CMA-9000.pdf

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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.

CMA-9000

OPERATIONAL PROGRAM

S/W 169-614876-056

Esterline CMC Electronics

600 Dr. Frederik Philips Boulevard Ville Saint-Laurent, Quebec, Canada

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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

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WE VALUE YOUR COMMENTS

PLEASE EVALUATE OUR PUBLICATION

AND LET US KNOW

Although we constantly strive for accuracy and clarity, we may make errors on occasion. If we do, we would appreciate your comments to improve this manual.

Please use the following Customer Comments form at:

http://www.cmcelectronics.ca/customer-support-request-form.aspx to inform us of any correction or send us a marked-up copy of this publication. We will acknowledge your comments and notify you of any intended action.

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PUBLICATION TITLE: MANUAL P/N: DATE OF ISSUE: REVISION DATE: COMMENTS: PAGE NO. PARA-GRAPH LINE NO. FIGURE NO. TABLE NO.

CHANGE AND REASON

NAME: POSITION: TELEPHONE: E-MAIL ADDRESS:

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CMC Electronics Inc.

CUSTOMER SUPPORT

600 DR. FREDERIK PHILIPS BOULEVARD VILLE ST. LAURENT, QUEBEC,

CANADA H4M 2S9

FOLD BACK

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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 PAGE DATE

Title T-1 July 17/13

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Lists of Effective Pages LEP-1 July 17/13

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Record of Revisions RR-1 July 17/13

RR-2 Blank

Table of Contents TC-1 July 17/13

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Purpose of Operator's Manual OR-1 July 17/13

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Page LEP-2 July 17, 2013

1 - Introduction 1-i July 17/13

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2 - Control and Display 2-i July 17/13

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3 - Preflight 3-i July 17/13

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LIST OF EFFECTIVE PAGES

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

4 - Departures 4-i July 17/13

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5 - Enroute 5-i July 17/13

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Page LEP-4 July 17, 2013 5-19 July 17/13 5-20 July 17/13 5-21 July 17/13 5-22 July 17/13 5-23 July 17/13 5-24 July 17/13 5-25 July 17/13 5-26 July 17/13 5-27 July 17/13 5-28 July 17/13 5-29 July 17/13 5-30 July 17/13 5-31 July 17/13 5-32 July 17/13 5-33 July 17/13 5-34 July 17/13 5-35 July 17/13 5-36 Blank

6 - Arrivals 6-i July 17/13

7 - Approach 7-i July 17/13

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LIST OF EFFECTIVE PAGES

7-21 July 17/13 7-22 July 17/13 7-23 July 17/13 7-24 July 17/13 7-25 July 17/13 7-26 July 17/13 7-27 July 17/13 7-28 Blank

8 - Post-Flight Procedures 8-i July 17/13

8-ii Blank

8-1 July 17/13

8-2 July 17/13

9 - Direct-To/Intercept 9-i July 17/13

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10 - Holding Pattern Navigation 10-i July 17/13

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11 - Tactical Functions 11-i July 17/13

11-ii Blank 11-1 July 17/13 11-2 July 17/13 11-3 July 17/13 11-4 July 17/13 11-5 July 17/13 11-6 July 17/13 11-7 July 17/13 11-8 July 17/13 11-9 July 17/13 11-10 July 17/13 11-11 July 17/13

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Page LEP-6 July 17, 2013 11-13 July 17/13 11-14 July 17/13 11-15 July 17/13 11-16 July 17/13 11-17 July 17/13 11-18 July 17/13 11-19 July 17/13 11-20 July 17/13 11-21 July 17/13 11-22 July 17/13 11-23 July 17/13 11-24 July 17/13 11-25 July 17/13 11-26 July 17/13 11-27 July 17/13 11-28 Blank

12 -Navigation Sensors 12-i July 17/13

13 - Radio Tuning Pages 13-i July 17/13

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LIST OF EFFECTIVE PAGES

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

14 -Performance Functions 14-i July 17/13

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15 - RNP Capability 15-i July 17/13

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15-1 July 17/13

15-2 July 17/13

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15-5 July 17/13

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16 –MCDU Functions 16-i July 17/13

