the crew to place the VHF radio in either the VOICE or DATA mode. RADIO [6L]: Access to the RADIO top level page where the VHF is located. LIBRARY [6R]: Access to the access to the VHF Library page.

COMMUNICATION RADIOS (VHF RADIO Page 2/2) This page allows the pilot to control the operation of up to two VHF units. NOTE: This page is only displayed if radio test is configured. Display the second VHF 2/2 page from the horizontal configuration by pressing [RADIO], , [NEXT] or [RADIO], [NEXT], , [NEXT] or [RADIO], [RADIO], , [NEXT]. Display the second VHF 2/2 page from the vertical configuration by pressing [RADIO], [NEXT], , [NEXT] or [RADIO], , , [NEXT] or [RADIO], [RADIO], , [NEXT].

VHF

2/2

1L

1R

2L

2R

3L

3R

4L 5L

VHF1 TEST >R E A D Y

6L

TUNE GUARD

3L

>AM

4L

>TR_G

5L

>TUNE 243

6L



6R

NOTE: The COM VUF radio equipment name can also be configured as “COM" or "VUF". The VUF ident suffix "x" (e.g. VUF, VUF1...) and the side (left or right) where the radio units appear is depending on the installation configuration. The tables below provide examples. NOTE: If single VUHF installed and configured name is VUF, then the display will show VUHF. NOTE: If the EMERGENCY discrete is configured to DISABLE, when an emergency signal is received FMS tuning of the VUHF radio is inhibited, MODE (3L/3R), and RX MODE (4L/4R) operator inputs are

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Page 13-36 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) ignored and the FMS will display the alert message “VUHFx CONTROL LOST” since the FMS cannot control the identified COM radio. VUFx [1L]/[1R]: Display and modify the active/standby preset number and frequency/channel of the VUF1 radio. For installations which support Have Quick (ECCM) functionality, this field will also accept net number entries (if configured) of the form AXX.XYY (where XX.X ranges from 00.0 through 99.9 and YY can be either 00, 25, or 50). Note that entry of a net number in this field will change the MODE field to HVQK (Have Quick). Entry from the keyboard is validated and then the frequency and preset/channel, if available, or net number, are placed in the standby field below the active field, otherwise an error message is displayed in the scratchpad. If the scratchpad is empty it toggles between active/standby identifiers. During the tuning process, the active frequency field is displayed in large font reverse white color. If the tuning operation is not successful, the active frequency field is displayed in small font amber font color as a warning to the pilot. Preset and channel are displayed in small font green color. Maritime channel numbers are shown in the form Cxx (where xx=the maritime channel number). Additionally, guard and emergency 243 activation will be shown next to the text VUFx. To indicate activation of these, GUARD and EMER, respectively, will be displayed just next to the title text VUFx in reverse white font to inform the crew of the selection of these prompts. NOTE: It is possible to have "-" in one or both of the active and standby fields after FMS maintenance. Toggling is not allowed when "-" are present in the standby field. At that time, a frequency/channel needs to be entered in the standby field first before the active/standby field toggling is allowed, otherwise a warning message will be displayed in the scratchpad. TUNE GUARD [2L]/[2R]: Selection of this prompt will tune the radio to emergency frequency corresponding to the currently active frequency band. When configured to operate with an external radio control panel, and if an appropriate feedback is received from the V/UHF radio, the TUNE GUARD function will be activated. For operations without an external control head, during an FMS warm start, the last TUNE GUARD setting will be restored. That is, once this prompt is selected, the active frequency will be commanded to 40.500, 121.500, 156.800 (“C16” will also be shown in preset field), or 243.000 MHz (refer to table of Figure 13-4), and the previously active frequency will be moved into the standby field. The receiver mode (RX MODE) will also change to TR and “GUARD” will be annunciated next to the text at LSK 1L/1R as well on the corresponding V/UHF radio’s line on the top RADIO page (e.g. RADIO 1/X or 2/X). Also, once this prompt is activated, the prompt itself is removed from view until the operator makes another V/UHF radio parameter selection which causes the guard state to no longer be maintained. When TUNE 243 is activated or while in HVQK (Have Quick) mode, this prompt is removed from view and unavailable for selection.

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Page 13-37 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

MODE [3L]/[3R]: As a function of the entered active frequency field value, this prompt will then offer any possible toggle options for the given active field entry currently at LSK 1L/1R. Depending on the frequency field value entered, the mode displayed can be either AM, FM, MAR (with qualifier SHIP or COAST), or HVQK (if ECCM is configured). The possible MODE options for the various frequency bands shown in the table shown of Figure 13-4 are described here: • when the entered active frequency lies within a frequency range having only AM as a possible modulation, the MODE will change to "AM" with this being the only possible toggle setting • when the entered active frequency lies within a frequency range having only FM as a possible modulation and is not a maritime band frequency having an associated maritime channel, the MODE will change to "FM" with this being the only possible toggle setting • when the entered active frequency lies within a frequency range having only FM as a possible modulation and the entered frequency is a maritime band frequency, the possible mode settings is "FM" or "MAR" (with MAR showing qualifier 'SHIP' or 'COAST' next to it). The FMS will change MODE as follows: • upon initial entry of the maritime band frequency, MODE will be set to "FM" and the operator can then (optionally) toggle to the MAR mode (refer to NOTE) • if already in MAR mode and a maritime band frequency is entered: • MODE remains MAR (showing qualifier 'SHIP' or 'COAST' next to it) if the entered frequency has an associated maritime channel (per Table 2); otherwise, • MODE will be set to "FM" if the entered frequency does not have an associated maritime channel • •

when the active frequency lies within a frequency range having either AM or FM as a possible modulation, the available mode settings are "AM" or "FM". when the active frequency field contains a net number (for Have Quick installations), the only available mode setting is "HVQK".

NOTE: If when toggling to MAR mode, the active frequency has an associated maritime channel, then this channel will be displayed using the Cxx format, otherwise two dashes are displayed in the channel/preset field. RX MODE [4L]/[4R]: Toggles and displays VUHF receiver mode options. The possible values are: TR, TR_G TUNE 243 [5L]/[5R]: Selection activates the emergency 243 guard precedence mode within the V/UHF radio. The FMS will then set the V/UHF control parameters as follows: • When configured to operate with an external radio control panel, and if an appropriate feedback is received from the V/UHF radio, the active frequency will be set to 243.000. For operations without an external control head, during an FMS warm start, the last TUNE 243 setting will be restored. • the previously active frequency field content will be moved into the standby field • mode will be set to AM • receiver mode set to TR_G • SQUELCH will be set OFF on VUF page 2/2 (or page VUF 3/3 for Have Quick installations) • “EMER” will be annunciated next to the text at LSK 1L/1R as well on the corresponding V/UHF radio’s line on the top RADIO page (e.g. RADIO 1/X or 2/X). • the TUNE 243 prompt will be removed and only returns once emergency 243 is exited NOTE: Activation of the emergency discrete will yield the same result as when selecting the TUNE 243 prompt with the exception that the EMERGENCY ENGAGED scratchpad message will also be triggered when the emergency discrete is activated. RADIO [6L]: Access to the RADIO top level page where the VUHF is located. LIBRARY [6R]: Access the VUF LIBRARY 1/N page.

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Page 13-38 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

COMMUNICATION RADIOS (VUF RADIO Page X/X) NOTE: Page number will change as follows: X=2 for non-Have Quick installations and X=3 for Have Quick installations. This page allows the pilot to control the operation of up to 2 VUHF radios. For non-Have Quick installations, display this page from the horizontal configuration by pressing [RADIO], , [NEXT] or [RADIO], [NEXT], , [NEXT] or [RADIO], [RADIO], , [NEXT]. For Have Quick installations, display this page from the horizontal configuration by pressing [RADIO], , [NEXT] [NEXT] or [RADIO], [NEXT], , [NEXT] [NEXT] or [RADIO], [RADIO], , [NEXT], [NEXT].

VUF VUF1 LVL 1L

>FULL PWR

2L

>ON

3L

>ON

4L

>SHIP

5L

>READY

6L

RECEIVE TOD

5L

>SEND TOD

6L

GPS

1R

1L

2R

2L

2R

3R

3L

3R

4R

4L

5R

5L

6R

6L

1R

>SYNCH TOD

4R

RESET TOD<

3R

4L

BKA

2044

290T/ 20>

4R

5L

KILLA

2127

280T/ 15>

5R

6L



6R

T

H. Units configured to lbs using 5R prompt on FUEL page:

ACT RTE 1 LEGS ETA 1/4 1L

CAFTA

ETA 1916

EFA(L B ) 2927

2L

YZP

1950

2612

3L

MOCA1

2000

2599

4L

BKA

2044

2094

4R

5L

KILLA

2127

1746

5R

6L



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1R 2R 3R

6R

A-110 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) WAYPOINT IDENTIFIER [1L, 2L, 3L, 4L, 5L]: Displays the same identifiers as on the corresponding RTE LEGS Y/X page. ETA (1L,2L,3L,4L,5L): Displays ETA of the waypoint identified on the same line. The ETA is based on current TAS and predicted wind, which results from blending the forecast wind the system wind. If a route discontinuity exists, subsequent ETAs are based on an assumed great circle course across the discontinuity. When not configured to AIR TRANSPORT, a "z" is appended after the time (HHMMz) when using UTC time to differentiate between UTC and local time. NOTES: • On ground, ETEs are displayed instead of ETAs if the PLAN DATA page is configured. If it is not configured, the field is blank. • For the inactive route, this information is not provided when: - Performance VNAV is configured or - the FUEL page is not configured. LEGS [6L]: Access to the corresponding RTE LEGS Y/X page. To display the RTE LEGS 1/X page and the active waypoint, press the LEGS function key. ERASE [6L]: Erases route modifications (if any). CANCEL [6L]: Cancel the changes made to the inactive route. RESTORE [6L]: Displayed only when the route's origin is deleted in flight or on ground. It will cause a return to the previous route and ACT RTE status. EFA (1R, 2R, 3R, 4R, 5R): Estimated Fuel at Arrival. Estimated remaining Fuel quantity at waypoint based on the fuel consumption rate. If a route discontinuity exists, subsequent EFAs are based on an assumed great circle course across the discontinuity. Field is not displayed when fuel weight (excluding reserve) or fuel flow or true airspeed or wind are not available. For the active route, this field is not displayed if the FUEL page is not configured. Units are toggled from the 5R field on the FUEL 1/2 page (units of kg or lb). NOTE: • For the inactive route, this information is not provided when: - Performance VNAV is configured or - the FUEL page is not configured. WIND [1R, 2R, 3R, 4R, 5R]: The WIND field is displayed only if EFA is not configured. When single wind level is configured: Allows manual entry. Default is zero. It is possible to enter a forecast wind at a single altitude (flight level) for any downtrack waypoint. This wind is propagated forward to the end of the route, or until the occurrence of the next forecast wind. Pilot-entered winds are displayed in large font and propagated winds in small font. When four wind levels is configured: Allows access to the corresponding wind page : • A filled prompt “►” will be displayed next to a waypoint for which specific wind data has been entered. • An empty prompt “>” indicates that the wind information was propagated for that waypoint. In addition, the wind column displays the computed wind for each waypoint (e.g. the predicted wind that is used in the ETA calculations). Winds are displayed in small fonts. LEGS POS [6R]: Access to the corresponding RTE LEGS POS Y/X page. Display only if the fuel page is not configured . LEGS WIND [6R]: Access to the RTE LEGS WIND Y/X page. Displayed only if the fuel page is configured. CONFIRM [6R]: Confirm the changes made to the inactive route.

