Honeywell SPZ-8000 Manual

Printed in U.S.A. Pub. No. A28--1146--055--02 Apr 1988
Revised September 1999
Business and Commuter Aviation Systems
Honeywell Inc.
Box 29000
Phoenix, Arizona 85038--9000
U.S.A.
SPZ--8000 Digital Integrated
Flight Control System
for the
Challenger CL 601--3A/3R
Pilot’s Manual

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MEMBER
Member of GAMA
General Aviation
Manufacturer’s Association
E
LASEREF, LASERTRAK, and PRIMUS are U.S. registered trademarks of Honeywell Inc.
E1999 Honeywell Inc.
PROPRIETARY NOTICE
This document and the information disclosed herein are proprietary
data of Honeywell Inc. Neither this document nor the information
contained herein shall be used, reproduced, or disclosed to others
without the written authorization of Honeywell Inc., 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 Inc. The
information disclosed herein falls within exemption (b) (4) of 5 USC 552
and the prohibitions of 18 USC 1905.
S99

SPZ--8000 Digital Integrated Flight Control System
Record of Revisions
A28--1146--055
REV 2 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of superseded pages.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
initials HI are used when Honeywell Inc. is the incorporator of the
revision.
Revision
Number
Revision
Date
Insertion
Date By
1 Oct 1991 Oct 1991 HI
2Sep 1999 Sep 1999 HI

SPZ--8000 Digital Integrated Flight Control System
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Record of Temporary Revisions
Record of Temporary Revisions
Upon receipt of a temporary revision, insert the yellow temporary
revision pages according to the filing instructions on each page. Then,
enter the temporary revision number, issue date, and insertion date on
this page.
Temporary
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No. Issue Date
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by a Regular
Revision
Insertion of
Temporary
Revision,
Date/By
Removal of
Temporary
Revision,
Date/By
1Jan 1993 Jul 1999 ---- ----
2Feb 1996 Jul 1999 ---- ----

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List of Effective Pages
List of Effective Pages
Original 0. . . . Apr 1988
Revision 1. . . . Oct 1991
Revision 2. . . . Sep 1999
Subheading and Page Revision Subheading and Page Revision
Title Page H2
Record of Revisions
RR--1/RR--2 H2
Record of Temporary Revisions
RTR--1/RTR--2 H2
List of Effective Pages
LEP--1 H2
LEP--2 H2
LEP--3 H2
LEP--4 H2
Table of Contents
TC--1 H2
TC--2 H2
TC--3 H2
TC--4 H2
TC--5 H2
TC--6 H2
TC--7 H2
TC--8 H2
TC--9 H2
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TC--12 H2
Introduction
1--1 H2
1--2 H2
1--3 H2
1--4 H2
F 1--5/1--6 H2
System Description
2--1 H2
2--2 H2
2--3 H2
2--4 H2
2--5 H2
2--6 H2
2--7 H2
2--8 H2
2--9 H2
2--10 H2
2--11/2--12 H2
F 2--13/2--14 H2
Air Data System (ADS)
3--1 H2
3--2 H2
3--3 H2
3--4 H2
3--5 H2
3--6 H2
3--7/3--8 H2
Electronic Flight Instrument System
(EFIS)
4--1 H2
4--2 H2
4--3 H2
4--4 H2
4--5 H2
4--6 H2
F 4--7/4--8 H2
4--9 H2
4--10 H2
4--11 H2
4--12 H2
4--13 H2
4--14 H2
4--15 H2
4--16 H2
4--17 H2
Hindicates changed, added or deleted pages.
F indicates right foldout page with a blank back.

