Kln89B

Pilot’s Guide

KLN 89
KLN 89B
Bendix/King®
GPS Navigation Systems

ORS 01/02

N

WARNING
Prior to export of this document, review for export license requirement is needed.

COPYRIGHT NOTICE
Copyright ©1997-2002 Honeywell International Inc. All rights reserved.
Reproduction of this publication or any portion thereof by any means without the
express written permission ofHoneywell International Inc. is prohibited. For further information contact the Manager, Technical Publications; Honeywell; One
Technology Center; 23500 West 105th Street; Olathe, Kansas 66061.
Telephone: (913) 782-0400.

KLN 89/89B Pilot’s Guide
006-08786-0000
for KLN 89 and KLN 89B
with
Operational Revision Status
ORS 01 and 02

IMPORTANT: Special installation procedures must befollowed in
order for the KLN 89B to be certified for IFR En route, Terminal and
Non-precision Approach use. If these procedures are followed, the
KLN 89B can be used for IFR use. Consult the KLN 89B Flight
Manual Supplement for the operating limitations of this unit.

September 2002

IMPORTANT:
This Pilot’s Guide covers both the KLN 89 (VFR only) and KLN
89B (IFR approved for Enroute,Terminal, and Non-precision
Approach phases of flight). There are numerous places
throughout this guide which discuss features and operational
characteristics which specifically apply to KLN 89B, and not to
KLN 89. These parts of the Pilot’s Guide refer specifically to
KLN 89B, and often are marked with a double dagger symbol (‡).
Likewise, chapter 5, “Approaches and SID/STARs” appliesonly
to KLN 89B. For features that apply to both KLN 89 and KLN
89B, a generic reference to “KLN 89(B)” is used.

NOTE: A “whiskers” border is used around data
on some of the figures in this Pilot's Guide to
indicate that the data inside the border is
flashing.

åå.ånm| ZBV
116.70
åååååå|BIMINI
# Leg|
N 25°42.10'
25°
VOR 1 |
W 79°17.10'
79°

WARNING: The KLN 89 and KLN 89Bdisplay GPS-derived altitude on the OTH 1 page. Do not use the GPS-derived altitude for
navigation. Due to Selective Availability position degradation
and other factors, the GPS altitude is normally 300 feet or more
in error, which is unacceptable for vertical navigation.

Revision History and Instructions
Manual

KLN 89/KLN 89B Pilot’s Guide

Revision

5, September 2002

PartNumber

006-08786-0000

This revision contains the following changes:
Changed AlliedSignal to Honeywell throughout.
Editorial Corrections:

Inside Front Cover, Title Page, R-1
through R-4, 3-26, 3-56, 4-11, 4-37
Back Cover

Database Change:

Database Card, 2-0, 2-1, 2-6, 3-6

SET 2 Corrections:

3-9, 3-60, 3-61, 4-47

Misc. Corrections:

4-29, 5-20, 5-22, B-5, B-6, C-1, D-2R-1

Revision History and Instructions
Manual

KLN 89/KLN 89B Pilot’s Guide

Revision

4, May 1998

Part Number

006-08786-0000

This revision contains the following changes:
Text corrections to pages 3-64, 3-66, 4-47, and B-5.
Figure 3-196 changed to show new software numbering display
and the addition of the database number.
Added statements explaining the double dagger(‡) symbol to
pages B-1 and C-1.
Added more description to APT, CAL, NAV, OTH and SET page
listings in the index.

R-2

Revision History and Instructions
Manual

KLN 89/KLN 89B Pilot’s Guide

Revision

3, March 1997

Part Number

006-08786-0000

This revision corrects a typographic error on page 4-47.

R-3

This page intentionally left blank.

R-4

KLN89/KLN 89BPilot’s Guide
INTRODUCTION

Table of Contents

.........................................................................i

KLN 89(B) SNEAK PREVIEW .......................................................ii
HOW-TO INDEX

.......................................................................iv

1. KLN 89(B) SYSTEM COMPONENTS ....................................1-1
2. DATA BASE...