Garmin Cessna Caravan G1000 Manual

G1000
TM
Pilot’s Guide for Beechcraft 58/G58

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58 190-00629-00 Rev. B
Part Number Change Summary
190-00629-00
Rev. A
190-00629-00
Rev. B
Corrected figure numbering sequence in Section 7
Record of Revisions
Revision Date of Revision Revision Page Range Description
A
B
10/18/05
11/09/05
-------------
All
Initial release

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58
190-00629-00 Rev. B i
COPYRIGHT
Copyright © 2005 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0500.01 or later.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: [phone] Fax: [phone]
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
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Garmin (Europe) Ltd., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K.
Tel: [phone] Fax: [phone]
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone] Fax: [phone]
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or
stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission
to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to
be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text
of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is
strictly prohibited.
Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000™ is a trademark of Garmin Ltd. or its subsidiaries.
These trademarks may not be used without the express permission of Garmin.
Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc., Silver Crown Plus™ is a trademark of
Honeywell International, Inc.; NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and Skywatch® are registered
trademarks of L-3 Communications; TCAD® is a registered trademark of Ryan International, Inc.; and XM® is a registered trademark
of XM Satellite Radio, Inc.
November 2005 190-00629-00 Rev. B Printed in the U.S.A.

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58 190-00629-00 Rev. Bii
WARNINGS & CAUTIONS
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain
function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for
terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings
during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not
certified for use in applications requiring a certified terrain awareness system. Terrain data is obtained
from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be
relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING: The Garmin G1000, as installed in Beechcraft 58/G58 aircraft, has a very high degree of
functional integrity. However, the pilot must recognize that providing monitoring and/or self-test
capability for all conceivable system failures is not practical. Although unlikely, it may be possible for
erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility
of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level
and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A
Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in
aircraft.
WARNING: The Jeppesen database used in the G1000 system must be updated regularly in order to
ensure that its information remains current. Updates are released every 28 days. A database information
packet is included in the G1000 package. Pilots using an outdated database do so entirely at their own
risk.

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58
190-00629-00 Rev. B iii
WARNINGS & CAUTIONS
WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non-
navigational situational awareness. Any basemap indication should be compared with other navigation
sources.
CAUTION: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or
giving an intense radar echo.”
CAUTION: The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy
and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision
electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the
G1000 can be misused or misinterpreted and, therefore, become unsafe.
CAUTION: To reduce the risk of unsafe operation, carefully review and understand all aspects of the
G1000 Pilot’s Guide documentation. Thoroughly practice basic operation prior to actual use. During
flight operations, carefully compare indications from the G1000 to all available navigation sources,
including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always
resolve any discrepancies before continuing navigation.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made
by an authorized Garmin service center. Unauthorized repairs or modifications could void both the
warranty and the pilot’s authority to operate this device under FAA/FCC regulations.
CAUTION: The GDU 1040 PFD and MFD displays use a lens coated with a special anti-reflective coating
that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA
WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-
free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings.

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58 190-00629-00 Rev. Biv
WARNINGS & CAUTIONS
NOTE: All visual depictions contained within this document, including screen images of the G1000 panel
and displays, are subject to change and may not reflect the most current G1000 system. Depictions of
equipment may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE: There are several atmospheric phenomena in addition to nearby thunderstorms that can cause
isolated discharge points in the strike display mode. However, clusters of two or more discharge points
in the strike display mode do indicate thunderstorm activity if these points reappear after the screen
has been cleared. Avoid the clusters to avoid the thunderstorms. In the cell display mode, even a single
discharge point may represent thunderstorm activity and should therefore be avoided.