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16-1 July 17/13

16-2 July 17/13

16-3 July 17/13

16-4 July 17/13

17 - Abnormal Procedures 17-i July 17/13

18A - Performance VNAV For A300/310 18A-i July 17/13

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LIST OF EFFECTIVE PAGES

18A-30 July 17/13 18A-31 July 17/13 18A-32 July 17/13 18A-33 July 17/13 18A-34 July 17/13 18A-35 July 17/13 18A-36 July 17/13 18A-37 July 17/13 18A-38 July 17/13 18A-39 July 17/13 18A-40 July 17/13 18A-41 July 17/13 18A-42 July 17/13 18A-43 July 17/13 18A-44 July 17/13 18A-45 July 17/13 18A-46 July 17/13 18A-47 July 17/13 18A-48 July 17/13 18A-49 July 17/13 18A-50 July 17/13 18A-51 July 17/13 18A-52 July 17/13 18A-53 July 17/13 18A-54 July 17/13 18A-55 July 17/13 18A-56 Blank

18B - Performance VNAV For SUPERJET 100 18B-i July 17/13

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Page LEP-10 July 17, 2013 18B-23 July 17/13 18B-24 July 17/13 18B-25 July 17/13 18B-26 July 17/13 18B-27 July 17/13 18B-28 July 17/13 18B-29 July 17/13 18B-30 July 17/13 18B-31 July 17/13 18B-32 July 17/13 18B-33 July 17/13 18B-34 July 17/13 18B-35 July 17/13 18B-36 July 17/13 18B-37 July 17/13 18B-38 July 17/13 18B-39 July 17/13 18B-40 July 17/13 18B-41 July 17/13 18B-42 July 17/13 18B-43 July 17/13 18B-44 July 17/13 18B-45 July 17/13 18B-46 July 17/13 18B-47 July 17/13 18B-48 July 17/13 18B-49 July 17/13 18B-50 July 17/13 18B-51 July 17/13 18B-52 Blank

19 - Datalink Functions 19-i July 17/13

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

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LIST OF EFFECTIVE PAGES

19-18 July 17/13 19-19 July 17/13 19-20 July 17/13 19-21 July 17/13 19-22 July 17/13 19-23 July 17/13 19-24 July 17/13 19-25 July 17/13 19-26 July 17/13 19-27 July 17/13 19-28 July 17/13 19-29 July 17/13 19-30 July 17/13 19-31 July 17/13 19-32 July 17/13 19-33 July 17/13 19-34 July 17/13 19-35 July 17/13 19-36 July 17/13 19-37 July 17/13 19-38 July 17/13 19-39 July 17/13 19-40 July 17/13 19-41 July 17/13 19-42 July 17/13 19-43 July 17/13 19-44 July 17/13

Appendix A - FMS Pages - Detailed Descriptions A-i July 17/13

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

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Page LEP-12 July 17, 2013 A-23 July 17/13 A-24 July 17/13 A-25 July 17/13 A-26 July 17/13 A-27 July 17/13 A-28 July 17/13 A-29 July 17/13 A-30 July 17/13 A-31 July 17/13 A-32 July 17/13 A-33 July 17/13 A-34 July 17/13 A-35 July 17/13 A-36 July 17/13 A-37 July 17/13 A-38 July 17/13 A-39 July 17/13 A-40 July 17/13 A-41 July 17/13 A-42 July 17/13 A-43 July 17/13 A-44 July 17/13 A-45 July 17/13 A-46 July 17/13 A-47 July 17/13 A-48 July 17/13 A-49 July 17/13 A-50 July 17/13 A-51 July 17/13 A-52 July 17/13 A-53 July 17/13 A-54 July 17/13 A-55 July 17/13 A-56 July 17/13 A-57 July 17/13 A-58 July 17/13 A-59 July 17/13 A-60 July 17/13 A-61 July 17/13 A-62 July 17/13 A-63 July 17/13 A-64 July 17/13 A-65 July 17/13 A-66 July 17/13 A-67 July 17/13 A-68 July 17/13 A-69 July 17/13 A-70 July 17/13 A-71 July 17/13 A-72 July 17/13

