Garmin Beechcraft G58 Reference Guide

®

G1000

Cockpit Reference Guide for the Beechcraft G58

Integrated Flight Deck

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 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software 0857.09 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.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: [phone] Fax: [phone]

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone] Fax [phone]

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Southampton, SO40 9RB, U.K.
Tel: [phone] Fax: [phone]

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone] Fax: [phone]

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied,
transmitted, disseminated, downloaded or stored in any storage medium, for any purpose
without the express written permission of Garmin. Garmin hereby grants permission to
download a single copy of this manual and of any revision to this manual onto a hard drive or
other electronic storage medium to be viewed for personal use, provided that such electronic
or printed copy of this manual or revision must contain the complete text of this copyright
notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.

Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®,
FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and SkyWatch® are
registered trademarks of L-3 Communications; SiriusXM Satellite Radio and SiriusXM Weather
are provided by SiriusXM Satellite Radio, Inc.;

March, 2012 190-00526-03 Rev. A Printed in the U.S.A.

Warnings, Cautions & Notes

WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74A Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the G1000
PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.

WARNING: Traffic information shown on the G1000 Multi Function Display
is provided as an aid in visually acquiring traffic. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition of
conflicting traffic.

WARNING: Use of the Stormscope is not intended for hazardous weather
penetration (thunderstorm penetration). Stormscope information, as
displayed on the G1000 MFD, is to be used only for weather avoidance, not
penetration.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Warnings, Cautions & Notes

WARNING: Do not use data link weather products (e.g., XM WX Satellite
Weather, GFDS World Wide Weather, or FIS-B) for hazardous weather
penetration. Weather information provided by these products is aged by
up to several minutes and may not depict actual weather conditions as they

currently appear.

WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.

WARNING: The Garmin G1000, as installed in the Beechcraft G58 aircraft, has
a very high degree of functional integrity. However, the pilot must recognize
that providing monitoring and/or self-test capability for all conceivable system
failures is not practical. Although unlikely, it may be possible for erroneous
operation to occur without a fault indication shown by the G1000. It is
thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the
cockpit.

WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.

WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Beechcraft G58 Pilot’s Operating Handbook (POH). Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Warnings, Cautions & Notes

WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”

WARNING: Lamp(s) inside this product may 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/aboutGarmin/
environment/disposal.jsp.

WARNING: Because of variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications. North of 72° North latitude at all longitudes. South of
70° South latitude at all longitudes. North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude
between longitude 70° W and 128° W. (Northern Canada). North of 70° North
latitude between longitude 85° E and 114° E. (Northern Russia). South of
55° South latitude between longitude 120° E and 165° E. (Region south of
Australia and New Zealand).

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.

CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI­REFLECTIVE COATING. It is very important to clean the lens using a clean,
lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti­reflective coatings.

CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Warnings, Cautions & Notes

NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.

NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.

NOTE: 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.

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: 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: 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 G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Pilot’s Guide for this aircraft.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Warnings, Cautions & Notes

Blank Page

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Record of Revisions

Part Number Change Summary

190-00526-00 Initial release.
190-00526-01

Rev A

Changed to smaller format
Added Airways, WAAS, VNAV, and Charts
Updated G1000 System Messages
Added other GDU 8.10 parameters

Rev B

Removed FD Formatting feature

190-00526-02 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 Added Profile View

Added new weather product symbols and legend
Added MV DB update procedure
Added other GDU 11.13 parameters

Revision Date of Revision Affected Pages Description

A March, 2012 All Production release.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

RR-1

Record of Revisions

Blank Page

RR-2

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

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

Enter a Transponder Code....................................................................................................... 9

Activate ADS-B Transmit ......................................................................................................... 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

FLIGHT PLANNING ...................................................................................................................... 21

Trip Planning ............................................................................................................................ 21

Create a User Waypoint Defined by Latitude & Longitude ........................................... 23

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

i

Table of Contents

Create a User Waypoint Defined by Radials from Other Waypoints ........................... 23

Create a User Waypoint Defined by a Radial & Distance from Another Waypoint ..25

Delete a User Waypoint ......................................................................................................... 26

Create a Flight Plan ................................................................................................................ 27

Import a Flight Plan from an SD Card ................................................................................ 28

Insert a Waypoint in the Active Flight Plan ...................................................................... 29

Enter an Airway in a Flight Plan .......................................................................................... 29

Invert An Active Flight Plan .................................................................................................. 30

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 30

Store a Flight Plan .................................................................................................................. 31

Edit a Stored Flight Plan ....................................................................................................... 31

Delete a Waypoint from the Flight Plan ............................................................................ 31

Invert and Activate a Stored Flight Plan ........................................................................... 32

Copy a Flight Plan ................................................................................................................... 32

Delete a Flight Plan ................................................................................................................ 32

Graphical Flight Plan Creation ............................................................................................. 33

Export a Flight Plan to an SD Card ..................................................................................... 33

PROCEDURES ................................................................................................................................. 35

Load and Activate a Departure Procedure ....................................................................... 35

Activate A Departure Leg ..................................................................................................... 35

Load An Arrival Procedure .................................................................................................... 35

Activate An Arrival Leg ......................................................................................................... 36

Load and/or Activate an Approach Procedure ................................................................. 37

Activate An Approach in the Active Flight Plan ............................................................... 38

Activate a Vector to Final Approach Fix ............................................................................ 38

Activate A Missed Approach in the Active Flight Plan ................................................... 38

HAZARD AVOIDANCE ................................................................................................................ 39

Customizing the Hazard Displays on the Navigation Map ............................................ 39

STORMSCOPE® (Optional) ..................................................................................................... 39

SiriusXM Weather (Optional) ............................................................................................... 41

Traffic Systems ........................................................................................................................ 43

Terrain Awareness & Warning System (TAWS-B) Display ............................................... 45

Airborne Color Weather Radar ............................................................................................ 47

ADDITIONAL FEATURES ........................................................................................................... 51

Synthetic Vision ....................................................................................................................... 51

Terminal Procedure Charts ................................................................................................... 52

AOPA Airport Directory ......................................................................................................... 54

SiriusXM Radio Entertainment ............................................................................................ 55

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Table of Contents

ABNORMAL OPERATION..........................................................................................................57

Reversionary Mode ................................................................................................................ 57

Abnormal COM Operation .................................................................................................... 57

Hazard Displays with Loss of GPS Position ....................................................................... 57

Unusual Attitudes ................................................................................................................... 58

Dead Reckoning ...................................................................................................................... 59

ANNUNCIATIONS & ALERTS ................................................................................................... 61

WARNING Annunciation ........................................................................................................ 61

CAUTION Annunciation .......................................................................................................... 61

ADVISORY Annunciation........................................................................................................ 62

Alert Message .......................................................................................................................... 62

AFCS ALERTS ............................................................................................................................ 62

TAWS-B Alerts .......................................................................................................................... 63

TAWS-B System Status Annunciations ............................................................................... 65

Voice Alerts .............................................................................................................................. 66

MFD & PFD Message Advisories .......................................................................................... 67

Database Message Advisories ............................................................................................. 68

GMA 1347 Message Advisories ............................................................................................ 70

GIA 63W Message Advisories ............................................................................................... 71

GEA 71 Message Advisories .................................................................................................. 74

GTX 33 Message Advisories .................................................................................................. 74

GRS 77 Message Advisories .................................................................................................. 75

GDC 74A Message Advisories ............................................................................................... 75

GMU 44 Message Advisories ................................................................................................ 76

GDL 69/69A Message Advisories ......................................................................................... 76

GWX 68 Message Advisories ................................................................................................ 76

GTS 820 Message Advisories ................................................................................................ 77

Miscellaneous Message Advisories ..................................................................................... 77

Flight Plan Import/Export Messages .................................................................................. 81

APPENDIX ....................................................................................................................................... 83

PFD Softkey Map .................................................................................................................... 83

MFD Softkey Map ................................................................................................................... 88

Database Updates .................................................................................................................. 90

INDEX .........................................................................................................................................Index-1

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Table of Contents

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iv

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

1)

Press the PFD Softkey.

2)

Press the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

Press the PFD Softkey to display the second-level softkeys.

2)

Press the ALT UNIT Softkey.

3)

Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).

