Garmin Beechcraft G58 Reference Guide

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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

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: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138

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Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

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

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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.

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Record of Revisions

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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

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

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

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Table of Contents

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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)

Press the PFD Softkey.

Press the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

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

Press the ALT UNIT Softkey.

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

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

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

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.

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.

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

Flight Instruments

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

Flight

InstrumentsEIS

Press the OBS Softkey to select OBS Mode.

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.

Press the OBS Softkey again to disable OBS Mode.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GENERIC TIMER

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.

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

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

Press the TMR/REF Softkey.

Turn the

large

FMS Knob to highlight the desired Vspeed.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

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).

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

Turn the

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

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

Press the TMR/REF Softkey.

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

Turn the small FMS Knob clockwise to BARO.

Press the ENT Key.

Use the small FMS Knob to enter the desired altitude.

Press the ENT Key.

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

DISPLAYING WIND DATA

Press the PFD Softkey.

Press the WIND Softkey to display wind data to the left of the HSI.

Press one of the OPTN softkeys to change how wind data is displayed.

To remove the Wind Data Window, press the OFF Softkey.

CHANGING HSI FORMAT

Press the PFD Softkey.

Press the HSI FRMT Softkey.

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

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

Flight Instruments

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

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

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

Press the ENGINE Softkey.

Features

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.

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

Engine Indication System

ENGINE SYSTEM DISPLAY

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Press the ENGINE Softkey, then the SYSTEM Softkey to display the SYSTEM Engine Page.

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

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)

Press the DME Softkey.

Turn the large FMS to select the DME source ﬁeld.

Turn the small FMS Knob to select the desired Nav radio.

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

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

Press the CODE Softkey to display the transponder code selection softkeys, for digit entry.

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

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

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

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

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

To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).

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

Press the small tuning knob to select the desired radio for tuning. A light blue box highlights the radio frequency to be tuned.

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.

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

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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.

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

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Avoidance

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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

Alerts Appendix Index

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Nav/Com/XPDR/Audio Panel

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

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Hazard

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Features

Additional

Abnormal

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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

APR

Key press activates ﬂight director.

Planning Procedures

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Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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

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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

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

HDG

GPS

VOR

LOC

GPS

LOC

Instruments EIS

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XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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Abnormal

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Alerts Appendix Index

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Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

AFCS

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

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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

Press the Direct-to

Enter the waypoint identiﬁer.

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

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

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

Enter the desired altitude.

Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 9.

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

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

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

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Avoidance

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Features

Direct-to Navigation from the PFD

Press the Direct-to Key

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

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

Press the ENT Key.

The cursor is now ﬂashing on ‘ACTIVATE?’. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 6.

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

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

( )

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

Turn the small FMS Knob to enter the desired altitude.

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.

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.

Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired ﬂight plan

Press the ACTIVE Softkey. The conﬁrmation window is now displayed.

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

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

AlertsAppendixIndex

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

Press the ACT LEG Softkey on the MFD.

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.

With ‘Activate’ highlighted, press the ENT Key.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

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

Press the MENU Key to display the Page Menu Window.

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

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

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Large Text

Small Text

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

Turn the large FMS Knob to select the ‘AUX’ page group.

Turn the small FMS Knob to select the ﬁrst rectangular page icon.

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.

For Direct-to planning:

Press the WPTS Softkey and verify that the starting waypoint ﬁeld indicates ‘P.POS’ (present position).

If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’.

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

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

Or:

For point-to-point planning:

Enter the identiﬁer of the starting waypoint.

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

Again, enter the identiﬁer of the ending waypoint.

Press the ENT Key to accept the waypoint.

Or:

For ﬂight plan leg planning:

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

Turn the small FMS Knob to select the desired ﬂight plan (already stored in memory), by number.

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

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Avoidance

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Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Flight Planning

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

Enter the departure time. Press the ENT Key when ﬁnished. Departure time may be entered in local or UTC time, depending upon system settings.

The ﬂashing cursor moves to the ground speed (GS) ﬁeld. Enter the ground

Flight

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Additional

Abnormal

Operation

AlertsAppendixIndex

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

The ﬂashing cursor moves to the fuel ﬂow ﬁeld. Enter the fuel ﬂow. Press the ENT Key when ﬁnished. Note that in ‘AUTOMATIC’ page mode, fuel ﬂow is provided by the system.

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

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Flight Planning

CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

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

Turn the small FMS Knob to select the User WPT Information Page.

Press the NEW Softkey. A waypoint is created at the current aircraft position.

Enter the desired waypoint name.

Press the ENT Key.

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.

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

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.

With the cursor in the ‘WAYPOINT TYPE’ ﬁeld, turn the small FMS Knob to display a list of waypoint types.

Turn the small FMS Knob to select LAT/LON (latitude and longitude).

Press the ENT Key.

CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS

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

Turn the small FMS Knob to select the User WPT Information Page.

Press the NEW Softkey. A waypoint is created at the current aircraft position.

Enter the desired waypoint name.

Press the ENT Key.

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

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

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XPDR/Audio AFCS GPS Nav

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Planning Procedures

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Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Flight Planning

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

Flight

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AlertsAppendixIndex

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display a list of waypoint types.