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LIST OF EFFECTIVE PAGES

A-73 July 17/13 A-74 July 17/13 A-75 July 17/13 A-76 July 17/13 A-77 July 17/13 A-78 July 17/13 A-79 July 17/13 A-80 July 17/13 A-81 July 17/13 A-82 July 17/13 A-83 July 17/13 A-84 July 17/13 A-85 July 17/13 A-86 July 17/13 A-87 July 17/13 A-88 July 17/13 A-89 July 17/13 A-90 July 17/13 A-91 July 17/13 A-92 July 17/13 A-93 July 17/13 A-94 July 17/13 A-95 July 17/13 A-96 July 17/13 A-97 July 17/13 A-98 July 17/13 A-99 July 17/13 A-100 July 17/13 A-101 July 17/13 A-102 July 17/13 A-103 July 17/13 A-104 July 17/13 A-105 July 17/13 A-106 July 17/13 A-107 July 17/13 A-108 July 17/13 A-109 July 17/13 A-110 July 17/13 A-111 July 17/13 A-112 July 17/13 A-113 July 17/13 A-114 July 17/13 A-115 July 17/13 A-116 July 17/13 A-117 July 17/13 A-118 July 17/13 A-119 July 17/13 A-120 July 17/13 A-121 July 17/13 A-122 July 17/13 A-123 July 17/13

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Page LEP-14 July 17, 2013 A-125 July 17/13 A-126 July 17/13 A-127 July 17/13 A-128 July 17/13 A-129 July 17/13 A-130 July 17/13 A-131 July 17/13 A-132 July 17/13 A-133 July 17/13 A-134 July 17/13 A-135 July 17/13 A-136 July 17/13 A-137 July 17/13 A-138 July 17/13 A-139 July 17/13 A-140 July 17/13 A-141 July 17/13 A-142 July 17/13 A-143 July 17/13 A-144 Blank

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

Detailed Descriptions A300-A-i July 17/13

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

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LIST OF EFFECTIVE PAGES

A300-A-27 July 17/13 A300-A-28 July 17/13 A300-A-29 July 17/13 A300-A-30 July 17/13 A300-A-31 July 17/13 A300-A-32 July 17/13 A300-A-33 July 17/13 A300-A-34 July 17/13 A300-A-35 July 17/13 A300-A-36 July 17/13 A300-A-37 July 17/13 A300-A-38 July 17/13 A300-A-39 July 17/13 A300-A-40 July 17/13 A300-A-41 July 17/13 A300-A-42 July 17/13 A300-A-43 July 17/13 A300-A-44 July 17/13 A300-A-45 July 17/13 A300-A-46 July 17/13 A300-A-47 July 17/13 A300-A-48 July 17/13 A300-A-49 July 17/13 A300-A-50 July 17/13 A300-A-51 July 17/13 A300-A-52 July 17/13 A300-A-53 July 17/13 A300-A-54 July 17/13 A300-A-55 July 17/13 A300-A-56 July 17/13 A300-A-57 July 17/13 A300-A-58 July 17/13 A300-A-59 July 17/13 A300-A-60 July 17/13 A300-A-61 July 17/13 A300-A-62 July 17/13 A300-A-63 July 17/13 A300-A-64 July 17/13 A300-A-65 July 17/13 A300-A-66 July 17/13 A300-A-67 July 17/13 A300-A-68 July 17/13 A300-A-69 July 17/13 A300-A-70 July 17/13 A300-A-71 July 17/13 A300-A-72 July 17/13 A300-A-73 July 17/13 A300-A-74 Blank

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- Detailed Descriptions SSJ 100-A-i July 17/13

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

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LIST OF EFFECTIVE PAGES

SSJ 100-A-49 July 17/13 SSJ 100-A-50 July 17/13 SSJ 100-A-51 July 17/13 SSJ 100-A-52 July 17/13 SSJ 100-A-53 July 17/13 SSJ 100-A-54 July 17/13 SSJ 100-A-55 July 17/13 SSJ 100-A-56 July 17/13 SSJ 100-A-57 July 17/13 SSJ 100-A-58 July 17/13 SSJ 100-A-59 July 17/13 SSJ 100-A-60 July 17/13 SSJ 100-A-61 July 17/13 SSJ 100-A-62 July 17/13 SSJ 100-A-63 July 17/13 SSJ 100-A-64 July 17/13 SSJ 100-A-65 July 17/13 SSJ 100-A-66 Blank

