Garmin | G1000: Beechcraft Baron G58 | Garmin G1000: Beechcraft Baron G58 G1000 Cockpit Reference Guide Beechcraft G58 - SSV 0857.10

Garmin G1000: Beechcraft Baron G58 G1000 Cockpit Reference Guide Beechcraft G58 - SSV 0857.10
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Beechcraft G58
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2005, 2007-2012, 2019 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0857.10 or later for the Beechcraft
G58 . Some differences in operation may be observed when comparing the information in this
manual to earlier or later software versions.
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Garmin AT, Inc.
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Garmin Corporation
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Contact Garmin Product Support or view warranty information at
www.flygarmin.com.
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permission of Garmin.
Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.;
Becker® is a registered trademark of Becker Flugfunkwerk GmbH; NavData® is a registered
trademark of Jeppesen, Inc. SiriusXM Weather and SiriusXM Satellite Radio are provided by
SiriusXM Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
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consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
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to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”)
expressly disclaim all warranties with respect to the AC-U-KWIK information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK
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allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of
action, claims or losses related to any actual or alleged inaccuracies in the information arising
out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to licensee.
Printed in the U.S.A
Warnings, Cautions & Notes
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation from terrain and obstacles. Garmin obtains
terrain and obstacle data from third party sources and cannot independently
verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for
verification of displayed aeronautical information. Displayed aeronautical
data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic
control altitude requirements. The primary barometric altimeter must be used
for compliance with all air traffic control altitude regulations, requirements,
instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the
sole means of navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered only an aid to
enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
WARNING: Do not use data link weather information for maneuvering in,
near, or around areas of hazardous weather. Information contained within
data link weather products may not accurately depict current weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be older than the indicated weather product age.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Warnings, Cautions & Notes
WARNING: The displayed minimum safe altitude (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: Always obtain qualified instruction prior to operational use of
this equipment.
WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints
are derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
WARNING: Do not rely on the autopilot to level the aircraft at the MDA/DH
when flying an approach with vertical guidance. The autopilot will not level
the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision
avoidance resolution advisories and does not under any circumstances or
conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability
upon which to solely base decisions and/or plan maneuvers to avoid terrain,
obstacles, or traffic.
WARNING: Do not use the Garmin SVT runway depiction as the sole means
for determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Warnings, Cautions & Notes
WARNING: Do not rely on information from a lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: Do not use TAWS information for primary terrain or obstacle
avoidance. TAWS is intended only to enhance situational awareness.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners
containing ammonia. They will harm the anti-reflective coating.
CAUTION: Do not allow repairs to be made by anyone other than an authorized
Garmin service center. Unauthorized repairs or modifications could void both
the warranty and affect the airworthiness of the aircraft.
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
NOTE: Do not rely solely upon data link services to provide Temporary Flight
Restriction (TFR) information. Always confirm TFR information through official
sources such as Flight Service Stations or Air Traffic Control.
NOTE All visual depictions contained within this document, including screen
images of the system panel and displays, are subject to change and may not
reflect the most current system and aviation databases. Depictions of equipment may differ slightly from the actual equipment.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Warnings, Cautions & Notes
NOTE: 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 system utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information
presented by the system can be misused or misinterpreted and, therefore,
become unsafe.
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: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields can cause sensor differences that may result
in nuisance miscompare annunciations during start up, shut down, or while
taxiing. If one or more of the sensed values are unavailable, the annunciation
indicates no comparison is possible.
NOTE: The system responds to a terminal procedure based on data coded
within that procedure in the Navigation Database. Differences in system
operation may be observed among similar types of procedures due to differences in the Navigation Database coding specific to each procedure.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Warnings, Cautions & Notes
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and
advisory guidance and information related to the use of databases in the
National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained
from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen
that have a Type 2 Letter of Authorization (LOA) from the FAA are assured
compliance with all data quality requirements (DQRs). A copy of the Type
2 LOA is available for each applicable database and can be viewed at
http://fly.garmin.com by selecting ‘Aviation Database Declarations.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to
operate in accordance with established pertinent aircraft documents and
regulatory guidance or limitations as applicable to the pilot, the aircraft,
and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.
com by selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The
database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation
Database Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Warnings, Cautions & Notes
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or
any other displayed item used for navigation or communication in the air or
on the ground. Go to FlyGarmin.com and select ‘Aviation Data Error Report’.
NOTE: Electronic aeronautical charts displayed on this system have been
shown to meet the guidance in AC 120-76D as a Type B Electronic Flight Bag
(EFB) for FliteCharts and ChartView. The accuracy of the charts is subject to
the chart data provider. Own-ship position on airport surface charts cannot be
guaranteed to meet the accuracy specified in AC 120-76D. Possible additional
requirements may make a secondary source of aeronautical charts, such as
traditional paper charts or an additional electronic display, necessary on the
aircraft and available to the pilot. If the secondary source of aeronautical
charts is a Portable Electronic Device (PED), its use must be consistent with
the guidance in AC 120-76D.
NOTE: The navigation databases used in Garmin navigation systems contain Special Procedures. Prior to flying these procedures, pilots must have
specific FAA authorization, training, and possession of the corresponding
current, and legitimately-sourced chart (approach plate, etc.). Inclusion of
the Special Procedure in the navigation database DOES NOT imply specific
FAA authorization to fly the procedure.
NOTE: Terrain and obstacle alerting is not available north of 89º North latitude
and south of 89º South latitude. This is due to limitations present within the
Terrain database and the system’s ability to process the data representing
the affected areas.
NOTE: The nose of the ‘own ship’ symbol represents the location of the aircraft. The center of any traffic symbol represents the location of that traffic.
The traffic and own ship symbols are an abstract representation and do not
reflect the physical extent of the aircraft/traffic, and should not replace other
methods for identifying traffic.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Warnings, Cautions & Notes
NOTE: Lamp(s) inside this product contain mercury (HG) and must be recycled
or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/en-US/company/environment/
recycling
NOTE: When using Stormscope, 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.
NOTE: Operate G1000 system power through at least one cycle in a period
of four days of continuous operation to avoid an autonomous system reboot.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a
resource with which to find operating instructions on the major features of
the system more easily. It is not intended to be a comprehensive operating
guide. Complete operating procedures for the system are found in the Pilot’s
Guide for this aircraft..
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Software License Agreement
SOFTWARE LICENSE AGREEMENT
BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN
(“THE GARMIN PRODUCT”), YOU AGREE TO BE BOUND BY THE TERMS AND CONDITIONS
OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT
CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the
software embedded in the Garmin Product (the “Software”) in binary executable form in the
normal operation of the Garmin Product. Title, ownership rights, and intellectual property rights
in and to the Software remain with Garmin and/or its third-party providers. You acknowledge
that the Software is the property of Garmin and/or its third-party providers and is protected
under the United States of America copyright laws and international copyright treaties. You
further acknowledge that the structure, organization, and code of the Software are valuable
trade secrets of Garmin and/or its third-party providers and that the Software in source code
form remains a valuable trade secret of Garmin and/or its third-party providers. You agree not
to reproduce, decompile, disassemble, modify, reverse assemble, reverse engineer, or reduce to
human readable form the Software or any part thereof or create any derivative works based on
the Software. You agree not to export or re-export the Software to any country in violation of
the export control laws of the United States of America.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Software License Agreement
Blank Page
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Record of Revisions
Record of Revisions
Part Number
Revision
Date
Page
Range
190-00526-00
A
October, 2005
All
Initial release.
190-00526-01
A
December,
2007
All
Changed to smaller format
Added Airways, WAAS, VNAV, and
Charts
Updated G1000 System Messages
Added other GDU 8.10 parameters
B
December,
2007
All
Removed FD Formatting feature
190-00526-02
A
May, 2010
All
Added GDU 11.01 parameters
Added Synthetic Vision System
Added flight plan import/export
Updated procedure for entering User
Waypoints
Updated XM weather products
Updated TAWS annunciations
Added CDI operation in Dead
Reckoning mode
Added AOPA Airport Directory
Added temporary user waypoints
Added database synchronization
Added GTS 820 TAS
Removed support for non-WAAS
systems
Various clerical corrections
190-00526-03
A
March, 2012
All
Added Profile View
Added new weather product symbols
and legend
Added MV DB update procedure
Added other GDU 11.13 parameters
190-00526-04 Rev. B
Description
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
RR-1
Record of Revisions
Record of Revisions
Part Number
Revision
Date
Page
Range
190-00526-04
A
June, 2019
All
Added Software License Agreement
Updated Warnings, Cautions, and
Notes section
Added support for ADS-B out
Added User Defined Holds
Updated Approach types
Added Temperature Compensated
Altitudes
Updated TAWS-B information
Updated Transponder information
Updated Sirius XM radio information
Updated to GDU SW version13.31
B
June, 2019
All
Updated FliteCharts Information
RR-2
Description
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Table of Contents
Flight Instruments........................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Change Navigation Sources.................................................................................................... 1
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs Individually...................................................................................... 2
Set Barometric Minimum Descent Altitude......................................................................... 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 3
Engine Indication System......................................................................................................... 5
Engine Display............................................................................................................................ 5
Lean Engine Display.................................................................................................................. 6
Engine System Display............................................................................................................. 8
Nav/Com/Transponder/Audio Panel.................................................................................... 9
ADF Tuning (Optional)............................................................................................................... 9
DME Tuning (Optional).............................................................................................................. 9
Selecting A Transponder Mode............................................................................................... 9
Enter a Transponder Code....................................................................................................... 9
Selecting a COM Radio........................................................................................................... 10
Selecting a NAV Radio............................................................................................................ 10
NAV/COM Tuning...................................................................................................................... 10
Split COM................................................................................................................................... 10
Digital Clearance Recorder and Player............................................................................... 11
Intercom System (ICS) Isolation........................................................................................... 11
Automatic Flight Control System...................................................................................... 13
Flight Director Activation...................................................................................................... 13
Vertical Modes.......................................................................................................................... 14
Lateral Modes........................................................................................................................... 15
GPS Navigation............................................................................................................................ 17
Direct-to Navigation............................................................................................................... 17
Activate a Stored Flight Plan................................................................................................ 18
Activate a Flight Plan Leg...................................................................................................... 18
Stop Navigating a Flight Plan............................................................................................... 19
Vertical Navigation (VNAV)................................................................................................... 19
Altitude Constraints................................................................................................................ 20
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
i
Table of Contents
Flight Planning............................................................................................................................. 25
Trip Planning............................................................................................................................. 25
Create a User Waypoint Defined by Latitude & Longitude............................................ 27
Create a User Waypoint Defined by Radials from Other Waypoints............................ 27
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 29
Delete a User Waypoint.......................................................................................................... 30
Create a Flight Plan................................................................................................................. 31
Import a Flight Plan from an SD Card................................................................................. 32
Insert a Waypoint in the Active Flight Plan....................................................................... 33
Enter an Airway in a Flight Plan........................................................................................... 33
Invert An Active Flight Plan................................................................................................... 34
Entering An Along Track Offset Distance........................................................................... 34
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 35
User Defined Holding Patterns............................................................................................. 35
Activating Temperature Compensated Altitude............................................................... 38
Cancelling Temperature Compensated Altitude............................................................... 38
Store a Flight Plan................................................................................................................... 39
Edit a Stored Flight Plan........................................................................................................ 39
Delete a Waypoint from the Flight Plan............................................................................. 39
Invert and Activate a Stored Flight Plan............................................................................ 40
Copy a Flight Plan.................................................................................................................... 40
Delete a Flight Plan................................................................................................................. 40
Graphical Flight Plan Creation.............................................................................................. 41
Export a Flight Plan to an SD Card...................................................................................... 41
Procedures...................................................................................................................................... 43
Load and Activate a Departure Procedure........................................................................ 43
Activate A Departure Leg...................................................................................................... 43
Load An Arrival Procedure..................................................................................................... 43
Activate An Arrival Leg.......................................................................................................... 44
Load and/or Activate an Approach Procedure.................................................................. 45
Approach Type and Downgrade Support........................................................................... 46
Activate An Approach in the Active Flight Plan................................................................ 46
Activate a Vector to Final Approach Fix............................................................................. 46
Activate A Missed Approach in the Active Flight Plan.................................................... 47
Hazard Avoidance....................................................................................................................... 49
Customizing the Hazard Displays on the Navigation Map............................................. 49
STORMSCOPE® (Optional)...................................................................................................... 49
SiriusXM Weather (Optional)................................................................................................ 51
Traffic Systems......................................................................................................................... 53
Terrain Awareness & Warning System (TAWS-B) Display................................................ 55
Airborne Color Weather Radar............................................................................................. 57
ii
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Table of Contents
Additional Features................................................................................................................... 63
Synthetic Vision........................................................................................................................ 63
Terminal Procedure Charts.................................................................................................... 64
Airport Directory..................................................................................................................... 67
SiriusXM Radio Entertainment............................................................................................. 68
Pilot Profiles............................................................................................................................. 70
Abnormal Operation................................................................................................................. 75
Reversionary Mode................................................................................................................. 75
Abnormal COM Operation..................................................................................................... 75
Hazard Displays with Loss of GPS Position........................................................................ 75
Unusual Attitudes.................................................................................................................... 76
Dead Reckoning....................................................................................................................... 77
Annunciations & Alerts............................................................................................................ 79
WARNING Annunciation......................................................................................................... 79
CAUTION Annunciation........................................................................................................... 79
ADVISORY Annunciation........................................................................................................ 80
Alert Message........................................................................................................................... 80
AFCS ALERTS............................................................................................................................. 80
TAWS-B Alerts........................................................................................................................... 81
TAWS-B System Status Annunciations................................................................................ 83
Voice Alerts............................................................................................................................... 84
MFD & PFD Message Advisories........................................................................................... 85
Database Message Advisories.............................................................................................. 86
GMA 1347 Message Advisories............................................................................................. 88
GIA 63W Message Advisories................................................................................................ 89
GEA 71 Message Advisories................................................................................................... 92
GTX 33 Message Advisories................................................................................................... 92
GRS 77 Message Advisories................................................................................................... 93
GDC 74A Message Advisories................................................................................................ 94
GMU 44 Message Advisories................................................................................................. 94
GDL 69/69A Message Advisories.......................................................................................... 94
GWX 68 Message Advisories................................................................................................. 94
GTS 820 Message Advisories................................................................................................. 95
Miscellaneous Message Advisories...................................................................................... 95
Flight Plan Import/Export Messages................................................................................... 99
Pilot Profile Import/Export Messages............................................................................... 101
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
iii
Table of Contents
Appendix........................................................................................................................................ 103
PFD Softkey Map................................................................................................................... 103
MFD Softkey Map.................................................................................................................. 108
Database Updates................................................................................................................. 111
Index............................................................................................................................................Index-1
iv
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
AFCS
Turn the BARO Knob to select the desired setting.
2)
Press the STD BARO Softkey to set standard barometric pressure.
Flight
Planning
Press the PFD Softkey.
GPS Nav
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1)
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Hazard
Avoidance
Press the PFD Softkey to display the second-level softkeys.
Procedures
1)
Additional
Features
Or:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
Abnormal
Operation
4)
CHANGE NAVIGATION SOURCES
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.
3)
Press the CDI Softkey a third time to return to GPS.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
2)
Appendix
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
Annun/
Alerts
1)
190-00526-04 Rev. B
Nav/Com/
XPDR/Audio
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
EIS
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
1
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Press the OBS Softkey to select OBS Mode.
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.
Additional
Features
CONFIGURE VSPEED BUGS INDIVIDUALLY
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
AFCS
GENERIC TIMER
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Index
Appendix
Annun/
Alerts
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Instruments
Flight
Instruments
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1) Press the TMR/REF Softkey.
Turn the small FMS Knob clockwise to BARO.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
AFCS
3)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
EIS
2)
2)
Press the WIND Softkey to display wind data to the left of the HSI.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
Procedures
Press the PFD Softkey.