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A-111 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

RTE x LEGS POS 1/X Provides the position in latitude and longitude, using the WGS 84 Earth model, for each waypoint on the corresponding RTE LEGS Y/X page. Display ACT RTE LEGS POS 1/X page by pressing [LEGS], and (if the fuel page is not configured) or [LEGS], , , (if Performance VNAV or the fuel page is configured). A. Normal ACTIVE format, Fuel page not configured:

ACT RTE 1 LEGS POS 1/2 1L

CAFTA

2L

YZP

3L

MOCA1

4L

BKA

5L

KILLA

RNP 1.00N M . N51o17.72 W129o05.32 RNP 1.00N M N53o15.13 W131o48.42 N54o30.18 W133o01.90 N56o51.57 W135o33.08

1R 2R 3R 4R 5R

N58o44.98 W140o35.10

6L



6R

B. LEGS POS during a MOD:

MOD RTE 1 LEGS POS 1/2 1L

CAFTA

2L

YZP

3L

MOCA1

4L

BKA

5L

KILLA

6L



1R 2R 3R 4R 5R 6R

C. LEGS POS Index of INACTIVE route during a mod:

RTE 2 LEGS POS 1/2 1L

CAFTA

2L

YZP

3L

MOCA1

4L

BKA

5L

KILLA

6L



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1R 2R 3R 4R 5R 6R

A-112 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

ACT RTE 1 LEGS POS 1/2 1L

CAFTA

2L

YZP

3L

MOCA1

4L

BKA

5L

KILLA

RNP 1.00N M . N51o17.72 W129o05.32 RNP 1.00N M N53o15.13 W131o48.42 N54o30.18 W133o01.90 N56o51.57 W135o33.08

1R 2R 3R 4R 5R

N58o44.98 W140o35.10

6L



6R

WAYPOINT IDENTIFIER (1L,2L,3L,4L,5L): Displays the same identifiers as on the corresponding RTE LEGS Y/X page. LEGS ETA [6L]: Access to the corresponding RTE LEGS ETA Y/X page. The prompt is displayed if the fuel page is not configured. LEGS WIND [6L]: Access to the corresponding RTE LEGS WIND Y/X page. The prompt is displayed if the fuel page is configured. ERASE [6L]: Erase route modifications. RESTORE [6L]: Displayed only when the route's origin is deleted in flight or on ground. It will cause a return to the previous route and ACT RTE status. CANCEL [6L]: Cancel the changes made to the inactive route. RNP (1R, 2R, 3R, 4R, 5R): Displays leg’s RNP value extracted from the database. NOTE: The RNP value will only be displayed if there is an RNP value defined for this leg in the Navigation Database. LAT-LONG (1R, 2R, 3R, 4R, 5R): Display position of the waypoint identified on the previous line. LEGS [6R]: Returns to the corresponding RTE LEGS Y/X page. CONFIRM [6R]: Confirm the changes made to the inactive route. NOTE: Flight plan waypoint modifications are not permitted on the LEGS POS page.

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A-113 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

RTE x LEGS WND 1/X This page provides the ETE and wind for each waypoint on the corresponding RTE LEGS Y/X page. Display ACT RTE LEGS WND 1/X page by pressing [LEGS], and . A. Normal ACTIVE format, one wind level configured:

ACT RTE 1 LEGS WND 1/4 1L

CAFTA

ETE 00+49

280T / 12

WIND

2L

YZP

01+05

280T/ 12

3L

MOCA1

01+15

280T/ 12 T

1R 2R 3R

4L

BKA

01+22

290 / 17

4R

5L

KILLA

01+42

290T/ 17

5R

6L



6R

B. Normal ACTIVE format, four wind levels configured :

ACT RTE 1 LEGS WND 1/4 ETE 00+49

WIND 000T/

0>

1R

1L

CAFTA

2L

YZP

01+05

300 / 90►

2R

3L

MOCA1

01+15

300T/ 85>

3R

4L

BKA

01+22

290 / 20>

4R

5L

KILLA

01+42

280T/ 15>

5R

6L



6R

T

T

WAYPOINT IDENTIFIER [1L, 2L, 3L, 4L, 5L]: Displays the same identifiers as on the corresponding RTE LEGS Y/X page. ETE (1L,2L,3L,4L,5L): Displays ETE to the waypoint identified on the same line. The ETA is based on current TAS and predicted wind, which results from blending the forecast wind the system wind. If a ROUTE DISCONTINUITY exists, subsequent ETEs are based on an assumed great circle course across the discontinuity. LEGS ETA [6L]: Access to the corresponding RTE LEGS ETA Y/X page. To display the RTE LEGS 1/X page and the active waypoint, press the LEGS function key.

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A-114 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

ERASE [6L]: Erases route modifications (if any). CANCEL [6L]: Cancel the changes made to the inactive route. RESTORE [6L]: Displayed only when the route's origin is deleted in flight or on ground. It will cause a return to the previous route and ACT RTE status. WIND [1R, 2R, 3R, 4R, 5R]: When single wind level is configured: Allows manual entry. Default is zero. It is possible to enter a forecast wind at a single altitude (flight level) for any downtrack waypoint. This wind is propagated forward to the end of the route, or until the occurrence of the next forecast wind. Pilot-entered winds are displayed in large font and propagated winds in small font. When four wind levels is configured: Allows access to the corresponding wind page : • A filled prompt “►” will be displayed next to a waypoint for which specific wind data has been entered. • An empty prompt “>” indicates that the wind information was propagated for that waypoint. In addition, the wind column displays the computed wind for each waypoint (e.g. the predicted wind that is used in the ETA calculations). Winds are displayed in small fonts. LEGS POS [6R]: Access to the corresponding RTE LEGS POS Y/X page. CONFIRM [6R]: Confirm the changes made to the inactive route. (SAVE?): Displayed between the CANCEL/CONFIRM prompts when the inactive route is in modification.

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A-115 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

SELECT CO ROUTE 1/X Display SELECT CO ROUTE 1/1 page by pressing [RTE] and .

SELECT CO ROUTE 1L

1201

2L

1202

1/1 1401

2R

3L 4L

1R

3R 4R

LOAD

5L

>DIRECT

5R

6L

INVERSE

5R

6L

MAG

1R

2L

2R

3L

3R

4L

4R

FMS OPERATION

5L

>SYNCHRONIZED

6L



6R

Non-Air Transport typical configuration:

FMS1 SETUP

1/1

DISPLAY

1L

>MAG

2L

>UTC

3L

>LAT_LONG

4L

TIME

OFFSET

+5.0H R S

COORD

DATUM

WGS84<

>SYNCHRONIZED

6L



6R

Independent mode selected (air-transport)

FMS1 SETUP

1/1

DISPLAY

1L

>MAG

1R

2L

2R

3L

3R

4L 5L 6L

4R

FMS OPERATION

SYNCHRONIZED

FORCE INDEPENDENT?



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5R 6R

A-119 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Synchronized mode selected from FMS2 (air-transport)

FMS1 SETUP

1/1

DISPLAY

1L

>MAG

1R

2L

2R

3L

3R

4L 5L

4R

FMS OPERATION

INDEPENDENT

5R

SYNC ALL FMS WITH FMS2?

6L



6R

DISPLAY [1L]: Display Reference of all courses, tracks and bearings and angular outputs to the EHSI. Toggle options: MAG/TRUE. When the A/C is in the polar area (see section 3), TRUE/MAG toggling is disabled, the > is not displayed, and TRUE is displayed in the data field. Otherwise, the display reference will be displayed in small font (the prompt ">" is not displayed). If an external TRUE/MAG input is configured, the current state of the TRUE/MAG setting is displayed. When the A/C is in the polar area, TRUE/MAG toggling is disabled, the ">" is not displayed, and TRUE is displayed in the data field. TIME [2L]: Toggle options: GPS Universal Coordinated Time (UTC) and LOCAL Time. COORD [3L]: Selection of displayed coordinate system: {LAT_LONG, UTM, MGRS, SWISS_GRID}. OFFSET [2R]: Entry for local time offset from the UTC time. Validity checking ensures entry is between +/-12.0 hours and steps are 0.5 hours. DATUM [3R]: Selection of Datum used to convert scratchpad entries from and also to display the position coordinates. For example if WGS72 is selected then displayed coordinates are in this datum and entries are assumed at this datum as well. Choices are any of the available datums (maximum of 8) defined in the FMS’s currently active configuration (WGS84, WGS72, etc.) NOTE: All navigation functions use Lat/Long in WGS84, this function only affect display/entry to pilot of positional information. When COORD is SWISS GRID, DATUM is forced to CH1903, displayed in white font and cannot be modified. NOTE: The TIME, COORD, OFFSET and DATUM options are not available when the Air Transport configuration option is enabled. FMS OPERATION [5L]: FMS cross-talk mode of operation. Toggle options: INDEPENDENT/SYNCHRONIZED. Mode changes need to be confirmed (Field is not displayed if the FMS is configured not to be synchronized. In synchronized. mode, ">" prompt is not displayed if configured as “ALWAYS”). CANCEL [6L]: Used to cancel request to change FMS cross-talk mode of operation. POS INIT [6L]: Accesses the POS INIT/REF 1/2 or 1/3 page. CONFIRM [6R]: Used to confirm request to change synchronized).

FMS cross-talk mode of operation (independent or

ROUTE [6R]: Accesses the RTE 1/1 page.

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A-120 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

TIMER 1/1 page (if TIMER PG is configured) Display TIMER 1/1 page by pressing [INIT REF], [NEXT] and . The TIMER page is used to generate a “TIMER ALARM” alert message after a user specified alarm time was reached (count-up timer) or a certain time duration has elapsed (countdown timer). A. Display when no data is entered or after pressing CLEAR:

TIMER ALARM TIME

1L

----:--

1/1

COUNTDOWN

0000:00

1R

2L

ADD 5 MIN>

2R

3L

ADD 15 MIN>

3R

4L

ADD 30 MIN>

4R

5L

5R

6L

6R

B. Display after an alarm time is entered:

TIMER ALARM TIME

1L

1234:12

1/1

COUNTDOWN

----:--

1R

2L

ADD 5 MIN>

2R

3L

ADD 15 MIN>

3R

4L

ADD 30 MIN>

4R

CLEAR>

5R

5L



2L

1R 2R

3L

3R

4L

4R

5L



6L

This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.