Appendix FANS-A – FMS FANS Pages - Detailed Descriptions FANS-A-i July 17/13 FANS-A-ii Blank FANS-A-1 July 17/13 FANS-A-2 July 17/13 FANS-A-3 July 17/13 FANS-A-4 July 17/13 FANS-A-5 July 17/13 FANS-A-6 July 17/13 FANS-A-7 July 17/13 FANS-A-8 July 17/13 FANS-A-9 July 17/13 FANS-A-10 July 17/13 FANS-A-11 July 17/13 FANS-A-12 July 17/13 FANS-A-13 July 17/13 FANS-A-14 July 17/13 FANS-A-15 July 17/13 FANS-A-16 July 17/13 FANS-A-17 July 17/13 FANS-A-18 July 17/13 FANS-A-19 July 17/13 FANS-A-20 July 17/13 FANS-A-21 July 17/13 FANS-A-22 July 17/13 FANS-A-23 July 17/13 FANS-A-24 July 17/13 FANS-A-25 July 17/13 FANS-A-26 July 17/13 FANS-A-27 July 17/13 FANS-A-28 July 17/13 FANS-A-29 July 17/13 FANS-A-30 July 17/13

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Page LEP-18 July 17, 2013 FANS-A-32 July 17/13 FANS-A-33 July 17/13 FANS-A-34 July 17/13 FANS-A-35 July 17/13 FANS-A-36 July 17/13 FANS-A-37 July 17/13 FANS-A-38 July 17/13 FANS-A-39 July 17/13 FANS-A-40 July 17/13

Appendix B - Navigation Leg Type Definitions B-i July 17/13

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

Appendix C - Navigation Displays C-i July 17/13

C-ii Blank C-1 July 17/13 C-2 July 17/13 C-3 July 17/13 C-4 July 17/13 C-5 July 17/13 C-6 July 17/13 C-7 July 17/13 C-8 July 17/13 C-9 July 17/13 C-10 Blank

Appendix D - CMA-9000 FMS Display Pages Flow Diagrams D-i July 17/13

D-ii Blank

D-1 July 17/13

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LIST OF EFFECTIVE PAGES

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

Appendix E - System Messages and Remote Annunciators E-i July 17/13

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

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Page LEP-20 July 17, 2013 E-32 July 17/13 E-33 July 17/13 E-34 July 17/13 E-35 July 17/13 E-36 July 17/13 E-37 July 17/13 E-38 July 17/13 E-39 July 17/13 E-40 July 17/13 E-41 July 17/13 E-42 July 17/13 E-43 July 17/13 E-44 July 17/13 E-45 July 17/13 E-46 July 17/13 E-47 July 17/13 E-48 July 17/13 E-49 July 17/13 E-50 July 17/13

Index IND-1 July 17/13

IND-2 July 17/13 IND-3 July 17/13 IND-4 July 17/13 IND-5 July 17/13 IND-6 Blank

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RECORD OF REVISIONS

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

ASSIGNED TO (JOB TITLE) LOCATION

REV. NO. REVISION DATE INSERTION DATE BY REV. NO. REVISION DATE INSERTION DATE BY 0 July 17/13

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Page RR-2 July 17, 2013 This Page Intentionally Left Blank

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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

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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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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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SECTION 1 - INTRODUCTION

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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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, en-route, 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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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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NAVIGATION MODES

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

Navigation modes Sensor

GPS TSO-C129a B1/C1 GPS sensor (or

TSO-C145/C146)

DME/DME TSO-C66c DME receiver

VOR/DME TSO-C66c DME receiver;

TSO-C40c VOR receiver

Inertial TSO-C4c, TSO-C6d IRS

Dead Reckoning Heading + TAS inputs

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 TSO-C145/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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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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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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"TO" WAYPOINT WIND DIRECTION (WD) CROS S WIND DRIFT ANGLE (DA) RIGHT GROUND TRACK ANGLE (TK) HEADING (HDG) BEARING TO WAYPOINT (BRG) WINDSPEED (WS) DESIRED COURSE LINE GREAT C IRCLE BE TWEEN W AYPOINT S. CROSS-TRACK DISTANCE (XTK) LEFT

TRACK ANGLE ERROR (TKE) LEFT 0012033 GROU ND SP EED ( GS) TRUE AIR SPE ED (T AS) HEAD WIN D WIND SPEE D (WS) DESIRED TRACK (DTK)

Figure 1-1 Navigation Relationships

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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.