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Electronic Flight Instrument System
(EFIS) (cont)
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4--25 H2
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4--66 H2
4--67/4--68 H2
Multifunction Display (MFD) System
5--1 H2
5--2 H2
5--3 H2
5--4 H2
5--5 H2
5--6 H2
5--7 H2
5--8 H2
5--9 H2
5--10 H2
5--11 H2
5--12 H2
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5--16 H2
5--17 H2
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5--20 H2
5--21 H2
5--22 H2
5--23/5--24 H2
Automatic Flight Control System
(AFCS)
6--1 H2
6--2 H2
6--3 H2
6--4 H2
6--5 H2
6--6 H2
6--7 H2
6--8 H2
6--9 H2
6--10 H2
6--11 H2
6--12 H2
6--13 H2
6--14 H2
6--15 H2
6--16 H2
6--17/6--18 H2

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System Limits
7--1 H2
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Modes of Operation
8--1 H2
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8--46 H2
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8--50 H2
8--51 H2
8--52 H2
Troubleshooting
9--1 H2
9--2 H2
9--3 H2
9--4 H2
9--5 H2
9--6 H2
9--7 H2
9--8 H2
9--9 H2
9--10 H2
F 9 -- 11 / 9 -- 1 2 H2
9--13/9--14 H2
Honeywell Product Support
10--1 H2
10--2 H2
10--3 H2
10--4 H2
Acronyms and Abbreviations
11--1 H2
11--2 H2
11--3 H2
11--4 H2
11--5/11--6 H2

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Appendix A
A--1 H2
A--2 H2
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A--4 H2
A--5 H2
A--6 H2
A--7 H2
A--8 H2
A--9 H2
A--10 H2
Appendix B
B--1 H2
B--2 H2
B--3 H2
B--4 H2
B--5 H2
B--6 H2
B--7 H2
B--8 H2
B--9 H2
B--10 H2
B--11 H2
B--12 H2
B--13 H2
B--14 H2
Appendix C
C--1 H2
C--2 H2
C--3 H2
C--4 H2
C--5 H2
C--6 H2
C--7 H2
C--8 H2
C--9 H2
C--10 H2
C--11 H2
C--12 H2
C--13 H2
C--14 H2
C--15 H2
C--16 H2
C--17 H2
C--18 H2
Appendix D
D--1 H2
D--2 H2
D--3 H2
D--4 H2
D--5/D--6 H2
Index
Index--1 H2
Index--2 H2
Index--3 H2
Index--4 H2
Index--5 H2
Index--6 H2
Index--7 H2
Index--8 H2
Index--9 H2
Index--10 H2

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Table of Contents
TC--1
Table of Contents
Section Page
1. INTRODUCTION 1-1.............................
2. SYSTEM DESCRIPTION 2-1.....................
Air Data System (ADS) 2-3.......................
Electronic Flight Instrument System (EFIS) 2-4......
Multifunction Display System (MFD) 2-5............
Dual Flight Guidance System (FGS) 2-5............
Flight Management System (FMS) 2-6.............
Radio Altimeter System 2-7.......................
PRIMUSR650 Weather Radar System 2-8..........
PRIMUSR870 Weather Radar System 2-8..........
LASEREFRII/III Inertial Reference System (IRS) 2-9.
LASERTRAKRSwitch (Serial No. 5087
and Later) 2-9...............................
Lightning Sensor System (LSS) (Optional) 2-10.......
Traffic Alert and Collision Avoidance System
(TCAS II) (Optional) 2-10.........................
Other Switches and Controls 2-11...................
Autopilot Disconnect Switches 2-11..............
Touch Control Steering (TCS) 2-11...............
Go--Around Switches 2-11......................
EFIS Reversionary Switches 2-11................
3. AIR DATA SYSTEM (ADS) 3-1....................
Mach/Airspeed Indicator 3-2......................
Barometric Altimeter 3-3..........................
Vertical Speed Indicator (VSI) 3-5..................
Digital Air Data Computer (DADC)
Self--Test Mode 3-6.............................
Air Data Display Parameters 3-7...................
4. ELECTRONIC FLIGHT INSTRUMENT SYSTEM
(EFIS) 4-1.....................................
Electronic Display Controls 4-2....................
Display Controller 4-2.........................
Instrument Remote Controllers 4-5..............
Electronic Attitude Director Indicator (EADI) 4-6......
EADI Displays and Annunciators 4-9............