Flight
Planning
1)
GPS Nav
DISPLAYING WIND DATA
CHANGING HSI FORMAT
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Additional
Features
Press the PFD Softkey.
Hazard
Avoidance
1)
Or:
Abnormal
Operation
Press the ARC HSI Softkey to display the arc style HSI.
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
Blank Page
4
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Engine Indication System
Flight
Instruments
ENGINE INDICATION SYSTEM
ENGINE DISPLAY
EIS
Nav/Com/
XPDR/Audio
In all cases green indicates normal operation, yellow indicates caution, and red
indicates warning.
Pressing the ENGINE Softkey makes available the LEAN and SYSTEM softkeys
which in turn provide access to the Lean Page and the System Page, respectively.
AFCS
GPS Nav
Manifold
Pressure
Gauge
(Left Engine)
Flight
Planning
RPM Gauge
(Left Engine)
Propeller Sync
Indicator
Fuel Flow
Indicator
Procedures
Fuel Flow
Numeric
Readout
Hazard
Avoidance
Cylinder Head
Temperature
Indicator
Additional
Features
Oil Temperature
Indicator
Oil Pressure
Indicator
Abnormal
Operation
Ammeter
Fuel Quantity
Indicator
Annun/
Alerts
Default Engine Page
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
5
LEAN ENGINE DISPLAY
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
AFCS
Fuel Flow Leaning
Marker
Difference between peak
and current temperature
of selected cylinder
(Right Engine)
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
EGT peak
temperature
(Left Engine)
Exhaust Gas
Temperature
Bar Graphs
(Left Engine)
Cylinder Head
Temperature
Bar Graphs
(Left Engine)
Lean Engine Display
Additional
Features
Accessing the EIS Lean Display:
1) Press the ENGINE Softkey.
2) Press the LEAN Softkey.
3) To return to the default Engine Display, press the ENGINE or BACK
Softkey.
Abnormal
Operation
Annun/
Alerts
CHT Readout
For Selected
Cylinder
(Right Engine)
From the Lean Display, the CYL SLCT and ASSIST Softkeys can be utilized
to obtain information about specific cylinders on both the EGT and CHT graphs.
Pressing the CYL SLCT Softkey cycles through the cylinders; the selected cylinder
number is displayed in light blue. The CYL SLCT Softkey is disabled during warning
or caution conditions or when the ASSIST Softkey is pressed.
Index
Appendix
EGT Readout
For Selected
Cylinder
(Right Engine)
6
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Engine Indication System
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Monitoring the desired cylinder’s EGT and CHT:
From the Lean Display, press the CYL SLCT Softkey to cycle through each
cylinder and view its EGT and CHT. The selected cylinder is shown in light
blue.
When the ASSIST Softkey is selected, the system initially highlights and selects
the cylinder number with the hottest EGT and displays its temperature below the EGT
bar graph. A readout showing the difference between peak (DPEAK) and the current
temperature for the selected cylinder is displayed above the EGT bar graph.
As the mixture is leaned, a light blue line will appear above each cylinder to indicate
EGT peak.
When the system detects the first cylinder to peak, the cylinder numbers below the
EGT graph disappear, and the letter “R” is annunciated below the first peaked cylinder
to indicate the other cylinders are rich of peak. As the mixture is further leaned, the
letter “L” is annunciated below the last peaked cylinder indicating all cylinders are
lean of peak. Refer to the POH and AFM for the recommended mixture adjustment
procedures.
Monitoring of the cylinder continues until the ASSIST Softkey is pressed again
which disables lean assist and removes the peak lines from the bar graph and the
temperature deviation from peak (DPEAK). The system then returns to seeking the
hottest cylinder.
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
7
ENGINE SYSTEM DISPLAY
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
1)
Press the ENGINE Softkey, then the SYSTEM Softkey to display the
SYSTEM Engine Page.
2)
If desired, use the DEC FUEL, INC FUEL, 166 GAL, and 194 GAL
softkeys to adjust the amount of fuel remaining for totalizer calculations.
Procedures
Flight
Planning
GPS Nav
AFCS
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and
are calculated from the last time the fuel was reset.
Hazard
Avoidance
System
Information
Additional
Features
Fuel Calculation
Information
Annun/
Alerts
Abnormal
Operation
Electrical
Information
Index
Appendix
SYSTEM Engine Page
8
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ADF TUNING (OPTIONAL)
EIS
Tune the ADF using the remote ADF control head.
Nav/Com/
XPDR/Audio
DME TUNING (OPTIONAL)
2)
Turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
GPS Nav
Press the DME Softkey.
AFCS
1)
SELECTING A TRANSPONDER MODE
Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2)
Press the desired softkey to activate the transponder mode.
Procedures
The transmission of the ADS-B information is enabled/disabled by pressing the
ADS-B TX Softkey. ADS-B transmission defaults to enabled at each power cycle.
Flight
Planning
1)
Hazard
Avoidance
ENTER A TRANSPONDER CODE
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
Annun/
Alerts
2)
Abnormal
Operation
Press the XPDR Softkey to display the transponder mode selection softkeys.
Additional
Features
1)
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
9
SELECTING A COM RADIO
Transmit/Receive
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
Receive Only
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
NAV/COM TUNING
Procedures
Flight
Planning
GPS Nav
AFCS
SELECTING A NAV RADIO
1)
Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
SPLIT COM
During Split COM operation, both the pilot and the copilot can transmit
simultaneously over separate radios. The pilot can still monitor NAV1, NAV2, ADF,
DME, and MKR Audio as selected, but the copilot is only able to monitor COM2.
When Split COM operation is selected, COM1 is used by the pilot and COM2 is
used by the copilot. The COM1 MIC Annunciator flashes when the pilot’s microphone
PTT is pressed. The COM2 MIC Annunciator flashes when the copilot’s microphone
PTT is pressed.
Pressing the COM 1/2 Key selects Split COM operation. The COM 1/2 Annunciator
is illuminated indicating Split COM operation. COM1 and COM2 frequencies are
displayed in green indicating that both transceivers are active. Split COM operation
is cancelled by pressing the COM 1/2 Key again, at which time the annunciator is
extinguished.
10
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Nav/Com/XPDR/Audio Panel
Passenger
Hears
Selected
radios; pilot;
copilot;
passengers;
music
Selected
radios; pilot;
copilot;
passengers;
music
Copilot;
passengers;
music
Copilot;
passengers;
music
PILOT
ON
OFF
Selected
radios; pilot
Copilot
Selected
radios; pilot;
passengers;
music
Selected
radios; pilot;
copilot
Passengers;
music
COPILOT
OFF
ON
Selected
radios; pilot;
passengers;
music
CREW
ON
ON
Selected
radios; pilot;
copilot
Appendix
OFF
Annun/
Alerts
OFF
Abnormal
Operation
ALL
Selected
radios; pilot;
copilot;
passengers;
music
Additional
Features
Copilot
Hears
Hazard
Avoidance
Pilot Hears
Procedures
PILOT KEY
COPLT KEY
ANNUNCIATOR ANNUNCIATOR
Flight
Planning
Mode
GPS Nav
Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/
Com radios and music.
AFCS
INTERCOM SYSTEM (ICS) ISOLATION
Nav/Com/
XPDR/Audio
• Pressing PLAY once plays the latest recorded memory block, then returns to
normal operation.
• Pressing MKR/MUTE while playing a memory block stops play.
• Pressing the PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next
previously recorded block.
EIS
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
Flight
Instruments
DIGITAL CLEARANCE RECORDER AND PLAYER
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
11
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
12
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
AFCS
AFCS
FLIGHT DIRECTOR ACTIVATION
Modes Selected
Heading Select
HDG
PIT
GP
GS
PIT
Annun/
Alerts
HDG Key
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
Abnormal
Operation
Approach**
PIT
Additional
Features
APR Key
GPS
VAPP
LOC
Pitch Hold (default)
Hazard
Avoidance
Navigation**
Procedures
NAV Key
ROL
ROL
ROL
GA
ROL
ROL
ROL
GPS
VOR
LOC
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Go Around (in air)
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight
Planning
FD Key
AP Key
CWS Switch
GA Switch
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Go Around (in air)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
GPS Nav
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
Control Pressed
Nav/Com/
XPDR/Audio
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
EIS
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV or APR Key press activates flight director.
Appendix
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
13
VERTICAL MODES
Vertical Mode
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
Pitch Hold
Selected Altitude
Armed
Vertical Speed
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Altitude Hold
Flight Level Change
VNAV
VNAV Target Altitude
Armed (GDU 1045
only)
Glidepath
Glideslope
Go Around
Description
Holds the current aircraft pitch
attitude; may be used to climb/
descend to the Selected Altitude
AFCS armed to capture the altitude
displayed in the Selected Altitude
window
Holds the current Altitude
Reference
Maintains the current aircraft
vertical speed; may be used to climb/
descend to the Selected Altitude
Maintains the current aircraft
airspeed in IAS while the aircraft is
climbing/descending to the Selected
Altitude
Captures and tracks the VNAV flight
path
AFCS armed to capture the altitude
displayed in the VNAV Target
Altitude window
Captures and tracks the SBAS
glidepath on approach
Captures and tracks the ILS
glideslope on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level
Control
Annunciation
(default)
PIT
*
ALTS
ALT Key
ALT
nnnnn ft
VS Key
VS
nnnn fpm
FLC Key
FLC
nnn kt
VNV Key
VPTH
**
ALTV
GP
APR Key
GS
GA
Switch
GA
* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude
is to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
14
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
AFCS
Lateral Mode
Flight
Planning
BC
Procedures
GPS
APR
Key
Hazard
Avoidance
VAPP
LOC
GA
Abnormal
Operation
GA
Switch
Additional
Features
Approach, GPS (Glidepath
mode automatically armed if
vertical guidance is available) Captures and tracks the
selected navigation source
Approach, VOR
(GPS, VOR, LOC)
Approach, LOC (Glideslope
Mode automatically armed)
Disengages the autopilot and
Go Around
commands a constant pitch
angle and wings level
GPS Nav
Navigation, Backcourse
Captures and tracks a
localizer signal for backcourse
approaches
AFCS
Navigation, GPS
Navigation, VOR (Enroute
Mode)
Navigation, LOC (Glideslope
will not arm or capture)
Nav/Com/
XPDR/Audio
Heading Select
EIS
Roll Hold
Description
Control Annunciation
Holds the current aircraft roll
attitude or rolls the wings
(default)
ROL
level, depending on the
commanded bank angle
Captures and tracks the HDG
HDG
Selected Heading
Key
GPS
Captures and tracks the
VOR
selected navigation source
(GPS, VOR, LOC)
NAV
LOC
Key
Flight
Instruments
LATERAL MODES
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
15
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
Blank Page
16
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
2)
3)
6)
9)
12)
1)
2)
5)
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
17
Index
6)
Appendix
4)
).
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Annun/
Alerts
3)
Press the Direct-to Key (
Abnormal
Operation
Direct-to Navigation from the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
) Key.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
AFCS
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EIS
Direct-to Navigation from the MFD
EIS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the OFFSET distance field.
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Press the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
Press the ACT LEG Softkey on the MFD.
3)
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
4)
With ‘Activate’ highlighted, press the ENT Key.
Index
Appendix
OR
18
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This does not delete the stored flight plan, only the active flight plan.
VERTICAL NAVIGATION (VNAV)
AFCS
Enabling VNV guidance
2)
Press the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable
VNV’, and press the ENT Key. Vertical navigation is enabled, and vertical
guidance begins with the waypoint shown in the CURRENT VNV PROFILE
box (defaults first waypoint in the active flight plan with an altitude
enabled for vertical navigation (e.g., HABUK)).
Flight
Planning
Press the FPL Key to display the Active Flight Plan Page on the MFD.
GPS Nav
1)
Procedures
Disabling VNV guidance
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel
VNV’, and press the ENT Key. Vertical navigation is disabled.
Hazard
Avoidance
1)
2)
Press the FMS Knob to activate the cursor and turn the FMS Knob to
highlight the desired waypoint.
Abnormal
Operation
Press the FPL Key to display the Active Flight Plan Page on the MFD.
Additional
Features
Activating a vertical navigation direct-to
1)
Appendix
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
Press the VNV Direct-To Softkey; or press the MENU Key, highlight
‘VNV Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to:
NNNNNFT at XXXXXX?’ confirmation window is displayed.
190-00526-04 Rev. B
Annun/
Alerts
NOTE: The selected waypoint must have a designated altitude constraint
(light blue number) to be used. If not, the first waypoint in the flight plan
with a designated altitude constraint is selected.
3)
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EIS
1)
19
Flight
Instruments
GPS Navigation
5)
Press the FMS Knob to remove the flashing cursor.
Nav/Com/
XPDR/Audio
EIS
Modifying the VS TGT and FPA
AFCS
GPS Nav
Flight
Planning
Procedures
Press the ENT Key. Vertical guidance begins to the altitude constraint for
the selected waypoint.
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the VNV PROF Softkey; or press the MENU Key, highlight ‘Select
VNV Profile Window’, and press the ENT Key. The cursor is now located in
the CURRENT VNV PROFILE box.
3)
Turn the FMS Knobs as needed to edit the values.
4)
Press the FMS Knob to remove the flashing cursor.
ALTITUDE CONSTRAINTS
The G1000 system can use altitude constraints associated with lateral
waypoints to give guidance for vertical navigation. These altitudes are,
depending on the specific instance, manually entered or retrieved from the
published altitudes in the navigation database. The navigation database
only contains altitudes for procedures that call for “Cross at” altitudes. If the
procedure states “Expect to cross at,” then the altitude is not in the database.
In this case the altitude may be entered manually.
Additional
Features
Hazard
Avoidance
4)
Abnormal
Operation
Large White
Text
Annun/
Alerts
Large Light
Blue Text
Small Light
Blue Text
Appendix
Small Light
Blue Subdued
Text
Index
Small White Text
with Altitude
Restriction Bar
20
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
GPS Navigation
Flight
Instruments
Cross AT or ABOVE 5,000 ft
Cross AT 2,300 ft
EIS
Cross AT or BELOW 3,000 ft
Light Blue
Subdued Text
Altitude has been entered
by the pilot. Altitude is
designated for use in
giving vertical flight path
guidance. Altitude does
not match the published
altitude in navigation
database or no published
altitude exists.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Small Text
Altitude is not designated
to be used in determining
vertical flight path
guidance. Altitude has
been retrieved from the
navigation database and
is provided as a reference.
Altitude is designated
for use in giving vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches a
published altitude in the
navigation database.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Flight
Planning
Altitude calculated by the
system estimating the
altitude of the aircraft as it
passes over the navigation
point. This altitude is
provided as a reference
and is not designated to
be used in determining
vertical flight path
guidance.
GPS Nav
Large Text
AFCS
Light Blue Text
Nav/Com/
XPDR/Audio
White Text
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Altitudes associated with approach procedures are “auto-designated”. This means
the system automatically uses the altitudes loaded with the approach for giving vertical
speed and deviation guidance. Note that these altitudes are displayed as blue text up
to, but not including, the FAF. The FAF is always a “reference only” altitude and cannot be designated, unless the selected approach does not provide vertical guidance. In
this case, the FAF altitude can be designated.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
21
Altitudes that have been designated for use in vertical guidance can be “un-designated” using the CLR Key. The altitude is now displayed only as a reference. It is
not used to give vertical guidance. Other displayed altitudes may change due to recalculations or be rendered invalid as a result of manually changing an altitude to a
non-designated altitude.
Designating a waypoint altitude to be used for vertical guidance
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
GPS Navigation
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude.
3)
Turn the small FMS Knob to enter editing mode.
4)
Press the ENT Key. The altitude is now shown in blue, indicating it is usable
for vertical guidance.