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A - Above (altitude)

AA - Air-To-Air

AAIM - Aircraft Autonomous Integrity Monitoring

AAR - Air-To-Air Refuelling

AC - Aircraft

ACARS - Aircraft Communications Addressing and Reporting System

ACCUR - Accuracy

ACID - Aircraft Identifier

ACT - Active

ACMS - Aircraft Conditioning Monitoring System

ACQ - Acquisition mode

ADC - Air Data Computer

ADF - Automatic Direction Finder

ADIRS - Air Data Inertial Reference System ADS - Automatic Dependent Surveillance

ADx - Primary (AD1) or Secondary (AD2) ADF radio

AF - Initial Approach Fix

AFCS - Automatic Flight Control System AFMS - Airplane Flight Manual Supplement AFN - ATS Facilities Notification

AG - Air-To-Ground

AGC - Automatic Gain Control

AGL - Above Ground Level

AHRS - Attitude Heading Reference System

ALT - Altitude

AMLCD - Active Matrix Liquid Crystal Display ANP - Actual Navigation Performance

ANT - Antenna

AOC - Airline Operational Communications AP/FD - Autopilot/Flight Director

APPR - Approach

APU - Auxiliary Power Unit

ARC - Arc to Fix/Radius to Fix

ARINC - Aeronautical Radio Incorporated

ARPT - Airport

ARR - Arrival

ATA - Actual Time of Arrival ATC - Air Traffic Control

ATK - Along Track Distance

ATT - Attitude

ATS - Air Traffic Services

BARO - Barometric

BRT - Brightness

BRG - Bearing

BW - Back Course Marker

Cx - COM radio (primary : C1, secondary : C2)

CAP - Capable

CARP - Calculated Air Release Point

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CDI - Course Deviation Indicator CDU - Control Display Unit

CF - Final Approach Course to fix

CFG - Configuration

CHK - Checker

CLR - Clear

CMx - Primary (CM1) or Secondary (CM2) COM radio CMA - Canadian Marconi (Avionics)

CMD - Command

CMU - Communications Management Unit

COM - Communication

COMMS - Communication Radios

CON - Connection

CONC - Concentrator

COORD - Coordinates

CPDLC - Controller Pilot Datalink Communication

CPS - Compass

CRP - Computed Air Release Point

CRS - Course (desired track) of route leg or to waypoint

CRZ - Cruise CTR - Center DA - Drift Angle DEL - Delete DEP - Departure DES - Destination DESEL - Deselected DEST - Destination DF - Direct To Fix

DGNSS - Differential Global Navigation Satellite System

DIFF - Differential

DISCON - Route Discontinuity

DIS - Distance

DIST - Distance

DLU - Data Loader Unit

DME - Distance Measurement Equipment

DOD - Department Of Defense

DOP - Dilution of Precision

DR - Dead Reckoning

DTG - Distance To Go

DTK - Desired Track

DTO - Direct To

DTRA - Transition Distance

DTW - Distance To Waypoint

E - East

E/W - East/West

EDT - Edit

EFA - Estimated Fuel at Arrival

EFIS - Electronic Flight Instrumentation System EHE - Estimated Horizontal Error

EHSI - Electronic Horizontal Situation Indicator

ENRT - En-Route

EQUIP - Equipment

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EW - Electronic Warfare

EXEC - Execute

FAF - Final Approach Fix

FDE - Failure Detection and Exclusion

FF - Final Approach Fix

FFK - Front panel Function Key FIR - Flight Information Region

FL - Flight Level

FLT - Flight

FMS - Flight Management System

FMU - Flight Management Unit

F/O - First Officer

FOM - Figure of Merit

FPU - Floating Point Unit

FR - From

FREQ - Frequency

FSD - Full Scale Deflection

FT - Feet

FTE - Flight Technical Error

GD - Guard

GDOP - Geometric Dilution of Precision

GLNS - GLONASS

GLONASS - Global Navigation Satellite System (Russian)

