Honeywell Primus System Description and Operation Manual

Cessna Citation XLS · Systems Description

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Overview

This document is the System Description and Operation Manual for the Cessna Citation XLS, specifically detailing the Primus 1000 Integrated Avionics System. It includes revisions, operational procedures, and technical data relevant to the system's functionality and maintenance.

Document revision date is 11 May 2007.
Contains proprietary data from Honeywell International Inc.
Includes instructions for replacing the IC-615 battery.
Updated customer support information.
Subject to U.S. export regulations.
License agreement governs the use of the materials.
No copies of the materials may be made without permission.
Honeywell retains all rights to the materials.

Document

Source

Originally published by archive.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Systems Description
Year: 2007
File size: 8.4 MB
Publisher: archive.org
Language: en

About this document

What is the Honeywell Primus System Description and Operation Manual?

The Honeywell Primus System Description and Operation Manual is a systems description for the Cessna Citation XLS, dated 2007.

Where does the Honeywell Primus System Description and Operation Manual come from?

This copy of the Honeywell Primus System Description and Operation Manual was originally published by archive.org and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Honeywell Primus System Description and Operation Manual published?

The Honeywell Primus System Description and Operation Manual — the Cessna Citation XLS systems description on file — is dated 2007.

Documentation completeness

2/7

Most owners only have the POH. Here's the essential set for the Cessna Citation XLS.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More Cessna Citation XLSmanuals & documents

In this document

Revision Information

Details the changes made in the latest revision, including updated pages and new information added.

License Agreement

Outlines the terms under which the materials can be used, including confidentiality and limitations on liability.

Customer Support

Provides updated contact information for customer support related to the Primus 1000 Integrated Avionics System.

Battery Replacement Procedure

Describes the procedure for replacing the IC-615 battery, including the location of the battery cover.

Proprietary Notice

States that the document contains trade secrets and is confidential, prohibiting unauthorized use or duplication.

Record of Revisions

A section for tracking revisions made to the manual, including dates and incorporator initials.

Safety notes

Do not copy the document without express permission from Honeywell.
Failure to comply with the License Agreement may result in termination of the license.
Honeywell is not liable for any incidental or consequential damages.

Full document text

Honeywell International Inc. 21111 N. 19th Ave. Phoenix, AZ 85027-2708 U.S.A. CAGE: 58960 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page HL--1 Telephone: (800) 601--3099 (U.S.A.) Telephone: (602) 365--3099 (International) TO HOLDERS OF SYSTEM DESCRIPTION AND OPERATION MANUAL, PUB. NO. A15--1146--096, PRIMUS 1000 INTEGRATED AVIONICS SYSTEM REVISION NO. 001 DATED 11 MAY 2007 This revision replaces some data in the manual. All changed pages have a new date, as identified in the List of Effective Pages. Revision bars identify the changed data. Put the changed pages in the manual and remove and discard all replaced pages. Write the revision number, revision date, and replacement date on the Record of Revisions page. Page Description of Change T--1 thru T--4 Changed to show the revision date. Replaced the Proprietary Notice with the new Honeywell Materials License Agreement. LEP--1 thru LEP--8 Changed to show the changed pages in the manual. TC--1 thru TC--20 Changed to show where information is located in the manual. INTRO--3 Updated the Customer Support data. 2--1--3 Added IC--615 IAC Leading Particulars information to Table 2--1--1. 2--5--4 Added IC--615 IAC Leading Particulars information to Table 2--5--1. 2--6--4 Added IC--615 IAC Leading Particulars information to Table 2--6--1. 4--13, 4--14, 4--14.1, 4--14.2 Added procedure to replace the IC--615 battery. Added Figure 4--3, IC--615 Battery Cover Location. Relocated some data. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page HL--2 Blank Page RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 7E994, no license required. Honeywell International Inc. 21111 N. 19th Ave. Phoenix, AZ 85027-2708 U.S.A. CAGE: 58960 Publication Number A15--1146--096, Revision 001 Page T--1 Revised 11 May 2007 1 Nov 2004  Honeywell International Inc. Do not copy without express permission of Honeywell. Telephone: (800) 601--3099 (U.S.A.) Telephone: (602) 365--3099 (International) System Description and Operation Manual PRIMUS 1000 Integrated Avionics System Cessna Citation XLS RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page T--2 Honeywell--Confidential THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., CONTAIN TRADE SECRETS AND MAY NOT, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED. Honeywell Materials License Agreement The documents and information contained herein (“the Materials”) are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc (collectively “Honeywell”). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell--authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned--subsidiaries or a formally designated third party service provider thereunder; and direct recipients of Materials from Honeywell’s Aerospace Technical Publication Distribution. The terms and conditions of this License Agreement govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgement. 1. License Grant -- If you are a party to an applicable product support agreement, a Honeywell Service Center agreement, or an authorized repair facility agreement, Honeywell hereby grants you a limited, non--exclusive license to use these Materials to operate, maintain, or repair Honeywell aerospace products only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell’s Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair of Honeywell aerospace products, Honeywell hereby grants you a limited, non--exclusive license to use these Materials to maintain or repair the subject Honeywell aerospace products only at the facility to which these Materials have been shipped (“the Licensed Facility”). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell. 2. Rights In Materials -- Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. No license to use any Honeywell trademarks or patents is granted under this License Agreement. 3. Confidentiality -- You acknowledge that these Materials contain information that is confidential and proprietary to Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials. 4. Assignment And Transfer -- This License Agreement may be assigned to a formally designated service