5R 6R

A-121 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) D

Display after timer is activated. Countdown decrements:

TIMER ALARM TIME

1L

1234:12

1/1

COUNTDOWN

2329:53

1R

2L

ADD 5 MIN>

2R

3L

ADD 15 MIN>

3R

4L

ADD 30 MIN>

4R

CLEAR>

5R

5L



2R

3L

ADD 15 MIN>

3R

4L

ADD 30 MIN>

4R

CLEAR>

5R

5L 6L

----ACCUR

2L

1R o

3L 4L

o

.

.

ACCUR POS DIFF o

IRS

B.

3R 4R

5L 6L

2R

5R



6R

UPDATE POS 1/1 waypoint ID entered, MARK key is pressed and IRS is selected.

UPDATE POS REF

1L

---o /-.--N M

>CYUL

ACCUR 0.27N M o

o

N45 28.08 W073 44.48

2L 3L 4L

1/1

BRG/DIST

DIRECT

6L



6R

B. When route is deleted:

USER ROUTES

1/1

0001M0009M

WPT01WPT09

2L

WPT01WPT10

STATION010

3L

STATION015

----------

1L

4L

>DIRECT

6L



6R

ROUTE [1L,2L,3L,4L,5L,1R,2R,3R,4R,5R]: User Route name. When a name is entered from the scratchpad in the field containing dashes, the CANCEL and CONFIRM prompts are displayed. Press CONFIRM in order to save a new user route identical to the route that is being displayed on the RTE and LEGS pages. Pressing [CLR], then the LSK key on a user route name will bring up the CANCEL and CONFIRM prompts. Press CONFIRM for the deletion of that user route. Selecting a user route name with the scratchpad empty will bring forth the RTE page with the selected user route loaded (but not activated).

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A-127 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

NOTE: When airborne, a user route name selected on page USER ROUTES 1/1 will replace the current active route without replacing the origin. When a route name is entered over an existing one, the advisory message “!INVALID ENTRY” will be displayed. In the case where an 11th route name would have to be entered (which is not allowed in the system), one of the existing 10 route names has to be deleted in order to make room for that new route since the maximum number of user routes is 10. LOAD [5L]:

Toggle DIRECT/INVERSE direction of the route to be loaded. DIRECT is the default.

ROUTE [6L]:

Return to the RTE X 1/1 page.

DELETE ALL [6R]: Delete all user routes. Pressing this key causes the CANCEL and CONFIRM prompts to appear. Press CONFIRM to delete. This prompt only appear if at least one user route exists. (DELETE?): Displayed between the CANCEL/CONFIRM prompts upon deletion of a user waypoint. CANCEL [6L]: Cancels the creation of a new user route or deletion of a single user route or of all user routes, as applicable. CONFIRM [6R]: Confirms the creation of a new user route or deletion of a single user route or of all user routes, as applicable. Cross-talks the creation or deletion to the cross-side FMS if FMSs are in synchronized mode. NOTE: An advisory message “!USER ROUTE EXISTS” will be displayed if a duplicated name of user route is entered. The entry will be rejected.

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A-128 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

USER WPT 1/2 Display the USER WPT 1/2 page, press [INIT REF], ,. The USER WPT pages allow for the creation or modification of user waypoints. Moving waypoints can be created or modified if Moving waypoint is configured. This page is only available when the USER DBASE configuration option is enabled. When any moving waypoint identifier that is present in the active route is entered, an ACT RTE caption is displayed in reverse video. When any identifier is entered and all mandatory fields are entered, CANCEL/CONFIRM prompts will appear. Leaving the USER WPT pages without confirmation will automatically perform a CANCEL. A. Page displayed for creation of a new fixed user waypoint:

USER WPT 1L 2L 3L 4L

ID/POS o . BRG/DIS

1/2

FREE= 457 o .

T

--- /---N M >FIXED

REF WPT ID

RAD/DIS o

----o

1R 2R

TYPE

REF WPT POS

USER WPT

/

NM

o

3R 4R

5L

--- --.-- ---- --.--

5R

6L



1L

ID/POS o . BRG/DIS T

1/2

FREE= 457 o . TK/GS T

/

1R

2L

--- /---N M

3L

>MOVING

4L

-----

5L

---o--.-- ----o--.--

5R

6L



2R 3R 4R

B. After modifying data for an existing moving waypoint identifier in the active route:

ADFF 1L

USER WPT ID/POS

1/2

ACT RTE

N45o12.23 W043o32.12

BRG/DIS

TK/GS

T

2L

223 /115N M

3L

>MOVING

T

111 /222K T

TYPE

REF WPT ID

RAD/DIS o

4L

ADED

000 /0.00N M

5L

N45o12.23 W043o32.12

6L



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1R 2R 3R 4R 5R 6R

A-129 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

C. After entering a new identifier and all mandatory fields or modifying data for an existing fixed waypoint identifier or moving waypoint identifier is not in the active route:

USER WPT

ADFF 1L 2L 3L 4L

ID/POS

1/2 ADFF

FREE= 457

N45o12.23 W043o32.12

BRG/DIS

223T/115N M TYPE

FIXED

REF WPT ID

RAD/DIS o

----

/ .

NM

REF WPT POS

5L

---o--.-- ----o--.--

6L



DELETE?

1R

1L

USER WPT ID/POS

1/2

FREE= 457

N45o12.23 W043o32.12

BRG/DIS

TK/GS

T

T

2R

2L

223 /115N M

111 /222K T

3R

3L

>MOVING

4R

4L

ADED

5R

5L

N45o12.23 W043o32.12

6R

6L



6R

D. After entering DELETE on an existing user waypoint identifier:

ADFF 1L

USER WPT ID/POS

1/2

FREE= 457

N45o12.23 W043o32.12

BRG/DIS T

2L

223 /115N M

3L

>MOVING

TK/GS

111 /222N M

TYPE

REF WPT ID

1R

T

RAD/DIS o

4L

ADED

000 /0.00N M

5L

N45o12.23 W043o32.12

6L



2R 3R 4R 5R 6R

ID [1L]:User waypoint identifier (5 characters max.). When the identifier entered exists as a non-user waypoint, the entry is allowed and an advisory message !DUPLICATE WAYPOINT appears. When the identifier entered exists as a user waypoint during the creation of a new user waypoint, the entry is not allowed and an advisory message !DUPLICATE USER WAYPOINT appears. However entering an existing waypoint identifier during user waypoint edition will trigger the display of the NAV DATA page with the associated entered waypoint information. If a modification is in progress, entering a new identifier will delete the previously displayed information and display the information corresponding to the newly entered identifier. Pressing [CLR] in this field will bring the DELETE? prompt. The default value is boxes. POS [1R]: User waypoint position in the selected coordinate system and datum. Automatically displayed if the user waypoint identifier entered exists. Manual entry forces default value to appear in the REF WPT ID and REF WPT POS and RAD/DIS fields and automatically updates the BRG/DIS field. The default value is boxes. FREE: Number of user waypoint free slots in user database (458 user waypoints max.) (458 - no of fixed waypoints- no of moving waypoint). BRG/DIS [2L]: Bearing and distance from the current aircraft position to the waypoint. Manual entry forces default value to appear in the REF WPT ID and REF WPT POS and RAD/DIS fields and automatically updates the POS field. BRG and DIS values may be entered individually or simultaneously; a ‘/’ symbol preceding a

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A-130 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) value in the scratchpad indicates only the DIS value must be updated. The values will be recomputed and displayed at a minimum rate of once every second. The default value is boxes, and the minimum/ maximum values for the track angle are 0/360 degrees and 0/999 nm for the distance. TYPE [3L]: FIXED or MOVING waypoint type indication. The default upon entry in the page will be FIXED, as applicable. The toggling is only possible when adding a new user waypoint. REF WPT ID [4L]: Reference waypoint identifier with dashes as default value. Entry of an identifier will display its position in the REF WPT POS field and the POS and BRG/DIS fields will be automatically updated. RAD/DIS[4R]: Radial/distance from the reference position to the desired user waypoint position. The default values are blanked, when no REF WPT POS is defined, otherwise zeros are displayed as the default values. No entries are allowed, when the fields are blanked. Manual entry automatically updates the POS and BRG/DIS fields. RAD and DIS values may be entered individually or simultaneously; a ‘/’ symbol preceding a value in the scratchpad indicates only the DIS value must be updated. The minimum/maximum values for the radial are 0/360 degrees and 0/999 nm for the distance. REF WPT POS [5L]: Reference position with dashes as default value. It corresponds to the position of the reference waypoint identifier or a manually entered value. Upon entry of a value, the REF ID field will be set to dash symbols and the POS and BRG/DIS fields will be automatically updated. NAV DATA [6L]: Access to the NAV DATA 1/1 page. (SAVE?): Displayed between the CANCEL/CONFIRM prompts upon modification of a user waypoint. (DELETE?): Displayed between the CANCEL/CONFIRM prompts upon deletion of a user waypoint. CANCEL [6L]: Cancels the definition, modifications, or deletion of a user waypoint. All the fields return to their default value (when cancelling the creation of a user waypoint), or to their original value (when cancelling a user waypoint modification). NOTE: If one user waypoint has been created, some new changes are made and cancelled, all the latest changes are lost. WPT LIST [6R]: Access to the USER WPT LIST 1/N page. CONFIRM [6R]: Confirms the definition, modifications, or deletion of a user waypoint. NOTE: Changes are still allowed while CONFIRM is on the screen.

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A-131 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

USER WPT 2/2 Display USER WPT 2/2 page to modify parameters of an existing waypoints by pressing [INIT_REF], , and [NEXT]. This page is only available when the USER DBASE configuration option is enabled. The USER WPT pages allows for the creation of new user waypoints of different class and types or the modification of existing user waypoints. USER WPT 1/2 allows to enter basic property of waypoint such its identifier and position. USER WPT 2/2 allows the definition of the type and class of the new waypoint along with their additional properties.(mandatory and optional field): When the new waypoint created is of type other than WAYPOINT, mandatory fields must be entered as indicated by the display of the page.

USER WPT ID

FREE=459

1L

YUL

2L

CAN/CY

AIRPORT>

6L

SAVE?

USER WPT ID

1L 2L 3L 4L

FREE=459

YKL REGION

---/--

2R

3R

3L

3R

4R

4L

4R

10323F T

5R

5L

5R

CONFIRM>

6R

6L

5L

----

6L



SAVE?

