Honeywell SPZ-8000 Manuale

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

ASSOCIATE

MEMBER

Member of GAMA

General Aviation

Manufacturer’s Association

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of superseded pages.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

A28--1146--055

REV 2 RTR--1/(RTR--2 blank)

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

Revision

No. Issue Date

Date the

Temporary

Revision Was

Incorporated

by a Regular

Revision

Insertion of

Temporary

Revision,

Date/By

Removal of

Temporary

Revision,

Date/By

1Jan 1993 Jul 1999 ---- ----

2Feb 1996 Jul 1999 ---- ----

SPZ--8000 Digital Integrated Flight Control System

A28--1146--055

REV 2 LEP--1

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

TC--10 H2

TC--11 H2

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.

SPZ--8000 Digital Integrated Flight Control System

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LEP--2

Subheading and Page Revision Subheading and Page Revision

Electronic Flight Instrument System

(EFIS) (cont)

4--18 H2

4--19 H2

4--20 H2

4--21 H2

4--22 H2

4--23 H2

4--24 H2

4--25 H2

4--26 H2

4--27 H2

4--28 H2

4--29 H2

4--30 H2

4--31 H2

4--32 H2

4--33 H2

4--34 H2

4--35 H2

4--36 H2

4--37 H2

4--38 H2

F 4--39/4--40 H2

4--41 H2

4--42 H2

4--43 H2

4--44 H2

4--45 H2

4--46 H2

4--47 H2

4--48 H2

4--49 H2

4--50 H2

4--51 H2

4--52 H2

4--53 H2

4--54 H2

4--55 H2

4--56 H2

4--57 H2

4--58 H2

4--59 H2

4--60 H2

4--61 H2

4--62 H2

4--63 H2

4--64 H2

4--65 H2

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

5--13 H2

5--14 H2

5--15 H2

5--16 H2

5--17 H2

5--18 H2

5--19 H2

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

SPZ--8000 Digital Integrated Flight Control System

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List of Effective Pages

Subheading and Page Revision Subheading and Page Revision

System Limits

7--1 H2

7--2 H2

7--3 H2

7--4 H2

7--5 H2

7--6 H2

7--7 H2

7--8 H2

7--9 H2

7--10 H2

7--11/7--12 H2

Modes of Operation

8--1 H2

8--2 H2

8--3 H2

8--4 H2

8--5 H2

8--6 H2

8--7 H2

8--8 H2

8--9 H2

8--10 H2

8--11 H2

8--12 H2

8--13 H2

8--14 H2

8--15 H2

8--16 H2

8--17 H2

8--18 H2

8--19 H2

8--20 H2

8--21 H2

8--22 H2

8--23 H2

8--24 H2

8--25 H2

8--26 H2

8--27 H2

8--28 H2

8--29 H2

8--30 H2

8--31 H2

8--32 H2

8--33 H2

8--34 H2

8--35 H2

8--36 H2

8--37 H2

8--38 H2

8--39 H2

8--40 H2

8--41 H2

8--42 H2

8--43 H2

8--44 H2

8--45 H2

8--46 H2

8--47 H2

8--48 H2

8--49 H2

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

SPZ--8000 Digital Integrated Flight Control System

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List of Effective Pages

LEP--4

Subheading and Page Revision Subheading and Page Revision

Appendix A

A--1 H2

A--2 H2

A--3 H2

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............

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