Or

:

Press the HPA Softkey to display the barometric pressure setting in
hectopascals.

4)

Press the BACK Softkey to return to the top-level softkeys.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

CHANGE NAVIGATION SOURCES

1)

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.

2)

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.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

1

Flight Instruments

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

Flight

1)

InstrumentsEIS

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GENERIC TIMER

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.

Flight

PlanningProcedures

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.

CONFIGURE VSPEED BUGS INDIVIDUALLY

Hazard

Avoidance

1)

Press the TMR/REF Softkey.

2)

Turn the

large

FMS Knob to highlight the desired Vspeed.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

3)

Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
speed has been changed from a default value, an asterisk appears next to
the speed).

4)

Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field

5)

Turn the

6)

To remove the window, press the CLR Key or the TMR/REF Softkey.

2

small

FMS Knob clockwise to ON or counterclockwise to OFF.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Instruments

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)

Press the TMR/REF Softkey.

2)

Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.

3)

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.

DISPLAYING WIND DATA

1)

Press the PFD Softkey.

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.

CHANGING HSI FORMAT

1)

Press the PFD Softkey.

2)

Press the HSI FRMT Softkey.

3)

Press the 360 HSI Softkey to display the full size HSI.

Or

:

Press the ARC HSI Softkey to display the arc style HSI.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Annun/

Alerts Appendix Index

3

Flight Instruments

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

4

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Engine Indication System

ENGINE INDICATION SYSTEM

ENGINE DISPLAY

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.

Manifold

Pressure

Gauge

(Left Engine)

RPM Gauge

(Left Engine)

Fuel Flow

Indicator

Oil Temperature

Indicator

Ammeter

Default Engine Page

Propeller Sync
Indicator

Fuel Flow
Numeric
Readout

Cylinder Head
Temperature
Indicator

Oil Pressure
Indicator

Fuel Quantity
Indicator

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

5

Engine Indication System

LEAN ENGINE DISPLAY

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

EGT peak

temperature

(Left Engine)

Exhaust Gas

Flight

Hazard

PlanningProcedures

Avoidance

Temperature

Bar Graphs

(Left Engine)

Cylinder Head

Temperature

Bar Graphs

(Left Engine)

Fuel Flow Leaning
Marker

Difference between peak
and current temperature
of selected cylinder
(Right Engine)

EGT Readout
For Selected
Cylinder
(Right Engine)

CHT Readout
For Selected
Cylinder
(Right Engine)

LEAN Engine Page

1)

Press the ENGINE Softkey.

Features

2)

Additional

Press the LEAN Softkey to display the LEAN Engine Page.

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

Abnormal

Operation

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

AlertsAppendixIndex

Annun/

conditions or when the ASSIST Softkey is pressed.

6

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Engine Indication System

Monitoring the desired cylinder’s EGT and CHT:

From the Lean Display, press the CYL SLCT Softkey to cycle through each

Instruments EIS

Flight

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

XPDR/Audio AFCS GPS Nav

Nav/Com/

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

Planning Procedures

Flight

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.

Avoidance

Hazard

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

7

Engine Indication System

ENGINE SYSTEM DISPLAY

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

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.

NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and
are calculated from the last time the fuel was reset.

System

Information

Fuel Calculation
Information

Abnormal

Operation

AlertsAppendixIndex

Annun/

Electrical
Information

SYSTEM Engine Page

8

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

Tune the ADF using the remote ADF control head.

DME TUNING (OPTIONAL)

1)

Press the DME Softkey.

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.

Nav/Com/XPDR/Audio Panel

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

ENTER A TRANSPONDER CODE

1)

Press the XPDR Softkey to display the transponder mode selection softkeys.

2)

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.

ACTIVATE ADS-B TRANSMIT

1)

Press the XPDR Softkey to display the transponder mode selection softkeys.

2)

Press the ADS-B TX Softkey to enable transmission of three-dimensional
aircraft position and aircraft heading.

3)

Press the ADS-B TX Softkey again to disable transmission.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

9

Nav/Com/XPDR/Audio Panel

SELECTING A COM RADIO

Flight

Transmit/Receive

InstrumentsEIS

Press the COM1 MIC, COM2 MIC
installed) on the audio panel.

Receive Only

Press the COM1, COM2

Nav/Com/

XPDR/AudioAFCSGPS Nav

audio panel.

SELECTING A NAV RADIO

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

Flight

PlanningProcedures

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

Hazard

Avoidance

enters kHz.

3)

Press the Frequency Transfer Key to place the frequency into the active
frequency field.

, or

COM3 MIC Key (optional COM, if

, or

COM3 Key (optional COM, if installed) on the

Features

Additional

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,

Abnormal

Operation

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

AlertsAppendixIndex

Annun/

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

190-00526-03 Rev. A

Nav/Com/XPDR/Audio Panel

DIGITAL CLEARANCE RECORDER AND PLAYER

NOTE: Only the audio for the selected

COM MIC

Key is recorded. Audio is

not recorded for COM3 MIC.

• 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.

INTERCOM SYSTEM (ICS) ISOLATION

Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/

Com radios and music.

Mode

PILOT KEY

ANNUNCIATOR

ALL OFF OFF

PILOT ON OFF

COPLT KEY

ANNUNCIATOR

Pilot Hears

Selected
radios; pilot;
copilot;
passengers;
music

Selected
radios; pilot

Copilot

Hears

Selected
radios; pilot;
copilot;
passengers;
music

Copilot;
passengers;
music

Passenger

Hears

Selected
radios; pilot;
copilot;
passengers;
music

Copilot;
passengers;
music

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

COPILOT OFF ON

CREW ON ON

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Selected
radios; pilot;
passengers;
music

Selected
radios; pilot;
copilot

Copilot

Selected
radios; pilot;
copilot

Selected
radios; pilot;
passengers;
music

Passengers;
music

11

Alerts Appendix Index

Annun/

Nav/Com/XPDR/Audio Panel

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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12

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

AFCS

AUTOMATIC FLIGHT CONTROL SYSTEM

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.

NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.

FLIGHT DIRECTOR ACTIVATION

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Control Pressed

Modes Selected

Lateral Vertical
FD Key Roll Hold (default) ROL Pitch Hold (default) PIT
AP Key Roll Hold (default) ROL Pitch Hold (default) PIT

CWS Switch Roll Hold (default) ROL Pitch Hold (default) PIT

GA Switch Go Around (in air) GA Go Around (in air) GA

ALT Key Roll Hold (default) ROL Altitude Hold ALT

VS Key Roll Hold (default) ROL Vertical Speed VS

VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH

GPS

NAV Key Navigation**

VOR

Pitch Hold (default) PIT

LOC

APR Key Approach**

GPS

VAPP

LOC

Pitch Hold (default)

Glidepath

Glideslope

PIT
GP
GS

HDG Key Heading Select HDG Pitch Hold (default) PIT

*Valid VNV flight plan must be entered before VNV Key press activates flight director.

**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.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

13

AFCS

VERTICAL MODES

Flight

InstrumentsEIS

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch

Pitch Hold

Nav/Com/

XPDR/AudioAFCSGPS Nav

Selected Altitude
Armed

Altitude Hold

Vertical Speed

Flight

PlanningProcedures

Flight Level Change

VNAV

Hazard

Avoidance

VNAV Target Altitude
Armed (GDU 1045
only)

Features

Additional

Glidepath

Abnormal

Operation

Glideslope

AlertsAppendixIndex

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Go Around

* 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

attitude; may be used to climb/

(default) PIT

descend to the Selected Altitude
AFCS armed to capture the altitude

displayed in the Selected Altitude
window

Holds the current Altitude
Reference

ALT Key ALT nnnnn fT

Maintains the current aircraft
vertical speed; may be used to climb/

VS Key VS nnnn fpm

descend to the Selected Altitude
Maintains the current aircraft

airspeed in IAS while the aircraft is
climbing/descending to the Selected

FLC Key FLC nnn kT

Altitude
Captures and tracks the VNAV flight

path

VNV Key VPTH

AFCS armed to capture the altitude
displayed in the VNAV Target
Altitude window

Captures and tracks the SBAS
glidepath on approach

APR Key

Captures and tracks the ILS
glideslope on approach

Disengages the autopilot and
commands a constant pitch attitude
and wings level

Switch

* ALTS

** ALTV

GP

GS

GA

GA

14

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

AFCS

LATERAL MODES

Lateral Mode Description Control Annunciation

Holds the current aircraft roll

Roll Hold

Heading Select

Navigation, GPS
Navigation, VOR (Enroute

Mode)
Navigation, LOC (Glideslope

will not arm or capture)