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designee to the extent allowed under an applicable product support agreement or transferred to a subsequent owner or operator of an aircraft containing the subject Honeywell aerospace products. However, the recipient of any such assignment or transfer must assume all of your obligations under this License Agreement. No assignment or transfer shall relieve any party of any obligation that such party then has hereunder. 5. Copies of Materials -- Unless you have the express written permission of Honeywell, you may not make or permit making of copies of the Materials. Notwithstanding the foregoing, you may make copies of only portions of the Material for your internal use. You agree to return the Materials and any copies thereof to Honeywell upon the request of Honeywell. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page T--3 6. Term -- This License Agreement is effective until terminated as set forth herein. This License Agreement will terminate immediately, without notice from Honeywell, if you fail to comply with any provision of this License Agreement or will terminate simultaneously with the termination or expiration of your applicable product support agreement, authorized repair facility agreement, or your formal designation as a third party service provider. Upon termination of this License Agreement, you will return these Materials to Honeywell without retaining any copies and will have one of your authorized officers certify that all Materials have been returned with no copies retained. 7. Remedies -- Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement. 8. Limitation of Liability -- Honeywell does not make any representation regarding the use or sufficiency of the Materials. THERE ARE NO OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT LIMITED TO, (i) WARRANTIES ARISING FROM COURSE OF PERFORMANCE, DEALING, USAGE, OR TRADE, WHICH ARE HEREBY EXPRESSLY DISCLAIMED, OR (ii) WARRANTIES AGAINST INFRINGEMENT OF INTELLECTUAL PROPERTY RIGHTS OF THIRD PARTIES, EVEN IF HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT. IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIAL DAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BY APPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, TORT (INCLUDING BUT NOT LIMITED TO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE. 9. Controlling Law -- This License shall be governed and construed in accordance with the laws of the State of New York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties. Copyright -- Notice Copyright 2007, Honeywell International Inc. All rights reserved. Honeywell, PRIMUS, and SPEX are registered trademarks of Honeywell International Inc. All other marks are owned by their respective companies. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page T--4 Blank Page RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 1 Nov 2004  Honeywell International Inc. Do not copy without express permission of Honeywell. Page RR--1 RECORD OF REVISIONS For each revision, put the revised pages in your manual and discard the superseded pages. Write the revision number and date, date put in manual, and the incorporator’s initials in the applicable columns on the Record of Revisions. The initial H shows Honeywell is the incorporator. Revision Number Revision Date Date Put In Manual By Revision Number Revision Date Date Put In Manual By 1 11 May 2007 11 May 2007 H RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 1 Nov 2004  Honeywell International Inc. Do not copy without express permission of Honeywell. Page RR--2 Blank Page RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 1 Nov 2004 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page RTR--1 RECORD OF TEMPORARY REVISIONS Instructions on each page of a temporary revision tell you where to put the pages in your manual. Remove temporary revision pages only when discard instructions are given. For each temporary revision, put the applicable data in the record columns on this page. Temporary Revision Number Temporary Revision Date Temporary Revision Status Date Put in Manual By * Date Removed from Manual By * * The initial H in this column shows Honeywell has done this task. * The initial H in this column shows Honeywell has done this task. ** Temporary revisions are incorporated in the manual by normal revision. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 1 Nov 2004 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page RTR--2 Blank Page RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--1 LIST OF EFFECTIVE PAGES Subheading and Page Date Subheading and Page Date Title T--1 H 11 May 2007 T--2 H 11 May 2007 T--3 H 11 May 2007 T--4 H 11 May 2007 Record of Revisions RR--1 1 Nov 2004 RR--2 1 Nov 2004 Record of Temporary Revisions RTR--1 1 Nov 2004 RTR--2 1 Nov 2004 List of Effective Pages LEP--1 H 11 May 2007 LEP--2 H 11 May 2007 LEP--3 H 11 May 2007 LEP--4 H 11 May 2007 LEP--5 H 11 May 2007 LEP--6 H 11 May 2007 LEP--7 H 11 May 2007 LEP--8 H 11 May 2007 Table of Contents TC--1 H 11 May 2007 TC--2 H 11 May 2007 TC--3 H 11 May 2007 TC--4 H 11 May 2007 TC--5 H 11 May 2007 TC--6 H 11 May 2007 TC--7 H 11 May 2007 TC--8 H 11 May 2007 TC--9 H 11 May 2007 TC--10 H 11 May 2007 TC--11 H 11 May 2007 TC--12 H 11 May 2007 TC--13 H 11 May 2007 TC--14 H 11 May 2007 TC--15 H 11 May 2007 TC--16 H 11 May 2007 TC--17 H 11 May 2007 TC--18 H 11 May 2007 TC--19 H 11 May 2007 TC--20 H 11 May 2007 Introduction INTRO--1 1 Nov 2004 INTRO--2 1 Nov 2004 INTRO--3 H 11 May 2007 INTRO--4 1 Nov 2004 INTRO--5 1 Nov 2004 INTRO--6 1 Nov 2004 INTRO--7 1 Nov 2004 INTRO--8 1 Nov 2004 INTRO--9 1 Nov 2004 INTRO--10 1 Nov 2004 INTRO--11 1 Nov 2004 INTRO--12 1 Nov 2004 System Overview 1--1 1 Nov 2004 1--2 1 Nov 2004 1--3 1 Nov 2004 1--4 1 Nov 2004 1--5 1 Nov 2004 1--6 1 Nov 2004 F 1--7/1--8 1 Nov 2004 F 1--9/1--10 1 Nov 2004 F 1--11/1--12 1 Nov 2004 F 1--13/1--14 1 Nov 2004 1--15 1 Nov 2004 1--16 1 Nov 2004 1--17 1 Nov 2004 1--18 1 Nov 2004 1--19 1 Nov 2004 1--20 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--2 Subheading and Page Date Subheading and Page Date 1--21 1 Nov 2004 1--22 1 Nov 2004 F 1--23/1--24 1 Nov 2004 1--25 1 Nov 2004 1--26 1 Nov 2004 1--27 1 Nov 2004 1--28 1 Nov 2004 1--29 1 Nov 2004 1--30 1 Nov 2004 1--31 1 Nov 2004 1--32 1 Nov 2004 1--33 1 Nov 2004 1--34 1 Nov 2004 System Description 2--1 1 Nov 2004 2--2 1 Nov 2004 Electronic Display System 2--1--1 1 Nov 2004 2--1--2 1 Nov 2004 2--1--3 H 11 May 2007 2--1--4 1 Nov 2004 2--1--5 1 Nov 2004 2--1--6 1 Nov 2004 2--1--7 1 Nov 2004 2--1--8 1 Nov 2004 2--1--9 1 Nov 2004 2--1--10 1 Nov 2004 2--1--11 1 Nov 2004 2--1--12 1 Nov 2004 2--1--13 1 Nov 2004 2--1--14 1 Nov 2004 2--1--15 1 Nov 2004 2--1--16 1 Nov 2004 2--1--17 1 Nov 2004 2--1--18 1 Nov 2004 2--1--19 1 Nov 2004 2--1--20 1 Nov 2004 F 2--1--21/2--1--22 1 Nov 2004 2--1--23 1 Nov 2004 2--1--24 1 Nov 2004 F 2--1--25/2--1--26 1 Nov 2004 2--1--27 1 Nov 2004 2--1--28 1 Nov 2004 2--1--29 1 Nov 2004 2--1--30 1 Nov 2004 2--1--31 1 Nov 2004 2--1--32 1 Nov 2004 2--1--33 1 Nov 2004 2--1--34 1 Nov 2004 2--1--35 1 Nov 2004 2--1--36 1 Nov 2004 2--1--37 1 Nov 2004 2--1--38 1 Nov 2004 F 2--1--39/2--1--40 1 Nov 2004 2--1--41 1 Nov 2004 2--1--42 1 Nov 2004 F 2--1--43/2--1--44 1 Nov 2004 F 2--1--45/2--1--46 1 Nov 2004 2--1--47 1 Nov 2004 2--1--48 1 Nov 2004 2--1--49 1 Nov 2004 2--1--50 1 Nov 2004 F 2--1--51/2--1--52 1 Nov 2004 2--1--53 1 Nov 2004 2--1--54 1 Nov 2004 2--1--55 1 Nov 2004 2--1--56 1 Nov 2004 2--1--57 1 Nov 2004 2--1--58 1 Nov 2004 2--1--59 1 Nov 2004 2--1--60 1 Nov 2004 2--1--61 1 Nov 2004 2--1--62 1 Nov 2004 2--1--63 1 Nov 2004 2--1--64 1 Nov 2004 2--1--65 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--3 Subheading and Page Date Subheading and Page Date 2--1--66 1 Nov 2004 2--1--67 1 Nov 2004 2--1--68 1 Nov 2004 2--1--69 1 Nov 2004 2--1--70 1 Nov 2004 2--1--71 1 Nov 2004 2--1--72 1 Nov 2004 2--1--73 1 Nov 2004 2--1--74 1 Nov 2004 2--1--75 1 Nov 2004 2--1--76 1 Nov 2004 2--1--77 1 Nov 2004 2--1--78 1 Nov 2004 2--1--79 1 Nov 2004 2--1--80 1 Nov 2004 2--1--81 1 Nov 2004 2--1--82 1 Nov 2004 2--1--83 1 Nov 2004 2--1--84 1 Nov 2004 2--1--85 1 Nov 2004 2--1--86 1 Nov 2004 2--1--87 1 Nov 2004 2--1--88 1 Nov 2004 2--1--89 1 Nov 2004 2--1--90 1 Nov 2004 2--1--91 1 Nov 2004 2--1--92 1 Nov 2004 2--1--93 1 Nov 2004 2--1--94 1 Nov 2004 2--1--95 1 Nov 2004 2--1--96 1 Nov 2004 2--1--97 1 Nov 2004 2--1--98 1 Nov 2004 2--1--99 1 Nov 2004 2--1--100 1 Nov 2004 2--1--101 1 Nov 2004 2--1--102 1 Nov 2004 2--1--103 1 Nov 2004 2--1--104 1 Nov 2004 2--1--105 1 Nov 2004 2--1--106 1 Nov 2004 2--1--107 1 Nov 2004 2--1--108 1 Nov 2004 2--1--109 1 Nov 2004 2--1--110 1 Nov 2004 2--1--111 1 Nov 2004 2--1--112 1 Nov 2004 2--1--113 1 Nov 2004 2--1--114 1 Nov 2004 2--1--115 1 Nov 2004 2--1--116 1 Nov 2004 2--1--117 1 Nov 2004 2--1--118 1 Nov 2004 2--1--119 1 Nov 2004 2--1--120 1 Nov 2004 2--1--121 1 Nov 2004 2--1--122 1 Nov 2004 2--1--123 1 Nov 2004 2--1--124 1 Nov 2004 2--1--125 1 Nov 2004 2--1--126 1 Nov 2004 ADZ--950 Micro Air Data System 2--2--1 1 Nov 2004 2--2--2 1 Nov 2004 2--2--3 1 Nov 2004 2--2--4 1 Nov 2004 F 2--2--5/2--2--6 1 Nov 2004 F 2--2--7/2--2--8 1 Nov 2004 2--2--9 1 Nov 2004 2--2--10 1 Nov 2004 2--2--11 1 Nov 2004 2--2--12 1 Nov 2004 2--2--13 1 Nov 2004 2--2--14 1 Nov 2004 2--2--15 1 Nov 2004 2--2--16 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--4 