USER WPT

TYPE

CHAN

o

WAYPOINT<

2L

HIGH LEVEL< DECLIN

2/2 TYPE

2R

ELEVATION

1013M B -3.00o

1R 2R 3R 4R 5R 6R

B. Active VNAV approach (LNAV/VNAV). Baro-corrected altitude available to the FMS from the Air Data Computer:

ACT 1L 2L 3L 4L 5L 6L

VNAV NDB24L

1/1

MINIMA MDA-DA LNAV/VNAV 660 239o 6.2N M -3.00 o ZUL FAF 1500A 10.0N M -3.00 o 239o RW24L / o M A P 167 MAG W I N D GS VDEV >2 4 3 o / 3 0 K T 1 3 0 K T 34 CYUL TEMP TGT VS ---o C -1200F P M VPA -3.00o

1R 2R 3R 4R 5R 6R

C. Destination Airport temperature is entered:

ACT

VNAV NDB24L

1/1

MDA-DA 1L 2L 3L 4L 5L 6L

999

239o AGBEK 239o L

308N M

-3.00o

314N M

-3.00o

2785 FAF

MAG W I N D >2 4 3 o / 3 0 K T CYUL TEMP -10o C QNH >1 0 1 3 M B

2348

GS 130K T

VDEV

34 TGT VS

1R 2R 3R 4R

-1200F P M

5R

VPA -3.00o

6R

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A-137 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) D. Destination Airport Temperature and MISSED APPR prompt in view.

ACT 1L 2L 3L 4L 5L 6L

239o

ZUL

VNAV NDB24L MINIMA LNAV 1.2N M

FAF

239o

1/1 MDA-DA

999

-3.00

o

1R

o

2R

2785

10.0N M -3.00

RW24L / o M A P 2348 MAG W I N D GS VDEV >2 4 3 o / 3 0 K T 1 3 0 K T 34 CYUL TEMP -10o C QNH >1 0 1 3 M B

TGT VS

3R 4R

-1200F P M

5R

MISSED APPR>

6R

TITLE:“ACT” is displayed when the VNAV approach (glide path) is active. Destination approach/runway identifier of the active route is displayed. “MOD” is displayed if the active route is being modified. MINIMA : This field indicates the current active approach minima . Possible values are LNAV/VNAV, and LNAV. This field is displayed when the approach in the active route is authorized for one or more approach minima (as indicated by the navigation database). This field is available only when LP/LPV or BARO LNAV/VNAV is configured. NOTE: LP and LPV will not be displayed here when they are the active approach minima because the entire page is blanked in that case since the approach is not considered valid for VNAV approach. COURSE / DISTANCE / WAYPOINT IDENTFIER [2L, 3L]: Displays leg course/heading and distance-to-go to the active and next waypoints respectively. Field is blank if the information is undefined (e.g. for a route discontinuity). The Course/Distance field of the active waypoint can be replaced by “HOLD AT” if active procedure is hold. Additionally, active and next waypoint identifiers may be followed by one of the following special procedures: • "/H" : Holding pattern • "/O" : Fly over waypoint • "/T" : Tactical direct-to TRUE/MAG WIND and GS [4L]: Displays current wind direction and speed and ground speed. Wind direction is crew selectable to magnetic or true North reference when the A/C is outside the polar area (see section 3), TRUE/MAG toggling is disabled and TRUE is displayed in the title line when the A/C is in the polar area. Destination Airport TEMP [5L]: Enables entry of surface air temperature reported for the destination airport. When the entered temperature differs from the ISA temperature, entry is used to provide temperature correction of MDA-DA, approach and approach transition waypoint altitudes, vertical deviation and target vertical speed. Corrected altitudes and vertical deviation are displayed in reverse video white. Valid airport temperature range is -55°C to +55 °C. QNH [6L]: When no baro-corrected altitude from an Air Data Computer is available to the FMS, and pressure or INS baro-inertial altitude is available, then this field allows manual entry and display of the altimeter setting (QNH). The allowable entry format can be either in inches of mercury within a range of 27.00 to 32.00, or in millibars within a range of 915 to 1083. The QNH unit type is automatically detected from the entered value. The decimal point entry is not required. The entered QNH value is displayed in large fonts.

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A-138 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Pressing LSK 6L with the scratchpad empty toggles the displayed QNH unit type between inches of mercury and millibars. The altimeter setting entries (including unit reference toggling) are propagated between VNAV and PROGRESS pages, and cross-talked between FMS. Upon leaving the terminal area, a manual entry of QNH is cancelled (the field display reverts to boxes (" " or dashes “-----“). ERASE [6L]: Prompt appears while flight plan is in MOD status, caused by lateral or vertical modifications. EXEC key required to activate any change. MDA-DA [1R]: Enables manual entry of minimum descent altitude/decision altitude in feet. Temperature compensated if a temperature is entered at LSK [5L]. Valid MDA-DA range is between the MAP altitude and the FAF altitude. Temperature compensated MDA is displayed in reverse video white. Field is always displayed in LARGE font. VPA | ALTITUDE [2R]: Displays (VPA) and altitude restriction for active waypoint. VPA field is blank if the waypoint is not the FAF or MAP or step-down fix. Temperature-compensated altitude constraints are displayed in reverse video white. The altitude is displayed in NORMAL font if the altitude is coming from the navigation database. The altitude is displayed in LARGE font if it is a manually entered altitude. VPA | ALTITUDE [3R]: Displays vertical path angle and altitude restriction for "NEXT" waypoint. VPA field is blank if the waypoint is not FAF or MAP. Temperature-compensated altitude constraints are displayed in reverse video white. The altitude is displayed in NORMAL font if the altitude is coming from the navigation database. The altitude is displayed in LARGE font if it is a manually entered altitude. VDEV [4R]: Displays the vertical deviation in feet with respect to the computed approach vertical profile (negative value indicates aircraft below vertical path). Maximum displayed value is 9999 feet. The vertical deviation is displayed in reverse video white. TGT VS [5R]: Displays target vertical speed (feet/min) based on current ground speed and the approach vertical path angle (VPA). This value is temperature compensated if a temperature is entered at LSK 5L. The field is blank when the vertical deviation is invalid. The target vertical speed is displayed in reverse video white. VPA (6R): Displays glide-path descent angle in degrees when approach selected and missed approach prompt is not displayed. ARR [6R]: Prompt appears when no approach selected and [VNAV] key is pressed. Provides access to the ARRIVALS page. MISSED APPR [6R]: If configured for display by the selected configuration, this prompt enables transition within the FMS to the missed approach phase of flight, allowing sequencing of MAP waypoint. If the display of this prompt is configured, the prompt is displayed after transition to GPS approach mode (normally occurs at 2 nm inbound to the FAF if all GPS approach conditions are met). The function of this key is limited to the FMS, and has no impact on any missed approach or take-off/go-around mode of the flight guidance system.

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A-139 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

VOR/DME/TCN STATUS 1/1 Page (if VOR, DME or TACAN interfaces are configured) The VOR/DME/TCN page displays the VOR, DME, and TACAN sensor inputs used in FMS radial/distance radio navigator and the resulting position fix. Display VOR/DME/TCN STATUS 1/1 page by pressing [INIT REF], , and or or . NOTE: The title will change to VOR/DME or TACAN, as applicable, if some of the equipment is not configured. A. Single VOR and DME and Single TACAN configuration:

VOR/DME/TCN STATUS 1/1 1L

SOURCE/ID FREQ RAD/DME YJN 115.80 260° VOR DME YJN 115.80 130N M

2L 3L

2R TCN

UHU 99X 150°/ 110N M

4L N45°00.00

5L 6L

1R



3R 4R 5R 6R

B. Dual VOR, single DME (configured as "single", "single_1" or "single_2"), and single TACAN configuration:

VOR/DME/TCN STATUS 1/1 1L 2L 3L

SOURCE/ID FREQ RAD/DME 115.80 260° VOR1 YJN DME YJN 115.80 130N M VOR2 YUL 116.30 180° DME IABC 109.30H 12.0N M TCN

UHU 99X 150°/ 110N M

4L 5L 6L

N45°00.00



This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.

1R 2R 3R 4R 5R 6R

A-140 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

C. Dual VOR, Dual DME and single TACAN configuration:

VOR/DME/TCN STATUS 1/1 1L 2L 3L 4L 5L 6L

SOURCE/ID FREQ RAD/DME 115.80 260° VOR1 YJN DME YJN 115.80 130N M VOR2 YUL 116.30 180° DME IABC 109.30H 12.0N M TCN

UHU 99X 150°/ 110N M POSITION 19T 263560 04987374



1R 2R 3R 4R 5R 6R

VORx ID/FREQ/RAD (1L-Line 3, 2L-Line 5): Displays VOR station identifier, tuning frequency (MHz) and radial from the station (always in MAG). The fields are blanked when the FMS is unable to find the requested station (e.g.invalid bearing) or when the value of the frequency is changed and the FMS is searching for the new station identifier. The frequency and radial are values received from the radio interface. DMEx ID/FREQ/DME Slant range (1L-Line 4, 2L- Line 6): Display of DME station identifier, tuned frequency (MHz) and slant range from the station (always in nautical mile). The fields are blanked when the FMS is unable to find the requested station (e.g. invalid distance) or when the value of the frequency is changed and the FMS is searching for the new station ident. A reversed video white "H" appears next to the frequency when the DME is in "HOLD" mode. The frequency and slant range are values received from the radio interface TCN ID/CHAN RAD/DME Slant range (4L -Line 8): If TACAN is configured, display of TACAN station identifier, tuned channel radial from station (always in MAG) and TACAN slant range from station. The fields are blanked when the FMS is unable to find the requested station (e.g. either due to invalid channel, bearing, or distance) or when the value of the channel is changed and the FMS is searching for the new station ident. The radial and slant range are values received from the radio interface. NAV STATUS [6L]: Returns to NAV STATUS INDEX 1/1 page. POSITION (5R): Displays position LATITUDE and LONGITUDE or UTM. VOR DESEL[6L]: Access to VHF NAV DESELECT 1/1 page.

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A-141 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

WIND X/Y (If 4-Level Winds is configured) Allows entry and display of wind magnitude and speed for the selected waypoints at up to four different levels. Display WIND X/Y page by pressing [LEGS], , , “>” or “►” A. Normal ACTIVE format:

ACT CAFTA 1L

WIND

ALT F L ---

1/12

DIR/SPD 1R

2L

2R

3L

F L 355

310T / 95

3R

4L

F L 100

280T /110

4R

5L

5R

LEGS WIND>

6L

6R

B. Wind page in AOC operation

ACT CAFTA 1L

ALT FL---

WIND

1/5

DIR/SPD 1R

2L

FL---

3L

F L 150

135T / 40

3R

4L

F L 200 WIND

140T / 3 0

4R

5L 6L

2R

REQUEST WIND UPLINK READY

5R

LOAD>

6R

TITLE LINE: Displays the waypoint name, page number and the ACT/MOD status. . The active waypoint name is displayed in reverse video magenta, other waypoint names are displayed in green. ALT [1Lto 4L]: Flight level corresponding to wind data. NOTE: The altitude data can only be entered at LSK 1L. Altitudes are displayed in descending order at (1L), (2L), (3L), (4L). If four altitudes already exist, one of these must be deleted prior to the manual entry of a new altitude. WIND [5L]: Displayed only in AOC operation. Allow the crew to request wind or provide the status of the wind request (REQUEST, WAIT, REQUESTING, REQUESTED).