Navigation, Backcourse

Approach, GPS (Glidepath
mode automatically armed if
vertical guidance is available)

Approach, VOR VAPP
Approach, LOC (Glideslope

Mode automatically armed)

Go Around

attitude or rolls the wings
level, depending on the

(default) ROL

commanded bank angle
Captures and tracks the

Selected Heading

Captures and tracks the
selected navigation source
(GPS, VOR, LOC)

Captures and tracks a
localizer signal for backcourse
approaches

Captures and tracks the
selected navigation source
(GPS, VOR, LOC)

Disengages the autopilot and
commands a constant pitch
angle and wings level

Switch

HDG

Key

NAV

Key

APR

Key

GA

HDG

GPS

VOR

LOC

BC

GPS

LOC

GA

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

15

Alerts Appendix Index

Annun/

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

AFCS

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

16

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

1)

Press the Direct-to

2)

Enter the waypoint identifier.

3)

Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.

4)

If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.

5)

Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.

6)

Enter the desired altitude.

7)

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.

8)

Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

9)

Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.

10)

Enter the desired offset distance before (-) the waypoint.

11)

Press the ENT Key. The ‘Activate?’ field is highlighted.

12)

Press the ENT Key to activate.

( )

Key.

GPS Navigation

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Direct-to Navigation from the PFD

1)

Press the Direct-to Key

2)

Turn the large FMS Knob to place the cursor in the desired selection field.

3)

Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.

4)

Press the ENT Key.

5)

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.

6)

Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

( )

Operation

Abnormal

.

Annun/

Alerts Appendix Index

17

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude.

8)

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

ACTIVATE A STORED FLIGHT PLAN

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

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’.

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.

12)

Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to

highlight the ‘CRS’ field.

13)

Turn the small FMS Knob to enter the desired course to the waypoint.

14)

Press the ENT Key to highlight ‘ACTIVATE?’.

15)

Press the ENT again to activate the Direct-to.

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

Abnormal

Operation

1)

From the Active Flight Plan Page, press the FMS Knob to activate the cursor

AlertsAppendixIndex

Annun/

and turn the large FMS Knob to highlight the desired waypoint.

2)

Press the ACT LEG Softkey on the MFD.

OR

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.

18

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)

Press the FPL Key to display the Active Flight Plan Page.

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

VERTICAL NAVIGATION (VNAV)

The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.

Planning Procedures

Flight

Large White

Text

Large Light

Blue Text

Avoidance

Small Light

Blue Text

Hazard

190-00526-03 Rev. A

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

19

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

Altitudes associated with approach procedures are “auto-designated”. This means

the system automatically uses the altitudes loaded with the approach for giving vertical

Flight

InstrumentsEIS

flight path guidance outside the FAF. Note these altitudes are displayed as small light
blue text.

Altitudes associated with arrival procedures are “manually-designated”. This means
the system does not use the altitudes loaded with the arrival for giving vertical flight
path guidance until designated to do so by the pilot. Note that these altitudes are
initially displayed as white text. These altitudes may be “designated” by placing the

Nav/Com/

XPDR/AudioAFCSGPS Nav

cursor over the desired altitude and pressing the ENT Key. After designation, the text
changes to light blue.

Altitudes that have been designated for use in vertical navigation may also be
made “non-designated” by placing the cursor over the desired altitude and pressing
the CLR Key. The altitude is now displayed only as a reference. It will not be used
to give vertical flight path guidance. Other displayed altitudes may change due to
re-calculations or rendered invalid as a result of manually changing an altitude to a
non-designated altitude.

Flight

PlanningProcedures

White Text Light Blue Text Light Blue

Subdued Text

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Large Text

Small Text

20

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

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.

guidance.

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.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

The system cannot
use this altitude in
determining vertical

flight path guidance.

The system cannot
use this altitude in
determining vertical

flight path guidance.

190-00526-03 Rev. A

TRIP PLANNING

1)

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:

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’.

c)

Press the ENT Key and the flashing cursor moves to the ending
waypoint field.

d)

Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.

Or:

For point-to-point planning:

a)

Enter the identifier of the starting waypoint.

b)

Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.

c)

Again, enter the identifier of the ending waypoint.

d)

Press the ENT Key to accept the waypoint.

Or:

For flight plan leg planning:

a)

Press the FPL Softkey (at the bottom of the display).

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.

FLIGHT PLANNING

Flight Planning

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

21

Flight Planning

d)

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

5)

Turn the large FMS Knob to highlight the departure time (DEP TIME) field.

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

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

speed. Press the
mode, ground speed is provided by the system.

8)

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.

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.

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.

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.

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.

NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.

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.

ENT

Key when finished. Note that in ‘automatic’ page

22

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Planning

CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

1)

Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.

2)

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.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

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.

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 LAT/LON (latitude and longitude).

9)

Press the ENT Key.

CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS

1)

Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.

2)

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.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

23

Flight Planning

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

display a list of waypoint types.

8)

Turn the small FMS Knob to select RAD/RAD (radial/radial).

9)

Press the ENT Key.

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:

a)

b)

c)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter

the desired radial from the reference waypoint.

When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

Turn the small FMS Knob to the right to display the ‘USER’ waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

24

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Planning

12)

Press the ENT Key.

13)

Repeat step 10 to enter the next waypoint name.

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.

15)

Press the ENT Key.

16)

Press the FMS Knob to remove the flashing cursor.

CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM

ANOTHER WAYPOINT

1)

Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.

2)

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.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

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.

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/DIS (radial/distance).

9)

Press the ENT Key.

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:

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.

c)

Press the ENT Key.

Instruments EIS

Flight

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Planning Procedures

Flight

Avoidance

Hazard

Additional

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Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

25

Flight Planning

Or:

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

a)

b)

c)

d)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired

distance from the reference waypoint.

14)

Press the ENT Key.

15)

Press the FMS Knob to remove the flashing cursor.

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

Turn the small FMS Knob to the right to display the ‘USER’ waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

DELETE A USER WAYPOINT

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.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Planning

4)

Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.

5)

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

NOTE: When creating a flight plan in the Active Flight Plan Window, the first

leg is activated automatically after it is created.

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

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.

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Alerts Appendix Index

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Flight Planning

4)

Turn the small FMS Knob to display the Waypoint Information Window.

Flight

InstrumentsEIS

(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)

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

IMPORT A FLIGHT PLAN FROM AN SD CARD

NOTE: See the Annunciations & Alerts section for flight plan import message

descriptions.

Flight

PlanningProcedures

1)

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.

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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28

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.

If an empty flight plan is selected, a list of the available flight plans on
the SD card will be displayed.

Or:

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.

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

190-00526-03 Rev. A

Flight Planning

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

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.

4)

Turn the small FMS Knob. The Waypoint Information Window is now
displayed.

5)

Enter the new flight plan waypoint by one of the following:

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

Or:

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 ‘NRST’ airport
waypoints to the aircraft’s current position.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

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.

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.

Instruments EIS

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XPDR/Audio AFCS GPS Nav

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Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

ENTER AN AIRWAY IN A FLIGHT PLAN

1)

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.

190-00526-03 Rev. A

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29

Flight Planning

4)

Turn the small FMS Knob one click clockwise and press the LD AIRWY

Flight

InstrumentsEIS

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”

Nav/Com/

XPDR/AudioAFCSGPS Nav

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)

Flight

PlanningProcedures

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)

Hazard

Avoidance

With ‘OK’ highlighted, press the ENT Key to invert the flight plan.

REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT

PLAN

Features

Additional

Abnormal

Annun/

Operation

AlertsAppendixIndex

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

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.

d)

Turn the large FMS Knob to highlight the desired flight plan.

e)

Press the EDIT Softkey.

2)

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.

30

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Planning

3)

Press the CLR Key to display a confirmation window.

4)

With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.

STORE A FLIGHT PLAN

1)

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.