Designating a procedure waypoint altitude to be used for vertical
guidance
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude.
3)
Press the ENT Key. The altitude is now shown in blue, indicating it is usable
for vertical guidance.
Altitude constraints are displayed and entered in feet mean sea level (MSL) values
to the nearest hundred. An altitude constraint in feet above ground level (AGL) format
is supported for airports. When a database altitude restriction is displayed, the G1000
allows entry of a different altitude when creating a waypoint, effectively overriding the
database restriction (only before the FAF). When a database altitude restriction of type
“AT or ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the
restriction to define the vertical profile.
An altitude constraint is invalid if:
• Meeting the constraint requires the aircraft to climb
Annun/
Alerts
Abnormal
Operation
1)
Appendix
• Meeting the constraint requires the maximum flight path angle or
maximum vertical speed to be exceeded
Index
• The altitude constraint results in a TOD behind the aircraft present
position
22
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
GPS Navigation
EIS
• The altitude constraint is added to the FAF of an approach that provides
vertical guidance (i.e., ILS or GPS SBAS approach)
Flight
Instruments
• The constraint is within a leg type for which altitude constraints are not
supported
• The altitude constraint is added to a waypoint past the FAF.
Nav/Com/
XPDR/Audio
Entering/modifiying an altitude constraint
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Enter an altitude constraint value using the FMS Knobs. To enter altitudes
as a flight level, turn the small FMS Knob counter-clockwise past zero
or clockwise past 9 on the first character, and the system automatically
changes to show units of Flight Level. Turn the large FMS Knob clockwise
to highlight the first zero and enter the three digit flight level.
AFCS
1)
4)
Select ‘OK’ and press the ENT Key.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation
window is displayed.
Appendix
3)
Annun/
Alerts
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
Abnormal
Operation
2)
Additional
Features
Press the FPL Key to display the Active Flight Plan Page on the MFD.
Hazard
Avoidance
1)
Procedures
Deleting an altitude constraint provided by the navigation database
Flight
Planning
Press the ENT Key to accept the altitude constraint; if the selected
waypoint is an airport, an additional choice is displayed. Turn the small
FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the
altitude.
Altitude constraints can be modified or deleted after having been added to the
flight plan. In the event an altitude constraint is deleted and the navigation database
contains an altitude restriction for the lateral waypoint, the G1000 displays the altitude
restriction from the database provided no predicted altitude can be provided. The
G1000 also provides a way to reinstate a published altitude constraint that has been
edited.
GPS Nav
4)
23
GPS Navigation
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove or Revert to published VNV altitude of
nnnnnFT?’ confirmation window is displayed.
4)
Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is
deleted (it is replaced by a system calculated altitude, if available).
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Deleting an altitude constraint that has been manually entered
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Reverting a manually entered altitude constraint back to the
navigation database value
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove or Revert to published VNV altitude of
nnnnnFT?’ confirmation window is displayed.
4)
Select ‘REVERT’ and press the ENT Key. The altitude is changed to the
navigation database value.
5)
Press the FMS Knob to remove the flashing cursor.
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. An ‘Edit or Revert to published VNV altitude of
nnnnnFT?’ confirmation window is displayed.
4)
Select ‘EDIT’ and press the ENT Key.
5)
Edit the value using the FMS Knobs, and press the ENT Key.
6)
Press the FMS Knob to remove the flashing cursor.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Modifying a system calculated altitude constraint:
24
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
Flight
Instruments
FLIGHT PLANNING
TRIP PLANNING
Turn the large FMS Knob to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the first rectangular page icon.
3)
The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL
Softkey.
4)
For Direct-to planning:
EIS
1)
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
a) Press the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Flight
Planning
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
Procedures
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
Hazard
Avoidance
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Additional
Features
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
Abnormal
Operation
c) Again, enter the identifier of the ending waypoint.
d) Press the ENT Key to accept the waypoint.
Or:
Annun/
Alerts
For flight plan leg planning:
a) Press the FPL Softkey (at the bottom of the display).
Appendix
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
25
Flight Planning
EIS
Flight
Instruments
d) Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ is an available option to display planning data for the
remainder of the flight plan.
Nav/Com/
XPDR/Audio
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
AFCS
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Flight
Planning
GPS Nav
NOTE: The departure time on the Trip Planning Page is used for preflight
planning. Refer to the Utility Page for the actual flight departure time.
6)
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
7)
The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.
Hazard
Avoidance
Procedures
8)
Additional
Features
9)
The flashing cursor moves to the fuel onboard field. Enter the fuel onboard.
Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel
onboard is provided by the fuel totalizer.
Abnormal
Operation
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
Index
Appendix
Annun/
Alerts
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
26
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
AFCS
2)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
EIS
1)
Flight
Instruments
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
GPS Nav
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Appendix
Turn the small FMS Knob to select the User WPT Information Page.
Annun/
Alerts
2)
Abnormal
Operation
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
Additional
Features
1)
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
190-00526-04 Rev. B
Hazard
Avoidance
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
Procedures
7)
Flight
Planning
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
27
EIS
Flight
Instruments
Flight Planning
7)
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
Nav/Com/
XPDR/Audio
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
AFCS
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
b) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
c) Press the ENT Key.
Or:
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Procedures
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Hazard
Avoidance
Or:
Additional
Features
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Abnormal
Operation
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Annun/
Alerts
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Appendix
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Index
d) Press the ENT Key.
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
28
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
Nav/Com/
XPDR/Audio
16) Press the FMS Knob to remove the flashing cursor.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Procedures
Turn the small FMS Knob to select the User WPT Information Page.
Flight
Planning
2)
GPS Nav
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
AFCS
CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
1)
Hazard
Avoidance
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/DIS (radial/distance).
9)
Press the ENT Key.
Annun/
Alerts
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Index
b) Turn the large FMS Knob to select the desired waypoint.
Appendix
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
c) Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Abnormal
Operation
7)
Additional
Features
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
190-00526-04 Rev. B
EIS
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
Flight
Instruments
12) Press the ENT Key.
29
Flight Planning
Flight
Instruments
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EIS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Nav/Com/
XPDR/Audio
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Flight
Planning
d) Press the ENT Key.
Or:
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Additional
Features
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Abnormal
Operation
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
15) Press the FMS Knob to remove the flashing cursor.
DELETE A USER WAYPOINT
Index
Appendix
Annun/
Alerts
14) Press the ENT Key.
30
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
Turn the small FMS Knob to highlight the desired waypoint.
6)
Press the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
CREATE A FLIGHT PLAN
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.
GPS Nav
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
4) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
AFCS
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
Nav/Com/
XPDR/Audio
5)
EIS
Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
Flight
Instruments
4)
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
31
4)
Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
5)
Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6)
Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7)
When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
GPS Nav
IMPORT A FLIGHT PLAN FROM AN SD CARD
Procedures
Insert the SD card containing the flight plan in the top card slot on the
MFD.
2)
Press the FPL Key on the MFD to display the Active Flight Plan Page.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Press the IMPORT Softkey.
Additional
Features
1)
Hazard
Avoidance
Flight
Planning
NOTE: See the Annunciations & Alerts section for flight plan import message
descriptions.
Abnormal
Operation
If an empty flight plan is selected, a list of the available flight plans on
the SD card will be displayed.
Or:
Index
Appendix
Annun/
Alerts
If an existing flight plan is selected, an ‘Overwrite existing flight plan?
OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to
overwrite the selected flight plan and see a list of the available flight
plans on the SD card. If overwriting the existing flight plan is not
desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select
another existing or empty flight plan, and again press the IMPORT
Softkey.
32
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
1)
Press the FPL Key to display the active flight plan.
2)
If required, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
EIS
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
Nav/Com/
XPDR/Audio
Flight
Instruments
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
5)
Enter the new flight plan waypoint by one of the following:
AFCS
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
Or:
Procedures
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
Or:
Additional
Features
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Abnormal
Operation
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
e) Press the ENT Key again to accept the waypoint.
Annun/
Alerts
ENTER AN AIRWAY IN A FLIGHT PLAN
Press the FPL Key.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
33
Index
190-00526-04 Rev. B
Appendix
1)
4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
INVERT AN ACTIVE FLIGHT PLAN
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
4)
Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5)
With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the along track
offset.
3)
Press the ATK OFST Softkey (MFD only); or press the MENU Key, highlight
‘Create ATK Offset Waypoint’, and press the ENT Key.
4)
Enter a positive or negative offset distance in the range of +/- 1 to 99 nm
(limited by leg distances).
5)
Press the ENT Key to create the offset waypoint.
6)
Turn the small FMS Knob to enter the desired altitude for the offset.
7)
Press the FMS Knob to remove the flashing cursor.
Index
Appendix
1)
Abnormal
Operation
ENTERING AN ALONG TRACK OFFSET DISTANCE
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
34
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
1)
EIS
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Flight
Instruments
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
Or, for a stored flight plan:
Nav/Com/
XPDR/Audio
a) Press the FPL Key on the MFD.
b) Turn the small FMS Knob to select the Flight Plan Catalog Page.
c) Press the FMS Knob to activate the cursor.
AFCS
d) Turn the large FMS Knob to highlight the desired flight plan.
e) Press the EDIT Softkey.
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
USER DEFINED HOLDING PATTERNS
Hazard
Avoidance
Creating a user-defined hold at an active flight plan waypoint
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key.
The HOLD AT window appears with the course field highlighted.
4)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Annun/
Alerts
2)
Abnormal
Operation
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Additional
Features
1)
190-00526-04 Rev. B
Procedures
3)
Flight
Planning
Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
GPS Nav
2)
35
EIS
Flight
Instruments
Flight Planning
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
Nav/Com/
XPDR/Audio
10) Press the ENT Key while ‘LOAD?’ is highlighted to insert the hold into the
flight plan.
Creating a user-defined hold at the aircraft present position
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the course field highlighted.
3)
If desired, use the FMS Knobs to edit the entry course, and press the ENT
Key.
4)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
5)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
6)
Use the FMS Knobs to edit the length, and press the ENT Key.
7)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
8)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
9)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to create an Offroute
Direct-to hold waypoint at the aircraft present position and activate the
hold.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
1)
Index
Appendix
Annun/
Alerts
Creating a user-defined hold at a direct-to waypoint
36
1)
Press a Direct-to Key and set up the direct-to waypoint as desired, but
select ‘HOLD?’ instead of ‘ACTIVATE?’ when finished (MFD or PFD).
2)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
3)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
4)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
Use the FMS Knobs to edit the length, and press the ENT Key.
6)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
7)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
8)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the direct-to
with the user-defined hold defined at the direct-to waypoint. (If the directto wayoint is part of the active flight plan, the HOLD is inserted into the
active flight plan. If the direct-to waypoint is not part of the active flight
plan, an off-route direct-to hold is created.)
Flight
Instruments
5)
EIS
Nav/Com/
XPDR/Audio
AFCS
Exiting a user-defined hold inserted into the active flight plan
GPS Nav
Flight
Planning
Press the SUSP Softkey. The system will provide guidance to follow the
holding pattern to the inbound course and resume automatic waypoint
sequencing.
Removing a user-defined hold inserted into the active flight plan
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the HOLD waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
Hazard
Avoidance
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
3)
Press the ENT Key. The holding pattern is removed.
Appendix
Press the MENU Key to display the PAGE MENU with the cursor on the
‘Cancel Direct-To NAV’ selection.
Annun/
Alerts
2)
Abnormal
Operation
Press a Direct To Key to display the DIRECT TO Window (PFD or MFD).
Additional
Features
Removing a user-defined hold at an off-route direct-to
1)
Procedures
1)
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
37
ACTIVATING TEMPERATURE COMPENSATED ALTITUDE
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
1)
From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4)
Use the small FMS Knob to select the temperature at the <airport>. The
AFCS
compensated altitude is computed as the temperature is selected.
5)
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
shown in the flight plan.
CANCELLING TEMPERATURE COMPENSATED ALTITUDE
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
NOTE: The temperature at the destination can be entered in the TEMPERATURE COMPENSATION Window on the MFD, or in the REFERENCES Window
on the PFD. There is only one compensation temperature for the system,
therefore, changing the temperature will affect both the loaded approach
altitudes and the minimums. Refer to the Flight Instruments section for
information about applying temperature compensation to the MDA/DH.
1)
From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4)
Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
5)
Press the ENT Key. The temperature compensated altitude at the FAF
Appendix
is cancelled.
Index
NOTE: Activating/cancelling temperature compensation for the loaded
approach altitudes does not select/deselect temperature compensated minimums (MDA/DH), nor does selecting/deselecting temperature compensated
minimums activate/cancel temperature compensated approach altitudes.
38
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
2)
Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
3)
With ‘OK’ highlighted, press the ENT Key to store the flight plan.
Nav/Com/
XPDR/Audio
EDIT A STORED FLIGHT PLAN
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Press the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
GPS Nav
Press the FPL Key on the MFD, then turn the small FMS Knob to display the
Flight Plan Catalog Page.
AFCS
1)
Flight
Planning
Procedures
DELETE A WAYPOINT FROM THE FLIGHT PLAN
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Additional
Features
Or, for a stored flight plan:
Hazard
Avoidance
1)
EIS
1)
Flight
Instruments
STORE A FLIGHT PLAN
a) Press the FPL Key on the MFD.
b) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Abnormal
Operation
c) Press the FMS Knob to activate the cursor.
d) Turn the large FMS Knob to highlight the desired flight plan.
Annun/
Alerts
e) Press the EDIT Softkey.
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
Appendix
2)
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
39
4)
With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
5)
Once all changes have been made, press the FMS Knob to remove the
cursor.
INVERT AND ACTIVATE A STORED FLIGHT PLAN
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
Additional
Features
Abnormal
Operation
1)
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
DELETE A FLIGHT PLAN
1)
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
Index
Appendix
Annun/
Alerts
1)
COPY A FLIGHT PLAN
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
40
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Flight Planning
5)
Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Nav/Com/
XPDR/Audio
GRAPHICAL FLIGHT PLAN CREATION
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
4)
Press the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
EXPORT A FLIGHT PLAN TO AN SD CARD
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
3)
Appendix
Press the FPL Key to display the Active Flight Plan Page on the MFD.
Annun/
Alerts
2)
Abnormal
Operation
Insert the SD card into the top card slot on the MFD.
Additional
Features
NOTE: See the Annunciations & Alerts section for flight plan export message
descriptions.
Hazard
Avoidance
3)
Procedures
Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
Flight
Planning
2)
GPS Nav
Press the FPL Key on the MFD to display the Active Flight Plan Page.
AFCS
1)
1)
EIS
Turn the large FMS Knob to highlight the flight plan to be deleted.
Flight
Instruments
4)
41
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Blank Page
42
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EIS
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
Hazard
Avoidance
Press the FPL Key on the MFD to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
departure.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
LOAD AN ARRIVAL PROCEDURE
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Appendix
1)
43
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Procedures
ACTIVATE A DEPARTURE LEG
190-00526-04 Rev. B
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
4)
Turn the large FMS Knob to highlight the desired arrival.
5)
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways may be displayed for the selected
arrival.
8)
Turn the large FMS Knob to highlight the desired runway.
9)
Press the ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.
AFCS
11) The arrival becomes part of the active flight plan.
GPS Nav
12) If an altitude associated with a waypoint in an arrival procedure is to be
used to calculate vertical guidance perform the following steps:
a) Press the FMS Knob to activate the cursor.
c) Press the ENT Key to designate the altitude for use in giving vertical
guidance.
ACTIVATE AN ARRIVAL LEG
1)
Press the FPL Key to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
b) Turn the large FMS Knob to highlight the desired waypoint altitude.
44
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Procedures
3)
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
6)
Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.
7)
Press the ENT Key. The cursor moves to the MINIMUMS field.
8)
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO.