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A-142 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) ERASE [6L]: Not Shown in the page example. Displayed only when a route modification is in progress. Pressing ERASE (LSK 6L) will undo all changes to the route and return to the ACT Route status. CANCEL [6L]: Not Shown in the page example. Cancel the changes made to the inactive route. DIR/SPD [1R, 2R, 3R, 4R]: Allows entry of wind direction and speed for the given waypoint at the corresponding flight level. Entry is only allowed once a flight level has been entered. Pilot-entered winds are displayed in large font and propagated winds in small font. LEGS WIND [6R]: Access to the corresponding RTE LEGS WIND Y/X page. CONFIRM [6R]: Not Shown in the page example. Confirm the changes made to the inactive route. LOAD [6R]: Initiate the wind transfer when wind is available for loading. This only display when configured for AOC datalink operation. (SAVE?): Not Shown in the page example. Displayed between the CANCEL/CONFIRM prompts when the inactive route is in modification.

WPT LISTS 1/1 Display WPT LISTS 1/1 page by pressing [INIT REF] and .

WPT LISTS 1L

1/1



6R

6L

G. • • • •

2R 3R

4L 5L

1R

While in cruise phase of flight, the crew commands a "Climb in Cruise": The FMS reverts to the CLB page which displays "CRZ CLB”; The original Climb speed schedule is dashed (LSK2L); The target speed during a cruise climb is the CRZ SPD (LSK4L); GO AROUND is displayed at LSK 6L instead of TAKEOFF.

ACT CRZ ALT 1L

FL350

2L

CLB SPD ---/----

CRZ CLB

1/4

MAX FL370

AT T/C FL350 TO T/C 2012z/8.4N M

3L

2R 3R

4L

CRZ SPD .800

5L



5R

GO AROUND>

6R

TITLE: The page title line displays the following if the Active flight plan is being displayed: 1. If no climb-in-cruise is in progress, the character string "CLB" preceded by the selected sub-mode or “MANUAL” if a manual speed has been entered at LSK[2L]. 2. During a climb-in-cruise, the character string "CRZ CLB". 3. The left side of the title line displays: • “ACT” if climb is active • “MOD” if the flight plan is in mode state • Blanks if climb is not active. CRZ ALT [1L]: Entry and display of the cruise altitude (MCDU entry or derived from the Selected Altitude). The value entered is propagated between the PERF INIT, CLB, CRZ, Engine Out and PROGRESS 1/3 pages. CRZ ALT can be a manual entry or a change in the Selected Altitude. Valid manual entry format is: XXX (flight level), FLXXX or XXXXX (feet). The minimum altitude that can be entered is the greater of the minimum default

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Page A300-A-13 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) value or the elevation of the departure runway (when on-ground and during the first climb after takeoff) or the destination runway (otherwise). The maximum altitude that can be entered is defined in the PDB. Deletion of the cruise altitude is not allowed. In climb, the FMS accepts the Selected Altitude change in the data field (of modified and active route) only if it is higher than the CRZ ALT of the active route (if defined) or otherwise the cruise altitude of the modified route; otherwise, there is no effect on the data field. Manual CRZ ALT entries in climb must be at or above the Selected altitude. In cruise, the FMS accepts the Selected Altitude change (higher or lower value than current CRZ ALT value) in the data field (of modified and active route) at any time, except when: - engine-out mode is not active; and - the aircraft is within 200 nautical miles before the top-of-descent; and - the Selected Altitude is lowered In descent, a change of the Selected Altitude has no effect on the data field. Manual CRZ ALT entries in descent must be at or below the Selected Altitude. The CRZ ALT value is displayed in large white font. When no cruise altitude has been entered or the data field has been deleted, the data line displays boxes. While airborne, if all the weight-related data fields (GWT, ZFW and FOB) contain data and the CRZ ALT data field is empty, the FCU Selected Altitude is copied in small font in the CRZ ALT data field when the EXEC is pressed. MAX: Displays the FMS-computed maximum cruise flight level The MAX flight level value is displayed in small white font. The title and data field are blank if the data is not available or the active mode is descent. XXX XXX [2L]: The field title displays the name of the selected climb sub-mode mode or by default the name of the first climb sub-mode in the policy file with "SPD" appended to the end of the displayed sub-mode name. An abbreviated name will be displayed if the sub-mode name is greater the 5 characters (e.g. MIN FUEL SPD will be abbreviated to MFUEL SPD). By default, the field title displays the name of the first climb sub-mode in the policy file (e.g. ECON, etc). The data field displays the speed schedule associated with the selected climb sub-mode or the manually entered speed schedule. During a Cruise Climb, the field title displays “CLB SPD” and the data field displays dashes. If the crew manually enters a speed in the data field, the field title displays "MAN SPD". Valid entry format is to enter an IAS and/or Mach value using the slash rule e.g. 280, 280/.820 or /.820. The valid IAS or Mach entry range is defined in the PDB (during CRZ CLB, entry of both IAS and Mach values are required to transition from a Cruise speed to a manual Climb speed) and lowered limited by V2+10 when a V2 speed is available. Deletion of a manual speed entry reverts the data field and title to the previously selected climb sub-mode. Deletion of a climb sub-mode speed is not allowed. Manual speed entry is displayed in large white font. A climb sub-mode speed is displayed in small white font. If the IAS or MACH displayed is the source of the FMS target speed, the speed is displayed in reverse video. Manual entries are inhibited when the active VNAV mode is Cruise. SPD REST [3L]: Entry and display of the climb Speed Restriction/Speed Restriction Altitude. Manual entry overrides the default value extracted from the navigation database, if available. Valid entry format is to enter a speed and/or altitude using the slash rule e.g. 250, 250/10000 or /10000. The valid range of the Speed Restriction/Speed Restriction Altitude is defined in the PDB Deletion of a manual entry reverts the data field to the default value extracted from the navigation database. Deletions of the values extracted from the navigation database are not allowed. Manual entry is displayed in large white font. Default value or value extracted from the navigation database is displayed in small white font. The speed restriction is displayed in reverse video if it is the source of the FMS target speed. XXX SPD [4L]: Displays the target speed if the target speed source is one of the following: • "SPD AT XXX", where XXX is a climb waypoint ahead of the aircraft

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Page A300-A-14 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) • • • • • • •

"CRZ SPD", during a cruise climb when the FMS target speed is the cruise speed “CRZ LIM SPD”, when the FMS target speed is being limited by the cruise speed "LIM SPD", when the FMS target speed is being limited for another reason "HOLD SPD", when flying a hold when in climb “REST SPD”, during a cruise climb when below the descent restriction altitude “T/O SPD”, below the acceleration altitude (aircraft on-ground or in take-off phase of flight) “GA SPD”, following a Go Around and aircraft is below the acceleration altitude

Manual entries are not permitted. The title and data field display blanks if either cruise/descent/approach mode is active or if the EXEC key is illuminated or if climb (or climb in cruise) mode is active while the speed schedule or climb restriction is the source of the FMS target speed. The data field displays the FMS target speed in reverse video small white font provided the aircraft is above the thrust reduction altitude, the EXEC key is not illuminated and the speed schedule and climb restriction are not the source of the FMS target speed. NOTE: The title field text (except for the waypoint name) is displayed in small green font. The waypoint name is displayed in small white font (if applicable). SCHED [5L]: Enables direct access to CLB SCHED 1/3 page. ERASE [6L]: "ERASE" is only displayed when an active flight plan modification is in progress. Pressing this key will undo all changes to the active flight plan and return to the ACT Route status. AT NNNNNNN [1R]: Displays the first (next) climb waypoint with speed and/or altitude constraint, if any; otherwise, it displays "AT T/C" with the cruise altitude. Manual entry of the speed and/or altitude constraint associated to the waypoint in the title is allowed. It overrides the value(s) from the navigation database and is propagated to/from LEGS page. Deletion of the manually entered speed/altitude constraint reverts the data field to the database-derived values which are then propagated to/from the LEGS page. An altitude constraint or a speed constraint associated with a waypoint altitude constraint are displayed as follows: 1) Manual entry is displayed in large magenta font. 2) Default values are displayed in small magenta font. The title and data field are blank if the climb mode is not active. 3) Problematic altitude constraints are displayed in yellow as per the LEGS page display format. Default color is white when not associated to a constraint. TO NNNNNNN [2R]: Displays the ETA and Distance-To-Go (DTG) to the waypoint displayed at 1R, if any; otherwise, it displays the ETA and DTG to the top-of-climb. The ETA and DTG are displayed in small white font. When [1R] title and data field are blank, the title and data field at [2R] are blank. When the aircraft is on ground, the field displays ETE instead of ETA. ERROR [3R]: Displays the predicted undershoot error to the waypoint displayed at [1R], if any. Displays XXXXLO/YYLONG where XXXX represents the predicted undershoot error with respect to the altitude constraint and YY represents the predicted distance error at the climb waypoint displayed at [1R]. The vertical error ranges from 200ft to 9990 feet rounded to the nearest 10 feet and the distance error range from 1nm to 99nm rounded to the nearest 1nm. The error data is displayed in small white font. When there is no waypoint displayed in [1R], the title and data field are blank. When the vertical error at the waypoint is predicted to be less than 200ft and/or the distance error is predicted to be less than 1 nm, the title and data field are blank.

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Page A300-A-15 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) ENGINE OUT [5R]: Enables access to ENGINE OUT CLB 1/4 page while in air and the aircraft is in clean configuration. TAKEOFF [6R]: GO AROUND [6R]: Enables direct access to the TAKEOFF page while on-ground, during takeoff and during the initial climb otherwise enables direct access to the GO AROUND page.

CLB SCHED 1/3 The CLB SCHEDule page is used to select the current CLIMB speed sub-mode that will be flown for the entire profile or the climb phase of flight only. A maximum of one Climb speed sub-mode can be selected at any time. Display the CLB SCHED 1/3 page by pressing: [VNAV], (When in Climb mode) [VNAV],,[PREV] (When in Cruise mode) [VNAV],,[NEXT] (When in Descent mode) A. Initial display after the CLIMB SCHED page was accessed and the default speed mode (ECON) is selected.

ACT

CLB SCHED

SPD SCHED 1L

ECON

2L

>M I N

FUEL

3L

>M I N

TIME

1/1

COST INDEX 65

1R 2R 3R

4L

4R

5L

5R

CLIMB>

6L

6R

B. A manual speed has been entered on the Climb page, as a result, all sub-modes are deselected.

ACT

CLB SCHED

1L

SPD SCHED >E C O N

2L

>M I N

FUEL

3L

>M I N

TIME

1/1

COST INDEX 65

1R 2R 3R

4L

4R

5L

5R

6L

CLIMB>

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6R

Page A300-A-16 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

C. The sub-mode in [1L] has been selected.

MOD

CLB SCHED

SPD SCHED 1L

ECON

2L

>M I N

FUEL

3L

>M I N

TIME

1/1

COST INDEX 65

1R 2R 3R

4L

4R

5L

5R

6L



6R

TITLE: 1.The title displays: • “ACT” if climb is active • “MOD” if the EXEC key is illuminated • Blanks if climb is not active followed by CLB SCHED XXX XXX [1L]: Displays the first climb speed sub-mode defined in the policy file. If the sub-mode has been selected, the submode is displayed in large font. When the prompt is displayed, pressing the adjacent LSK has the following effect: •

The sub-mode's speed schedule is copied into the Climb page data field at LSK2L;

•

The sub-mode’s name is copied into the CLB page title field at LSK2L with “SPD” appended to the end of the name if it is less than 6 characters in length (e.g. ECON SPD). An abbreviated sub-mode name is provided in all other cases (e.g. MIN FUEL will be displayed as MFUEL SPD);

•

Selection of a Climb speed sub-mode is propagated to the CRZ and DES pages if the selected sub-mode is applicable for those phases of flight.