EDIT A STORED FLIGHT PLAN

1)

Press the FPL Key on the MFD, then 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 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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

DELETE A WAYPOINT FROM THE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

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.

d)

Turn the large FMS Knob to highlight the desired flight plan.

e)

Press the EDIT Softkey.

2)

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.

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31

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Alerts Appendix Index

Flight Planning

4)

With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel

Flight

InstrumentsEIS

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

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 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

Flight

PlanningProcedures

inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.

COPY A FLIGHT PLAN

1)

Press the FPL Key on the MFD.

2)

Hazard

Avoidance

Features

Additional

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)

Abnormal

Operation

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

AlertsAppendixIndex

Annun/

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 deleted.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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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.

GRAPHICAL FLIGHT PLAN CREATION

1)

Press the FPL Key on the MFD to display the Active Flight Plan Page.

2)

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.

3)

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
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

ABOVE

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

NOTE: See the Annunciations & Alerts section for flight plan export message

descriptions.

1)

Insert the SD card into the top card slot on the MFD.

2)

Press the FPL Key to display the Active Flight Plan Page on the MFD.

3)

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.

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Additional

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Flight Planning

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XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

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34

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.

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.

Procedures

Instruments EIS

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XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

ACTIVATE A DEPARTURE LEG

1)

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.

LOAD AN ARRIVAL PROCEDURE

1)

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.

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35

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

Flight

InstrumentsEIS

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)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key.

10)

With ‘LOAD?’ highlighted, press the ENT Key.

11)

The arrival becomes part of the active flight plan.

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.

b)

Turn the large FMS Knob to highlight the desired waypoint altitude.

c)

Flight

PlanningProcedures

Press the ENT Key to designate the altitude for use in giving vertical
guidance.

ACTIVATE AN ARRIVAL LEG

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

36

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.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Procedures

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

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.

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT APPROACH’.

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
direction of the green arrow to change the display from OFF to BARO.

FMS

Knob in the

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

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Planning Procedures

Flight

Avoidance

Hazard

9)

Press the

FMS

ENT

Key. The cursor moves to the altitude field. Turn the small

Knob to enter the published DA/MDA for the selected approach

procedure.

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?’.

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.

12)

Press the ENT Key.

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37

Procedures

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

Flight

1)

InstrumentsEIS

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Flight

Hazard

PlanningProcedures

Avoidance

Press the PROC Key.

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.

Or:

Press the Go-around Button.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

38

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Hazard Avoidance

HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1)

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.

STORMSCOPE® (OPTIONAL)

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.

Displaying Stormscope Lightning Data on the Navigation Map Page

1)

Press the MAP Softkey.

2)

Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.

Lightning Age Symbol

Strike is less than 6 seconds old

Strike is between 6 and 60 seconds old

Instruments EIS

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Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old

Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode

1)

Press the MENU Key (with the Navigation Map Page displayed).

2)

Turn either FMS Knob to highlight ‘Map Setup’.

3)

Press the ENT Key.

4)

Turn the small FMS Knob to highlight ‘Weather’.

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Alerts Appendix Index

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Hazard Avoidance

5)

Press the ENT Key.

6)

Flight

InstrumentsEIS

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.

Clear Stormscope Lightning Data from the Navigation Map Page

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

Flight

Stormscope Page

PlanningProcedures

1)

2)

Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’

Hazard

Additional

Abnormal

Annun/

1)

Avoidance

2)

Features

Operation

AlertsAppendixIndex

Change the Viewing Mode Between 360˚ and 120˚

1)

2)

NOTE:

If heading input is lost, strikes and/or cells must be cleared manually
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.

Turn the large FMS Knob until the Map Page group is selected.

Turn the small FMS Knob until the Stormscope Page is selected.

Select the Stormscope Page.

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.

NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.

Select the Stormscope Page.

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.

Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Hazard Avoidance

SIRIUSXM WEATHER (OPTIONAL)

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.

Displaying SiriusXM Weather on the Navigation Map Page

1)

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.

Display METAR and TAF information on the Airport Information Page

1)

Turn the large FMS Knob to select the WPT Page Group.

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).

Displaying Weather on the Weather Data Link Page

1)

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.

Map Panning Information – Weather Data Link Page

1)

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.

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.

Instruments EIS

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XPDR/Audio AFCS GPS Nav

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Planning Procedures

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Additional

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Abnormal

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Alerts Appendix Index

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

41

Hazard Avoidance

SiriusXM Weather Products and Symbols

Flight

InstrumentsEIS

Wx Product

Status Icons

NEXRAD - Available for the US and Canada. The age of the displayed data

for each is shown at the right.

Description

Nav/Com/

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ECHO TOP - The age of the displayed data is shown at the right. Not

displayed when CLOUD TOP is displayed.

CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.

XM LIGHTNING - The age of the displayed data is shown at the right.

CELL MOVEMENT - The age of the displayed data is shown at the right.

SIGMET & AIRMET - The age of the displayed data for each is shown at the

right.

METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.

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.

FREEZING LEVEL - The age of the displayed data is shown at the right.

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.

COUNTY WARNING - The age of the displayed data is shown at the right.

42

CYCLONE WARNING - The age of the displayed data is shown at the right.

AIREP - The age of the displayed data is shown at the right.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Hazard Avoidance

Wx Product

Status Icons

Description

PIREP - The age of the displayed data is shown at the right. Urgent Pireps

are displayed in yellow.

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.

TRAFFIC SYSTEMS

• IfTrafcinformationService(TIS)iscongured,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.

Traffic Symbol Description

Non-Threat Traffic

(intruder is beyond 5 nm and greater than 1200’ vertical separation)

Proximity Advisory (PA) (Not available with TIS system)

(intruder is within 5 nm and less than 1200’ vertical separation)

Traffic Advisory (TA)

(closing rate, distance, and vertical separation meet TA criteria)

Instruments EIS

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Additional

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Traffic Symbol Description

Traffic Information Service (TIS)

NOTE: If the G1000 is configured to use a Traffic Advisory System (TAS), TIS
is not available for use.

NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.

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Traffic Advisory Off Scale

43

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Displaying Traffic on the Traffic Map Page

Flight

1)

InstrumentsEIS

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

‘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.

Displaying Traffic on the Navigation Map

1)

Ensure TIS is operating. With the Navigation Map displayed, press the

Flight

PlanningProcedures

MAP Softkey.

2)

Press the TRAFFIC Softkey. Traffic is now displayed on the map.

Traffic Advisory System (TAS)(If Installed)

Displaying Traffic on the Traffic Map Page

Hazard

Additional

Abnormal

Annun/

Avoidance

Features

Operation

AlertsAppendixIndex

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).

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Hazard Avoidance

System Self Test

1)

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.

Displaying Traffic on the Navigation Map

1)

Ensure TAS is operating.

2)

With the Navigation Map displayed, select the MAP Softkey.

3)

Select the TRAFFIC Softkey. Traffic is now displayed on the map.

TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY

NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.

Manual System Test

Instruments EIS

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XPDR/Audio AFCS GPS Nav

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Planning Procedures

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Avoidance

Hazard

1)

While the TAWS-B Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Test TAWS’.

3)

Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.

When all is in working order, “TAWS System Test, OK” is heard.

Display Terrain on 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.

3)

If desired, press the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Press the 360 Softkey to return to the 360° default display.

4)

Rotate the Joystick clockwise to display a larger area or rotate counter­clockwise to display a smaller area.

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45

Additional

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Annun/

Alerts Appendix Index

Hazard Avoidance

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Enable/Disable Aviation Data

1)

While the TAWS-B Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.

3)

Press the ENT Key.

TAWS Inhibit

Color Terrain/Obstacle Location

Red

Yellow

Black

Terrain/Obstacle above or within 100’
below current aircraft altitude.

Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Flight

PlanningProcedures

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Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Inhibit TAWS

While the TAWS-B Page is displayed, press the INHIBIT Softkey.

Or

:

1)

Press the MENU Key.

2)

Turn the small FMS Knob to select ‘Inhibit TAWS’.

3)

Press the ENT Key.

Enable TAWS

While the TAWS-B Page is displayed, press the INHIBIT Softkey.

Or

:

1)

While the TAWS-B Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Enable TAWS’.

3)

Press the ENT Key.

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.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Hazard Avoidance

AIRBORNE COLOR WEATHER RADAR

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.

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.