9)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
EIS
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Flight
Instruments
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Annun/
Alerts
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
Appendix
12) Press the ENT Key.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
45
APPROACH TYPE AND DOWNGRADE SUPPORT
HSI Annunciation
Description
LNAV
RNAV GPS approach using published LNAV minima
LNAV+V
RNAV GPS approach using published LNAV minima.
Advisory vertical guidance is provided
L/VNAV
RNAV GPS approach using published LNAV/VNAV
(available only if minima (downgrades to L/VNAV if SBAS unavailable)
SBAS available)
LP
RNAV GPS approach using published LP minima
(available only if (downgrades to LNAV if SBAS unavailable)
SBAS available)
LP+V
RNAV GPS approach using published LP minima
(available only if Advisory vertical guidance is provided (downgrades to
SBAS available) LNAV if SBAS unavailable)
LPV
RNAV GPS approach using published LPV minima
(available only if (downgrades to L/VNAV if SBAS unavailable)
SBAS available)
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
ACTIVATE A VECTOR TO FINAL APPROACH FIX
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
46
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Procedures
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Nav/Com/
XPDR/Audio
Press the PROC Key.
EIS
1)
Flight
Instruments
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
Or:
Press the Go-around Button.
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
47
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
Blank Page
48
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
2)
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.
EIS
1)
AFCS
Procedures
Press the MAP Softkey.
2)
Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Additional
Features
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Strike is between 1 and 2 minutes old
Annun/
Alerts
Strike is between 2 and 3 minutes old
3)
Press the ENT Key.
4)
Turn the small FMS Knob to highlight ‘Weather’.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
Turn either FMS Knob to highlight ‘Map Setup’.
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
2)
Hazard
Avoidance
1)
Press the MENU Key (with the Navigation Map Page displayed).
Flight
Planning
Displaying Stormscope Lightning Data on the Navigation Map Page
1)
GPS Nav
WARNING: The Stormscope system is not intended to be used for hazardous
thunderstorm penetration. Weather information on the G1000 MFD is
approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for
detailed operation.
Lightning Age
Strike is less than 6 seconds old
Nav/Com/
XPDR/Audio
STORMSCOPE® (OPTIONAL)
49
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
5)
Press the ENT Key.
6)
Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.
7)
Turn the small FMS Knob to display the ‘Cell/Strike’ window.
8)
Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
9)
Push the FMS Knob to return to the Navigation Map Page.
AFCS
Clear Stormscope Lightning Data from the Navigation Map Page
1)
Press the MENU Key (with the Navigation Map Page displayed).
2)
Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.
GPS Nav
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
Flight
Planning
after the execution of each turn. This is to ensure that the strike and/or cell
positions are depicted accurately in relation to the nose of the aircraft.
Procedures
Stormscope Page
1)
Turn the large FMS Knob until the Map Page group is selected.
2)
Turn the small FMS Knob until the Stormscope Page is selected.
1)
Select the Stormscope Page.
2)
Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey
to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box
located in the upper left corner of the Stormscope Page.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
Annun/
Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Appendix
Change the Viewing Mode Between 360˚ and 120˚
1)
Select the Stormscope Page.
2)
Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press
the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to
display a 120˚ viewing area.
Index
Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.
50
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
Press the MAP Softkey.
2)
Press the NEXRAD or XM LTNG Softkey to display the desired weather.
Press the applicable softkey again to remove weather data from the
Navigation Map Page.
AFCS
1)
Nav/Com/
XPDR/Audio
Displaying SiriusXM Weather on the Navigation Map Page
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Flight
Planning
Turn the large FMS Knob to select the WPT Page Group.
GPS Nav
Display METAR and TAF information on the Airport Information Page
1)
Procedures
Displaying Weather on the Weather Data Link Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Press the available softkeys to select the desired XM weather product.
4)
Press the LEGEND Softkey to view the legends for the selected products. If
necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.
Hazard
Avoidance
1)
Abnormal
Operation
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
or SIGMETs.
3)
Press the ENT Key to display pertinent information for the selected product.
Appendix
Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.
Annun/
Alerts
1)
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Additional
Features
Map Panning Information – Weather Data Link Page
190-00526-04 Rev. B
EIS
WARNING: Use of SiriusXM Weather for hazardous weather penetration is
not recommended. Weather information provided by SiriusXM Radio Service
is approved only for weather avoidance, not penetration.
Flight
Instruments
SIRIUSXM WEATHER (OPTIONAL)
51
Hazard Avoidance
Flight
Instruments
SiriusXM Weather Products and Symbols
EIS
Wx Product
Status Icons
Description
Nav/Com/
XPDR/Audio
NEXRAD - Available for the US and Canada. The age of the displayed data
for each is shown at the right.
ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.
AFCS
CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.
GPS Nav
XM LIGHTNING - The age of the displayed data is shown at the right.
Flight
Planning
CELL MOVEMENT - The age of the displayed data is shown at the right.
Procedures
SIGMET & AIRMET - The age of the displayed data for each is shown at the
right.
Hazard
Avoidance
METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.
Additional
Features
SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts
Surface Analysis. The lower symbol depicts City Forecast. The age of the
displayed data for each is shown at the right. The selected forecast period is
shown at the bottom.
Abnormal
Operation
FREEZING LEVEL - The age of the displayed data is shown at the right.
Annun/
Alerts
WINDS ALOFT - Available for the US and Canada. The age of the displayed
data for each is shown at the right. The altitude selection is shown at the
bottom.
Appendix
COUNTY WARNING - The age of the displayed data is shown at the right.
CYCLONE WARNING - The age of the displayed data is shown at the right.
Index
AIREP - The age of the displayed data is shown at the right.
52
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
Flight
Instruments
Wx Product
Status Icons
Description
EIS
PIREP - The age of the displayed data is shown at the right. Urgent Pireps
are displayed in yellow.
Nav/Com/
XPDR/Audio
TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.
ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.
AFCS
Description
Procedures
Traffic Symbol
Flight
Planning
• If Traffic information Service (TIS) is configured, STANDBY, OPERATE, and
TNA MUTE softkeys are displayed.
• If a Traffic Advisory System (TAS) is configured, STANDBY, NORMAL, TEST,
and ALT MODE softkeys are displayed.
GPS Nav
TRAFFIC SYSTEMS
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Hazard
Avoidance
Proximity Advisory (PA) (Not available with TIS system)
(intruder is within 5 nm and less than 1200’ vertical separation)
Additional
Features
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Abnormal
Operation
Traffic Advisory Off Scale
Traffic Symbol Description
Annun/
Alerts
Traffic Information Service (TIS)
NOTE: If the G1000 is configured to use a Traffic Advisory System (TAS), TIS
is not available for use.
Appendix
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
53
Hazard Avoidance
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Traffic on the Traffic Map Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6)
Press the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
Procedures
Flight
Planning
Displaying Traffic on the Navigation Map
1)
Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.
2)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Traffic Advisory System (TAS)(If Installed)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
54
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the OPERATE or NORMAL Softkey to begin displaying traffic.
‘OPERATING’ is displayed in the Traffic Mode field.
4)
Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
5)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
7)
Select the FLT ID Softkey to enable or disable Flight ID displayed with the
intruder information (GTS 820 only).
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
Flight
Instruments
System Self Test
With the Traffic Map Page displayed, set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert is heard (see
Alerts and Annunciations section). If the self test fails, the system reverts to
Standby Mode and a voice alert is heard.
EIS
1)
2)
With the Navigation Map displayed, select the MAP Softkey.
3)
Select the TRAFFIC Softkey. Traffic is now displayed on the map.
GPS Nav
Ensure TAS is operating.
AFCS
1)
Flight
Planning
TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY
Press the TERRAIN Softkey to display terrain and obstacle data.
Customizing terrain and obstacle display on the Navigation Map Page:
Select the Navigation Map Page.
2)
Press the MENU Key.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
1)
Appendix
2)
Annun/
Alerts
Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey).
Abnormal
Operation
Displaying terrain and obstacle information (maps other than the
TAWS-B Page):
Additional
Features
NOTE: Terrain data is not displayed when the aircraft is outside of the installed
terrain database coverage area.
Hazard
Avoidance
NOTE: The data contained in the TAWS databases comes from government
agencies. Garmin accurately processes and cross-validates the data but
cannot guarantee the accuracy and completeness of the data.
Procedures
WARNING: Do not use TAWS information for primary terrain avoidance.
TAWS is intended only to enhance situational awareness.
1)
Nav/Com/
XPDR/Audio
Displaying Traffic on the Navigation Map
55
EIS
Flight
Instruments
Hazard Avoidance
3)
With ‘Map Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key
.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
Nav/Com/
XPDR/Audio
• TERRAIN DATA – Turns the display of terrain data on or off and sets
maximum range at which terrain is shown
Flight
Planning
GPS Nav
AFCS
• OBSTACLE DATA – Turns the display of obstacle data on or off and sets maximum
range at which obstacles are shown
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Procedures
Displaying the TAWS-B Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the TAWS-B Page.
Additional
Features
Hazard
Avoidance
Changing the TAWS-B Page view
1)
Press the VIEW Softkey.
2)
Press the 360 or ARC Softkey to select the desired view.
Abnormal
Operation
Or:
1)
Press the MENU Key.
2)
Select ‘View Arc’ or ‘View 360º’ (choice dependent on current state) and press the ENT
Key to change the view
Annun/
Alerts
Showing/hiding aviation information on the TAWS-B Page
1)
Press the MENU Key.
Index
Appendix
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current
state) and press the ENT Key.
56
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Nav/Com/
XPDR/Audio
Red
EIS
Terrain/Obstacle Location
Flight
Instruments
Color
TAWS Inhibit
AFCS
Inhibiting/enabling TAWS-B alerting:
Select the TAWS-B Page.
2)
Press the INHIBIT Softkey to inhibit or enable TAWS (choice dependent on
current state).
Flight
Planning
Or:
a) Press the MENU Key.
Procedures
b) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current
state) and press the ENT Key.
Manually testing the TAWS-B System
Hazard
Avoidance
Select the TAWS-B Page.
2)
Press the MENU Key.
3)
Select ‘Test TAWS System’ and press the ENT Key to confirm the selection.
57
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Appendix
WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.
Annun/
Alerts
AIRBORNE COLOR WEATHER RADAR
Abnormal
Operation
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
Additional
Features
1)
190-00526-04 Rev. B
GPS Nav
1)
Flight
Instruments
Hazard Avoidance
EIS
CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Radar Page.
3)
Press the MODE Softkey.
4)
If the aircraft is on the ground, press the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar
enters Standby Mode. After the aircraft is airborne, press the WEATHER
Softkey.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Displaying Weather on the Weather Radar Page
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
If the aircraft is already airborne, press the WEATHER or GROUND Softkey.
The one-minute warm-up period is initiated, after which the radar begins
transmitting. The horizontal scan is initially displayed.
5)
Turn the Joystick to select the desired range.
6)
If desired, press the VERTICAL Softkey for vertical scanning.
Adjusting Antenna Tilt
Move the Joystick up or down to adjust the tilt of the antenna up or down. Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
Adjusting Antenna Bearing
Move the Joystick right or left to adjust the azimuth position of the antenna right
or left. Monitor the displayed bearing value in the BEARING field.
58
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
4)
Turn the Joystick to adjust the range.
5)
To select a new area to be vertically scanned, press the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.
Adjusting Gain
3)
Press the FMS Knob to remove the cursor.
4)
Press the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ is
displayed in the ‘GAIN’ field.
Appendix
Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.
Annun/
Alerts
2)
Abnormal
Operation
Press the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
Additional
Features
1)
Hazard
Avoidance
WARNING: Changing the gain in Weather Mode causes precipitation intensity
to be displayed as a color not representative of the true intensity. Remember
to return the gain setting to ‘Calibrated’ for viewing the actual intensity of
precipitation.
Procedures
Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.
Flight
Planning
3)
GPS Nav
Press the VERTICAL Softkey. A vertical ‘slice’ of the selected area is now
displayed.
AFCS
2)
Nav/Com/
XPDR/Audio
1) While in the Horizontal Scan view, move the Joystick to place the Bearing
Line on the desired storm cell, or other area, to be vertically scanned.
EIS
Vertically Scan a Storm Cell
Flight
Instruments
When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Bearing Line’.
3) Press the ENT Key.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
59
Hazard Avoidance
Press the MODE Softkey.
2)
Press the GROUND Softkey to place the radar in Ground Map Mode.
3)
Press the BACK Softkey.
4)
Press the FMS Knob to activate the cursor.
Nav/Com/
XPDR/Audio
5)
Turn the large FMS Knob to place the cursor in the ‘TILT’ field.
6)
Adjust the antenna tilt angle by turning the small FMS Knob to position the
ground returns as desired.
7)
Press the FMS Knob to remove the cursor.
EIS
1)
AFCS
Flight
Instruments
Ground Mapping
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Sector Scan
2)
Press the FMS Knob to display the cursor.
3)
Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
4)
Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.
5)
If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.
6)
Press the FMS Knob to remove the cursor.
Additional
Features
Antenna Stabilization
Abnormal
Operation
Annun/
Alerts
While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
becomes the center point of the Sector Scan.
1)
To activate or deactivate the antenna stabilization, press the MODE
Softkey.
2)
Press the STAB ON Softkey to activate antenna stabilization or press the
STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.
Weather Attenuated Color Highlight (WATCH®)
To activate or deactivate the WATCH® feature, press the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.
Index
Appendix
1)
60
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Hazard Avoidance
EIS
Nav/Com/
XPDR/Audio
Automatic Standby
When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system automatically switches to Standby Mode.
Flight
Instruments
Weather Alert
To activate or deactivate Weather Alert, press the WX ALRT Softkey. Activating and
deactivating also enables or inhibits the alert on the PFD.
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
61
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
Blank Page
62
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION
Additional
Features
Abnormal
Operation
Annun/
Alerts
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
3)
Appendix
Press the SYN VIS Softkey.
Hazard
Avoidance
2)
Procedures
Displaying SVS Terrain
Press the PFD Softkey.
Flight
Planning
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
1)
GPS Nav
•
•
•
•
•
•
•
AFCS
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 Integrated Flight Deck System.
SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).
SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVS enhancement to the PFD, the following feature enhancements
have been added to the PFD:
Nav/Com/
XPDR/Audio
WARNING: Do not use SVS runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
EIS
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational
awareness only and may not provide the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
63
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Pathways
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
AFCS
GPS Nav
Flight
Planning
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
Procedures
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Press the PFD Softkey.
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
64
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Additional Features
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR Softkey again cycles
back to the original map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
ChartView (Optional)
Annun/
Alerts
Appendix
3)
Press the ENT Key to display the chart.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
Turn the large FMS Knob to scroll through the OPTIONS Menu to Show
Chart.
Abnormal
Operation
2)
Additional
Features
Or:
Press the MENU Key to display the PAGE MENU.
Hazard
Avoidance
While viewing the Navigation Map Page, Nearest Airport Page, or Flight
Plan Page, press the SHW CHRT Softkey.
1)
Procedures
Selecting Terminal Procedures Charts
Flight
Planning
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable charts.
The geo-referenced aircraft position is indicated by an aircraft symbol displayed
on the chart when the current position is within the boundaries of the chart. Not all
charts are geo-referenced. These charts will display an Aircraft Not Shown Icon in the
lower right corner of the MFD.
The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.
GPS Nav
FliteCharts®
AFCS
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.
65
Additional Features
1)
While viewing the Navigation Map Page, Flight Plan Page, or Nearest
Airports Page, press the SHW CHRT Softkey. The airport diagram or
approach chart is displayed on the Airport Information Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to select either the Airport Identifier Box or the
Approach Box. (Press the APR Softkey if the Approach Box is not currently
shown).
4)
Turn the small and large FMS Knob to enter the desired airport identifier.
5)
Press the ENT Key to complete the airport selection.
6)
Turn the large FMS Knob to select the Approach Box.