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58
190-00629-00 Rev. B v
WARRANTY
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no
charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty does not
cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR
STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE,
STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING
FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of
incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole discretion.
SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit the
Garmin Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58 190-00629-00 Rev. Bvi
WARRANTY
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Garmin G1000 Pilot’s Guide for Beechcraft 58/G58
190-00629-00 Rev. B vii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 Introduction .................................................... 1-1
1.2 System Description ......................................... 1-1
1.3 Optional Equipment ....................................... 1-3
1.4 PFD/MFD Controls .......................................... 1-4
1.5 Secure Digital Cards ....................................... 1-6
1.6 System Power-up ............................................ 1-7
1.7 Display Backlighting ....................................... 1-9
1.8 System Operation ........................................... 1-9
Normal Mode .............................................................1-9
Reversionary Mode ..................................................1-10
AFCS Preflight Test ...................................................1-10
AHRS Operation .......................................................1-11
SECTION 2 PRIMARY FLIGHT DISPLAY
2.1 Introduction .................................................... 2-1
2.2 Backlighting ................................................... 2-4
2.3 Softkey Function ............................................ 2-5
2.4 Flight Instruments .......................................... 2-9
Airspeed Indicator ......................................................2-9
Attitude Indicator .....................................................2-10
Altimeter ..................................................................2-12
Vertical Deviation/Glideslope Indicator ....................2-14
Marker Beacon Annunciations ..................................2-14
Vertical Speed Indicator ...........................................2-14
Horizontal Situation Indicator ..................................2-15
2.5 Communication, Navigation, & Surveillance
(CNS) 2-21
Communication Frequency Window .........................2-21
Navigation Frequency Window .................................2-21
Navigation Status Bar ..............................................2-22
Transponder (XPDR) Status Bar ................................2-22
2.6 Supplemental Flight Data ..............................2-23
Outside Air Temperature Box ....................................2-23
System Time Box ......................................................2-23
Inset Map .................................................................2-23
Auxiliary Window Keys .............................................2-26
Working with Menus ................................................2-27
Auxiliary Windows ....................................................2-27
2.7 Reversionary Mode .......................................2-42
2.8 Alerts and Annunciations ...............................2-43
Alerts Window ..........................................................2-43
Annunciation Window ..............................................2-43
Softkey Annunciations ..............................................2-43
Terrain Awareness and Warning System (TAWS) Alert
Annunciations (optional) ..........................................2-44
Traffic Annunciation .................................................2-44
SECTION 3 NAV/COM
3.1 NAV/COM Description .................................... 3-1
Windows and Fields ...................................................3-2
Radio Selection ...........................................................3-2
Controls ......................................................................3-3
Tuning Box .................................................................3-4
Switching Between Radios .........................................3-4
Manually Tuning a Frequency .....................................3-4
Radio Indicators .........................................................3-5
Volume .......................................................................3-5
Frequency Transfer Arrow ...........................................3-5
3.2 Com Operation ............................................... 3-6
Frequency Spacing ......................................................3-6
Automatic Squelch .....................................................3-6
Selecting a COM Radio ...............................................3-6
Emergency Frequency (121.500 MHz) ........................3-7
Quick-Tuning and Activating121.500 MHz .................3-7
Stuck Microphone ......................................................3-7
3.3 NAV Operation ................................................ 3-8
Frequency Range ........................................................3-8
Morse Code Identifier .................................................3-8
NAV Radio Selection for Navigation ...........................3-8

Garmin G1000 Pilot’s Guide for Beechcraft 58/G58 190-00629-00 Rev. Bviii
TABLE OF CONTENTS
DME TUNING .............................................................3-9
3.4 Frequency Auto-Tuning ..................................3-10
Auto-Tuning on the PFD ...........................................3-10
Auto-Tuning on the MFD ..........................................3-11
NRST – Nearest Airports Window .............................3-14
NRST – Nearest VOR Window ...................................3-15
Auto-Tuning on Approach Activation (NAV Frequencies) .
3-17
SECTION 4 TRANSPONDER
4.1 Transponder Description ................................. 4-1
Transponder Softkeys .................................................4-1
Transponder Status Bar ..............................................4-1
Mode S Features .........................................................4-2
Traffic Information Service (TIS) ..................................4-2
4.2 Operation ....................................................... 4-3
Mode Selection ..........................................................4-3
Code Selection ...........................................................4-4
IDENT Function ..........................................................4-5
SECTION 5 AUDIO PANEL
5.1 Audio Panel Description ................................. 5-1
Transceivers ................................................................5-1
Mono/Stereo Headsets ...............................................5-2
Unmuted/Unswitched Inputs ......................................5-2
Front Panel Controls ...................................................5-2
5.2 Operation ....................................................... 5-4
Power-up and Fail-Safe Operation ..............................5-4
Key Annunciators ........................................................5-4
Lighting ......................................................................5-4
Transceiver Keys .........................................................5-4
Split COM Function ....................................................5-5
PA Function ................................................................5-5
Speaker ......................................................................5-5
Marker Beacon Receiver .............................................5-6
Navigation Radios ......................................................5-7
Intercom System (ICS) Isolation ..................................5-8
Intercom Volume and Squelch ....................................5-9
Entertainment Inputs ..................................................5-9
GDL 69A XM Radio System ......................................5-10
Master Avionics Squelch (MASQ) .............................5-10
Digital Clearance Recorder with Playback ................5-11
Reversionary Mode ..................................................5-11
SECTION 6 ENGINE INDICATION SYSTEM
6.1 Introduction .................................................... 6-1
EIS Pages ....................................................................6-1
EIS Indicators ..............................................................6-1
EIS Page Reversion .....................................................6-2
6.2 Engine Page .................................................... 6-3
6.3 Lean Page ....................................................... 6-4
6.4 System Page ................................................... 6-6
SECTION 7 MULTI FUNCTION DISPLAY
7.1 Introduction .................................................... 7-1
Description .................................................................7-1
Optional Equipment ...................................................7-1
MFD Power-up ............................................................7-2
MFD Backlighting .......................................................7-2
MFD Softkeys ............................................................7-2
Reversionary Mode ....................................................7-2
Electronic Checklists (optional) ..................................7-3
MFD Page Groups ......................................................7-7
Working With Menus ..................................................7-8
7.2 Navigation Map Page ..................................... 7-9
Navigation Map Page Operations ............................7-11
7.3 Traffic Map Page ............................................7-33
TIS Symbology ..........................................................7-34
Traffic Map Page Operations ....................................7-34
7.4 Terrain Proximity Page ...................................7-37
Terrain Proximity Page Operations ...........................7-38
Displaying Obstacle Data .........................................7-39