Displaying Weather on the Weather Radar Page

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.

Or

:

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Adjusting Antenna Tilt

Move the

Joystick

up or down to adjust the tilt of the antenna up or down. Moni-

tor 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.

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47

Alerts Appendix Index

Annun/

Hazard Avoidance

Adjusting Antenna Bearing

Flight

Move the

InstrumentsEIS

or left. Monitor the displayed bearing value in the BEARING field.

Joystick

right or left to adjust the azimuth position of the antenna right

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

2)

Turn the large FMS Knob to select ‘Show Bearing Line’.

3)

Press the ENT Key.

Vertically Scan a Storm Cell

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.

2)

Press the VERTICAL Softkey. A vertical ‘slice’ of the selected area is now

Flight

PlanningProcedures

displayed.

3)

Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.

4)

Turn the Joystick to adjust the range.

5)

To select a new area to be vertically scanned, press the HORIZON Softkey

Hazard

Avoidance

to return to the Horizontal Scan view and repeat the previous steps.

Adjusting Gain

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

48

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.

1)

Press the GAIN Softkey to activate the cursor in the ‘GAIN’ field.

2)

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.

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.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Hazard Avoidance

Ground Mapping

1)

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.

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.

Sector Scan

1)

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.

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Antenna Stabilization

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.

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Alerts Appendix Index

Hazard Avoidance

Weather Alert

Flight

To activate or deactivate Weather Alert, press the WX ALRT Softkey. Activating and

InstrumentsEIS

deactivating also enables or inhibits the alert on the PFD.

Automatic Standby

When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system automatically switches to Standby Mode.

Nav/Com/

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Features

Additional

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Operation

AlertsAppendixIndex

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50

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

SYNTHETIC VISION

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.

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.

Additional Features

ADDITIONAL FEATURES

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

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:

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Traffic

• Airport Signs

• Runway Display

Displaying SVS Terrain

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

Press the SYN TERR Softkey.

4)

Press the BACK Softkey to return to the previous page.

Planning Procedures

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Avoidance

Hazard

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Abnormal

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Alerts Appendix Index

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51

Additional Features

Displaying Pathways

Flight

Nav/Com/

Flight

Hazard

1)

InstrumentsEIS

XPDR/AudioAFCSGPS Nav

PlanningProcedures

Avoidance

Press the PFD Softkey.

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.

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 HRZN HDG Softkey.

5)

Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

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

Features

Additional

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

AlertsAppendixIndex

Annun/

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

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Additional Features

the DCLTR Softkey a third time removes the airport runway layout, unless the airport

Instruments EIS

Flight

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

XPDR/Audio AFCS GPS Nav

Nav/Com/

on the ground. This database is updated on a 56-day cycle.

ChartView (Optional)

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

Planning Procedures

Flight

function.

FliteCharts

®

FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable

Avoidance

Hazard

charts. Current aircraft position is not displayed on FliteCharts.

The FliteCharts database contains procedure charts for the United States only.

Additional

This database is updated on a 28-day cycle. If not updated within 180 days of the

Features

expiration date, FliteCharts will no longer function.

View Charts from the Navigation Map Page

1)

Press the SHW CHRT Softkey when displayed.

Or

:

Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.

2)

Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.

3)

Press the GO BACK Softkey to return to the previous page.

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Alerts Appendix Index

Additional Features

View Charts from the Active Flight Plan Page

Flight

1)

InstrumentsEIS

While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.

2)

Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.

3)

Press the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.

Nav/Com/

XPDR/AudioAFCSGPS Nav

4)

Press the GO BACK Softkey to return to the previous page.

Change Day/Night View

1)

While viewing a 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)

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

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.

5)

Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.

6)

In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.

7)

Press the FMS Knob when finished to remove the Chart Setup Menu.

AOPA AIRPORT DIRECTORY

Abnormal

Operation

AOPA Airport Directory adds enhanced airport information when viewing airports

on the WPT-Airport Information Page.

AlertsAppendixIndex

Annun/

This database is updated four times per year. Check fly.garmin.com for the current

database.

View Airport Directory Information

While viewing the WPT-Airport Information Page, if necessary, press the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.

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Additional Features

SIRIUSXM RADIO ENTERTAINMENT

Instruments EIS

Flight

The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.

Selecting the XM Radio Page

XPDR/Audio AFCS GPS Nav

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

Nav/Com/

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.

Planning Procedures

Flight

Selecting a Category

The Category Box of the XM Radio Page displays the currently selected category
of audio.

Avoidance

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

Hazard

Additional

Features

desired category with the small FMS Knob.

Operation

3)

Press the ENT Key.

Abnormal

Select an Available Channel within the Selected Category

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.

Or

:

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.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

55

Alerts Appendix Index

Annun/

Additional Features

Entering a Channel Directly

Flight

1)

InstrumentsEIS

While on the XM Radio Page, press the CHNL Softkey.

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.

4)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

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),

Flight

PlanningProcedures

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.

Adjusting Volume

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

56

1)

On the XM Radio Page, press the RADIO Softkey.

2)

Press the VOL Softkey to access the volume control softkeys.

3)

Press VOL + or VOL - softkeys to adjust the volume level.

4)

Press the MUTE Softkey to mute the radio audio.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Abnormal Operation

Instruments EIS

ABNORMAL OPERATION

Flight

REVERSIONARY MODE

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.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Reversionary display mode can be manually activated by pressing the DISPLAY

BACKUP Button on the audio panel.

NOTE: The Beechcraft G58 Pilot’s Operating Handbook (POH) always takes
precedence over the information found in this section.

ABNORMAL COM OPERATION

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.

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

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.

Loss of Hazard Functions with Loss of GPS

Position

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

57

Abnormal Operation

UNUSUAL ATTITUDES

Flight

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary

InstrumentsEIS

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:

• TrafcAnnunciations

• AFCSAnnunciations

Nav/Com/

XPDR/AudioAFCSGPS Nav

• Flightdirector

Command Bars

• InsetMap

• Temperatures

• DMEInformation

Window

• WindData

• SelectedHeadingBox

Flight

PlanningProcedures

• SelectedCourseBox

• TransponderStatus

Box

Hazard

Avoidance

• 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

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

58

Extreme Pitch Indication

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Abnormal Operation

DEAD RECKONING

Instruments EIS

Flight

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.

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.

XPDR/Audio AFCS GPS Nav

Nav/Com/

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

Planning Procedures

Flight

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.

Avoidance

Hazard

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

Additional

of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or

Features

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

Operation

Abnormal

DR while there is no heading and/or airspeed data available should not be used for
navigation.

Annun/

DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the

Alerts Appendix Index

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.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

59

Abnormal Operation

Flight

InstrumentsEIS

CDI ‘DR’ Indication on PFD

Symbolic Aircraft

(Map pages and Inset Map)

Nav/Com/

XPDR/AudioAFCSGPS Nav

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eldsexceptActiveLeg,TAS,andDTK

• GPSBearingPointer

• WinddataandpointersintheWindDataBoxonthePFD

Flight

• CurrentTrackIndicator

PlanningProcedures

• 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

Hazard

(airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to

Avoidance

function, but with degraded accuracy.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

60

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

ANNUNCIATIONS & ALERTS

WARNING ANNUNCIATION

Annunciation

Text

GEAR UP Gear up with power below 13 in Hg or flaps

L ALT INOP Left alternator offline. Repeating Tone
R ALT INOP Right alternator offline. Repeating Tone

L-R ALT INOP Right and Left alternators offline. Repeating Tone

FUEL FLOW HI L or R fuel flow is greater than 27.4 gph Repeating Tone

CHT HI L or R CHT is greater than 238 deg C. Repeating Tone

OIL TEMP HI L or R oil temp is greater than 116 deg C. Repeating Tone

OIL PRESS HI L or R oil press is greater than 100 psi. Repeating Tone

OIL PRESS LO L or R oil press is less than 10 psi. Repeating Tone

FUEL QTY LO L or R fuel qty is at zero. Repeating Tone

CAUTION ANNUNCIATION

Annunciation

Text

L START ENGD Left starter relay has power applied. Single Chime

R START ENGD Right starter relay has power applied. Single Chime

LBUS VOLT HI Left bus voltage greater than 30 VDC. Single Chime

RBUS VOLT HI Right bus voltage greater than 30 VDC. Single Chime
LBUS VOLT LO Left bus voltage less than 24 V. Single Chime
RBUS VOLT LO Right bus voltage less than 24 V. Single Chime

AFT DOOR Aft door not latched. Single Chime

L AIR PUMP Press Low — Ops in icing conditions not

approved.