Subheading and Page Date Subheading and Page Date PRIMUS 880 Weather Radar System 2--3--1 1 Nov 2004 2--3--2 1 Nov 2004 2--3--3 1 Nov 2004 2--3--4 1 Nov 2004 2--3--5 1 Nov 2004 2--3--6 1 Nov 2004 2--3--7 1 Nov 2004 2--3--8 1 Nov 2004 2--3--9 1 Nov 2004 2--3--10 1 Nov 2004 2--3--11 1 Nov 2004 2--3--12 1 Nov 2004 2--3--13 1 Nov 2004 2--3--14 1 Nov 2004 2--3--15 1 Nov 2004 2--3--16 1 Nov 2004 F 2--3--17/2--3--18 1 Nov 2004 2--3--19 1 Nov 2004 2--3--20 1 Nov 2004 2--3--21 1 Nov 2004 2--3--22 1 Nov 2004 2--3--23 1 Nov 2004 2--3--24 1 Nov 2004 2--3--25 1 Nov 2004 2--3--26 1 Nov 2004 2--3--27 1 Nov 2004 2--3--28 1 Nov 2004 PRIMUS II Integrated Radio System 2--4--1 1 Nov 2004 2--4--2 1 Nov 2004 2--4--3 1 Nov 2004 2--4--4 1 Nov 2004 2--4--5 1 Nov 2004 2--4--6 1 Nov 2004 2--4--7 1 Nov 2004 2--4--8 1 Nov 2004 2--4--9 1 Nov 2004 2--4--10 1 Nov 2004 2--4--11 1 Nov 2004 2--4--12 1 Nov 2004 2--4--13 1 Nov 2004 2--4--14 1 Nov 2004 2--4--15 1 Nov 2004 2--4--16 1 Nov 2004 2--4--17 1 Nov 2004 2--4--18 1 Nov 2004 2--4--19 1 Nov 2004 2--4--20 1 Nov 2004 2--4--21 1 Nov 2004 2--4--22 1 Nov 2004 2--4--23 1 Nov 2004 2--4--24 1 Nov 2004 F 2--4--25/2--4--26 1 Nov 2004 2--4--27 1 Nov 2004 2--4--28 1 Nov 2004 F 2--4--29/2--4--30 1 Nov 2004 F 2--4--31/2--4--32 1 Nov 2004 2--4--33 1 Nov 2004 2--4--34 1 Nov 2004 F 2--4--35/2--4--36 1 Nov 2004 F 2--4--37/2--4--38 1 Nov 2004 F 2--4--39/2--4--40 1 Nov 2004 2--4--41 1 Nov 2004 2--4--42 1 Nov 2004 F 2--4--43/2--4--44 1 Nov 2004 F 2--4--45/2--4--46 1 Nov 2004 2--4--47 1 Nov 2004 2--4--48 1 Nov 2004 F 2--4--49/2--4--50 1 Nov 2004 F 2--4--51/2--4--52 1 Nov 2004 2--4--53 1 Nov 2004 2--4--54 1 Nov 2004 2--4--55 1 Nov 2004 2--4--56 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--5 Subheading and Page Date Subheading and Page Date Flight Guidance System 2--5--1 1 Nov 2004 2--5--2 1 Nov 2004 2--5--3 1 Nov 2004 2--5--4 H 11 May 2007 2--5--5 1 Nov 2004 2--5--6 1 Nov 2004 2--5--7 1 Nov 2004 2--5--8 1 Nov 2004 2--5--9 1 Nov 2004 2--5--10 1 Nov 2004 2--5--11 1 Nov 2004 2--5--12 1 Nov 2004 2--5--13 1 Nov 2004 2--5--14 1 Nov 2004 2--5--15 1 Nov 2004 2--5--16 1 Nov 2004 2--5--17 1 Nov 2004 2--5--18 1 Nov 2004 2--5--19 1 Nov 2004 2--5--20 1 Nov 2004 F 2--5--21/2--5--22 1 Nov 2004 2--5--23 1 Nov 2004 2--5--24 1 Nov 2004 F 2--5--25/2--5--26 1 Nov 2004 2--5--27 1 Nov 2004 2--5--28 1 Nov 2004 2--5--29 1 Nov 2004 2--5--30 1 Nov 2004 2--5--31 1 Nov 2004 2--5--32 1 Nov 2004 2--5--33 1 Nov 2004 2--5--34 1 Nov 2004 2--5--35 1 Nov 2004 2--5--36 1 Nov 2004 2--5--37 1 Nov 2004 2--5--38 1 Nov 2004 2--5--39 1 Nov 2004 2--5--40 1 Nov 2004 2--5--41 1 Nov 2004 2--5--42 1 Nov 2004 2--5--43 1 Nov 2004 2--5--44 1 Nov 2004 2--5--45 1 Nov 2004 2--5--46 1 Nov 2004 2--5--47 1 Nov 2004 2--5--48 1 Nov 2004 2--5--49 1 Nov 2004 2--5--50 1 Nov 2004 2--5--51 1 Nov 2004 2--5--52 1 Nov 2004 2--5--53 1 Nov 2004 2--5--54 1 Nov 2004 2--5--55 1 Nov 2004 2--5--56 1 Nov 2004 2--5--57 1 Nov 2004 2--5--58 1 Nov 2004 2--5--59 1 Nov 2004 2--5--60 1 Nov 2004 2--5--61 1 Nov 2004 2--5--62 1 Nov 2004 2--5--63 1 Nov 2004 2--5--64 1 Nov 2004 2--5--65 1 Nov 2004 2--5--66 1 Nov 2004 F 2--5--67/2--5--68 1 Nov 2004 2--5--69 1 Nov 2004 2--5--70 1 Nov 2004 F 2--5--71/2--5--72 1 Nov 2004 2--5--73 1 Nov 2004 2--5--74 1 Nov 2004 2--5--75 1 Nov 2004 2--5--76 1 Nov 2004 2--5--77 1 Nov 2004 2--5--78 1 Nov 2004 2--5--79 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--6 Subheading and Page Date Subheading and Page Date 2--5--80 1 Nov 2004 2--5--81 1 Nov 2004 2--5--82 1 Nov 2004 2--5--83 1 Nov 2004 2--5--84 1 Nov 2004 2--5--85 1 Nov 2004 2--5--86 1 Nov 2004 2--5--87 1 Nov 2004 2--5--88 1 Nov 2004 2--5--89 1 Nov 2004 2--5--90 1 Nov 2004 2--5--91 1 Nov 2004 2--5--92 1 Nov 2004 2--5--93 1 Nov 2004 2--5--94 1 Nov 2004 2--5--95 1 Nov 2004 2--5--96 1 Nov 2004 2--5--97 1 Nov 2004 2--5--98 1 Nov 2004 2--5--99 1 Nov 2004 2--5--100 1 Nov 2004 2--5--101 1 Nov 2004 2--5--102 1 Nov 2004 2--5--103 1 Nov 2004 2--5--104 1 Nov 2004 2--5--105 1 Nov 2004 2--5--106 1 Nov 2004 2--5--107 1 Nov 2004 2--5--108 1 Nov 2004 2--5--109 1 Nov 2004 2--5--110 1 Nov 2004 Autopilot/Yaw Damper System 2--6--1 1 Nov 2004 2--6--2 1 Nov 2004 2--6--3 1 Nov 2004 2--6--4 H 11 May 2007 2--6--5 1 Nov 2004 2--6--6 1 Nov 2004 2--6--7 1 Nov 2004 2--6--8 1 Nov 2004 2--6--9 1 Nov 2004 2--6--10 1 Nov 2004 2--6--11 1 Nov 2004 2--6--12 1 Nov 2004 F 2--6--13/2--6--14 1 Nov 2004 2--6--15 1 Nov 2004 2--6--16 1 Nov 2004 2--6--17 1 Nov 2004 2--6--18 1 Nov 2004 F 2--6--19/2--6--20 1 Nov 2004 2--6--21 1 Nov 2004 2--6--22 1 Nov 2004 2--6--23 1 Nov 2004 2--6--24 1 Nov 2004 F 2--6--25/2--6--26 1 Nov 2004 2--6--27 1 Nov 2004 2--6--28 1 Nov 2004 2--6--29 1 Nov 2004 2--6--30 1 Nov 2004 F 2--6--31/2--6--32 1 Nov 2004 2--6--33 1 Nov 2004 2--6--34 1 Nov 2004 2--6--35 1 Nov 2004 2--6--36 1 Nov 2004 F 2--6--37/2--6--38 1 Nov 2004 2--6--39 1 Nov 2004 2--6--40 1 Nov 2004 2--6--41 1 Nov 2004 2--6--42 1 Nov 2004 Enhanced Ground Proximity Warning System 2--7--1 1 Nov 2004 2--7--2 1 Nov 2004 F 2--7--3/2--7--4 1 Nov 2004 2--7--5 1 Nov 2004 2--7--6 1 Nov 2004 2--7--7 1 Nov 2004 2--7--8 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--7 Subheading and Page Date Subheading and Page Date Traffic Alert and Collision Avoidance System 2--8--1 1 Nov 2004 2--8--2 1 Nov 2004 2--8--3 1 Nov 2004 2--8--4 1 Nov 2004 AA--300 Radio Altimeter System 2--9--1 1 Nov 2004 2--9--2 1 Nov 2004 2--9--3 1 Nov 2004 2--9--4 1 Nov 2004 2--9--5 1 Nov 2004 2--9--6 1 Nov 2004 2--9--7 1 Nov 2004 2--9--8 1 Nov 2004 System Interconnect 3--1 1 Nov 2004 3--2 1 Nov 2004 Maintenance Practices 4--1 1 Nov 2004 4--2 1 Nov 2004 4--3 1 Nov 2004 4--4 1 Nov 2004 4--5 1 Nov 2004 4--6 1 Nov 2004 4--7 1 Nov 2004 4--8 1 Nov 2004 4--9 1 Nov 2004 4--10 1 Nov 2004 4--11 1 Nov 2004 4--12 1 Nov 2004 4--13 H 11 May 2007 4--14 H 11 May 2007 4--14.1 H 11 May 2007 4--14.2 H 11 May 2007 4--15 1 Nov 2004 4--16 1 Nov 2004 4--17 1 Nov 2004 4--18 1 Nov 2004 4--19 1 Nov 2004 4--20 1 Nov 2004 4--21 1 Nov 2004 4--22 1 Nov 2004 4--23 1 Nov 2004 4--24 1 Nov 2004 Shipping/Handling and Storage 5--1 1 Nov 2004 5--2 1 Nov 2004 Honeywell Support 6--1 1 Nov 2004 6--2 1 Nov 2004 6--3 1 Nov 2004 6--4 1 Nov 2004 6--5 1 Nov 2004 6--6 1 Nov 2004 System Test and Fault Isolation 7--1 1 Nov 2004 7--2 1 Nov 2004 H indicates a changed page. F indicates a foldout page. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP--8 Blank Page RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--1 TABLE OF CONTENTS Subject Page INTRODUCTION INTRO--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. How to Use This Manual INTRO--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General INTRO--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. How This Manual Is Organized INTRO--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Weights and Measurements INTRO--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Customer Support INTRO--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Honeywell Aerospace Online Technical Publications Web Site INTRO--3 . . . . . . . . . . . B. Customer Response Center (CRC) INTRO--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. References INTRO--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Honeywell Publications INTRO--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Other Publications INTRO--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4. Acronyms and Abbreviations INTRO--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 1 SYSTEM OVERVIEW 1--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 1--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 1--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. System Description 1--16 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 1--16 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Electronic Display System 1--16 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. ADZ--950 Micro Air Data System 1--17 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. PRIMUS 880 Weather Radar System 1--18 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. PRIMUS II Integrated Radio System 1--18 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. Flight Guidance System 1--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. Autopilot/Yaw Damper System 1--20 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . H. Enhanced Ground Proximity Warning System 1--21 . . . . . . . . . . . . . . . . . . . . . . . . . . I. Traffic Alert and Collision Avoidance System 1--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . J. AA--300 Radio Altimeter System 1--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . K. LSZ--860 Lightning Sensor System (Optional) 1--21 . . . . . . . . . . . . . . . . . . . . . . . . . . L. KFH--1050 HF Communication System (Optional) 1--22 . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--2 Subject Page 3. Digital Data Buses 1--22 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 1--22 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. RSB 1--22 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Digital Audio Bus 1--26 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. CDSB 1--28 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. ARINC 429 1--28 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. RS--422 1--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. RS--232 1--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . H. SCI 1--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . I. WXPD 1--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . J. ICB 1--34 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . K. Symbol Generator/Display Unit Bus 1--34 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2 SYSTEM DESCRIPTION 2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--1 ELECTRONIC DISPLAY SYSTEM 2--1--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--1--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--1--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Descriptions and Locations 2--1--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. IC--615 IAC 2--1--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. DU--1080 DUs 2--1--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. DC--550 Display Controller 2--1--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. RI--553 Remote Instrument Controller 2--1--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. RI-552 Remote Instrument Controller 2--1--13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. MC--800 MFD Controller 2--1--14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--1--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. EDS Bus Interfaces 2--1--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. AHRS Interface 2--1--30 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. PFD 2--1--48 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. MFD 2--1--92 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--3 Subject Page 4. Fault Monitoring and Display System Reversionary Modes 2--1--123 . . . . . . . . . . . . . . . . . . A. General 2--1--123 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. DU-1080 Display Unit Failure 2--1--124 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. DC-550 Display Controller Failures 2--1--125 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. MC-800 MFD Controller Failure 2--1--125 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. DC-550 Display Controller Power-Up Defaults 2--1--126 . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--2 ADZ-950 MICRO AIR DATA SYSTEM 2--2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Descriptions and Locations 2--2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. AZ-950 MADC 2--2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--2--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Pilot’s Air Data System 2--2--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Copilot’s Air Data System 2--2--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Modes of Operation 2--2--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. MADC Monitoring 2--2--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. SSEC 2--2--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. Operational Range 2--2--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. Overspeed Warning 2--2--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4. Fault Monitoring 2--2--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--2--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. PFD 2--2--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. MFD 2--2--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--3 PRIMUS 880 WEATHER RADAR SYSTEM 2--3--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--3--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--3--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Descriptions and Locations 2--3--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. WU-880 Weather Radar RTA 2--3--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. WC-880 Weather Radar Controller 2--3--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--4 Subject Page 3. Operation 2--3--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Introduction 2--3--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Weather Radar System Functions 2--3--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Mode and Warning Annunciations 2--3--14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. Hidden Modes 2--3--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. PRIMUS 880 Weather Radar Interface Diagram 2--3--16 . . . . . . . . . . . . . . . . . . . . . . . . 4. Fault Monitoring 2--3--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--3--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. PFD 2--3--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. MFD 2--3--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. PRIMUS 880 Weather Radar Test Mode 2--3--22 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--4 PRIMUS II INTEGRATED RADIO SYSTEM 2--4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Descriptions and Locations 2--4--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. RM--850 RMU 2--4--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. CD--850 CDH 2--4--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. DI--851 DME Indicator 2--4--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. AV--850A Audio Panel 2--4--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. RCZ--851E Integrated COM Unit 2--4--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. RNZ--850/RNZ--850B Integrated NAV Unit 2--4--17 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. AT--860 ADF Combined Sense/Loop Antenna 2--4--19 . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--4--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Introduction 2--4--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. RM--850 RMU Interface 2--4--23 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. CD--850 CDH Interface 2--4--27 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. DI--851 DME Indicator Interface 2--4--27 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. AV--850A Audio Panel Interface 2--4--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. RCZ--851E Integrated COM Unit Interface 2--4--41 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. RNZ--850/850B Integrated NAV Unit Interface 2--4--47 . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--5 Subject Page 4. Fault Monitoring 2--4--53 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--4--53 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. PFD Indications 2--4--53 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. RMU Display 2--4--55 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--5 FLIGHT GUIDANCE SYSTEM 2--5--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--5--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--5--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Flight Director Data Management 2--5--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Flight Director Couple Switching 2--5--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. Flight Director Mode Annunciator 2--5--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. Master/Slave Air Data Target Switching 2--5--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. Flight Director Command Bar Logic 2--5--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. ASEL Function 2--5--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Descriptions and Locations 2--5--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. IC--615 IAC 2--5--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. MS-560 Mode Selector 2--5--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. DC-550 Display Controller 2--5--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. RI-553 Remote Instrument Controller 2--5--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. RI-552 Remote Instrument Controller 2--5--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. PC-400 Autopilot Controller 2--5--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--5--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Flight Director Functions 2--5--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Flight Director Lateral (Roll) Channel Functional Operation 2--5--15 . . . . . . . . . . . . . . C. Flight Director Vertical (Pitch) Channel Functional Operation 2--5--61 . . . . . . . . . . . . . 4. Fault Monitoring 2--5--110 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--5--110 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--6 AUTOPILOT/YAW DAMPER SYSTEM 2--6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Autopilot 2--6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--6 Subject Page C. Yaw Damper 2--6--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. Autopilot/Yaw Damper System 2--6--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Descriptions and Locations 2--6--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. IC--615 IAC 2--6--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. PC--400 Autopilot Controller 2--6--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. SM--200 Servo Drive and SB--201 Servo Bracket 2--6--6 . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--6--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--6--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Modes of Operation 2--6--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Autopilot/Yaw Damper Engage Logic 2--6--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. Roll Axis Autopilot Servo Loop 2--6--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. Pitch Axis Autopilot Servo Loop 2--6--27 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. Pitch Axis Autopilot Trim 2--6--29 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. Rudder Axis Yaw Damper Servo Loop 2--6--34 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4. Fault Monitoring 2--6--39 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Autopilot/Yaw Damper Monitoring Overview 2--6--39 . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Hardover/Slowover Malfunction Protection 2--6--39 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. System Response to Failures 2--6--39 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D. Monitor Description 2--6--40 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--7 ENHANCED GROUND PROXIMITY WARNING SYSTEM 2--7--1 . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Description and Location 2--7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. EGPWS Computer 2--7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--7--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. System Operation 2--7--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Modes 2--7--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--7 Subject Page SECTION 2--8 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM 2--8--1 . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--8--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--8--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Location and Description 2--8--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. TCAS II Computer 2--8--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. TCAS Top and Bottom Antennas 2--8--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--8--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. System Operation 2--8--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 2--9 AA--300 RADIO ALTIMETER SYSTEM 2--9--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 2--9--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 2--9--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Component Description and Location 2--9--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. RT--300 Radio Altimeter Receiver Transmitter 2--9--1 . . . . . . . . . . . . . . . . . . . . . . . . . . B. AT--300 Radio Altimeter Antenna 2--9--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Operation 2--9--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Introduction 2--9--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Modes of Operation 2--9--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4. Fault Monitoring 2--9--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. PFD Fault Indications 2--9--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 3 SYSTEM INTERCONNECT 3--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 3--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 3--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 4 MAINTENANCE PRACTICES 4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Antenna Information 4--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--8 Subject Page 2. Equipment and Materials 4--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 4--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Equipment 4--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Materials 4--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Procedure for the AZ--950 MADC 4--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4. Procedure for the RM--855 RMU 4--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5. Procedure for the RNZ--850/850B Integrated NAV Unit 4--5 . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6. Procedure for the RNZ--850/RCZ--851E Strap Board Assembly 4--9 . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7. Procedure for the DC--550 Display Controller 4--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8. Procedure for the IC--615 IAC 4--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Checklist Loading Procedures 4--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9. Procedure for the MC--800 MFD Controller 4--14.1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--14.1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--14.1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--14.2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--9 Subject Page 10. Procedure for the MS--560 Mode Selector 4--14.2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--14.2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11. Procedure for the PC--400 Autopilot Controller 4--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--16 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12. Procedure for the RI--552 and RI--553 Remote Instrument Controllers 4--17 . . . . . . . . A. Removal and Installation Procedures 4--17 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--17 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--17 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13. Procedure for the SM--200 Servo Drive and SB--201 Drum and Bracket Assembly 4--18 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--18 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14. Procedure for the WC--880 Weather Radar Controller 4--20 . . . . . . . . . . . . . . . . . . . . . . . A. Removal and Installation Procedures 4--20 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--20 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Repair Procedures 4--20 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15. Procedure for the WU--880 Antenna and Receiver Transmitter Unit 4--21 . . . . . . . . . . . A. Removal and Installation Procedures 4--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Adjustment Procedures 4--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 5 SHIPPING/HANDLING AND STORAGE 5--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Overview 5--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 5--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 6 HONEYWELL SUPPORT 6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Worldwide Exchange/Rental Program for Corporate Operators 6--1 . . . . . . . . . . . . . . . A. General 6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B. Exchange 6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C. Rental 6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--10 Subject Page D. Warranty 6--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E. Warranty Statement 6--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F. Routine Repair Piece Part Orders 6--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G. Exchange and Rental Ordering 6--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . H. Ordering Information 6--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . I. Return Shipping Procedures 6--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. Test Equipment 6--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. Special Test Equipment 6--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3. Customer Engineering 6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4. Training 6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5. Honeywell Product Support Centers 6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION 7 SYSTEM TEST AND FAULT ISOLATION 7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1. Test and Fault Isolation 7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A. General 7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--11 List of Illustrations Figure Page Figure 1-1. PRIMUS 1000 Integrated Avionics System Flow Diagram 1--7 . . . . . . . . Figure 1-2. Cessna Citation XLS Cockpit Layout 1--9 . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-3. Cessna Citation XLS Component Locations 1--15 . . . . . . . . . . . . . . . . . . . . Figure 1-4. Radio System Bus 1--23 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-5. RSB Data Field Structure 1--26 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-6. Digital Audio Data Sequence 1--28 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-7. Octal Label 274 1--29 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-8. Data Field (Bits 11 thru 29) 1--29 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-9. BCD Bit Assignments 1--30 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-10. Selected Course Data Word 1--30 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-11. DME Distance Data Word 1--31 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-12. Present Position Longitude Data Word 1--31 . . . . . . . . . . . . . . . . . . . . . . . . Figure 1-13. ARINC 429 Transmission Waveforms 1--32 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--1. IC--615 IAC 2--1--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--2. DU--1080 Display Unit 2--1--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--3. DC--550 Display Controller 2--1--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--4. RI--553 Remote Instrument Controller 2--1--11 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--5. RI-552 Remote Instrument Controller 2--1--13 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--6. MC--800 MFD Controller Without TCAS 2--1--14 . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--7. MC--800 MFD Controller With TCAS 2--1--14 . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--8. Display Bus Interface 2--1--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--9. DC--IC Data Bus 2--1--23 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--10. DU Status and Wraparound 2--1--24 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--11. Reversionary Interconnect 2--1--27 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--12. Weather Radar Control and Picture Buses 2--1--28 . . . . . . . . . . . . . . . . . . . . . Figure 2--1--13. IC--IC Bus/RS--232 Cabin Interface 2--1--30 . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--14. AHRS (Pilot) Interface 2--1--31 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--15. AHRS (Copilot) Interface 2--1--31 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--16. Navigation Receiver to IC--615 IAC Interface 2--1--34 . . . . . . . . . . . . . . . . . . . Figure 2--1--17. DME to IC--615 IAC Interface 2--1--35 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--18. Radio Altimeter Interface 2--1--36 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--19. LRN Interface 2--1--37 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--12 List of Illustrations (cont) Figure Page Figure 2--1--20. MADC Interface 2--1--39 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--21. DC--550 Display Controller Interface (Pilot’s) 2--1--43 . . . . . . . . . . . . . . . . . . . Figure 2--1--22. DC--550 Display Controller Interface (Copilot’s) 2--1--45 . . . . . . . . . . . . . . . . . Figure 2--1--23. RI--553 to DC--550 Interface 2--1--47 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--24. MC--800 MFD Controller Interface 2--1--48 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--25. PFD Functional Divisions 2--1--49 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--26. PFD ADI Displays and Annunciators 2--1--51 . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--27. ADI Pitch Scale 2--1--56 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--28. HSI Compass Display on PFD 2--1--63 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--29. HSI Partial Compass Format 2--1--71 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--30. Airspeed Display 2--1--76 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--31. Altitude Display 2--1--79 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--32. Vertical Speed Display 2--1--82 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--33. Full Test Mode With Failure Flags 2--1--88 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--34. Arc Test Mode With Failure Flags 2--1--89 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--35. PFD Failure Flags and Annunciators 2--1--90 . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--36. MFD Functional Divisions 2--1--93 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--37. MFD Map Display 2--1--95 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--38. MFD Map Mode With Weather Display 2--1--100 . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--39. MFD Failure and Warning Displays 2--1--104 . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--40. MFD Plan Mode Format 2--1--107 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--41. MFD Plan Format Failure Displays 2--1--109 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--42. Typical Checklist Display 2--1--111 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--43. MFD TCAS Display Symbols 2--1--112 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--44. Top Level MFD Menu Page 2--1--117 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--45. VNAV Submenu Page 2--1--118 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--46. T/O SPEEDS Submenu Page 2--1--120 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--1--47. LNDG SPEEDS Submenu Page 2--1--121 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--2--1. AZ--950 MADC 2--2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--2--2. Pilot’s MADC Interface 2--2--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--2--3. Copilot’s MADC Interface 2--2--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--2--4. Vmo/Mmo Curve 2--2--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--13 List of Illustrations (cont) Figure Page Figure 2--2--5. PFD MADC Failure Indications 2--2--14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--2--6. MFD Map Mode MADC Failure Indications 2--2--15 . . . . . . . . . . . . . . . . . . . . . Figure 2--3--1. WU--880 Weather Radar RTA 2--3--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--3--2. MPEL Boundary 2--3--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--3--3. WC-880 Weather Radar Controller 2--3--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--3--4. PRIMUS 880 Weather Radar System Interface Diagram 2--3--17 . . . . . . . . . Figure 2--3--5. PFD Weather Radar Failure Indication 2--3--20 . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--3--6. MFD Weather Radar Failure Indication 2--3--21 . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--3--7. PRIMUS 880 MFD Weather Radar Test Mode Indications 2--3--24 . . . . . . . Figure 2--4--1. Typical RM--850 RMU 2--4--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--2. CD--850 CDH 2--4--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--3. DI--851 DME Indicator 2--4--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--4. AV--850A Audio Panel 2--4--13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--5. RCZ--851E Integrated COM Unit 2--4--16 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--6. RNZ--850/850B Integrated NAV Unit 2--4--18 . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--7. AT--860 ADF Antenna 2--4--20 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--8. Radio System Data Buses 2--4--22 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--9. RMU Interface Diagram 2--4--25 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--10. CD--850 CDH Interface Diagram 2--4--29 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--11. DME Indicator Interface Diagram 2--4--31 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--12. AV--850A Audio Panel Interface Diagram 2--4--35 . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--13. RCZ--851E Integrated COM Unit Interface Diagram 2--4--43 . . . . . . . . . . . . . Figure 2--4--14. RNZ--850/850B NAV Unit Interface Diagram 2--4--49 . . . . . . . . . . . . . . . . . . . Figure 2--4--15. PFD Radio System Failure Indications 2--4--54 . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--4--16. RMU Failure Indications 2--4--55 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--1. IC--615 IAC (FD Function) 2--5--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--2. MS-560 Mode Selector 2--5--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--3. DC-550 Display Controller 2--5--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--4. RI-553 Remote Instrument Controller 2--5--8 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--5. RI-552 Remote Instrument Controller 2--5--10 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--6. PC-400 Autopilot Controller 2--5--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--7. Flight Director Lateral Mode Interface -- Pilot’s Side 2--5--21 . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--14 List of Illustrations (cont) Figure Page Figure 2--5--8. Flight Director Lateral Mode Interface - Copilot’s Side 2--5--25 . . . . . . . . . . . Figure 2--5--9. VOR Arm Pictorial 2--5--30 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--10. VOR (NAV) Mode Armed 2--5--31 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--11. VOR Capture Pictorial 2--5--32 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--12. VOR (NAV) Mode Capture 2--5--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--13. VOR Course Cut Limiting 2--5--34 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--14. VOR Track 2--5--35 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--15. VOR Over Station 2--5--37 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--16. Localizer Arm Pictorial 2--5--43 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--17. Localizer (NAV) Mode Arm 2--5--44 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--18. Localizer Capture Pictorial 2--5--45 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--19. Localizer Capture 2--5--46 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--20. Localizer Track Profile View 2--5--47 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--21. Localizer Track 2--5--48 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--22. Back Course Mode Pictorial 2--5--49 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--23. Back Course Arm 2--5--50 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--24. Back Course Capture 2--5--51 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--25. Back Course Track 2--5--52 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--26. LNAV Capture and Tracking Pictorial 2--5--57 . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--27. LNAV Tracking 2--5--58 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--28. Flight Director Vertical Mode Interface - Pilot’s Side 2--5--67 . . . . . . . . . . . . . Figure 2--5--29. Flight Director Vertical Mode Interface - Copilot’s Side 2--5--71 . . . . . . . . . . . Figure 2--5--30. Vertical Speed Hold Mode 2--5--75 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--31. Flight Level Change Mode 2--5--79 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--32. ASEL Mode Pictorial 2--5--84 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--33. Prior to Descent -- Altitude Hold Mode 2--5--86 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--34. During Descent -- ASEL Armed Mode 2--5--87 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--35. Start of Flare -- ASEL Capture 2--5--88 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--36. Level at New Altitude -- Altitude Hold Mode 2--5--89 . . . . . . . . . . . . . . . . . . . . Figure 2--5--37. ALT Hold Mode 2--5--94 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--38. ILS Approach (LOC/GS) Arm Pictorial 2--5--95 . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--39. ILS Approach (LOC/GS) Arm 2--5--96 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--15 List of Illustrations (cont) Figure Page Figure 2--5--40. ILS Approach Mode -- Localizer Capture 2--5--97 . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--41. ILS Glideslope Tracking Pictorial 2--5--98 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--42. ILS Glideslope Tracking 2--5--99 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--43. ILS Glideslope Gain Programming 2--5--100 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--44. VNAV Mode Menu Select 2--5--104 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--45. VNAV Preselect Plan View 2--5--105 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--46. Go--Around Mode 2--5--108 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--5--47. Flight Director Failure Indications 2--5--110 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--1. IC--615 IAC (Autopilot Function) 2--6--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--2. PC--400 Autopilot Controller 2--6--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--3. SM--200 Servo Drive and SB--201 Servo Bracket 2--6--7 . . . . . . . . . . . . . . . Figure 2--6--4. Autopilot/Yaw Damper Interface 2--6--13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--5. Autopilot/Yaw Damper Engage/Disengage Logic 2--6--19 . . . . . . . . . . . . . . . Figure 2--6--6. Servo Amplifier Drive Enable 2--6--21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--7. Autopilot Roll Axis Servo Loop 2--6--25 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--8. Autopilot Pitch Axis Servo Loop 2--6--31 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--6--9. Autopilot Yaw Damper Servo Loop 2--6--37 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--7--1. EGPWS Computer 2--7--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--7--2. EGPWS Block Diagram 2--7--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--8--1. TCAS II Computer 2--8--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--8--2. TCAS Antenna 2--8--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--9--1. RT--300 Radio Altimeter Receiver Transmitter 2--9--1 . . . . . . . . . . . . . . . . . . Figure 2--9--2. AT--300 Radio Altimeter Antenna 2--9--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 2--9--3. Radio Altimeter System Interface 2--9--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 4-1. NAV Unit Adjustment Locations 4--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 4-2. Checklist Loading Page 4--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Figure 4-3. IC--615 Battery Cover Location 4--14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--16 List of Tables Table Page Table 1-1. System Components 1--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 1-2. Optional System Components 1--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 1-3. RSB Message Numbers (Normal Mode) 1--11 . . . . . . . . . . . . . . . . . . . . . . . Table 1-4. Sign Status Matrix Bit Assignments 1--31 . . . . . . . . . . . . . . . . . . . . . . . . . . Table 1-5. Transmission Waveform Voltages 1--33 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2-1. System Description Subsections 2--1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--1. IC--615 IAC Leading Particulars 2--1--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--2. DU--1080 Display Unit Configurations 2--1--5 . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--3. DU--1080 Display Unit Leading Particulars 2--1--5 . . . . . . . . . . . . . . . . . . . . Table 2--1--4. DC--550 Display Controller Leading Particulars 2--1--7 . . . . . . . . . . . . . . . . Table 2--1--5. PFD Selections With DC-550 Display Controller Invalid 2--1--8 . . . . . . . . . Table 2--1--6. Bearing Sources 2--1--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--7. RI--553 Remote Instrument Controller Leading Particulars 2--1--11 . . . . . . Table 2--1--8. RI-552 Remote Instrument Controller Leading Particulars 2--1--13 . . . . . . . Table 2--1--9. MC--800 MFD Controller Leading Particulars 2--1--15 . . . . . . . . . . . . . . . . . . Table 2--1--10. Reversionary Control 2--1--25 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--11. Power-Up Priority Assignment 2--1--30 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--12. Radio System Bus Interface 2--1--32 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--13. DME Data from Dual and Single DME Systems 2--1--33 . . . . . . . . . . . . . . . . Table 2--1--14. LRN ARINC 429 Output Word Labels 2--1--37 . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--15. IAC ARINC 429 Transmitter Outputs 2--1--38 . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--16. Air Data ARINC 429 Output Word Labels 2--1--41 . . . . . . . . . . . . . . . . . . . . . Table 2--1--17. Lateral Mode Annunciators 2--1--53 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--18. Vertical Mode Annunciators 2--1--53 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--19. Autopilot Status Annunciations 2--1--54 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--20. Vertical Deviation Scale 2--1--57 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--21. Marker Beacons 2--1--57 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--22. Onside Source Mode Annunciators 2--1--59 . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--23. Comparison Monitor Annunciators 2--1--61 . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--24. Heading Source Annunciators 2--1--64 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--25. Bearing Sources 2--1--66 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--26. Lateral Deviation Scale 2--1--67 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--17 List of Tables (cont) Table Page Table 2--1--27. Weather Annunciators 2--1--72 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--28. Selectable Radar Ranges 2--1--74 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--29. Weather Radar Return Color Code 2--1--74 . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--30. Vspeed Bug Parameters 2--1--77 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--31. TCAS Status Messages (PFD) 2--1--85 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--32. Selectable MFD Control Ranges 2--1--101 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--33. Weather Radar Mode Annunciations on MFD 2--1--102 . . . . . . . . . . . . . . . . . . Table 2--1--34. MFD Weather Radar Color Code 2--1--103 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--35. Fan Failure Warning Messages 2--1--104 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--36. IC Overheat Warning Messages 2--1--105 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--37. DU Wraparound Failure Warning Messages 2--1--105 . . . . . . . . . . . . . . . . . . . Table 2--1--38. Traffic Symbols 2--1--113 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--39. MFD TCAS Messages 2--1--116 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--40. VNAV Data Parameters 2--1--118 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--41. T/O Vspeed Data Parameters 2--1--120 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--42. LNDG Vspeed Data Parameters 2--1--122 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--43. Attitude Reversionary Switch Functions 2--1--123 . . . . . . . . . . . . . . . . . . . . . . . Table 2--1--44. Heading Reversionary Switch Functions 2--1--124 . . . . . . . . . . . . . . . . . . . . . . Table 2--1--45. Air Data Computer Reversionary Switch Functions 2--1--124 . . . . . . . . . . . . . Table 2--2--1. AZ-950 MADC Leading Particulars 2--2--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--2--2. AZ-950 MADC Performance Accuracy 2--2--9 . . . . . . . . . . . . . . . . . . . . . . . . Table 2--2--3. MADC Functional Test Outputs 2--2--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--3--1. WU--880 Weather Radar RTA Leading Particulars 2--3--2 . . . . . . . . . . . . . . Table 2--3--2. WC-880 Weather Radar Controller Leading Particulars 2--3--6 . . . . . . . . . Table 2--3--3. Target Intensity Levels 2--3--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--3--4. Target Alert Range and Depth 2--3--13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--3--5. PFD and MFD WX Mode and Warning Annunciators 2--3--14 . . . . . . . . . . . Table 2--3--6. Hidden Modes 2--3--15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--3--7. PRIMUS 880 Fault Codes 2--3--25 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--4--1. RM--850 RMU Leading Particulars 2--4--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--4--2. CD--850 CDH Leading Particulars 2--4--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--4--3. DI--851 DME Indicator Leading Particulars 2--4--11 . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--18 List of Tables (cont) Table Page Table 2--4--4. Parameter Display and Select 2--4--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--4--5. AV--850A Audio Panel Leading Particulars 2--4--13 . . . . . . . . . . . . . . . . . . . . Table 2--4--6. RCZ--851E Integrated COM Unit Leading Particulars 2--4--16 . . . . . . . . . . . Table 2--4--7. RNZ--850/850B Integrated NAV Unit Leading Particulars 2--4--18 . . . . . . . . Table 2--4--8. AT--860 ADF Antenna Leading Particulars 2--4--20 . . . . . . . . . . . . . . . . . . . . Table 2--5--1. IC--615 IAC Leading Particulars 2--5--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--2. MS-560 Mode Selector Leading Particulars 2--5--6 . . . . . . . . . . . . . . . . . . . Table 2--5--3. DC-550 Display Controller Leading Particulars 2--5--7 . . . . . . . . . . . . . . . . . Table 2--5--4. RI-553 Remote Instrument Controller Leading Particulars 2--5--9 . . . . . . . Table 2--5--5. RI-552 Remote Instrument Controller Leading Particulars 2--5--10 . . . . . . . Table 2--5--6. PC-400 Autopilot Controller Leading Particulars 2--5--11 . . . . . . . . . . . . . . . Table 2--5--7. Heading Select Mode Operating Limits 2--5--28 . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--8. VOR/VOR Approach Mode Operating Limits 2--5--38 . . . . . . . . . . . . . . . . . . Table 2--5--9. Localizer and Back Course Mode Operating Limits 2--5--53 . . . . . . . . . . . . . Table 2--5--10. LNAV Mode Operating Limits 2--5--57 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--11. Pitch Attitude Hold Operating Limits 2--5--74 . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--12. Vertical Speed Hold Operating Limits 2--5--75 . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--13. Flight Level Change Mode Operating Limits 2--5--79 . . . . . . . . . . . . . . . . . . . Table 2--5--14. ASEL Mode Operating Limits 2--5--90 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--15. ALT Hold Mode Operating Limits 2--5--94 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--16. ILS Glideslope Mode Operating Limits 2--5--101 . . . . . . . . . . . . . . . . . . . . . . . . Table 2--5--17. VNAV Mode Operating Limits 2--5--105 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--6--1. IC--615 IAC Leading Particulars 2--6--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--6--2. PC-400 Autopilot Controller Leading Particulars 2--6--5 . . . . . . . . . . . . . . . Table 2--6--3. SM--200 Servo Drive and SB--201 Servo Bracket Leading Particulars 2--6--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--6--4. SM--200 Servo Drive Dash Number Differences 2--6--8 . . . . . . . . . . . . . . . . Table 2--6--5. Autopilot Roll Axis Operating Limits 2--6--24 . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--6--6. Pitch Channel Axis Operating Limits 2--6--29 . . . . . . . . . . . . . . . . . . . . . . . . . . Table 2--7--1. EGPWS Computer Leading Particulars 2--7--2 . . . . . . . . . . . . . . . . . . . . . . . Table 2--8--1. TCAS II Computer Leading Particulars 2--8--2 . . . . . . . . . . . . . . . . . . . . . . . . Table 2--8--2. TCAS Antenna Leading Particulars 2--8--3 . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--19 List of Tables (cont) Table Page Table 2--9--1. RT--300 Radio Altimeter Receiver Transmitter Leading Particulars 2--9--2 Table 2--9--2. AT--300 Radio Altimeter Antenna Leading Particulars 2--9--4 . . . . . . . . . . . Table 2--9--3. Radio Altimeter System Performance Accuracy 2--9--6 . . . . . . . . . . . . . . . . Table 2--9--4. Decision Height Set 2--9--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 4--1. HMN Materials 4--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 11 May 2007  Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC--20 Blank Page RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 1 Nov 2004 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page INTRO--1 INTRODUCTION 1. How to Use This Manual A. General (1) The purpose of this manual is to help the avionics specialist better understand the operation and troubleshooting of the PRIMUS 1000 Integrated Avionics System to the line replaceable unit (LRU) level, as installed on the Cessna Citation XLS aircraft. (2) This manual provides overall system and subsystem general description, LRU leading particulars, and subsystem functional operation. This manual covers subsystem and overall system interface and interconnect information to aid the avionics specialist in a general understanding of the system. (3) This manual is not designed or approved to conduct maintenance on the aircraft. The aircraft maintenance manual (AMM) should be used for all maintenance procedures, practices, and LRU part number references. (4) Additional information on subsystems installed as part of the PRIMUS 1000 Integrated Avionics System is available in the publications shown in paragraph 3. of this Introduction. (5) Warnings, cautions, and notes in this manual give the data that follows: • A WARNING gives a condition or tells personnel what part of an operation or maintenance procedure, that if not obeyed, can cause injury or death. • A CAUTION gives a condition or tells personnel what part of an operation or maintenance procedure, that if not obeyed, can cause damage to the equipment. • A NOTE gives data, not commands. The NOTE aids personnel when they do the related instruction. (6) Warnings and cautions go before the applicable paragraph or step. Notes follow the applicable paragraph or step. B. How This Manual Is Organized (1) The material in this manual has been arranged so that experienced maintenance and service personnel can refer directly to those sections that relate to their work, while the less experienced reader can find the manual a valuable introduction to the PRIMUS 1000 Integrated Avionics System. This manual is organized into the seven sections that follow: (2) Section 1 - System Overview (a) The purpose of this section is to give the reader a brief overview of how the entire PRIMUS 1000 Integrated Avionics System is organized, define terms used in the sections that follow, and to serve as a guide for further study of these sections. The numerous digital data buses used within the PRIMUS 1000 Integrated Avionics System are also discussed here. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437 SYSTEM DESCRIPTION AND OPERATION MANUAL Cessna Citation XLS 1 Nov 2004 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. Page INTRO--2 (3) Section 2 - System Description (a) This section is divided into nine subsections that give information about Honeywell manufactured subsystems for the PRIMUS 1000 Integrated Avionics System. Each subsection describes the function and interface of the LRU of each subsystem, as well as subsystem operation and cockpit displays. Block diagrams of subsystem interface, figures, and tables are included as an aid to understanding system operation. The nine subsections are as follows: • Section 2--1 -- Electronic Display System • Section 2--2 -- ADZ--950 Micro Air Data System • Section 2--3 -- PRIMUS 880 Weather Radar System • Section 2--4 -- PRIMUS II Integrated Radio System • Section 2--5 -- Flight Guidance System • Section 2--6 -- Autopilot/Yaw Damper System • Section 2--7 -- Enhanced Ground Proximity Warning System • Section 2--8 -- Traffic Alert and Collision Avoidance System • Section 2--9 -- AA--300 Radio Altimeter System (4) Section 3 -- System Interconnect (a) This section refers to a Honeywell engineering document which contains wiring data for the PRIMUS 1000 Integrated Avionics System and to the approved aircraft maintenance documents. Use the approved aircraft maintenance documents to check the components of the PRIMUS 1000 Integrated Avionics System for correct installation and proper operation. (5) Section 4 -- Maintenance Practices (a) This section describes the procedures to remove and reinstall the Honeywell LRUs. Procedures are also supplied to replace lamps, set screws, and knobs. Where applicable, adjustment data is also supplied. This section is divided into paragraphs that are in alphabetical order according to the unit type designator. (6) Section 5 -- Shipping/Handling and Storage (a) This section refers the user to a Honeywell document for shipping, handling, and storage of all system components. (7) Section 6 -- Honeywell Support (a) This section briefly describes Honeywellís worldwide exchange/rental program (commonly referred to as SPEX) for spares. Telephone numbers and addresses of Honeywellís support centers are also included. (8) Section 7 -- System Test and Fault Isolation (a) This section refers the user to the approved aircraft maintenance documents for system test and fault isolation procedures. Use these documents to check the components of the PRIMUS 1000 Integrated Avionics System for correct installation and proper operation. RELEASED FOR THE EXCLUSIVE USE BY: MARSHALL AVIATION SERVICES LTD UP762437

All Cessna Citation XLS systems description