The font will change from large to small when another climb speed sub-mode is selected or a manual speed entry is made in LSK2L on the CLB page. Selection of the sub-mode cancels CP-Speed Intervention if previously active. XXX XXX [2L]: Displays the second climb speed sub-mode defined in the policy file. If the sub-mode has been selected, the sub-mode is displayed in large font. Behavior of this prompt upon selection is equivalent to the first climb speed sub-mode selection LSK1L. XXX XXX [3L]: Displays the third climb speed sub-mode defined in the policy file. If the sub-mode has been selected, the sub-mode is displayed in large font. Behavior of this prompt upon selection is equivalent to the first climb speed sub-mode selection LSK1L.

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Page A300-A-17 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

ERASE [6L]: “ERASE” is only displayed when an active flight plan modification is in progress. Pressing this key will undo all changes to the active flight plan and return to the ACT Route status. COST INDEX [1R]: Displays the Cost Index selected on the PERF INIT page for reference purposes. The Cost Index can be modified from this page in order to modify the speed schedule associated with the ECON sub-mode. CLIMB [6R]: Enables direct access to the VNAV CLB page.

CRZ 2/4 The CRZ page is used to select and display Cruise vertical mode data. Display the CRZ 2/4 page by pressing: [VNAV] (When in Cruise mode) or [VNAV] [NEXT] (When in Climb mode) or [VNAV] [PREV] (When in Descent mode) or [VNAV] [NEXT] [NEXT] (When in VNAV Approach mode) or from ENG OUT CRZ 2/4 page or from PROFILE page. A. The "MIN FUEL" sub-mode has been selected and the aircraft is in cruise. • The MIN FUEL active target speed is .820 (highlighted); • An altitude-constrained cruise waypoint is ahead of the aircraft (OMBLY). The constraining altitude is displayed at 1R; • The FMS displays the computed ETA and DTG to the step point at 2R.

ACT

MIN FUEL CRZ

2/4

CRZ ALT

1L 2L

MAX AT OMBLY FL300 FL380 FL320 MFUEL SPD TO STEP .820 2012z /20.1N M

1R 2R

3L

3R

4L

4R

5L 6L



5R

DES FORECAST>

6R

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Page A300-A-18 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) B.

The cruise "ECON" sub-mode has been selected and the aircraft is in cruise. A pre-planned Step Climb has been selected ([1R]/2R]) and the FCU has been dialed-up to the entered Step To altitude and pulled. As a result, a CLB NOW prompt is available at [3R] in order to perform an Immediate Climb to the entered Step To altitude prior to reaching the S/C pseudo-waypoint.

ACT

ECON CRZ

2/4

CRZ ALT

2L

MAX AT OMBLY FL350 FL380 FL370 ECON SPD TO STEP .805 2030z/45.5N M

3L

CLB NOW<

1L

4L 5L

2R 3R 4R



5R

DES FORECAST>

6R

A manually entered value of .800M is displayed in [2L]. The aircraft is within 999nm from the top-ofdescent (T/D), hence the FMS displays the computed ETA and DTG to the top-of-descent.

ACT CRZ ALT 1L

FL350 MAN SPD

2L

.800

ECON CRZ

2/4

MAX FL380 TO T/D 2045z/105N M

1R 2R

3L

3R

4L

4R

5L



5R

DES FORECAST>

6R

D. The aircraft is stepping-down in altitude while in cruise. • The page title changes to “CRZ DES”. • MIN FUEL cruise sub-mode is selected (displayed at 2L);

ACT

CRZ DES

2/4

CRZ ALT

1L 2L

MAX FL350 FL380 MFUEL SPD TO T/D .805 2045z/148N M

1R 2R

3L

3R

4L

4R

5L 6L



5R

DES FORECAST>

6R

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Page A300-A-19 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) E. The aircraft is within 200 nm of the T/D and the FCU has been dialed-down and pulled. The pilot can decide to perform an Early Descent (EARLY DES prompt) or perform a Cruise Descent (CRZ DES prompt).

ACT

MIN FUEL CRZ

2/4

CRZ ALT

2L

MAX FL350 FL380 MFUEL SPD TO T/D .805 2045z/148N M

3L

EARLY DES<

3R

4L

CRZ DES<

4R

ENGINE OUT>

5R

DES FORECAST>

6R

1L

5L 6L

MAX CERT LDG WT



1R 2R 3R 4R 5R 6R

TITLE: The page title displays the name of the selected approach of the active flight plan when available. O (EST) [1L]: S (EST) [2L]: F (EST) [3L]: These data fields present to the crew the following Estimated speeds (in Knots) as computed by the FMS: • Minimum Speed for Flap Retraction (F) • Minimum Speed for Slat Retraction (S) • Green dot Speed (O) These speeds are computed based on the predicted aircraft landing Gross Weight. NOTE: These speeds may be different than the actual FAC-computed F,S,O speeds, as a result, they should not be used in-lieu of the actual FAC speeds. VLS (EST) [4L]: VAPP (EST) [5L]: These data fields present to the crew the following Estimated speeds (in Knots) as computed by the FMS: • Lowest Selectable speed VLS for the planned landing configuration • Final Approach speed VAPP for the planned landing configuration These speeds are computed based on the predicted aircraft landing Gross Weight.

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Page A300-A-44 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

NOTE: • FMS-computed VLS may be different than the actual FAC-computed VLS speed, as a result, it should not be used in-lieu of the actual FAC speed. • FMS-computed VAPP is an estimated speed based on predicted landing gross weight and should not be used in-lieu of the FMS-commanded Final Approach Speed that is displayed on the VNAV APPR page and based on the actual FAC-provided VLS speed. GWT > MAX CERT LDG WT (status line between [5L] and [6L]): When the predicted landing Gross Weight is greater than the maximum certified landing weight, an associated status line will be used to annunciate to the pilot that the speeds displayed on the page are applicable to an overweight landing scenario. APPROACH [6L]: Pressing this LSK provides direct access to the APPR page. ERASE [6L]: "ERASE" is only displayed when an active flight plan modification is in progress. Pressing this key will undo all changes to the active flight plan and return to the ACT Route status. LDG CONF [1R]: This field allows crews selection of the planned aircraft landing configuration which can be 30_40 or 15_20 for A300 aircraft or 30_40 or 20_20 for A310 aircraft. MDA-DA [2R]: This field allows crew entry and displays the non-precision approach minima (MDA or DA) or precision approach minima (e.g. DA for ILS CAT1). The valid MDA or DA entry range is between the MAP altitude (else 50ft above the runway elevation if there is no MAP waypoint) and 8192ft. . Temperaturecompensated value is displayed in reverse video to the left of the (non-compensated) manual entry when applicable. DH [3R]: This field allows crew entry and displays the precision approach decision height (DH). Entry is limited from 0 to 999ft. APPR WIND [4R]: Entry and display of the destination airport wind. Valid range for approach wind direction/speed is: 0°-359°/0-99kt. Deletion of the manual entry is allowed. When no value is entered, the data field displays "---°/---KT". WIND CORR [5R]: Entry and display of the wind correction to be applied to the Final Approach Speed computation. Default value is the wind correction computed as a result of the destination airport wind entry performed at [4R]. Manual entry is permitted and overrides the default wind correction (valid range is 0-15 kt). Deletion of the manual entry is allowed and reverts to the default wind correction. When no destination airport wind entry has been performed at [4R] or no wind correction has been entered at [5R], the data field displays "--KT". GO AROUND [6R]: Pressing this LSK provides direct access to the GO AROUND 1/1 page.

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Page A300-A-45 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

GO AROUND 1/1 The GO-AROUND page is used to display the GO-AROUND-related information in preparation for, or during a Go-Around as the result of a Missed Approach initiation. Display the GO AROUND page by pressing: [INIT REF] when the first climb is complete, or [INIT REF] [PERF INIT] when the first climb is complete, or [VNAV] [CLB] when the first climb is complete, or [INIT REF] at any time. A. GO-AROUND page.

GO AROUND

1/1

1L ACCEL ALT 3000

2L 3L

2R 3R

5L

F (EST) 144 S (EST) 185

6L



6R

TITLE: The page title line displays GO AROUND. F (EST) [4L]: This field displays the Estimated minimum speed (in Knots) for flaps retraction as computed by the FMS and based on the predicted landing Gross Weight. NOTE: This speed may be different than the actual FAC-computed F speed and should not be used in-lieu of the actual FAC speed. S (EST) [5L]: This field displays the Estimated minimum speed (in Knots) for slats retraction as computed by the FMS and based on the predicted landing Gross Weight. NOTE: This speed may be different than the actual FAC-computed S speed and should not be used in-lieu of the actual FAC speed. APPR REF (6L) OR CLIMB (6L): If the GO AROUND page was accessed from the CLB page, enables direct access to this page. Otherwise, enables direct access to the APPR REF page. ACCEL ALT [2R]: This data field displays the acceleration altitude for the destination airport in preparation for (or during) a Go Around. Manual selection is only possibly during Cruise, Descent, Approach, or following a Go-Around. O (EST) [5R]: This field displays the Estimated Green Dot speed (in Knots) as computed by the FMS and based on the predicted landing Gross Weight. NOTE: This speed may be different than the actual FAC-computed O speed and should not be used in-lieu of the actual FAC speed. INIT/REF [6R]: Enables direct access to the INIT/REF INDEX 1/2 page.

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Page A300-A-46 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

DES FORECAST 1/2 This page is used to enter and display the destination airport's temperature, predicted QNH and specified transition level. Display the DES FORECAST 1/2 by pressing [VNAV], , (When in Cruise or Descent mode)

MOD

DES FORECAST

TRANS LVL 1L

FL180

2L

CYUL TEMP ---°C

1/2

CYUL QNH

30.25I N H G <

1R 2R

LDG ELEV

1000

3L

FT

3R

4L

4R

5L

5R

6L



6R

TITLE: The page title line displays “DES FORECAST 1/2”. modification is in progress.