R AIR PUMP Press Low — Ops in icing conditions not

approved.

Alerts Window Message Audio Alert

down.

(received through the

Alerts Window Message Audio Alert

Continuous Tone

G1000 audio from

another source)

Single Chime

Single Chime

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

61

Annunciations & Alerts

Annunciation

Flight

InstrumentsEIS

Text

OIL PRESS LO L or R oil press is between 30 and 10 psi. Single Chime

Alerts Window Message Audio Alert

FUEL QTY LO L or R fuel qty is less than or equal to 13 gal. Single Chime

ALT LOAD L or R alternator load exceeds 100 amps. Single Chime

ADVISORY ANNUNCIATION

Nav/Com/

XPDR/AudioAFCSGPS Nav

Annunciation

Alerts Window Message Audio Alert

Text

BUSES TIED Right Bus is tied to Left Bus. None

ALERT MESSAGE

Alerts Window Message Audio Alert

PFD FAN FAIL – The cooling fan for the PFD is inoperative.

Flight

PlanningProcedures

MFD FAN FAIL – The cooling fan for the MFD is inoperative.
AVIONICS FAN – The cooling fan for remote avionics is inoperative.

AFCS ALERTS

Condition Annunciation Description

Hazard

Pitch Failure Pitch axis control failure. AP is inoperative.

Avoidance

None
None
None

Roll Failure Roll axis control failure. AP is inoperative.

Features

Additional

MET Switch Stuck, or Pitch
Trim Axis Control Failure

Abnormal

Operation

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.

AlertsAppendixIndex

Annun/

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.

62

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

Condition Annunciation Description

Elevator Mistrim Down 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.

Preflight system test has failed.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

TAWS-B ALERTS

Alert Type

Excessive Descent
Rate Warning (EDR)

Reduced Required
Terrain Clearance
Warning (RTC)

190-00526-03 Rev. A

PFD/MFD
TAWS-B Page
Annunciation

MFD

Pop-Up Alert

or

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

or

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

63

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

Flight

Alert Type

InstrumentsEIS

Imminent Terrain
Impact Warning (ITI)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Reduced Required
Obstacle Clearance
Warning (ROC)

Imminent Obstacle
Impact Warning
(IOI)

Flight

PlanningProcedures

Reduced Required
Terrain Clearance
Caution (RTC)

Hazard

Avoidance

Imminent Terrain
Impact Caution (ITI)

Features

Additional

Reduced Required
Obstacle Clearance

Abnormal

Operation

Caution (ROC)

AlertsAppendixIndex

Annun/

Imminent Obstacle
Impact Caution (IOI)

Premature Descent
Alert Caution (PDA)

PFD/MFD

TAWS-B Page

Annunciation

MFD

Pop-Up Alert

or

or

or

or

or

or

or

Aural Message

Terrain Ahead, Pull Up; Ter-

rain 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; Cau-

tion, Obstacle”

or

“Obstacle Ahead; Obstacle

Ahead”

“Obstacle Ahead; Obstacle

Ahead”

or

“Caution, Obstacle; Cau-

tion, Obstacle”

“Too Low, Terrain”

64

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

Alert Type

Altitude Callout

PFD/MFD
TAWS-B Page
Annunciation

None None “Five-Hundred”

MFD

Pop-Up Alert

Aural Message

“500”

Excessive Descent

“Sink Rate”

Rate Caution (EDR)

Negative Climb
Rate Caution (NCR)

or

“Don’t Sink”

or

“Too Low, Terrain”

TAWS-B SYSTEM STATUS ANNUNCIATIONS

PFD/MFD

Alert Type

Alert

Annunciation

System Test in Progress TAWS TEST None

System Test Pass None None

TAWS Alerting is disabled

MFD Terrain or Obstacle
database unavailable or invalid.
TAWS operating with PFD
Terrain or Obstacle databases

TAWS-B System Test Fail TAWS FAIL

Terrain or Obstacle database
unavailable or invalid, invalid
software configuration, system
audio fault

No GPS position NO GPS POSITION

Excessively degraded GPS
signal, Out of database
coverage area

Sufficient GPS signal received
after loss

None TERRAIN DATABASE FAILURE None

None None

TAWS-B Page
Annunciation

None None

TAWS FAIL

None

Aural

Message

“TAWS System

Test OK”

“TAWS System

Failure”

“TAWS System

Failure”

“TAWS Not

Available”

“TAWS Not

Available”

“TAWS

Available”

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

65

Annunciations & Alerts

VOICE ALERTS

Flight

InstrumentsEIS

Voice Alert Description

“Minimums, minimums” The aircraft has descended below the preset barometric minimum

descent altitude.

“Vertical track” The aircraft is one minute from Top of Descent. Issued only when

vertical navigation is enabled.

Nav/Com/

XPDR/AudioAFCSGPS Nav

“Traffic” Played when a Traffic Advisory (TA) is issued (TIS and GTS 820).

“TIS Not Available” The aircraft is outside the Traffic Information Service (TIS) coverage

area.

“Traffic, Traffic” Played when a Traffic Advisory (TA) is issued (Skywatch TAS system).

“Traffic Advisory System

Test Passed”

“Traffic Advisory 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.

Test Failed”

Flight

PlanningProcedures

“TAS System Test

Passed”

“TAS System Test

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.

Failed”

“One o’clock” through

Hazard

“Twelve o’clock”

Avoidance

Intruder bearing (GTS 820 only)

or “No Bearing”

“High”, “Low”, “Same

Features

Altitude” (if within 200

Additional

Intruder relative altitude (GTS 820 only)

feet of own altitude), or

“Altitude not available”

Abnormal

Operation

“Less than one mile”,

Intruder distance (GTS 820 only)

“One Mile” through

“Ten Miles”, or “More

AlertsAppendixIndex

Annun/

than ten miles”

66

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Message Comments

DATA LOST

– Pilot stored data was

lost. Recheck settings.

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.

XTALK ERROR

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

The MFD and PFD are not communicating with
each other. The system should be serviced.

The PFD and/or MFD self-test has detected a
problem. The system should be serviced.

service. Return unit for repair.

MANIFEST

mismatch, communication halted.

MANIFEST

– PFD1 software

– MFD1 software

The PFD and/or MFD has incorrect software
installed. The system should be serviced.

mismatch, communication halted.

PFD1 CONFIG

– PFD1 config error.

Config service req’d.

The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.

MFD1 CONFIG

– MFD1 config

error. Config service req’d.

The MFD configuration settings do not match
backup configuration memory. The system should
be serviced.

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

PFD1 COOLING

– PFD1 has poor

cooling. Reducing power usage.

The MFD and PFD have different software versions
installed. The system should be serviced.

The PFD and/or MFD is overheating and is reducing
power consumption by dimming the display. If

MFD1 COOLING

– MFD1 has poor

problem persists, the system should be serviced.

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

MFD1 KEYSTK

Key is stuck.

CNFG MODULE

configuration module is inoperative.

– PFD1 [key name]

– MFD [key name]

– PFD1

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.

The PFD1 configuration module backup memory
has failed. The system should be serviced.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

67

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

PFD1 VOLTAGE

Message Comments

– PFD1 has low

voltage. Reducing power usage

MFD1 VOLTAGE

– MFD1 has low

voltage. Reducing power usage

Nav/Com/

XPDR/AudioAFCSGPS Nav

DATABASE MESSAGE ADVISORIES

Message Comments

MFD1 DB ERR

– MFD1 navigation

database error exists.

PFD1 DB ERR

– PFD1 navigation

database error exists.

MFD1 DB ERR

Flight

PlanningProcedures

database error exists.

PFD1 DB ERR

– MFD1 basemap

– PFD1 basemap

database error exists.

MFD1 DB ERR

– MFD1 terrain

database error exists.

Hazard

Avoidance

PFD1 DB ERR

– PFD1 terrain

database error exists.

MFD1 DB ERR

Features

Additional

database missing.