7)
Turn the small FMS Knob to show the approach chart selection choices.
8)
Turn either FMS Knob to scroll through the available charts.
9)
Press the ENT Key to complete the chart selection.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Selecting a chart
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Selecting Additional Information
1)
While viewing the Airport Taxi Diagram, press the FULL SCN Softkey to
display the information windows (AIRPORT, INFO).
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the AIRPORT, INFO, RUNWAYS, or
FREQUENCIES Box (INFO Box shown).
4)
Turn the small FMS Knob to select the INFO Box choices. If multiple choices
are available, scroll to the desired choice with the large FMS Knob and press
the ENT Key to complete the selection.
5)
Press the FMS Knob again to deactivate the cursor.
1)
While viewing a terminal chart press the MENU Key to display the Page
Menu OPTIONS.
2)
Turn the large FMS Knob to highlight the Chart Setup Menu Option and
press the ENT Key.
Index
Appendix
Annun/
Alerts
Selecting full screen On or Off
66
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Additional Features
Turn the large FMS Knob to move between the FULL SCREEN and COLOR
SCHEME Options.
4)
Turn the small FMS Knob to choose between the On and Off Full Screen
Options.
Flight
Instruments
3)
EIS
Selecting Day, Night, or Automatic View
Nav/Com/
XPDR/Audio
While viewing a terminal chart press the MENU Key to display the Page
Menu OPTIONS.
2)
Turn the large FMS Knob to highlight the Chart Setup Menu Option and
press the ENT Key.
3)
Turn the large FMS Knob to move to the COLOR SCHEME Option.
4)
Turn the small FMS Knob to choose between Day, Auto, and Night Options.
5)
If Auto Mode is selected, turn the large FMS Knob to select the percentage
field. Use the small FMS Knob to change the percentage value. The
percentage value is the day/night crossover point based on the percentage
of backlighting intensity. For example, if the value is set to 15%, the day/
night display changes when the display backlight reaches 15% of full
brightness.
AFCS
1)
Procedures
Hazard
Avoidance
Press the FMS Knob when finished to remove the Chart Setup Menu.
Flight
Planning
6)
GPS Nav
The display must be changed in order for the new setting to become active.
This may be accomplished by selecting another page or changing the
display range.
Additional
Features
AIRPORT DIRECTORY
Abnormal
Operation
Annun/
Alerts
Appendix
The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK Airport Directory databases offer detailed information regarding services, hours of operation, lodging options, and more. This information is viewed on the Airport Information Page by selecting the INFO Softkey until INFO-2 is displayed.
Both Airport Directories are available for downloading at flygarmin.com. However,
copy only one of the databases to the Supplemental Data Card. The system cannot
recognize both databases simultaneously.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
67
Additional Features
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the AIRPORT INFORMATION Page.
Initially, information for the airport closest to the aircraft’s present position
is displayed.
3)
If necessary, select the INFO softkey until INFO-2 is displayed.
SIRIUSXM RADIO ENTERTAINMENT
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
Selecting the XM Radio Page
1)
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3)
Press the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Active Channel and Channel List
The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.
Selecting a channel from the channel list
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Selecting the Airport Directory Page:
1)
While on the XM Radio Page, press the CHNL Softkey.
2)
Press the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
1)
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
2)
Press the ENT Key to activate the selected channel.
Index
Appendix
Annun/
Alerts
Or:
68
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Additional Features
2)
Press the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Press the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
Nav/Com/
XPDR/Audio
While on the XM Radio Page, press the CHNL Softkey.
EIS
1)
Flight
Instruments
Selecting a channel directly
Selecting a Category
Press the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Hazard
Avoidance
2)
Additional
Features
Or:
Abnormal
Operation
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
3)
With the desired channel highlighted, press the ENT Key.
Press the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Press the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
2)
Appendix
While on the XM Radio Page, press the CHNL Softkey.
Annun/
Alerts
Entering a Channel Directly
1)
Procedures
While on the XM Radio Page, press the CHNL Softkey.
Flight
Planning
1)
GPS Nav
Select an Available Channel within the Selected Category
AFCS
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Press the CATGRY Softkey on the XM Radio Page.
2) Press the CAT + and CAT - Softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
69
Additional Features
Flight
Instruments
Assigning Channel Presets
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, while listening to an Active Channel that is wanted
for a preset, press the PRESETS Softkey to access the first five preset
channels (PS1 - PS5).
2) Press the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.
3) Press the SET Softkey.
4) Press any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
Procedures
Flight
Planning
Adjusting Volume
1)
With the XM Radio Page displayed, press the VOL Softkey.
2)
Press the VOL – Softkey to reduce volume or press the VOL + Softkey to
increase volume. (Once the VOL Softkey is pressed, the volume can also be
adjusted using the small FMS Knob.)
Unmuting SiriusXM audio:
Hazard
Avoidance
With the XM Radio Page displayed, press the MUTE Softkey to restore
(unmute) SiriusXM Audio.
1)
While the XM – Radio Page, press the MENU Key to display the PAGE
MENU.
2)
Turn the large FMS Knob to select the Unmute option.
3)
Press the ENT Key to restore (unmute) SiriusXM Audio.
PILOT PROFILES
Creating a profile
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Or:
1) Select the AUX - SYSTEM SETUP Page.
Index
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
70
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Additional Features
Press the ENT Key. A ‘Create Profile’ window is displayed.
Flight
Instruments
4)
5) Use the FMS Knob to enter a profile name up to 16 characters long and
In the next field, use the small FMS Knob to select the desired settings
upon which to base the new profile. Profiles can be created based on
Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or current system settings.
7)
Press the ENT Key.
Nav/Com/
XPDR/Audio
6)
EIS
press the ENT Key. Pilot profile names cannot begin with a blank as the
first letter.
AFCS
8) With ‘CREATE’ highlighted, press the ENT Key to create the profile
Or:
GPS Nav
Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the
ENT Key to activate the new profile.
To cancel the process, select ‘CANCEL’ with the large FMS Knob and press
the ENT Key.
Procedures
Selecting an active profile
1) Select the AUX - SYSTEM SETUP Page.
Press the FMS Knob momentarily to activate the flashing cursor.
Hazard
Avoidance
2)
Flight
Planning
9)
3) Turn the large FMS Knob to highlight the active profile field in the Pilot
Profile Box.
Additional
Features
4) Turn the small FMS Knob to display the pilot profile list and highlight the
desired profile.
Abnormal
Operation
5) Press the ENT Key. The G1000 loads and displays the system settings for
the selected profile.
Renaming a profile
Annun/
Alerts
1) Select the AUX - SYSTEM SETUP Page.
Press the FMS Knob momentarily to activate the flashing cursor.
Appendix
2)
3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box.
4)
Press the ENT Key.
rename.
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
71
Index
5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to
Additional Features
Flight
Instruments
6)
Press the ENT Key.
7) Use the FMS Knob to enter a new profile name up to 16 characters long
and press the ENT Key.
EIS
8) With ‘RENAME’ highlighted, press the ENT Key.
Nav/Com/
XPDR/Audio
9)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
Deleting a profile
AFCS
1) Select the AUX - SYSTEM SETUP Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
GPS Nav
3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box.
4)
Press the ENT Key.
5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to
Flight
Planning
delete.
6)
Press the ENT Key.
Procedures
7) With ‘DELETE’ highlighted, press the ENT Key.
8)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
Hazard
Avoidance
press the ENT Key.
Abnormal
Operation
Additional
Features
Importing a profile from an SD card
1)
Insert an SD card containing the pilot profile(s) into the top card slot on the
MFD.
2)
Turn the FMS Knob to select the AUX - SYSTEM SETUP Page.
3)
Select the IMPORT Softkey.
Or:
Annun/
Alerts
a) Press the MENU Key.
Appendix
b) Turn the FMS Knob to highlight ‘Import Pilot Profile’ and press the ENT
Key.
Index
4)
72
The system displays the Pilot Profile Importing window with ‘IMPORT’
highlighted. To change the selected profile to be imported from the SD card
(shown as ‘SELECT FILE’), turn the large FMS Knob to highlight the profile
file name, then turn the small FMS Knob to highlight a profile from the list,
and press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Additional Features
8)
If successful, the system displays ‘Pilot profile import succeeded.’ in the
IMPORT RESULTS window below. With ‘OK’ highlighted, press the ENT or
CLR Keys or press the FMS Knob to return to the AUX - SYSTEM SETUP
Page. The imported profile becomes the active profile.
Exporting a profile to an SD card
Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
2)
Turn the FMS Knob to select the AUX - SYSTEM SETUP Page.
3)
If necessary, activate the desired pilot profile to export. Only the currently
active Pilot Profile can be exported.
4)
Select the EXPORT Softkey. The system displays the Pilot Profile Exporting
window.
Procedures
1)
Hazard
Avoidance
Appendix
To export the pilot profile using the current supplied name, press the ENT
Key with ‘EXPORT’ highlighted. To change the profile file name turn the
large FMS Knob to highlight the ‘SELECT FILE’ field, then enter the new
name with the large and small FMS Knobs, then press the ENT Key. Then
press the ENT Key with ‘EXPORT’ highlighted.
Annun/
Alerts
b) Turn the FMS Knob to highlight ‘Export Pilot Profile’ and press the ENT
Key.
Abnormal
Operation
a) Press the MENU Key.
Additional
Features
Or:
5)
Flight
Planning
If the imported profile name is the same as an existing profile on the
system, the system displays an ‘Overwrite existing file? OK or CANCEL’
prompt. Press the ENT Key to replace profile on the system with the profile
imported from the SD card, or turn the FMS Knob to highlight ‘CANCEL’
and press the ENT Key to return to the Pilot Profile Importing window.
GPS Nav
7)
AFCS
With ‘IMPORT’ highlighted, press the ENT Key.
Nav/Com/
XPDR/Audio
6)
EIS
If desired, the profile name to be used after profile has been imported can
be changed by turning the FMS Knob to highlight the ‘PROFILE NAME’
field, then use the large and small FMS Knobs to enter the name, and press
the ENT Key. Imported profile names cannot begin with a blank space or
be named ‘DEFAULT’, ‘GARMIN DEFAULTS’ or ‘DEFAULT SETTINGS’.
Flight
Instruments
5)
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
73
6)
If the profile name to be exported is the same as an existing profile file
name on the SD card, the system displays an ‘Overwrite existing file? OK
or CANCEL’ prompt. Press the ENT Key to replace the profile on the SD
card with the profile to be exported, or turn the FMS Knob to highlight
‘CANCEL’ and press the ENT Key to return to the Pilot Profile Exporting
window without exporting the profile.
7)
If successful, the EXPORT RESULTS window displays ‘Pilot profile export
succeeded.’ With ‘OK’ highlighted, press the ENT or CLR Keys, or press the
FMS Knob to return to the AUX - SYSTEM SETUP Page.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Additional Features
74
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Nav/Com/
XPDR/Audio
Reversionary display mode can be manually activated by pressing the DISPLAY
BACKUP Button on the audio panel.
EIS
Should a system detected failure occur in either display, the G1000 automatically
enters reversionary mode. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.
AFCS
ABNORMAL COM OPERATION
Flight
Planning
Procedures
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.
GPS Nav
NOTE: The Beechcraft G58 Pilot’s Operating Handbook (POH) always takes
precedence over the information found in this section.
Hazard
Avoidance
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Additional
Features
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Abnormal
Operation
Annun/
Alerts
Loss of Hazard Functions with Loss of GPS
Position
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
75
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight director
Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
– DME Tuning
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath,
and Vertical Deviation
Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Extreme Pitch Indication
76
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Abnormal Operation
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message
appears on the PFD.
Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
Nav/Com/
XPDR/Audio
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the G1000 stops
navigating in GPS Mode.
EIS
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
Flight
Instruments
DEAD RECKONING
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
77
EIS
Flight
Instruments
Abnormal Operation
Symbolic Aircraft
(Map pages and Inset Map)
Dead Reckoning Indications
As a result of operating in DR Mode, all GPS-derived data is computed based upon
an estimated position and is displayed as yellow text on the display to denote degraded
navigation source information. This data includes the following:
• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
• Wind data and pointers in the Wind Data Box on the PFD
• Current Track Indicator
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE values
Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20
minutes. TAWS are also disabled. Additionally, the accuracy of all nearest information
(airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to
function, but with degraded accuracy.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
CDI ‘DR’ Indication on PFD
78
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
WARNING ANNUNCIATION
Gear up with power below 13 in Hg or flaps
down.
Continuous Tone
(received through the
G1000 audio from
another source)
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
AFCS
GPS Nav
Flight
Planning
Procedures
Left alternator offline.
Right alternator offline.
Right and Left alternators offline.
L or R fuel flow is greater than 27.4 gph
L or R CHT is greater than 238 deg C.
L or R oil temp is greater than 116 deg C.
L or R oil press is greater than 100 psi.
L or R oil press is less than 10 psi.
L or R fuel qty is at zero.
Audio Alert
Nav/Com/
XPDR/Audio
L ALT INOP
R ALT INOP
L-R ALT INOP
FUEL FLOW HI
CHT HI
OIL TEMP HI
OIL PRESS HI
OIL PRESS LO
FUEL QTY LO
Alerts Window Message
EIS
Annunciation
Text
GEAR UP
Hazard
Avoidance
CAUTION ANNUNCIATION
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Annun/
Alerts
Appendix
Single Chime
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
190-00526-04 Rev. B
Left starter relay has power applied.
Right starter relay has power applied.
Left bus voltage greater than 30 VDC.
Right bus voltage greater than 30 VDC.
Left bus voltage less than 24 V.
Right bus voltage less than 24 V.
Aft door not latched.
Press Low — Ops in icing conditions not
approved.
Press Low — Ops in icing conditions not
approved.
Audio Alert
Abnormal
Operation
R AIR PUMP
Alerts Window Message
Additional
Features
Annunciation
Text
L START ENGD
R START ENGD
LBUS VOLT HI
RBUS VOLT HI
LBUS VOLT LO
RBUS VOLT LO
AFT DOOR
L AIR PUMP
79
Annunciation
Text
OIL PRESS LO
FUEL QTY LO
ALT LOAD
Annunciation
Text
BUSES TIED
Audio Alert
L or R oil press is between 30 and 10 psi.
L or R fuel qty is less than or equal to 13 gal.
L or R alternator load exceeds 100 amps.
Single Chime
Single Chime
Single Chime
Alerts Window Message
Audio Alert
Right Bus is tied to Left Bus.
None
ALERT MESSAGE
Alerts Window Message
PFD FAN FAIL – The cooling fan for the PFD is inoperative.
MFD FAN FAIL – The cooling fan for the MFD is inoperative.
AVIONICS FAN – The cooling fan for remote avionics is inoperative.
Audio Alert
None
None
None
AFCS ALERTS
Condition
Annunciation
Description
Pitch Failure
Pitch axis control failure. AP is inoperative.
Roll Failure
Roll axis control failure. AP is inoperative.
MET Switch Stuck, or Pitch
Trim Axis Control Failure
If annunciated when AP is engaged, take control
of the aircraft and disengage the autopilot. If
annunciated when AP is not engaged, move
each half of the MET switch separately to check
if a stuck switch is causing the annunciation.
Yaw Damper Failure
YD control failure; AP also inoperative
System Failure
AP and MET are unavailable. FD may still be
available.
Elevator Mistrim Up
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose up control wheel force upon
autopilot disconnect.
Index
Appendix
Alerts Window Message
ADVISORY ANNUNCIATION
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
80
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Annunciation
Description
Flight
Instruments
Condition
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose down control wheel force upon
autopilot disconnect.
Aileron Mistrim Left
A condition has developed causing the roll servo
to provide a sustained left force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
Aileron Mistrim Right
A condition has developed causing the roll servo to
provide a sustained right force. Ensure the slip/skid
indicator is centered and observe any maximum
fuel imbalance limits.