It also displays “MOD" when a flight plan

TRANS LVL [1L]: Entry and display of Transition Level. Manual entry overrides the default value extracted from the navigation database for the destination airport/procedure, if available, or the mandatory entry boxes if no default value exists. Valid manual range is greater than or equal to 100 ft and between the airport elevation and 45,000 ft. Deletion of a manually entered Transition Level reverts to the value extracted from the navigation database, if available, or to boxes. Deletion of Transition Level values extracted from the navigation database is not allowed. Manual Transition Level is displayed in large white font. A value extracted from the navigation database is displayed in small white font. The title and data field are blank while in descent if the QNH setting is not standard pressure. Destination Airport TEMP [2L]: Entry and display of air temperature reported at the destination airport. When the entered temperature differs from the ISA temperature, entry is used to provide temperature correction of MDA/DA, approach and approach transition waypoint navigation database altitude constraints, vertical deviation and target vertical speed. Cold temperature correction is not computed when the temperature entry is positive (above 0° C). Manual entry is allowed. Deletion of manual entry is allowed. Manual entry is displayed in white large font. When no temperature has been entered or an initial entry has been deleted, the data field displays dashes. ERASE [6L]: "ERASE" is only displayed when an active flight plan modification is in progress. Pressing this key will undo all changes to the active flight plan and return to the ACT Route status.

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Page A300-A-47 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Destination Airport QNH [1R]: Entry and display of predicted barometric correction at the destination airport. Entry is used to optimize the FMS-VNAV descent profile computation only. When no entry is made, the FMS assumes standard pressure (29.92 inches of mercury) at the destination. Valid range is either 27.00 to 32.00 (inches of mercury) or 915 to 1083 (millibars). The decimal point is not required and the FMS automatically detects which unit system from the value entered. Deletion of manual entry is allowed. Pressing the LSK while the scratchpad is empty toggles the displayed QNH unit system between inches of mercury and millibars. Manual entry is displayed in white large font. When no value has been entered or an initial entry has been deleted, the data line displays dashes. The field is blank while in descent and the actual QNH is set by the crew via an external system LDG ELEV [3R]: Entry and display of the airfield landing elevation (in feet). The landing elevation is extracted from the navigation database for the destination runway (if available); OR the destination airport. Manual entry is inhibited. CRUISE [6R]: DESCENT [6R]: "CRUISE" or “DESCENT” enables direct access to page.

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Page A300-A-48 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

DES FORECAST 2/2 This page is used to enter forecast descent winds at up to four (4) different altitudes/flight levels for adjustment of descent vertical profile. Current and forecast winds are blended. Display the DES FORECAST 2/2 by pressing [VNAV], ,[NEXT] (When in Cruise or Descent mode) A. Forecast descent wind at four (4) different altitudes/flight levels.

MOD

DES FORECAST 2/2

ALT

WIND

1L

FL300

035T / 158K T

2L

FL240

030 / 140K T

2R

3L

FL180

030T / 100K T

3R

4L

9000

025 / 090K T

4R

T

5L 6L

1R

T

5R



6R

TITLE: The page title line displays “DES FORECAST 2/2”. It displays “MOD" when a flight plan modification is in progress. ALT [1L to 4L]: Entry and display wind flight levels/altitudes. Manual entry can be done in any field [1L] to [4L]. The FMS automatically sorts the value in descending order. Valid manual entry format is: XXX (flight level), FLXXX or XXXXX (feet). The minimum altitude that can be entered is 1000 feet and the maximum altitude that can be entered is defined in the PDB. Deletion of a manual entry is allowed. Valid entry is displayed in large white font. Data field displays dashes when empty. ERASE [6L]: "ERASE" is only displayed when an active flight plan modification is in progress. Pressing this key will undo all changes to the active flight plan and return to the ACT Route status. WIND [1R to 4R]: Entry and display wind direction (TRUE) and speed (kt). Valid manual entry format is to enter a direction and/or speed using the slash rule e.g. 250, 250/90 or /100 on a line having an altitude entry already made. Deletion of a manual entry is allowed. Valid entry is displayed in large white font. Valid range for approach wind direction/speed is: 0-359°/0-99kt. Deletion of the manual entry is allowed. When no value is entered, the data field displays "---°/---KT". CRUISE [6R]: DESCENT [6R]: “CRUISE” or " DESCENT" enables direct access to page.

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Page A300-A-49 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

LEGS 1/X Only VNAV related items and functionalities are described in this document section. Refer to Appendix A – Detailed Page Descriptions for fields shown on the page and not documented in this section. Refer to Appendix A – Detailed Page Descriptions for page access. A. Initial display with a speed/altitude constraint at D173J.

ACT

RTE 1 LEGS

264°

1/2

12.8 N M 254/ 1954 113.4

1L

JOH

2L

D173J

250/

263°

10.6 250/ 1450 10.0 FAF 1 6 0 / 1250 5.1 / o MAP 1 6 0 / 1000

262°

3L

D233J

4L

ANC

5L

RW06R

6L



1R 2R 3R 4R 5R 6R

B. Altitude constraint at D173J cannot be honored.

ACT

RTE 1 LEGS

264°

1/2

12.8 N M 254/ 1954 113.4

1L

JOH

2L

D173J

250/

263°

10.6 250/ 1450 10.0 FAF 1 6 0 / 1250 5.1 / o MAP 1 6 0 / 1000

262°

3L

D233J

4L

ANC

5L

RW06R

6L



1R 2R 3R 4R 5R 6R

C. A constant speed segment is defined from waypoint JOH03 to JOH01, where the speed target reverts to the speed schedule.

ACT

RTE 1 LEGS

264° 1L

JOH03

2L

JOH02

3L

JOH01

4L

JOH

5L

D173J

6L



6R

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Page A300-A-50 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) SPEED CONSTRAINTS/RESTRICTIONS/SPEED TARGETS/CONSTANT SPEED SEGMENTS [1R] to [5R]: • Waypoint target speeds without a speed constraint are displayed in small white font. • Speed constraints are displayed in magenta font (large when manually-entered, small when NDB-defined). • Waypoint speed constraints which cannot be honored are displayed in amber. • The starting waypoint for a constant speed segment displays the speed in large magenta; subsequent and ending waypoint speeds are displayed in large white font. • If FCU-Selected Speed Intervention is active and the waypoint falls in the range affected by Selected speed, it displays the Selected speed. Constant Speed Segments: • A pilot-entered Mach or IAS speed on a cruise waypoint propagates from waypoint to waypoint, and ends at a cruise waypoint with an existing speed constraint, or the T/D anticipation point. • A constant speed segment end point is set by deleting the speed at the desired waypoint. • The constant speed segment can be removed by erasing the speed constraint at the starting waypoint. An OUT OF RANGE message displays when a pilot-entered speed is outside the aircraft speed envelope limits A !MACH CSTR IN CRZ ONLY message displays when a pilot enters a Mach speed on a climb or descent waypoint, or if no vertical profile exists. ALTITUDE CONSTRAINTS/RESTRICTIONS/CROSSING ALTITUDES [1R] to [5R]: waypoint altitude constraints or crossing altitudes as follows:

Waypoint Type

Achievable Altitude Constraint/Crossing Altitude Altitude Constraints/Crossing Altitudes that cause an unachievable path TemperatureCompensated Waypoint

TemperatureCompensated Altitude Constraints that cause an unachievable path

The FMS displays the

Altitude Constraint Display Font Waypoint with a Navigation Database defined Altitude Constraint small font magenta

Waypoint with a Pilot-entered Altitude Constraint large font magenta

small font white

Climb/Cruise/Desc ent/Approach

small font amber

large font amber

small font white

Climb/Cruise/Desc ent/Approach

small font reverse video magenta

large font magenta

small font reverse video white

Descent/Approach

small font reverse video amber

large font amber

N/A

Descent/Approach

(Manual entries of altitude constraint are not automatically compensated by the FMS. They are assumed intrinsically compensated as communicated by ATC.)

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Crossing Altitude Display Font Waypoint with no Altitude Constraint

Applicable VNAV mode

Page A300-A-51 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) NOTES: • Missed approach waypoints have no crossing altitude or speeds displayed. • No crossing altitude is displayed for manually-terminated climb and cruise waypoints • No crossing altitude is displayed for climb/cruise/descent/approach waypoints associated with the following leg types: heading or course to an intercept, heading or course to a DME distance, and heading or course to a radial. • Manually-terminated descent waypoints will display the crossing altitude where the aircraft will level off if no manual-termination occurs.

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Page A300-A-52 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

LEGS ETA 1/X Only VNAV related items and functionalities are described in this document section. Refer to Appendix A – Detailed Page Descriptions for fields shown on the page and not documented in this section. Refer to Appendix A – Detailed Page Descriptions for page access.

ACT RTE 1 LEGS ETA 1/2 1L

CAFTA

ETA 1916

EFOB 32.8

2L

YZP

1950

18.5

3L

MOCA1

2000

17.9

4L

BKA

2044

9.5

4R

5L

KILLA

2127

0.7

5R

6L



1R 2R 3R

6R

ETA [1L] to [5L]: Displays ETA at the indicated waypoint when a vertical profile has been computed. Value is displayed for the active and modified flight plan waypoints up to and including the runway waypoints, if present. FMS-computed value is displayed in white small font. Data field displays dashes when no vertical profile has been computed. The data field is blank for the inactive routes. On Ground the field displays ETE instead of ETA. EFOB [1R] to [5R]: Displays the Estimated Fuel On Board (EFOB) at the indicated waypoint when a vertical profile has been computed. Values are displayed for the active and modified flight plan waypoints up to and including the runway waypoints, if present. FMS-computed value is displayed in white small font. Data field displays dashes when no vertical profile has been computed. The data field is blank for the inactive routes.

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Page A300-A-53 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

HOLD 1/X Only VNAV related items and functionalities are described in this document section. Refer to Appendix A – Detailed Page Descriptions for fields shown on the page and not documented in this section, Refer to Appendix A – Detailed Page Descriptions for page access.

ACT

RTE 1 HOLD

1/1

FIX

5L

SPD/ALT KILLA 230/ 5000A TURN DIR ICAO SPD >RIGHT 208K T /230K T INBD CRS HOLD TIME 050° 01+45 LEG TIME/DIS FIX ETA 1.0M I N / - - . - N M 1424 EXIT TYPE STATUS MANUAL IN PROGRESS

6L

NAV MODE TO T/C . Applicable Sub-modes are defined in the airline policy table. The following table provides typical modes/submodes.

