Honeywell PRIMUS 1000 Manual

Highlights
Page 1 of 2
January 2003
Honeywell
AerospaceElectronic Systems
CES–Phoenix
P.O. Box 21111
Phoenix, Arizona 85036–1111
U.S.A.
TO: HOLDERS OF THE PRIMUSR1000 INTEGRATED
AVIONICS SYSTEM FOR THE CITATION ENCORE PILOT’S
MANUAL, HONEYWELL PUB. NO. A28–1146–134
REVISION NO. 1DATED JANUARY 2003
HIGHLIGHTS
Pages that have been revised are outlined below. Remove and insert
the affected pages listed. The revision number has been added to the
bottom of the revised pages and revision bars have been used to
indicate the revised or added text. Insert this highlights letter in the
manual in your possession ahead of page RR-1/RR-2, Record of
Revisions. The List of Effective Pages shows the order in which to insert
the attached new pages of front material into your manual.
Page No. Description of Change
Title Pages Revised to reflect Revision 1.
RR–1/RR–2 Revised to reflect Revision 1.
LEP–1 thru
LEP–4 Revised to reflect Revision 1.
TC–1 Deleted titles from Section 1. No revision bars
added.
1–3 thru 1–4 Added four rows, IC–600 to Table 1 and causing
table to shift.
1–7 thru 1–10 Added new Product Support Section. No revision
bars added.
3–83 Revised Figure 3–42.
6–4 Revised Figure 6–3.

Highlights
Page 2 of 2
January 2003
Page No. Description of Change
6–5 Revised Figure 6–4.
6–6 Revised Figure 6–5.
6–8 Revised Figure 6–7.
6–9 Revised Figure 6–8.
6–10 Revised Figure 6–9.
6–16 Revised Figure 6–12.
6–18 Revised Figure 6–14.
6–20 Revised Figure 6–16.
6–22 Revised Figure 6–18.
6–48 Revised Figure 6–35.
6–51 Revised Figure 6–38.
6–53 Revised Figure 6–40.
Index–1 thru
Index12 Revised to reflect Revision 1. No revision bars added.

Printed in U.S.A. Pub. No. A28–1146–134–01 April 2000
January 2003
Honeywell
Aerospace Electronic Systems
CES–Phoenix
P.O. Box 21111
Phoenix, Arizona 85036–1111
U.S.A.
PRIMUSR1000 Integrated
Avionics System
for the
Citation Encore
Pilot’s Manual

ASSOCIATE
MEMBER
Member of GAMA
General Aviation
Manufacturer’s Association
E
PRIMUS is a U.S. registered trademark of Honeywell.
Copyright  2003 Honeywell International Inc. All rights reserved.
PROPRIETARY NOTICE
This document and the information disclosed herein are proprietary
data of Honeywell. Neither this document nor the information contained
herein shall be used, reproduced, or disclosed to others without the
written authorization of Honeywell, except to the extent required for
installation or maintenance of recipient’s equipment.
NOTICE – FREEDOM OF INFORMATION ACT (5 USC 552) AND
DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY
(18 USC 1905)
This document is being furnished in confidence by Honeywell. The
information disclosed herein falls within exemption (b) (4) of 5 USC 552
and the prohibitions of 18 USC 1905.
All rights reserved. No part of this book, CD, or PDF may be reproduced
or transmitted in any form or by any means, electronic or mechanical,
including photocopying, recording, or by any information storage and
retrieval system, without the written permission of Honeywell
International, except where a contractual arrangement exists between
the customer and Honeywell.
S2003

PRIMUSR1000 Integrated Avionics System
Record of Revisions
A28–1146–134
REV 1 Jan/03 RR–1/(RR–2 blank)
Record of Revisions
Upon receipt of a revision, insert the latest revised pages and dispose
of superseded pages. Enter revision number and date, insertion date,
and the incorporator’s initials on this Record of Revisions. The typed
initial H is used when Honeywell is the incorporator of the revision.
Revision
Number Revision Date Insertion Date By
1 Jan 2003 Jan 2003 H

PRIMUSR1000 Integrated Avionics System
A28–1146–134
REV 1 Jan/03 LEP–1
List of Effective Pages
List of Effective Pages
Original 0. . . . Apr 2000
Revision 1. . . . Jan 2003
Subheadingand Page Revision Subheading and Page Revision
Title Page H1
Record of Revisions
RR–1/RR–2 H1
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Table of Contents
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Introduction
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System Description
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System Limits
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System Limits (cont)
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Modes of Operation
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Troubleshooting(cont)
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Acronyms and Abbreviations
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8–40
8–50
8–60
Appendix A
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Index
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