Rudder Mistrim Left
A condition has developed causing the yaw servo
to provide a sustained force. Ensure the slip/skid
indicator is centered and observe any maximum
fuel imbalance limits.
Rudder Mistrim Right
A condition has developed causing the yaw
servo to provide a sustained force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
Preflight Test
Performing preflight system test. Upon
completion of the test, the aural alert will be
heard.
EIS
Elevator Mistrim Down
Procedures
Hazard
Avoidance
Additional
Features
“Pull Up”
or
Appendix
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
190-00526-04 Rev. B
Aural Message
Annun/
Alerts
Reduced Required
Terrain Clearance
Warning (RTC)
Abnormal
Operation
Excessive Descent
Rate Warning (EDR)
Flight
Planning
MFD
Pop-Up Alert
GPS Nav
Alert Type
AFCS
TAWS-B ALERTS
PFD/MFD
TAWS-B Page
Annunciation
Nav/Com/
XPDR/Audio
Preflight system test has failed.
81
Alert Type
Imminent Terrain
Impact Warning (ITI)
Reduced Required
Obstacle Clearance
Warning (ROC)
Imminent Obstacle
Impact Warning
(IOI)
Reduced Required
Terrain Clearance
Caution (RTC)
Imminent Terrain
Impact Caution (ITI)
Reduced Required
Obstacle Clearance
Caution (ROC)
PFD/MFD
TAWS-B Page
Annunciation
MFD
Pop-Up Alert
or
or
or
or
or
or
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Imminent Obstacle
Impact Caution (IOI)
or
Premature Descent
Alert Caution (PDA)
82
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Aural Message
Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
“Caution, Terrain; Caution,
Terrain”
or
“Terrain Ahead; Terrain
Ahead”
“Terrain Ahead; Terrain
Ahead”
or
“Caution, Terrain; Caution,
Terrain”
“Caution, Obstacle; Caution, Obstacle”
or
“Obstacle Ahead; Obstacle
Ahead”
“Obstacle Ahead; Obstacle
Ahead”
or
“Caution, Obstacle; Caution, Obstacle”
“Too Low, Terrain”
190-00526-04 Rev. B
Annunciations & Alerts
MFD
Pop-Up Alert
Aural Message
None
None
“Five-Hundred”
Altitude Callout
“500”
Negative Climb
Rate Caution (NCR)
“Don’t Sink”
or
“Too Low, Terrain”
or
AFCS
“Sink Rate”
Nav/Com/
XPDR/Audio
Excessive Descent
Rate Caution (EDR)
EIS
PFD/MFD
TAWS-B Page
Annunciation
Flight
Instruments
Alert Type
PFD/MFD
Alert
Annunciation
GPS Nav
TAWS-B SYSTEM STATUS ANNUNCIATIONS
Aural
Message
TAWS TEST
None
None
“TAWS System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS-B System Test Fail
TAWS FAIL
“TAWS System
Failure”
Terrain or Obstacle database
unavailable or invalid, invalid
software configuration, system
audio fault
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
None
“TAWS
Available”
System Test in Progress
None
TAWS Alerting is disabled
None
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Appendix
190-00526-04 Rev. B
None
Annun/
Alerts
Sufficient GPS signal received
after loss
Abnormal
Operation
Excessively degraded GPS
signal, Out of database
coverage area
Additional
Features
No GPS position
Hazard
Avoidance
MFD Terrain or Obstacle
database unavailable or invalid.
TAWS operating with PFD
Terrain or Obstacle databases
Procedures
System Test Pass
Flight
Planning
TAWS-B Page
Annunciation
Alert Type
83
VOICE ALERTS
Voice Alert
“Minimums, minimums”
EIS
Flight
Instruments
Annunciations & Alerts
Nav/Com/
XPDR/Audio
“Vertical track”
“Traffic, Traffic”
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”
“TAS System Test
Passed”
“TAS System Test
Failed”
“One o’clock” through
“Twelve o’clock”
or “No Bearing”
“High”, “Low”, “Same
Altitude” (if within 200
feet of own altitude), or
“Altitude not available”
“Less than one mile”,
“One Mile” through
“Ten Miles”, or “More
than ten miles”
Played when the GTS 820 TAS system passes a pilot-initiated self
test.
Played when the GTS 820 TAS system fails a pilot-initiated self test.
Intruder bearing (GTS 820 only)
Intruder relative altitude (GTS 820 only)
Intruder distance (GTS 820 only)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
“Traffic”
“TIS Not Available”
Description
The aircraft has descended below the preset barometric minimum
descent altitude.
The aircraft is one minute from Top of Descent. Issued only when
vertical navigation is enabled.
Played when a Traffic Advisory (TA) is issued (TIS and GTS 820).
The aircraft is outside the Traffic Information Service (TIS) coverage
area.
Played when a Traffic Advisory (TA) is issued (Skywatch TAS system).
Played when the Skywatch TAS system passes a pilot-initiated self
test.
Played when the Skywatch TAS system fails a pilot-initiated self test.
84
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
The PFD and/or MFD has incorrect software
installed. The system should be serviced.
Flight
Planning
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Annun/
Alerts
The PFD1 configuration module backup memory
has failed. The system should be serviced.
Abnormal
Operation
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The system should be serviced if the
problem persists.
Additional
Features
The PFD and/or MFD is overheating and is reducing
power consumption by dimming the display. If
problem persists, the system should be serviced.
Hazard
Avoidance
The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The MFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The MFD and PFD have different software versions
installed. The system should be serviced.
Procedures
190-00526-04 Rev. B
The PFD and/or MFD self-test has detected a
problem. The system should be serviced.
GPS Nav
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
CNFG MODULE – PFD1
configuration module is inoperative.
AFCS
MFD1 CONFIG – MFD1 config
error. Config service req’d.
Nav/Com/
XPDR/Audio
XTALK ERROR – A flight display
crosstalk error has occurred.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MANIFEST – PFD1 software
mismatch, communication halted.
MANIFEST – MFD1 software
mismatch, communication halted.
PFD1 CONFIG – PFD1 config error.
Config service req’d.
Comments
The pilot profile data was lost. System reverts
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
The MFD and PFD are not communicating with
each other. The system should be serviced.
EIS
Message
DATA LOST – Pilot stored data was
lost. Recheck settings.
Flight
Instruments
MFD & PFD MESSAGE ADVISORIES
85
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MFD & PFD MESSAGE ADVISORIES (CONT.)
Message
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Comments
The PFD1 voltage is low. The system should be
serviced.
The MFD voltage is low. The system should be
serviced.
DATABASE MESSAGE ADVISORIES
Message
MFD1 DB ERR – MFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
86
Comments
The MFD and/or PFD detected a failure in the
navigation database. Attempt to reload the
navigation database. If problem persists, the
system should be serviced.
The MFD and/or PFD detected a failure in the
basemap database.
The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card is
properly inserted in display. Replace terrain card. If
problem persists, the system should be serviced.
The terrain database is present on another LRU, but
is missing on the specified LRU.
The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
87
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Procedures
The MFD detected a failure in the ChartView
database (optional feature). Ensure the data card
is properly inserted. Replace data card. If problem
persists, system should be serviced.
The MFD detected a failure in the FliteCharts
database (optional feature). Ensure the data card
is properly inserted. Replace data card. If problem
persists, system should be serviced.
The MFD detected a failure in the Airport Directory
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists, the
system should be serviced.
The PFD and MFD have different navigation
database versions or regions installed. Crossfill
is off. Check the AUX-SYSTEM STATUS Page
to determine versions or regions. Also, check
the AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be turned
off, then on.
Flight
Planning
190-00526-04 Rev. B
The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
GPS Nav
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
The airport terrain database is present on another
LRU, but is missing on the specified LRU.
AFCS
MFD1 DB ERR – MFD1 Airport
Directory database error exists.
The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data card
is properly inserted. Replace data card. If problem
persists, the system should be serviced.
Nav/Com/
XPDR/Audio
MFD1 DB ERR – MFD1 FliteCharts
database error exists.
Comments
EIS
Message
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
MFD1 DB ERR – MFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 airport
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Flight
Instruments
DATABASE MESSAGE ADVISORIES (CONT.)
DATABASE MESSAGE ADVISORIES (CONT.)
Message
DB MISMATCH – Terrain database
mismatch.
DB MISMATCH – Obstacle
database mismatch.
DB MISMATCH – Airport Terrain
database mismatch.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
NAV DB UPDATED – Active
navigation database updated.
TERRAIN DSP – [PFD1 or
MFD1] Terrain awareness display
unavailable.
Comments
The PFD and MFD have different terrain database
versions or regions installed. Check the AUXSYSTEM STATUS Page to determine versions or
regions. Also, check the AUX-SYSTEM STATUS
Page for a database synchronization function not
completed. After synchronization is complete,
power must be turned off, then on.
The PFD and MFD have different obstacle database
versions or regions installed. Check the AUXSYSTEM STATUS Page to determine versions or
regions. Also, check the AUX-SYSTEM STATUS
Page for a database synchronization function not
completed. After synchronization is complete,
power must be turned off, then on.
The PFD and MFD have different airport terrain
database versions or regions installed. Check the
AUX-SYSTEM STATUS Page to determine versions
or regions. Also, check the AUX-SYSTEM STATUS
Page for a database synchronization function not
completed. After synchronization is complete,
power must be turned off, then on.
System has updated the active navigation database
from the standby navigation database.
One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD or
MFD is missing or invalid.
GMA 1347 MESSAGE ADVISORIES
Message
MANIFEST – GMA1 software
mismatch, communication halted.
GMA1 FAIL – GMA1 is inoperative.
88
Comments
The audio panel has incorrect software installed. The
system should be serviced.
The audio panel self-test has detected a failure.
The audio panel is unavailable. The system should
be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Nav/Com/
XPDR/Audio
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
AFCS
Comments
The audio panel configuration settings do not
match backup configuration memory. The
system should be serviced.
The audio panel self-test has detected a problem
in the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.
EIS
Message
GMA1 CONFIG – GMA1 config error.
Config service req’d.
Flight
Instruments
GMA 1347 MESSAGE ADVISORIES (CONT.)
GIA 63W MESSAGE ADVISORIES
Comments
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
system should be serviced.
Flight
Planning
Procedures
The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.
Hazard
Avoidance
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Additional
Features
Abnormal
Operation
The GIA1 and/or GIA2 temperature is too high. If
problem persists, the system should be serviced.
Annun/
Alerts
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Appendix
190-00526-04 Rev. B
GPS Nav
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
89
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
MANIFEST – GFC software
mismatch, communication halted.
MANIFEST– COM1 software
mismatch, communication halted.
MANIFEST– COM2 software
mismatch, communication halted.
MANIFEST– NAV1 software
mismatch, communication halted.
MANIFEST– NAV2 software
mismatch, communication halted.
COM1 CONFIG – COM1 config
error. Config service req’d.
COM2 CONFIG – COM2 config
error. Config service req’d.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
90
Comments
A GIA mismatch has been detected, where only
one is SBAS capable.
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
COM1 and/or COM2 software mismatch. The
G1000 system should be serviced.
NAV1 and/or NAV2 software mismatch. The
G1000 system should be serviced.
The COM1 and/or COM2 configuration settings
do not match backup configuration memory. The
G1000 system should be serviced.
The system has detected an over temperature
condition in COM1 and/or COM2. The transmitter
is operating at reduced power. If the problem
persists, the system should be serviced.
The system has detected a failure in COM1 and/or
COM2. COM1 and/or COM2 may still be usable.
The system should be serviced when possible.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Loss of GPS navigation due to insufficient
satellites.
Procedures
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
Hazard
Avoidance
Abort approach due to loss of GPS navigation.
Additional
Features
Vertical guidance generated by SBAS is
unavailable, use LNAV only minimums.
Displayed after passing the first waypoint of a
true north approach when the nav angle is set to
‘AUTO’.
Abnormal
Operation
Annun/
Alerts
A failure has been detected in the GPS1 and/or
GPS2 receiver. The receiver may still be available.
The system should be serviced.
Appendix
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index
190-00526-04 Rev. B
GPS integrity is insufficient for the current phase
of flight.
Flight
Planning
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
GPS Nav
The COM1 and/or COM2 transfer switch is stuck
in the enabled (or “pressed”) position. Press the
transfer switch again to cycle its operation. If the
problem persists, the system should be serviced.
AFCS
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
LOI – GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS
navigation. Abort approach.
APR DWNGRADE – Approach
downgraded.
TRUE APR – True north approach.
Change HDG reference to TRUE.
Nav/Com/
XPDR/Audio
Comments
The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”)
position. Press the PTT switch again to cycle its
operation.
If the problem persists, the system should be
serviced.
EIS
Message
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk
key is stuck.
Flight
Instruments
GIA 63W MESSAGE ADVISORIES (CONT.)
91
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 FAIL – G/S1 is inoperative.
G/S2 FAIL – G/S2 is inoperative.
GEA 71 MESSAGE ADVISORIES
Message
GEA1 CONFIG – GEA1 config error.
Config service req’d.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Flight
Planning
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.
Procedures
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MANIFEST – GEA1 software
mismatch, communication halted.
Comments
The remote NAV1 and/or NAV2 transfer switch is
stuck in the enabled (or “pressed”) state. Press
the transfer switch again to cycle its operation.
If the problem persists, the system should be
serviced.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The system should
be serviced.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.
Comments
The GEA1 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
The #1 GEA 71 has incorrect software installed.
The G1000 system should be serviced.
GTX 33 MESSAGE ADVISORIES
Message
MANIFEST – GTX1 software
mismatch, communication halted.
GTX1 MANIFEST – GTX1 software
mismatch, communication halted.
XPDR1 ADS-B FAIL – Transponder:
XPDR1 is unable to transmit ADS-B
messages.
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
92
Comments
The transponder has incorrect software installed.
The system should be serviced.
The transponder has incorrect software installed.
The G1000 system should be serviced.
ADS-B is inoperative. The transponder may not be
receiving a valid GPS position. Other transponder
functions may be available. Service when possible.
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Comments
The #1 transponder should be serviced when
possible.
There is no communication with the #1
transponder.
EIS
Message
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is inoperative.
Flight
Instruments
GTX 33 MESSAGE ADVISORIES (CONT.)
Nav/Com/
XPDR/Audio
GRS 77 MESSAGE ADVISORIES
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
system should be serviced.
AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
GPS source.
be serviced when possible.
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
any GPS information.
system should be serviced.
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS information.
The system should be serviced.
backup GPS information.
The #1 AHRS is operating exclusively in no-GPS
AHRS1 GPS – AHRS1 operating
mode. The system should be serviced.
exclusively in no-GPS mode.
The #1 AHRS and #2 AHRS magnetic model
AHRS MAG DB – AHRS magnetic
database versions do not match.
model database version mismatch.
The #1 AHRS earth magnetic field model is out of
AHRS1 SRVC – AHRS1 Magneticdate. Update magnetic field model when practical.
field model needs update.
GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
South, no magnetic compass.
invalid.
The #1 AHRS has incorrect software installed. The
MANIFEST – GRS1 software
system should be serviced.
mismatch, communication halted.
AFCS
Message
AHRS1 TAS – AHRS1 not receiving
airspeed.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
93
Annunciations & Alerts
EIS
Flight
Instruments
GDC 74A MESSAGE ADVISORIES
Message
MANIFEST – GDC1 software
mismatch, communication halted.
Comments
The GDC 74A has incorrect software installed.
The G1000 system should be serviced.
Message
HDG FAULT – AHRS1 magnetometer
fault has occurred.
MANIFEST – GMU1 software
mismatch, communication halted.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GDL 69.
GDL69 FAIL – GDL 69 has failed.
The receiver is unavailable. The G1000 system
should be serviced
MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The
G1000 system should be serviced.
communication halted.
Message
GWX CONFIG – GWX config error.