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Page A300-A-55 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

Phase of Flight Takeoff/Climb

Active Sub-Mode sub mode name defined in the Policy File (ex:

sub mode name defined in the Policy File (ex:

Manual Speed

MANUAL

Engine-Out

E/O

sub mode name defined in the Policy File (ex:

sub mode name defined in the Policy File (ex:

Manual Speed

MANUAL

Engine-Out Cruise

E/O

Engine-Out Critical

E/O

CRT

Engine-Out Non-Critical

E/O

N-CRT

MIN FUEL)

Cruise

ECON)

Engine-Out Drift-Down

CLB

MIN FUEL)

CRZ

ECON)

Cruise Climb

N/A



CRZ CLB

Cruise Descent

N/A



CRZ DES

sub mode name defined in the Policy File (ex:

sub mode name defined in the Policy File (ex:

Descent

ECON)

Manual Speed Approach

N/A

DES

ECON)

MANUAL

APPROACH

FMS SPD [3L]: Displays the current FMS target speed. NOTE: No target speed entry is permitted from this page. Any change to the FMS target speed must be performed from the active VNAV page. As a result, only the target speed applicable to the Active route is displayed on this page. BRG/DIST - [4L]: TO WAYPOINT [4R]: Displays the bearing and distance from present position to the waypoint entered at [4R]. Bearing and distance will be with respect to the active waypoint by default until a manual entry is performed at [4R]. RNP/ANP [5L]: The data field will display the current Required Navigation Performance (RNP). The data field allows RNP crew manual entries to overwrite the current displayed RNP. The range of permitted entry of RNP values is between the minimum configured value (default to 0.3 nm) and 20.00 nm. The Actual Navigation Performance (ANP) value is displayed for the current active navigation mode. If the ANP is not available, stars are displayed in the ANP field.

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Page A300-A-56 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) NAV MODE [6L]: Current navigation mode. Pressing LSK 6L will access the POS INIT/REF 2/3 page. Possible navigation modes: GPS DME VOR/DME INERTIAL DR MAX ALT [1R]: STAB ALT [1R]: Displays the FMS-computed Maximum altitude for cruise. The MAX ALT value is displayed in small white font. The FMS-computed MAXimum altitude is a 1.2g buffetlimited altitude and is always limited to the aircraft's maximum certified altitude. The title and data fields correspond to the one-engine stabilizing altitude (STAB ALT) when engine-out mode is active. OPT ALT: The OPT ALT value is displayed in small white font. The FMS-computed OPTimum altitude is a 1.45g buffetlimited altitude and is always limited to the aircraft's maximum certified altitude. VDEV [2R]: Displays the vertical deviation relative to the FMS computed descent path with a resolution of 10 feet and a range of 0 to 9990. Positive values indicate that the aircraft is above the pre-computed descent path. Negative values indicate that the aircraft is below the pre-computed descent path. The title and data field are displayed when the aircraft has passed the T/D anticipation point or the descent mode is active. The FMS will blank the title and data field when vertical guidance is not available (ex: past the E/D if no approach procedure was selected). When present, the values are displayed in small white font. VDEV SCALE [3R]: Displays the current VDEV Full Scale Deviation (FSD) in small white font: • When in GPS Approach mode, FSD is +/-150 ft; otherwise • FSD is +/-400 ft. NOTE: This field is only displayed when the current vertical phase of flight is Descent/Approach. No entry is permitted in this field. FUEL [5R]: Provides access to the RTE x FUEL page (where x corresponds to the Active or Modified Active route number). TO T/C [6R]: TO T/D [6R]: TO E/D [6R]: TO S/C [6R]: TO S/D [6R]: Displays ETA and the DTG to the next along-track VNAV computed altitude profile point: • T/C when climb mode is active; OR • T/D when cruise mode is active and the aircraft is within 999 nm of T/D; OR • S/C when cruise mode is active and a pre-planned Step Climb exists in the active flight plan; OR • S/D when cruise mode is active and a pre-planned Step Descent exists in the active flight plan; OR • E/D when descent mode is active; OR • Field title and data are blanked when the data is not available.

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Page A300-A-57 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

PROGRESS 2/3 Display ACT PROGRESS 2/3 page by pressing [PROG] and then [NEXT]. When a FLT NO is displayed on the RTE page and both VOR receivers are tuned:

DLH1234 FROM 1L

SEA TO

2L

ARRIE

PROGRESS

2/3

ALT 1300 DTG 17.2

ATA 1803< ETA 1817<

1R

68.7

1830<

3R

2R

NEXT 3L

TOU DEST

5L

1279 2347< VDME1 VOR2 CRI/112.30A YRQ/112.80A

6L

RADIO>

4L

PANC

4R 5R 6R

Flight Number info on page title: If a Flight Number entry was made on RTE page field, then this entry will be displayed on the title line PROGRESS 2/3 page. FROM [1L]: Identifier of the last (FROM) waypoint overflown. Displays "GROUND" after takeoff before reaching the active waypoint if no departure runway was selected, else displays the departure runway. ALT [1L]: Crossing altitude over the FROM waypoint. Display can be either in feet or FL. If waypoint is before the midway point of the active route, Transition Altitude criterion is used. If waypoint is after the midway point of the active route, Transition Level criterion is used. ATA/FOB [1R]: Actual time of arrival at the FROM waypoint or Fuel on Board at the From waypoint. Selection of LSK 1R to 4R will toggle accordingly: - When FOB is shown at [1R], ETEs are shown at [2R] to [4R] - When ATA is shown at [1R], ETAs are shown at [2R] to [4R] TO [2L]: Identifier of active waypoint. DTG [2L]: Cumulative distance-to-go from present position to waypoint along the flight plan route. ETA [2R, 3R, 4R]: Estimated time of arrival at waypoint or destination. On selection will change to ETE (also effects a change on [1R]). ETE [2R, 3R, 4R]: (Not displayed) Displays Estimated time en-route at waypoint or destination. NEXT [3L]: Identifier of NEXT waypoint. DEST [4L]: Identifier of the Destination airport. The destination is defined as the airport entered on the RTE 1/X page, assuming a great circle from the last waypoint in the route to the destination airport.

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Page A300-A-58 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) VOR1/VDME1 [5L]: VOR2/VDME2 [5R]: Displays the tuned VOR frequency and the associated navigation database identifier. Field title is displayed as follows: • 'VOR' when a VOR-only station is being tuned. • ‘VDME' when a collocated VOR/DME station is being tuned. A reverse video 'A' is displayed next to the tuned frequency if the FMS is currently auto-tuning the VOR station. Dashes are displayed in this field (e.g. '---/---.--') if no VOR frequency is currently being tuned or the VOR receiver is failed. Tuning of a VOR frequency/identifier is inhibited from this page since this field is a read-only field. RADIO [6R]: Provides access to the RADIO page.

RTA PROGRESS 3/3

RTA function is not activated with Performance VNAV.

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Page A300-A-59 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

ENG OUT CLB 1/4 The Engine Out CLB page is used to activate and display engine out Climb vertical mode data. Predictions (i.e time, alt, fuel) are not provided while engine out climb mode is active Press [VNAV], (When in Climb mode and the aircraft is in a clean configuration) Press [VNAV] (When E/O climb mode is active) NOTE(S): • When the Engine Out climb page is accessed, while E/O mode is not active, the EXEC key illuminates and MOD is displayed on the title page. This allows the pilot to confirm the selection of FMS engine out mode. • The VNAV profile is failed when engine-out mode climb mode is active A. Engine Out has been selected on the CLB page; E/O CLB page is displayed (MOD state).

MOD

E/O CLB

CRZ ALT

1/4

STAB ALT FL280

1L

FL350

2L

G-DOT SPD 240

2R

3L 4L

3R ------ E/O MODE ----->CRITICAL

5L 6L

1R

4R 5R

C R I T I C A L

4R

5L

C R I T I C A L

5L 6L

4R 5R

C R I T I C A L

5L

M I N

FUEL

3L

>M I N

TIME

2/3

COST INDEX 35

1R 2R 3R

4L

4R

5L

5R

6L

CRUISE>

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6R

Page SSJ 100-A-17 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) B. A manual speed has been entered on the cruise page and the sub-modes are deselected. C.

ACT

CRZ SCHED

1L

SPD SCHED >E C O N

2L

>M I N

FUEL

3L

>M I N

TIME

2/3

COST INDEX 35

1R 2R 3R

4L

4R

5L

5R

CRUISE>

6L

6R

D. The sub-mode in [1L] has been selected. E.

MOD

CRZ SCHED

SPD SCHED 1L

ECON

2L

>M I N

FUEL

3L

>M I N

TIME

2/3

COST INDEX 35

1R 2R 3R

4L

4R

5L

5R

6L



6R

TITLE: 1.The title displays: • “ACT” if cruise is active • “MOD” if the EXEC key is illuminated • Blanks if cruise is not active followed by CRZ SCHED XXX XXX [1L]: Displays the first cruise speed sub-mode defined in the policy file. A selected sub-mode is displayed in large font. When the prompt is displayed, pressing the adjacent LSK has the following effect: • • •

The sub-mode's speed schedule is copied into the CRZ page data field at LSK 2L; The sub-mode's name is copied into the CRZ page title field at LSK 2L with "SPD" appended to the end of the name if it is less than 6 characters in length. An abbreviated sub-mode name is provided in all other cases (e.g. MIN FUEL will be displayed as MFUEL SPD); Selection of a CRZ speed sub-mode is propagated to the DES page if the selected sub-mode is applicable for that phase of flight.

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Page SSJ 100-A-18 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

The font will change from large to small when another cruise speed sub-mode is selected or a manual speed entry is made in LSK 2L on the CRZ page. NOTES: • The field title (e.g. “MIN FUEL”) is defined in the policy file. • Selection of the sub-mode cancels CP-Speed Intervention if previously active. • Selection of the sub-mode terminates an active speed constraint if previously active. XXX XXX [2L]/[3L]: “XXX XXX” is the name of the second/third cruise speed sub-mode in the policy file. Behavior of this prompt upon selection is equivalent to the first cruise speed sub-mode selection at LSK 1L. ERASE [6L]: “ERASE” is only displayed when an active flight plan modification is in progress. Pressing this key will undo all changes to the active flight plan and return to the ACT Route status. COST INDEX [1R]: Displays the Cost Index selected on the PERF INIT page for reference purposes. The Cost Index can be modified from this page in order to modify the speed schedule associated with the ECON sub-mode. CRUISE [6R]: Enables direct access to the VNAV CRZ page.

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Page SSJ 100-A-19 July 17, 2013

OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)

DES 3/4 The DES page is used to select and display Descent vertical mode data. Display the DES 3/4 page by pressing: [VNAV] (When in Descent mode) or [VNAV] [PREV] (When in Approach mode) or [VNAV] [NEXT] [NEXT] (When in Climb mode) or [VNAV] [NEXT] (When in Cruise mode) or from PROFILE page A. • • •

The descent sub-mode is defined in the policy file; The descent speed sub-mode is not active (speed target is not highlighted – ACT not displayed in the page title). The aircraft is within 50 nm of the Top of Descent, as a result the EARLY DES prompt is available.

There is no FAF in the active flight plan; hence the E/D data field shows the following: • The predicted E/D speed (195); • E/D location: DTG (15 nm) to the runway threshold, if any runway as been selected, or to the destination airport; • E/D height (3000 ft) relative to the runway elevation, if any runway has been selected, or to the airport elevation.

MIN FUEL DES 1L 2L 3L

3/4

E/D( K T / N M / F T ) AT T/D 195/15/3000 FL350 MFUEL SPD TO T/D 2022z/25.3N M .780/280 SPD REST WPT / ALT 250/10000 NOLLA/ 1 1 0 0 0 A < V/B V/S

4L 5L 6L

1R 2R 3R 4R