PFD1 DB ERR

database missing.

Abnormal

Operation

MFD1 DB ERR

– MFD1 terrain

– PFD1 terrain

– MFD1 obstacle

database error exists.

AlertsAppendixIndex

Annun/

PFD1 DB ERR

– PFD1 obstacle

database error exists.

MFD1 DB ERR

– MFD1 obstacle

database missing.

PFD1 DB ERR

– PFD1 obstacle

database missing.

The PFD1 voltage is low. The system should be
serviced.

The MFD voltage is low. The system should be
serviced.

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.

68

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

terrain database error exists.

MFD1 DB ERR

terrain database missing.

PFD1 DB ERR

– MFD1 airport

– PFD1 airport

– MFD1 airport

– PFD1 airport

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.

The airport terrain database is present on another
LRU, but is missing on the specified LRU.

terrain database missing.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

MFD1 DB ERR

database error exists.

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– MFD1 Chartview

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.

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.

MFD1 DB ERR

– MFD1 FliteCharts

database error exists.

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.

MFD1 DB ERR

– MFD1 Airport

Directory database error exists.

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.

DB MISMATCH

– Navigation

database mismatch. Xtalk is off.

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

69

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

DB MISMATCH

Message Comments

– Terrain database

mismatch.

Nav/Com/

XPDR/AudioAFCSGPS Nav

DB MISMATCH

– Obstacle

database mismatch.

Flight

PlanningProcedures

DB MISMATCH

– Airport Terrain

database mismatch.

Hazard

Avoidance

NAV DB UPDATED

Features

Additional

navigation database updated.

TERRAIN DSP

MFD1] Terrain awareness display

Abnormal

Operation

unavailable.

– Active

– [PFD1 or

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

AlertsAppendixIndex

Annun/

Message Comments

MANIFEST – GMA1 software

mismatch, communication halted.

GMA1 FAIL

70

– GMA1 is inoperative.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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.

190-00526-03 Rev. A

Annunciations & Alerts

GMA 1347 MESSAGE ADVISORIES (CONT.)

Message Comments

GMA1 CONFIG

– GMA1 config error.

Config service req’d.

The audio panel configuration settings do not
match backup configuration memory. The
system should be serviced.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

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.

GIA 63W MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG

Config service req’d.

– GIA1 config error.

The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The

GIA2 CONFIG

– GIA2 config error.

system should be serviced.

Config service req’d.

GIA1 CONFIG

error. Config service req’d.

GIA2 CONFIG

– GIA1 audio config

– GIA2 audio config

The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.

error. Config service req’d.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.

The GIA1 and/or GIA2 temperature is too high. If
problem persists, the system should be serviced.

The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.

71

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

HW MISMATCH

Message Comments

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

mismatch. GIA2 communication

Nav/Com/

XPDR/AudioAFCSGPS Nav

halted.

MANIFEST

– GIA hardware

– GIA1 software

mismatch, communication halted.

MANIFEST

– GIA2 software

mismatch, communication halted.

MANIFEST

– GFC software

mismatch, communication halted.

Flight

MANIFEST

PlanningProcedures

– COM1 software

mismatch, communication halted.

MANIFEST

– COM2 software

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

Hazard

Avoidance

MANIFEST

– NAV1 software

– NAV2 software

mismatch, communication halted.

Features

COM1 CONFIG

Additional

– COM1 config

error. Config service req’d.

COM2 CONFIG

Abnormal

Operation

error. Config service req’d.

COM1 TEMP

Reducing transmitter power.

AlertsAppendixIndex

Annun/

COM2 TEMP

– COM2 config

– COM1 over 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.

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.

72

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

COM1 PTT

– COM1 push-to-talk key

is stuck.

COM2 PTT

key is stuck.

– COM2 push-to-talk

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.

COM1 RMT XFR

transfer key is stuck.

COM2 RMT XFR

transfer key is stuck.

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

GPS NAV LOST

navigation. Insufficient satellites.

GPS NAV LOST

navigation. Position error.

GPS NAV LOST

navigation. GPS fail.

ABORT APR

navigation. Abort approach.

APR DWNGRADE

downgraded.

TRUE APR

Change HDG reference to TRUE.

– COM1 remote

– COM2 remote

– Loss of GPS

– Loss of GPS

– Loss of GPS

– Loss of GPS

– Approach

– True north approach.

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.

GPS integrity is insufficient for the current phase
of flight.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS navigation.

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’.

GPS1 SERVICE

service. Return unit for repair.

– GPS1 needs

A failure has been detected in the GPS1 and/or
GPS2 receiver. The receiver may still be available.

GPS2 SERVICE

– GPS2 needs

The system should be serviced.

service. Return unit for repair.

NAV1 SERVICE

service. Return unit for repair.

– NAV1 needs

A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.

NAV2 SERVICE

– NAV2 needs

The system should be serviced.

service. Return unit for repair.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

73

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

NAV1 RMT XFR

Message Comments

– NAV1 remote

transfer key is stuck.

NAV2 RMT XFR

– NAV2 remote

transfer key is stuck.

Nav/Com/

XPDR/AudioAFCSGPS Nav

G/S1 FAIL
G/S2 FAIL

G/S1 SERVICE

– G/S1 is inoperative.
– G/S2 is inoperative.

– G/S1 needs service.

Return unit for repair.

G/S2 SERVICE

– G/S2 needs service.

Return unit for repair.

Flight

PlanningProcedures

GEA 71 MESSAGE ADVISORIES

Message Comments

GEA1 CONFIG

– GEA1 config error.

Config service req’d.

Hazard

Avoidance

MANIFEST

– GEA1 software

mismatch, communication halted.

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.

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.

Features

Additional

GTX 33 MESSAGE ADVISORIES

Message Comments

Abnormal

Operation

XPDR1 CONFIG

– XPDR1 config
error. Config service req’d.

AlertsAppendixIndex

Annun/

MANIFEST

– GTX1 software

mismatch, communication halted.

XPDR1 SRVC

– XPDR1 needs

service. Return unit for repair.

XPDR1 FAIL

74

– XPDR1 is inoperative.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.

The transponder has incorrect software installed.
The system should be serviced.

The #1 transponder should be serviced when
possible.

There is no communication with the #1
transponder.

190-00526-03 Rev. A

Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES

Message Comments

AHRS1 TAS

– AHRS1 not receiving

airspeed.

AHRS1 GPS

– AHRS1 using backup

GPS source.

AHRS1 GPS

– AHRS1 not receiving

any GPS information.

AHRS1 GPS

– AHRS1 not receiving

backup GPS information.

AHRS1 GPS

– AHRS1 operating

exclusively in no-GPS mode.

AHRS MAG DB

– AHRS magnetic

model database version mismatch.

AHRS1 SRVC

– AHRS1 Magnetic-

field model needs update.

GEO LIMITS

– AHRS1 too far North/

South, no magnetic compass.

MANIFEST

– GRS1 software

mismatch, communication halted.

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.

The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.

The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.

The #1 AHRS is not receiving backup GPS information.
The system should be serviced.

The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.

The #1 AHRS and #2 AHRS magnetic model
database versions do not match.

The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.

The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
invalid.

The #1 AHRS has incorrect software installed. The
system should be serviced.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

GDC 74A MESSAGE ADVISORIES

Message Comments

MANIFEST

– GDC1 software

mismatch, communication halted.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

The GDC 74A has incorrect software installed.
The G1000 system should be serviced.

75

Alerts Appendix Index

Annun/

Annunciations & Alerts

GMU 44 MESSAGE ADVISORIES

Flight

InstrumentsEIS

HDG FAULT

Message Comments

– AHRS1 magnetometer

fault has occurred.

MANIFEST

Nav/Com/

XPDR/AudioAFCSGPS Nav

mismatch, communication halted.

– GMU1 software

GDL 69/69A MESSAGE ADVISORIES

Message Comments

GDL69 CONFIG

– GDL 69 config

error. Config service req’d.

Flight

PlanningProcedures

GDL69 FAIL

MANIFEST

– GDL 69 has failed.

– GDL software mismatch,

communication halted.

Hazard

Avoidance

GWX 68 MESSAGE ADVISORIES

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 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.
The receiver is unavailable. The G1000 system
should be serviced

The GDL 69 has incorrect software installed. The
G1000 system should be serviced.