Config service req’d.
Appendix
Abnormal
Operation
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GWX 68 MESSAGE ADVISORIES
Index
Comments
A fault has occurred in the #1 GMU 44. Heading
is flagged as invalid. The AHRS uses GPS for
backup mode operation. The G1000 system
should be serviced.
The GMU 44 has incorrect software installed.
The G1000 system should be serviced.
GDL 69/69A MESSAGE ADVISORIES
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
GMU 44 MESSAGE ADVISORIES
Comments
GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.
The GDU is not receiving status packet from the
GWX FAIL – GWX is inoperative.
GWX 68 or the GWX 68 is reporting a fault. The
GWX 68 radar system should be serviced.
GWX SERVICE – GWX needs service. A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
Return unit for repair.
94
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Comments
The GWX 68 has incorrect software installed. The
G1000 system should be serviced.
The GWX 68 indicates severe weather within ±10
degrees of the aircraft heading at a range of 80 to
320 nm.
EIS
Nav/Com/
XPDR/Audio
Message
MANIFEST – GWX software
mismatch, communication halted.
WX ALERT – Possible severe
weather ahead.
Flight
Instruments
GWX 68 MESSAGE ADVISORIES (CONT.)
Flight
Planning
Procedures
MANIFEST – GTS software
mismatch, communication halted.
Comments
The GTS and GDU have incompatible
configurations. This alert is also set when the GTS
has an invalid mode S address configured or the
mode S address does not match both XPDR mode
S addresses.
The GTS has incorrect software installed. The
G1000 system should be serviced.
GPS Nav
Message
GTS CONFIG – GTS config error.
Config service req’d.
AFCS
GTS 820 MESSAGE ADVISORIES
MISCELLANEOUS MESSAGE ADVISORIES
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
Upon power-up, the system detects that a stored
flight plan waypoint is locked. This occurs when
an navigation database update eliminates an
obsolete waypoint. The flight plan cannot find
the specified waypoint and flags this message.
This can also occur with user waypoints in a flight
plan that is deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database,
Or
update the waypoint name/identifier to reflect
the new information.
Hazard
Avoidance
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
95
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
FPL WPT MOVE – Flight plan
waypoint moved.
Comments
The system has detected that a waypoint coordinate
has changed due to a new navigation database
update. Verify that stored flight plans contain
correct waypoint locations.
TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has
expired.
This occurs when a stored flight plan contains
DB CHANGE – Database changed.
procedures that have been manually edited. This
Verify user modified procedures.
alert is issued only after an navigation database
update. Verify that the user-modified procedures
in stored flight plans are correct and up to date.
This occurs when a stored flight plan contains
DB CHANGE – Database changed.
an airway that is no longer consistent with the
Verify stored airways.
navigation database. This alert is issued only
after an navigation database update. Verify
use of airways in stored flight plans and reload
airways as needed.
This occurs when a newly installed navigation
FPL TRUNC – Flight plan has been
database eliminates an obsolete approach or
truncated.
arrival used by a stored flight plan. The obsolete
procedure is removed from the flight plan. Update
flight plan with current arrival or approach.
This occurs when the pilot attempts to activate a
LOCKED FPL – Cannot navigate
stored flight plan that contains locked waypoint.
locked flight plan.
Remove locked waypoint from flight plan.
Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
-[xxxx]
A steep turn is 15 seconds ahead. Prepare to turn.
STEEP TURN – Steep turn ahead.
The aircraft is inside the airspace.
INSIDE ARSPC – Inside airspace.
ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The
aircraft will penetrate the airspace within 10
than 10 minutes.
minutes.
96
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Additional
Features
A parallel course has been selected, causing the
vertical deviation to go invalid.
Hazard
Avoidance
The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
speed constraints. The system automatically
transitions to the next vertical waypoint.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
Procedures
190-00526-04 Rev. B
IAF waypoint for parallel offset has been passed.
Flight
Planning
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
IAF waypoint for parallel offset has been passed.
GPS Nav
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Unsupported leg
type in flight plan.
Bad parallel track geometry.
AFCS
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
past IAF.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach current
vertical waypoint.
Nav/Com/
XPDR/Audio
SLCT NAV – Select NAV on CDI for
approach.
Comments
Special use airspace is near and ahead of the
aircraft position.
Special use airspace is within 2 nm of the aircraft
position.
The system notifies the pilot that the loaded approach
is not active. Activate approach when required.
The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver.
Select the correct frequency for the approach.
The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct
NAV receiver.
EIS
Message
ARSPC NEAR – Airspace near and
ahead.
ARSPC NEAR – Airspace near – less
than 2 nm.
APR INACTV – Approach is not
active.
SLCT FREQ – Select appropriate
frequency for approach.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
97
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
Comments
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in error
as displayed. Do not use GPS to navigate to the
selected non-WGS84 waypoint.
The system is no longer receiving data from the
TRAFFIC FAIL – Traffic device has
traffic system. The traffic device should be serviced.
failed.
FAILED PATH – A data path has failed. A data path connected to the GDU, GSD 41, or
the GIA 63/W has failed.
MAG VAR WARN – Large magnetic The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
variance. Verify all course angles.
near the magnetic poles. Displayed magnetic
course angles may differ from the actual
magnetic heading by more than 2°.
SVS – SVS DISABLED: Out of available Synthetic Vision is disabled because the aircraft is
not within the boundaries of the installed terrain
terrain region.
database.
Synthetic Vision is disabled because a terrain
SVS – SVS DISABLED: Terrain DB
database of sufficient resolution (9 arc-second or
resolution too low.
better) is not currently installed.
Message criteria entered by the user.
SCHEDULER [#] – <message>.
Selected course for LOC1 differs from published
CHECK CRS – Database course for
localizer course by more than 10 degrees.
LOC1 / [LOC ID] is [CRS]°.
Selected course for LOC2 differs from published
CHECK CRS – Database course for
localizer course by more than 10 degrees.
LOC2 / [LOC ID] is [CRS]°.
The SD card was removed from the top card slot
[PFD1 or MFD1] CARD 1 REM –
of the PFD or MFD. The SD card needs to be
Card 1 was removed. Reinsert card.
reinserted.
The SD card was removed from the bottom card
[PFD1 or MFD1] CARD 2 REM –
slot of the PFD or MFD. The SD card needs to be
Card 2 was removed. Reinsert card.
reinserted.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
98
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Nav/Com/
XPDR/Audio
Comments
The SD card in the top card slot of the PFD or
MFD contains invalid data.
The SD card in the bottom card slot of the PFD or
MFD contains invalid data.
EIS
Message
[PFD1 or MFD1] CARD 1 ERR –
Card 1 is invalid.
[PFD1 or MFD1] CARD 2 ERR –
Card 2 is invalid.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
FLIGHT PLAN IMPORT/EXPORT MESSAGES
AFCS
In some circumstances, some messages may appear in conjunction with others.
Abnormal
Operation
Annun/
Alerts
Appendix
‘Too many points. Flight plan truncated.’
Additional
Features
‘File contained user waypoints only.’
Hazard
Avoidance
‘Flight plan partially imported.’
Procedures
‘No flight plan files found to import.’
‘Flight plan import failed.’
Flight
Planning
‘File contained user waypoints only. User
waypoints imported successfully. No
stored flight plan data was modified.’
Description
A flight plan file stored on the SD card was
successfully imported as a stored flight plan.
The file stored on the SD card did not contain
a flight plan, only user waypoints. These
waypoints have been saved to the system
user waypoints. No flight plans stored in the
system have been modified.
The SD card contains no flight plan data.
Flight plan data was not successfully
imported from the SD card.
Some flight plan waypoints were successfully
imported from the SD card, however others
had errors and were not imported. A partial
stored flight plan now exists in the system.
The file stored on the SD card did not contain
a flight plan, only user waypoints. One or
more of these waypoints did not import
successfully.
The flight plan on the SD card contains more
waypoints than the system can support.
The flight plan was imported with as many
waypoints as possible.
GPS Nav
Flight Plan Import/Export Results
‘Flight plan successfully imported.’
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
99
FLIGHT PLAN IMPORT/EXPORT MESSAGES (CONT.)
Flight Plan Import/Export Results
‘Some waypoints not loaded. Waypoints
locked.’
‘User waypoint database full. Not all
loaded.’
‘One or more user waypoints renamed.’
‘Flight plan successfully exported.’
‘Flight plan export failed.’
Description
The flight plan on the SD card contains one
or more waypoints that the system cannot
find in the navigation database. The flight
plan has been imported, but must be edited
within the system before it can be activated
for use.
The flight plan file on the SD card contains
user waypoints. The quantity of stored user
waypoints has exceeded system capacity,
therefore not all the user waypoints on the
SD card have been imported. Any flight plan
user waypoints that were not imported are
locked in the flight plan. The flight plan must
be edited within the system before it can be
activated for use.
One or more imported user waypoints were
renamed when imported due to naming
conflicts with waypoints already existing in
the system.
The stored flight plan was successfully
exported to the SD card.
The stored flight plan was not successfully
exported to the SD card. The SD card may
not have sufficient available memory or the
card may have been removed prematurely.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
100
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Annunciations & Alerts
Displayed if the maximum number for pilot profiles
has been reached.
Flight
Planning
Displayed if the importing operation fails for any
other reason.
Displayed if the importing operation succeeds.
GPS Nav
‘Pilot profile export succeeded.’
Displayed if the export operation succeeds.
Hazard
Avoidance
‘Pilot profile export failed.’
Displayed if the filename matches the name of an
existing file on the SD card.
Displayed if the export operation fails.
Procedures
‘Overwrite existing file?’
AFCS
‘Pilot profile import succeeded.’
Displayed if the SD card does not have one or
more valid pilot profile filenames.
Displayed if the profile name matches the name of
existing profile.
Displayed if the profile name is invalid.
Nav/Com/
XPDR/Audio
‘Profile name invalid. Enter a
different profile name.’
‘All available pilot profiles in use.
Delete a profile before importing
another.’
‘Pilot profile import failed.’
Description
EIS
Pilot Profile Import/Export
Results
‘No pilot profile plan files found to
import.’
‘Overwrite existing profile?’
Flight
Instruments
PILOT PROFILE IMPORT/EXPORT MESSAGES
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
101
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Blank Page
102
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
EIS
ALERTS
Nav/Com/
XPDR/Audio
AFCS
Top Level PFD Softkeys
ALERTS
(optional)
STRMSCP
(optional)
(optional)
METAR
ALERTS
Select the BACK Softkey
to return to the top-level softkeys.
TRFC-2
Hazard
Avoidance
Inset Map Softkeys
Level 2
Level 3
Additional
Features
Level 1
Description
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features
visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the
active flight plan
Displays icons and age on the Inset Map for
selected weather products (optional)
WX LGND
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
103
Index
DCLTR (3)
Appendix
Removes Inset Map
Annun/
Alerts
OFF
Abnormal
Operation
Displays Inset Map in PFD lower left corner
INSET
Procedures
TRFC-1
(optional)
Flight
Planning
(optional)
WX LGND
GPS Nav
(optional)
Level 1
Level 2
Level 3
Displays traffic information on Inset Map
TOPO
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Inset Map
Displays terrain information on Inset Map
Nav/Com/
XPDR/Audio
TERRAIN
Press to display the Stormscope lightning
data on the Inset Map (within a 200 nm
radius of the aircraft)
Displays NEXRAD weather and coverage
information on Inset Map (optional feature)
Displays XM lightning information on Inset
Map (optional feature)
Displays METAR flags on airport symbols
shown on the Inset Map (optional)
AFCS
STRMSCP
GPS Nav
NEXRAD
XM LTNG
METAR
Procedures
Flight
Planning
Description
TRAFFIC
EIS
Flight
Instruments
Appendix
(optional)
Hazard
Avoidance
ALERTS
HSI FRMT
SYN VIS
ALT UNIT
ALERTS
Abnormal
Operation
Additional
Features
Press the BACK Softkey to
return to the top-level softkeys
Annun/
Alerts
METERS
HPA
ARC HSI
Appendix
360 HSI
IN
ALERTS
ALERTS
ALERTS
SYN TERR HRZN HDG APTSIGNS
ALERTS
Index
PATHWAY
PFD Configuration Softkeys
104
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
Level 2
Level 3
PFD
Appendix
Index
105
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Abnormal
Operation
190-00526-04 Rev. B
Additional
Features
360 HSI
Hazard
Avoidance
HSI FRMT
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Procedures
DME
BRG1
Flight
Planning
WIND
GPS Nav
DFLTS
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings,
including changing units to standard
Displays softkeys to select wind data
parameters
Headwind/tailwind and crosswind
OPTN 1
arrows with numeric speed components
Wind direction arrow and numeric
OPTN 2
speed
Wind direction arrow with numeric
OPTN 3
direction and speed
Information not displayed
OFF
AFCS
SYN TERR
Nav/Com/
XPDR/Audio
PATHWAY
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
Displays rectangular boxes representing
the horizontal and vertical flight path of
the active flight plan
Enables synthetic terrain depiction
EIS
SYN VIS
Description
Flight
Instruments
Level 1
Flight
Instruments
Appendix
Level 1
Level 2
Level 3
ARC HSI
Description
Displays the HSI in an arc format
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays softkeys for setting the altimeter
and BARO settings to metric units
METERS
When enabled, displays altimeter in
meters
IN
Press to display the BARO setting as
inches of mercury
HPA
Press to display the BARO setting as
hectopacals
Nav/Com/
XPDR/Audio
EIS
BRG2
Flight
Planning
GPS Nav
AFCS
ALT UNIT
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
Procedures
STD BARO
Hazard
Avoidance
ALERTS
Additional
Features
ADS-B TX
ALERTS
Abnormal
Operation
Press the BACK Softkey to return
to the top-level softkeys.
ALERTS
Annun/
Alerts
Press the BACK Softkey to return
to the previous level softkeys.
Index
Appendix
Transponder Softkeys
106
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
Level 2
Level 3
Description
Flight
Instruments
Level 1
Displays transponder mode selection softkeys
XPDR
STBY
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
IDENT
GPS Nav
CODE
AFCS
VFR
Nav/Com/
XPDR/Audio
ALT
EIS
ON
Appendix
Selects standby mode (transponder does
not reply to any interrogations)
White (On-Ground) - Transponder
generates Mode A and Mode S replies, as
well as transmission of acquisition and
extended squitters, including ADS-B out.
Green (Airborne) - Transponder generates
Mode A and Mode S replies, as well as
transmission of acquisition and extended
squitters, including ADS-B out.
Selects Altitude Mode (selection is usually
automatic)
White (On-Ground) - Transponder does
not allow Mode A or Mode C replies
to interrogations, , but it does permit
acquisition and extended squitters
including ADS-B out, and replies to
discretely addressed Mode S interrogations.
Green (Airborne) - Transponder generates
Mode A, Mode C, and Mode S replies to
interrogations, as well as transmissions
of acquisition and extended squitters
including ADS-B out.
Automatically enters the VFR code (1200 in
the U.S.A. only)
Displays transponder code selection
softkeys 0-7
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
107
Level 1
Level 2
Level 3
0—7
BKSP
Removes numbers entered, one at a time
Nav/Com/
XPDR/Audio
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
ALERTS
Displays Alerts Window
IDENT
AFCS
GPS Nav
Flight
Planning
Description
Activates/deactivates transmission of the
aircraft’s three-dimensional position and
aircraft heading for reception by ADS-B
systems.
Use numbers to enter code
ADS-B TX
EIS
Flight
Instruments
Appendix
MFD SOFTKEY MAP
DCLTR
Procedures
MAP
(optional)
(optional)
SHW CHRT
CHKLIST
DCLTR-1
Press the BACK Softkey on
this level to return to the top
softkey level.