GMT - Greenwich Mean Time

GNS - Global Navigation System

GNSSU - Global Navigation System Sensor Unit GPIAL - GPS Position Integrity Alert Limit GPS - Global Positioning System

GS - Ground Speed

GSM - Global Navigation System Sensor Module

GWT - Gross Weight

/H - Holding Pattern

HARP - High Altitude Release Point

HAT - Height Above Terrain

HDG - Heading

HDOP - Horizontal Dilution of Precision

HF - High Frequency

HFOM - Horizontal Figure Of Merit HIL - Horizontal Integrity Limit

HOR - Horizontal

HR - Hour

HSI - Horizontal Situation Indicator

HT - Height

HW - Hardware

HYB - Hybrid

IAF - Initial Approach Fix

IAS - Indicated Airspeed

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IC - Intercom

ICAO - International Civil Aviation Organization

ID - Identifier

IDENT - Identifier

IDT - Identifier

IF - Intermediate Fix

IFR - Instrument Flight Rules in Hg - Inches of Mercury

ILS - Instrument Landing System

IM - Innner Marker

INBD - Inbound

INACT - Inactive

INIT - Initialize

INT - Integrity

INTC - Intercept Course

INS - Inertial Navigation System

IP - Identification Point

IRS - Inertial Reference System

ITU - Telecommunication Union

KG - Kilogram

KT - Knot(s)

L - Left

LAT - Latitude or Lateral

LB - Pound

LDA - Landing distance available LDR - Light Detect Resistor

LIB - Library

LNAV - Lateral Navigation mode of the autopilot/flight director system

LOC - Localizer

LOCB - Localizer Backcourse approach

LONG - Longitude

LP - Localizer Precision approach

LPV - Localizer Precision with Vertical guidance approach

LRU - Line Replaceable Unit

LSK - Line Select Key

LVL - Level

M - Meter

MA - Missed Approach Point when not RW

MAG - Magnetic

MAGVAR - Magnetic Variation

MAHP - Missed Approach Holding Point

MAINT - Maintenance

MAP - Missed Approach Point

MB - Millibars (hectopascal)

MC - Mission Computer

MCDU - Multipurpose Control and Display Unit

MDA - Minimum Descent Altitude

MDA-DA - Minimum Descent Altitude-Decision Altitude

MEW - Mean Effective Wind

MGRS - Military Grid Reference System

MHz - Mega Hertz

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MRK - Mark

MSG - Message

MSLA - Mean Sea Level Altitude MTBF - Mean Time Between Failures

N - North

Nx - NAV radio (primary : N1, secondary : N2)

NAV - Navigation or Navaid

NDB - Non-directional Beacon

NDBD - NDB approach with DME facility (GPS or NDB/(DME))

NM - Nautical Mile

NOTAMS - Notices To Airmen

NP - Navigation Performance

NPA - Non-Precision Approach

NVx - Primary (NV1) or secondary (NV2) NAV radio

NVM - Non-Volatile Memory

VNAV - Vertical Navigation

NVIS - Night Vision Imaging System

/O - Overfly Waypoint

OAT - Outside Air Temperature

OFST - Offset OM - Outer Marker OP - Operations (independent/synchronized) ORIG - Origin PBD - Place/Bearing/Distance PBPB - Place/Bearing-Place/Bearing