Features

Additional

GWX CONFIG

Config service req’d.

Abnormal

Operation

GWX FAIL

AlertsAppendixIndex

Annun/

GWX SERVICE

Return unit for repair.

76

Message Comments

– GWX config error.

GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.

– GWX is inoperative.

The GDU is not receiving status packet from the
GWX 68 or the GWX 68 is reporting a fault. The
GWX 68 radar system should be serviced.

– GWX needs service.

A failure has been detected in the GWX 68. The
GWX 68 may still be usable.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

GWX 68 MESSAGE ADVISORIES (CONT.)

Message Comments

MANIFEST

– GWX software

mismatch, communication halted.

WX ALERT

– Possible severe

weather ahead.

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.

GTS 820 MESSAGE ADVISORIES

Message Comments

GTS CONFIG

– GTS config error.

Config service req’d.

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.

MANIFEST

– GTS software

mismatch, communication halted.

The GTS has incorrect software installed. The
G1000 system should be serviced.

MISCELLANEOUS MESSAGE ADVISORIES

Message Comments

FPL WPT LOCK

– Flight plan

waypoint is locked.

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

77

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

FPL WPT MOVE

Message Comments

– Flight plan

waypoint moved.

TIMER EXPIRD

Nav/Com/

XPDR/AudioAFCSGPS Nav

DB CHANGE

– Timer has expired.

– Database changed.

Verify user modified procedures.

DB CHANGE

Verify stored airways.

Flight

PlanningProcedures

FPL TRUNC

truncated.

Hazard

Avoidance

Features

Additional

LOCKED FPL

– Database changed.

– Flight plan has been

– Cannot navigate

locked flight plan.

Abnormal

Operation

WPT ARRIVAL

AlertsAppendixIndex

Annun/

-[xxxx]

STEEP TURN
INSIDE ARSPC
ARSPC AHEAD

– Arriving at waypoint

– Steep turn ahead.

– Inside airspace.

– Airspace ahead less

than 10 minutes.

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.

The system notifies the pilot that the timer has
expired.

This occurs when a stored flight plan contains
procedures that have been manually edited. This
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
an airway that is no longer consistent with the
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
database eliminates an obsolete approach or
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
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan.
Update flight plan with current waypoint.

Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.

A steep turn is 15 seconds ahead. Prepare to turn.
The aircraft is inside the airspace.
Special use airspace is ahead of aircraft. The

aircraft will penetrate the airspace within 10
minutes.

78

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Message Comments

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.

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.

SLCT NAV

approach.

– Select NAV on CDI for

The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct
NAV receiver.

PTK FAIL

bad geometry.

PTK FAIL

past IAF.

PTK FAIL

past IAF.

UNABLE V WPT

vertical waypoint.

– Parallel track unavailable:

– Parallel track unavailable:

– Parallel track unavailable:

– Can’t reach current

Bad parallel track geometry.

IAF waypoint for parallel offset has been passed.

IAF waypoint for parallel offset has been passed.

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.

VNV

– Unavailable. Excessive track

angle error.

VNV

– Unavailable. Unsupported leg

type in flight plan.

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.

VNV

– Unavailable. Excessive

crosstrack error.

VNV

– Unavailable. Parallel course

selected.

The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.

A parallel course has been selected, causing the
vertical deviation to go invalid.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

79

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

NO WGS84 WPT

Message Comments

– Non WGS 84

waypoint for navigation -[xxxx]

Nav/Com/

XPDR/AudioAFCSGPS Nav

TRAFFIC FAIL

– Traffic device has

failed.

FAILED PATH

MAG VAR WARN

– A data path has failed.

– Large magnetic

variance. Verify all course angles.

Flight

PlanningProcedures

SVS

– SVS DISABLED: Out of available

terrain region.

SVS

– SVS DISABLED: Terrain DB

resolution too low.

Hazard

Avoidance

SCHEDULER [#]

Features

Additional

CHECK CRS

– <message>.

– Database course for

LOC1 / [LOC ID] is [CRS]°.

CHECK CRS

Abnormal

Operation

LOC2 / [LOC ID] is [CRS]°.

– Database course for

[PFD1 or MFD1] CARD 1 REM

AlertsAppendixIndex

Annun/

Card 1 was removed. Reinsert card.

[PFD1 or MFD1] CARD 2 REM

Card 2 was removed. Reinsert card.

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 system. The traffic device should be serviced.

A data path connected to the GDU, GSD 41, or
the GIA 63/W has failed.

The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
near the magnetic poles. Displayed magnetic
course angles may differ from the actual
magnetic heading by more than 2°.

Synthetic Vision is disabled because the aircraft is
not within the boundaries of the installed terrain
database.

Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second or
better) is not currently installed.

Message criteria entered by the user.
Selected course for LOC1 differs from published

localizer course by more than 10 degrees.
Selected course for LOC2 differs from published

localizer course by more than 10 degrees.
The SD card was removed from the top card slot

–

of the PFD or MFD. The SD card needs to be
reinserted.

The SD card was removed from the bottom card

–

slot of the PFD or MFD. The SD card needs to be
reinserted.

80

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Message Comments

[PFD1 or MFD1] CARD 1 ERR

–

Card 1 is invalid.

[PFD1 or MFD1] CARD 2 ERR

–

Card 2 is invalid.

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.

FLIGHT PLAN IMPORT/EXPORT MESSAGES

In some circumstances, some messages may appear in conjunction with others.

Flight Plan Import/Export Results Description

‘Flight plan successfully imported.’ A flight plan file stored on the SD card was

successfully imported as a stored flight plan.

‘File contained user waypoints only. User
waypoints imported successfully. No
stored flight plan data was modified.’

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.
‘No flight plan files found to import.’ The SD card contains no flight plan data.
‘Flight plan import failed.’ Flight plan data was not successfully

imported from the SD card.
‘Flight plan partially imported.’ 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.
‘File contained user waypoints only.’ 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.
‘Too many points. Flight plan truncated.’ 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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

81

Annunciations & Alerts

FLIGHT PLAN IMPORT/EXPORT MESSAGES (CONT.)

Flight

InstrumentsEIS

Flight Plan Import/Export Results Description

‘Some waypoints not loaded. Waypoints
locked.’

Nav/Com/

XPDR/AudioAFCSGPS Nav

‘User waypoint database full. Not all
loaded.’

Flight

PlanningProcedures

‘One or more user waypoints renamed.’ One or more imported user waypoints were

Hazard

Avoidance

‘Flight plan successfully exported.’ The stored flight plan was successfully

‘Flight plan export failed.’ The stored flight plan was not successfully

Features

Additional

Abnormal

Operation

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.

renamed when imported due to naming
conflicts with waypoints already existing in
the system.

exported to the SD card.

exported to the SD card. The SD card may
not have sufficient available memory or the
card may have been removed prematurely.

AlertsAppendixIndex

Annun/

82

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

PFD SOFTKEY MAP

Press the BACK Softkey to return to
the top-level softkeys.

STRMSCP

ALERTS

ALERTS

METAR

APPENDIX

Appendix

Instruments EIS

Flight

Level 1 Level 2 Level 3

INSET

OFF

DCLTR (3)

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Top Level PFD Softkeys

Inset Map Softkeys

Description

Displays Inset Map in PFD lower left corner

Removes Inset Map

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

ALERTS

83

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Appendix

(

optional)

Level 1 Level 2 Level 3

Flight

InstrumentsEIS

TRAFFIC

TOPO

TERRAIN

Nav/Com/

XPDR/AudioAFCSGPS Nav

STRMSCP

NEXRAD

XM LTNG

METAR

Flight

PlanningProcedures

SYN VIS

Hazard

Avoidance

Features

Additional

Description

Displays traffic information on Inset Map

Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Inset Map

Displays terrain information on Inset Map

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)

ALT UNIT

Press the BACK Softkey to
return to the top-level softkeys

HSI FRMT

ALERTS

ALERTS

Abnormal

Operation

AlertsAppendixIndex

Annun/

84

METERS IN HPA

360 HSI

ARC HSI ALERTS

SYN TERR

PATHWAY

HRZN HDG

APTSIGNS ALERTS

PFD Configuration Softkeys

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

ALERTS

ALERTS

190-00526-03 Rev. A