Hazard
Avoidance
DCLTR-2
(Default softkey
is dependant on
the selection made
in the map setup
options)
PROFILE
TOPO
TERRAIN
Additional
Features
TRAFFIC
AIRWAYS
DCLTR-3
(optional)
STRMSCP
(optional)
NEXRAD
AIRWY ON
(optional)
XM LTNG
(optional)
METAR
(optional)
LEGEND
BACK
Press the BACK Softkey on this
level to return to the top softkey level.
AIRWY LO
Abnormal
Operation
AIRWAY HI
194 GAL
BACK
Index
Appendix
Annun/
Alerts
166 GAL
MFD Softkeys
Level 1
Level 2
ENGINE
LEAN
108
Level 3
Description
Displays the LEAN and SYSTEM
softkeys
Displays the engine leaning softkeys
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
Level 2
Level 3
Description
Press to return to the top level softkeys
Abnormal
Operation
Enables second-level Navigation Map
softkeys
Displays traffic information on
Navigation Map
Displays/removes Profile View on
Navigation Map Page
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Navigation Map
Displays terrain information on
Navigation Map
Additional
Features
TERRAIN
BACK
Hazard
Avoidance
TOPO
Press to reset fuel to 194 gallons
Procedures
PROFILE
194 GAL
Flight
Planning
TRAFFIC
GPS Nav
MAP
AFCS
DEC FUEL Press to decrease fuel quantity in 1gallon increments
INC FUEL Press to increase fuel quantity in 1gallon increments
166 GAL Press to reset fuel to 166 gallons
Nav/Com/
XPDR/Audio
Displays fuel system softkeys
SYSTEM
EIS
CYL SLCT Selects the desired cylinder for
monitoring
Highlights the first cylinder that peaks
ASSIST
and displays information for that
cylinder
Press to return to the top level softkeys
BACK
Flight
Instruments
Level 1
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
109
Level 1
Level 2
AIRWAYS
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
GPS Nav
STRMSCP
Flight
Planning
NEXRAD
Procedures
XM LTNG
Hazard
Avoidance
METAR
BACK
DCLTR
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
LEGEND
110
Level 3
Description
Displays airways on the map; cycles
through the following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are
displayed
AIRWY LO: Only low altitude
airways are displayed
AIRWY HI: Only high altitude
airways are displayed
Displays Stormscope weather and
coverage information on Navigation
Map (optional feature)
Displays NEXRAD weather and
coverage information on Navigation
Map (optional feature)
Displays XM lightning information on
Navigation Map (optional feature)
Displays METAR flags on airport
symbols shown on the Inset Map
(optional)
Displays the legend for the selected
weather products. Available only
when NEXRAD, XM LTNG, and/or
METAR softkeys are selected.
Returns to top-level softkeys
Selects desired amount of map detail;
cycles through declutter levels:
DCLTR (No Declutter): All map
features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA
data
DCLTR-3: Removes everything
except the active flight plan
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
Level 2
SHW CHRT
Description
When available, displays optional
airport and terminal procedure charts
When available, displays optional
checklists
Nav/Com/
XPDR/Audio
DATABASE UPDATES
Appendix
Index
111
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Abnormal
Operation
Information regarding the various databases may be viewed on the AUX-System
Status Page.
Additional
Features
NOTE: Loading a database in the system prior to its effective date will result
in the expiration date on the power-up screen and the effective date on the
AUX-System Status Page being displayed in amber.
Hazard
Avoidance
NOTE: Loading a database in the system prior to its effective date will result
in the expiration date on the power-up screen and the effective date on the
AUX-System Status Page being displayed in amber.
Procedures
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
Flight
Planning
CAUTION: When downloading updates to the Jeppesen Navigation Database,
copy the data to an SD card other than a Garmin Supplemental Data Card.
Otherwise, data corruption can occur.
GPS Nav
The system uses Secure Digital (SD) cards to load and store various types of data.
For basic flight operations, SD cards are required for database storage as well as
Jeppesen navigation and Jeppesen ChartView database updates. Not all SD cards are
compatible with the G1000 system. Use only SD cards supplied by Garmin or the
aircraft manufacturer.
AFCS
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
190-00526-04 Rev. B
EIS
CHKLIST
Level 3
Flight
Instruments
Level 1
Jeppesen Databases
The Jeppesen navigation database is updated on a 28-day cycle. The
ChartView database is updated on a 14-day cycle. If the ChartView
database is not updated within 70 days of the expiration date, ChartView
will no longer function. Both of these databases are provided directly
from Jeppesen.
The ChartView database should be copied to the Garmin supplied
Supplemental Data Card which will reside in the bottom card slot on the
MFD. The navigation database must be installed from the Jeppesen or
user supplied SD data card. Contact Jeppesen (www.jeppesen.com) for
subscription and update information.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
NOTE: After the navigation database is installed, the card may be removed.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Updating the active Jeppesen navigation database (not using the
Dual Navigation Database or Automatic Database Synchronization
Features):
1)
With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated
(label of SD card facing left).
2)
Turn the system ON.
3)
4)
Press the NO Softkey to proceed to loading the active database.
Press the YES Softkey to update the active navigation database.
5)
After the update completes, the display starts in normal mode. Do not
remove power while the display is starting.
6)
Turn the system OFF and remove the SD card from the top card slot.
7)
Repeat steps 1 through 6 for the other display (PFD or MFD). Remove the SD
card when finished.
8)
Apply power to the system and press the ENT Key to acknowledge the startup
screen.
9)
Turn the large FMS Knob to select the AUX Page group on the MFD.
Index
10) Turn the small FMS Knob to select the System Status Page.
112
11) Press the Display Database Selection Softkey to show active navigation
database information for each display (MFD1 DB and PFD1 DB). Verify the
correct active navigation database cycle information is shown for each display.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
AFCS
After the navigation database files are copied to the bottom SD card, a
display will appear.
6)
7)
As instructed on the display, press any key to continue.
Press any key to continue. A display will now appear.
8)
Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
9)
Press the ENT Key to acknowledge the startup screen.
Procedures
5)
Hazard
Avoidance
Additional
Features
Abnormal
Operation
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
Annun/
Alerts
12) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
Appendix
13) Turn system power OFF.
14) Remove the SD card from the top card slot of the MFD.
Index
15) Turn system power ON.
16) Press the ENT Key to acknowledge the startup screen.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Flight
Planning
Turn the system ON.
Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
GPS Nav
3)
4)
190-00526-04 Rev. B
Nav/Com/
XPDR/Audio
Loading a standby navigation database:
1) With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the MFD.
2) Verify that an SD card is inserted in the bottom slot of each PFD and the
MFD.
EIS
The dual navigation database feature allows each display to store an
upcoming navigation database on the bottom SD card so that the system
can automatically load it to replace the active database when the new
database becomes effective (the next cycle becomes available seven days
prior to its effective date).
Flight
Instruments
Dual Navigation Database Feature
113
Appendix
Flight
Instruments
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
18) Turn the small FMS Knob to select the System Status Page.
Nav/Com/
XPDR/Audio
EIS
19) Press the Display Database Selection Softkey to show standby navigation
database information for each display (MFD1 DB and PFD1 DB). Verify
the correct standby navigation database cycle information is shown for
each display.
Garmin Databases
The following databases are stored on Supplemental Data Cards provided by
Garmin:
• Expanded basemap
• Terrain
• Airport terrain
Annun/
Alerts
Appendix
Index
• Obstacle
• SafeTaxi
• FliteCharts
• Airport Directory
(AOPA)
After subscribing to the desired database product updates, these updated databases
are copied to each Supplemental Data Card for each display (the card that contains the
FliteCharts or ChartView database resides in the MFD). Since these databases are not
stored internally in the displays, these Supplemental Data Cards must remain in the
bottom card slot of each display.
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
NOTE: The system compares the active databases on each PFD and the MFD,
and displays a system alert message ‘DB Mismatch’ if they are not identical.
Similarly, if the standby databases on each PFD and the MFD are not identical, the system will display a ‘DB Mismatch’ alert for the standby navigation
databases.
Obtaining Garmin Database Updates
The Garmin database updates can be obtained by following the instructions
detailed in the ‘Aviation Databases’ section of the Garmin website (fly.garmin.com).
Once the updated files have been downloaded from the website, a PC equipped with
an appropriate SD card reader is used to unpack and copy the new databases onto the
appropriate Supplemental Data Cards. Equipment required to perform the update is
as follows:
114
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
4)
Apply power to the system, check that the databases are initialized and
displayed on the power-up screen. If a ‘Verifying’ message is seen, wait for
the system to finish loading before proceeding to step 5.
5)
Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right most softkey.
6)
Turn the large FMS Knob to select the AUX Page group on the MFD.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete synching, indicated by ‘Complete’ being displayed.
9)
Remove and reapply power to the system.
Additional
Features
Insert the MFD database card into the bottom card slot of the MFD.
Annun/
Alerts
115
Index
12) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB or PFD1 DB). Verify the correct database cycle
information is shown for each database for each display.
Appendix
11) Turn the small FMS Knob to select the System Status Page.
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Abnormal
Operation
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
190-00526-04 Rev. B
Hazard
Avoidance
3)
Procedures
Update the basemap, SafeTaxi, airport terrain, obstacle and/or airport
directory databases on the MFD card.
Flight
Planning
2)
GPS Nav
With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
AFCS
1)
Nav/Com/
XPDR/Audio
These databases may be copied to one Supplemental Data Card, then
automatically synchronized to other card in the system:
EIS
Updating Basemap, SafeTaxi, Airport Terrain, Obstacle, and Airport
Directory Databases
Flight
Instruments
• Windows-compatible PC computer (running Windows XP, Vista, or Windows 7)
• SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or
equivalent
• Updated database obtained from the Garmin website
• Existing Supplemental Database SD Card (010-00330-41, -42, or -43) from the
MFD. The supplemental data card from the MFD should be used because all
databases (except the active navigation database) are required to reside on this
card.
Appendix
Flight
Instruments
With system power OFF, remove the Supplemental Data Card from the
bottom card slot of the MFD and PFDs.
EIS
2)
Copy the updated terrain database to each of the Supplemental Data Cards.
Copy the updated FliteCharts or ChartView database to one Supplemental
Data Card.
3)
Insert the updated Supplemental Data Cards into the bottom card slot of
the MFD and PFDs. The Supplemental Data Card containing the FliteCharts
or ChartView database is inserted in the MFD.
4)
Apply power to the system, check that the databases are initialized and
displayed on the power-up screen. A ‘Verifying’ message may be seen.
If this message is present, wait for the system to finish loading before
proceeding to step 5.
5)
Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right most softkey.
6)
Turn the large FMS Knob to select the AUX Page group on the MFD.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB or PFD1 DB). Verify the correct database cycle
information is shown for each database for each display.
9)
Remove power from the system.
Magnetic Field Variation Database Update
At startup, the system compares this version of the MV DB with that presently being
used by the AHRS (GRS). If the system determines the MV DB needs to be updated,
a prompt is displayed on the Navigation Map Page, as shown in the following figure.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
1)
Nav/Com/
XPDR/Audio
Updating Terrain, FliteCharts, and ChartView Databases
Index
GRS Magnetic Field Variation Database Update Prompt
116
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Appendix
Flight
Instruments
Loading the magnetic field variation database update:
With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key
on the MFD. A progress monitor is displayed as shown in the following
figure.
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Uploading Database to GRS
Flight
Planning
When the upload is complete, the system is ready for use.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
117
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
Blank Page
118
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Index
E
Procedures
Edit a flight plan 39
F
Additional
Features
Abnormal
Operation
FD 80
Flight Director 13
Flight path marker 63
Flight plan import/export messages 99,
100
FliteCharts® 64, 65
FPA 20
Frequency Transfer 10
Hazard
Avoidance
Annun/
Alerts
G
Gain 59
Ground mapping 60
Appendix
Index
190-00526-04 Rev. B
Flight
Planning
CDI 1, 10, 97
Cell 49, 50
Cell mode 50
Channel Presets 70
ChartView 64, 65
Clearance player 11
GPS Nav
C
AFCS
Barometric Altitude Minimums 3
Barometric pressure 106
Bearing line 59, 60
Databases 111
Database Synchronization 112
Database updates 111, 114
Day/Night views 67
DB Mismatch 114
DCLTR Softkey 64
Dead Reckoning 77
Declutter 76, 103, 110
Direct-to 17
DME 9, 10
DR mode 77, 78
Dual navigation database 113
Nav/Com/
XPDR/Audio
B
D
EIS
Activate a flight plan 18
Active Channel 68
Active database 112, 113
AC-U-KWIK 67
ADF 9, 10, 76
ADS-B 9, 108
AHRS 93, 94
Airport Directory 67
Airport Signs 63, 64
Airways 110
Along Track Offset 34
ALT 54
Altitude
Constraints 20
Altitude mode 54
Altitude volume 54
Antenna stabilization 60
Antenna tilt 58
AOPA 67
AP 80
Audio panel controls
NAV1, NAV2 10
Autopilot 80, 81
Clearance Recorder 11
Code selection softkeys 9
COM 10, 11, 75
Flight
Instruments
A
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index-1
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
H
HF 10
Horizon heading 63
Horizontal scan 59
Horizontal Situation Indicator (HSI) 46
I
Inset Map 103, 104
IOI 82
Navigation database 21
NEXRAD 51, 104, 110
O
OBS 2
Obstacles 88, 90
Overspeed Protection 14
P
Jeppesen 65
Jeppesen navigation database 112
Pathways 63, 64
Pilot Profile Import/Export Messages
101
Pilot Profiles 70
Profile View 109
L
R
Lightning 49, 50, 104
Radio 68
Reversionary mode 75
ROC 82
J
M
Map panning 51
Message advisories 85, 86, 87, 88, 89,
90, 91, 92, 93, 94, 95, 96, 97,
98, 99
MET 80
METAR 51
Minimums 84
Mistrim 80, 81
MKR/MUTE 11
Mode selection softkeys 9
Multi Function Display (MFD)
Softkeys 108
N
NAV 10
NAV1 1, 10
NAV2 1, 10
Navigation
Database 20
Index-2
S
SafeTaxi® 64
SBAS 14, 45, 57, 77, 90, 91
Sector scan 60
Secure Digital (SD) cards 111
SiriusXM 51, 52
Split COM operation 10
STAB 60
Standby 58
Standby Navigation Database 113, 114
Store Flight Plan 39
Stormscope lightning data 49, 50, 104
Strike 49
Strike mode 50
Supplemental Data Card 114
SVS 63, 98
Synthetic Vision System 63
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Index
WATCH® 60
Waypoint Selection Submenu 31, 32
Weather Attenuated Color Highlight 60
Weather data link page 51
Weather radar 57
Wind data 105
X
AFCS
XM lightning 104, 110
XM weather 51
Nav/Com/
XPDR/Audio
TA 84
TAF 51
TAS 54, 84, 93
TAWS 57, 81
Temperature Compensated Altitude 38
Terminal procedures charts 65
Terrain 88, 104, 109
Tilt line 58
Timer 96
Topographical data 104, 109
Traffic 49, 54, 104, 109
Traffic Advisory 53, 54, 84
Traffic map page 54, 55
Transponder 9, 107, 108
Transponder Mode 9
EIS
W
Flight
Instruments
T
GPS Nav
Flight
Planning
U
Procedures
User Defined Holding Pattern 35
User-Defined Holding Pattern 37
Hazard
Avoidance
V
Additional
Features
Vertical navigation 20
Direct-to 19
Vertical speed guidance 21
Vertical track 84
VNV 17, 76, 97
VNV guidance
Disabling 19
Enabling 19
Vspeed 2
VS TGT 20
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-04 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
Index-3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Beechcraft G58
190-00526-04 Rev. B
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Contact Garmin Product Support or view
warranty information at www.flygarmin.com.
© 2005, 2007-2012, 2019 Garmin Ltd. or its subsidiaries
190-00526-04 Rev. B
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