PEE - Position Estimation Error

PERF - Performance

PG - Page

PIT - Programmable Interrupt Timer

POF - Phase of Flight

POS - Position

PPOS - Present Aircraft Position

PREDEF - Predefined

PREV - Previous

PRN - Pseudo Range Number

PROG - Progress

P-T - Procedure Turn

PWR - Power

QFE - Field Elevation Pressure

QNH - Sea Level Pressure

/R - Radial-To

R - Right

RAD - Radial

RADALT - Radar Altitude

RAIM - Receiver Autonomous Integrity Monitor

RALT - Radio Altimeter

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RCU - Remote Control Unit

RCV - Receive only

REC - Flight Recorder

REF - Reference

REL - Relative

RES - Reserve

RESEL - Reselect

RF - Radio Frequency

RIB - Radio Interface Board

RMS - Radio Management System

RNAV - Required Navigation

RNG - Range

RNP - Required Navigation Performance RTA - Required Time of Arrival

RTC - Real Time Clock

RTE - Route

RW - Runway Threshold

/S - Search Pattern

S/W - Software

S - South

SAR - Search and Rescue

SAT - Satellite

SATCOM - Satellite Communication System

SD - Slowdown Point

SDF - Simplified Directional Facility

SEL - Selected

SID - Standard Instrument Departure

SMS - Short Message Service

SP - Space

SPD - Speed

SQK - Squawk

SSM - Sign Status Matrix

SSR - Secondary Surveillance Radar

STAR - Standard Terminal Arrival Routes

STAT - Status

STBY - Standby

STC - Supplemental Type Certificate

STS - Status

SURF - Surface

SYNC - Synchronization

/T - Tactical Direct-To

T - Angle referenced to True North TACAN - Tactical Air Navigation

TACT - Tactical

TAS - True Air Speed

TCN - TACAN

TD - Touchdown Fix when not RW

TE - Trailing Edge

TEL - Telephone

TEMP - Temperature

TERM - Terminal

TF - Track To Fix

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Page 1-14 July 17, 2013 TPDR - Transponder TR - Transmit/Receive TRANS - Transition TRK - Track TRG - Transmit on Guard

TSE - Total System Error

TSO - Technical Standard Order TTFF - Time To First Fix

TTG - Time To Go

TTS - Time To Station

TX1 - V/UHF1 Transmitting

TX2 - V/UHF2 Transmitting

UF - UHF radio

UHF - Ultra High Frequency

UTC - Universal Time Coordinates UTM - Universal Transverse Mercator

V - Velocity (VX, VY, VZ)

VAL - Value

VDOP - Vertical Dilution of Precision

VECT - Vector

VERT - Vertical

VFOM - Vertical Figure Of Merit VFR - Visual Flight Rules

VHF - Very High (30-300 MHz) Frequency

VNAV - Vertical Navigation

VUHF - Very Ultra High Frequency

VIR - VOR ILS Receiver

VIS - Visible

VOR - VHF Omni-directional Radio Range VORD - VOR/DME approach (GPS or VOR/DME)

W - West

WD - Wind Direction

WPT - Waypoint

WS - Windspeed

WT - Weight

WGS - World Geodetic System

WGT - Weight

WXR - Weather Radar

XFILL - Cross FMS Fill

XPDR - Transponder

XMT - Transmit

XTE - Extended Trailing Edge Point

XTK - Cross Track

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SECTION 2 - CONTROL AND DISPLAY

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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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 ARINC-739 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 twenty-four characters. The page format is divided in twenty-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

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

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

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

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Figure 2-5 Front Panel, Hardware variation 050

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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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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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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 Item 22 Item 20 Item 33 Item 17 Item 14

045/445 RADIO FMC COMM VNAV HOLD FIX

050 RADIO TACT VNAV HOLD ATC

060/460 ATC FMC COMM VNAV HOLD FIX

070/470/471 RADIO ATC VNAV HOLD 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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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 Item 2 Item 3 Item 4 Item 5 Item 6 Item 7 Item 8

045/445 FAIL MSG RNP OFST IND None ATC

050 FAIL MSG RNP OFST IND None ATC

060/460 FAIL MSG RNP OFST IND None ATC

070/470/471 FAIL MSG RNP OFST IND None 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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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 CMA-9000.

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.

CMA-9000.pdf

CMA-9000

OPERATIONAL PROGRAM

S/W 169-614876-056

FLIGHT MANAGEMENT SYSTEM

CMA-9000

OPERATIONAL PROGRAM

S/W 169-614876-056

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TABLE OF CONTENTS

Subject

Section/Appendix

PURPOSE OF OPERATOR'S MANUAL

SECTION 1 - INTRODUCTION

CONTENTS

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SECTION 1

INTRODUCTION

SECTION 2 - CONTROL AND DISPLAY

CONTENTS

Subject

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SECTION 2

CONTROL AND DISPLAY