Garmin G1000:Beechcraft Baron 58/G58 Manual

G1000
TM
pilot’s guide introduction
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190-00302-00 Rev. AGarmin G1000 Pilot’s Guide Introduction
Record of Revisions
Revision Date of Revision Revision Page Range Description
A 05/07/04 1-1 – 1-3 Initial release.
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190-00302-00 Rev. A Garmin G1000 Pilot’s Guide Introduction 1-1
INTRODUCTION
The Introduction describes the components of and
operating procedures associated with the Garmin G1000
Pilot’s Guide binder.
BINDER CONTENTS
The G1000 Pilot’s Guide binder consists of the follow-
ing documents:
•Front Matter: This document contains copyright
information, a record of current part numbers and
revision levels for each document contained in the
G1000 Pilot’s Guide binder, a table of contents, a
list of figures, a list of tables, warranty information
and warnings.
NOTE: The Front Matter and Index portions of
the G1000 Pilot’s Guide binder are assigned the
same part number and revision level.
•Tab “1 – Introduction”: This introductory docu-
ment should serve as a user’s guide to the G1000
Pilot’s Guide binder.
•Tab “2 – System Overview”: This document
describes all of the major components of the G1000
Integrated Cockpit System and includes both a
system block diagram and a brief explanation of
each Line Replaceable Unit (LRU).
•Tab “3 – Primary Flight Display”: This document
describes the operation of the Primary Flight Display
(PFD) and includes communication, navigation,
flight control, annunciations and alerts, and flight
planning information.
•Tab “4 – NAV/COM”: This document describes
the operation of the navigation (VOR/ILS) and radio
communication capability of the G1000 Integrated
Cockpit System.
•Tab “5 – Transponder”: This document describes
the operation of the G1000 Transponder.
•Tab “6 – Audio Panel”: This document describes
the operation of the G1000 Audio Panel and
includes an aircraft-specific supplemental section.
•Tab “7 – Engine Indication System”: This docu-
ment describes the operation of the G1000 Engine
Indication System and includes procedures on lean-
ing to maximize flight efficiency.
•Tab “8 – Multi Function Display”: This document
describes the operation of the G1000 Multi Func-
tion Display (MFD) and includes all GPS/Navigation
flight information.
•Tab “9 – Annunciations and Alerts”: This docu-
ment augments the information contained in the
Aircraft Flight Manual Supplement in that it lists
and describes all of the annunciations and alerts
that pertain to the operation of the AHRS, system
and aircraft interface.
•Tab “Appendices”: Information that is supple-
mental to the various pilot’s guide documents
is presented in the Appendices in the following
sequence:
• Appendix A – SD Card Use
• Appendix B – Abbreviations, Acronyms and
NAV Terms
• Appendix C – Questions & Answers
• Appendix D – Map Datums
• Appendix E – General TIS Information
• Appendix F – Map Symbols
• Appendix G – G1000 System Specifications
•Tab “Index”: This document contains an index for
the entire G1000 Pilot’s Guide binder.
)
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190-00302-00 Rev. AGarmin G1000 Pilot’s Guide Introduction
1-2
INTRODUCTION
CAUTION:The pilot should read and thoroughly
understand the Flight Manual Supplement for
information specific to the aircraft operation.The
Flight Manual Supplement always supersedes
information found in this Pilot’s Guide binder.
USING THE BINDER
Part Number Content
The documents contained in the G1000 Pilot’s Guide
binder are subject to change in both part numbers and
revision levels. In order to ensure that the G1000 Pilot’s
Guide binder contains the most current document part
numbers and revision levels, please refer to the Record
of Part Numbers presented in the Front Matter portion of
the binder.
Page Numbering Format
General
Page numbering is of the following format:
“
a - b ”
where
a = binder document tab number
b = page number within the said document
For example, page number “5-3” represents the third
page of the document located under the fifth tab of the
G1000 Pilot’s Guide binder – namely, the G1000 VHF
NAV/COM Pilot’s Guide.
NOTE: Page numbering for the Front Matter por-
tion G1000 Pilot’s Guide binder is presented in
Roman numerals without a prefix. For example,
page “ii” represents the second page of the Front
Matter portion of the binder.
Appendices
Page numbering for the Appendices reflects each ap-
pendix alphabetical level and is thus of the following
format:
“
c - d ”
where
c = appendix alphabetical level
d = page number within the said appendix
For example, page “B-3” represents the third page of
Appendix B.
Index
Page numbering for the Index portion of G1000 Pilot’s
Guide binder is of the following format:
“I-
e ”
where
e = page number within the Index
Section Numbering Format
Section numbering is of the following format:
“
a . f ”
where
a = binder document tab number
f = section number within the said document
For example, “8.2” corresponds to the second section
of the document located after the eighth tab of the G1000
Pilot’s Guide binder – namely, the G1000 Multi Function
Display Pilot’s Guide.
,
)
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190-00302-00 Rev. A Garmin G1000 Pilot’s Guide Introduction 1-3
INTRODUCTION
Figure/Table Numbering Format
Figure/table numbering is of the following format:
“
a . f . g ”
where
a = binder document tab number
f = section number within the said document
g = figure/table number within the said section
For example, “Figure 3.4.2” represents the second
figure of section 3.4 of the document located under the
third tab.
NOTE: Figure/table numbering in the Appendices
reflects the appendix alphabetical level and the
figure/table number within the corresponding
appendix. For example, “Figure F.1” represents
the first figure of Appendix F.
Table of Contents and List of Figures/Tables
The table of contents for the entire G1000 Pilot’s Guide
binder is provided in the Front Matter and is followed by
both a global list of figures and a global list of tables.
Index
A global index is provided as the last portion of the
G1000 Pilot’s Guide binder contents.
STORING THE BINDER
As opposed to the Cockpit Reference Guide and
Cockpit Reference Card, the G1000 Pilot’s Guide binder is
designed to be used as a reference and does not necessar-
ily need to be stored on board the aircraft.
)
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190-00302-00 Rev. A
Garmin International, Inc.
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Garmin AT, Inc.
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Garmin Corporation
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Shijr, Taipei County, Taiwan
P: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2004 Garmin Ltd. or its subsidiaries
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