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

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:

Or:

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.

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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

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

Turn the small FMS Knob to select the User WPT Information Page.

Press the NEW Softkey. A waypoint is created at the current aircraft position.

Enter the desired waypoint name.

Press the ENT Key.

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

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.

With the cursor in the ‘WAYPOINT TYPE’ ﬁeld, turn the small FMS Knob to display a list of waypoint types.

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

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:

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.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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Avoidance

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Additional

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Operation

Abnormal

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Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Flight Planning

Or:

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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Or:

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

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

Turn the small FMS Knob to select the User WPT Information Page.

Press the FMS Knob to activate the cursor.

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Flight Planning

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

Turn the small FMS Knob to highlight the desired waypoint.

Press the DELETE Softkey.

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:

Press the FPL Key.

Press the FMS Knob to activate the cursor (only on MFD).

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).

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.

Repeat step numbers 3 and 4 to enter each additional ﬂight plan waypoint.

When all waypoints have been entered, press the FMS Knob to remove the cursor.

Instruments EIS

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Avoidance

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Additional

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Operation

Abnormal

Creating a stored ﬂight plan:

Press the FPL Key.

Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.

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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Flight Planning

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

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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).

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.

Nav/Com/

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Repeat step numbers 4 and 5 to enter each additional ﬂight plan waypoint.

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

Insert the SD card containing the ﬂight plan in the top card slot on the MFD.

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

Turn the small FMS Knob to select the Flight Plan Catalog Page.

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Press the FMS Knob to activate the cursor.

Turn either FMS Knob to highlight an empty or existing ﬂight plan.

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.

Turn the small FMS Knob to highlight the desired ﬂight plan for importing.

Press the ENT Key.

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Flight Planning

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

Press the FPL Key to display the active ﬂight plan.

If required, press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired ﬂight plan waypoint. The new waypoint is inserted before the highlighted waypoint.

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

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

Enter the user waypoint identiﬁer, facility, or city.

Press the ENT Key.

Or:

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’ airport waypoints to the aircraft’s current position.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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.

Press the ENT Key again to accept the waypoint.

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Alerts Appendix Index

ENTER AN AIRWAY IN A FLIGHT PLAN

Press the FPL Key.

Press the FMS Knob to activate the cursor (not required on the PFD).

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.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Flight Planning

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

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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).

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”

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altitude airways, and then high altitude airways.

Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted.

Press the ENT Key. The system returns to editing the ﬂight plan with the new airway inserted.

INVERT AN ACTIVE FLIGHT PLAN

Flight

PlanningProcedures

Press the FPL Key to display the active ﬂight plan.

Press the MENU Key to display the Page Menu.

Turn the large FMS Knob to highlight ‘Invert Flight Plan’.

Press the ENT Key. The original ﬂight plan remains intact in its ﬂight plan catalog storage location.

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

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Abnormal

Annun/

Operation

AlertsAppendixIndex

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

Or, for a stored ﬂight plan:

Press the FPL Key on the MFD.

Turn the small FMS Knob to select the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

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

Press the EDIT Softkey.

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.

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Flight Planning

Press the CLR Key to display a conﬁrmation window.

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

STORE A FLIGHT PLAN

After creating a ﬂight plan on either the PFD or MFD, it may be saved by pressing the MENU Key.

Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.

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

EDIT A STORED FLIGHT PLAN

Press the FPL Key on the MFD, then turn the small FMS Knob to display the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

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

Press the EDIT Softkey.

Turn the large FMS Knob to place the cursor in the desired location.

Enter the changes, then press the ENT Key.

Press the FMS Knob to return to the Flight Plan Catalog Page.

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DELETE A WAYPOINT FROM THE FLIGHT PLAN

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

Or, for a stored ﬂight plan:

Press the FPL Key on the MFD.

Turn the small FMS Knob to select the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

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

Press the EDIT Softkey.

Turn the large FMS Knob to highlight the waypoint to be deleted.

Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation window.

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Flight Planning

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

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InstrumentsEIS

the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

Once all changes have been made, press the FMS Knob to remove the cursor.

INVERT AND ACTIVATE A STORED FLIGHT PLAN

Nav/Com/

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Press the FPL Key on the MFD.

Turn the small FMS Knob to select the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

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

Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is displayed.

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

Press the FPL Key on the MFD.

Hazard

Avoidance

Features

Additional

Turn the small FMS Knob to select the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the ﬂight plan to be copied.

Press the COPY Softkey. A ‘Copy to ﬂight plan #?’ conﬁrmation window is displayed.

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

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Press the FPL Key on the MFD.

Turn the small FMS Knob to select the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the ﬂight plan to be deleted.

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Flight Planning

Press the DELETE Softkey. A ‘Delete ﬂight plan #?’ conﬁrmation window is displayed.

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

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

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.

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.

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.

To change the user waypoint name, follow the procedure for modifying a user waypoint.

EXPORT A FLIGHT PLAN TO AN SD CARD

ABOVE

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Planning Procedures

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Avoidance

Hazard

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

descriptions.

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

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

Turn the small FMS Knob to select the Flight Plan Catalog Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the ﬂight plan to be exported.

Press the EXPORT Softkey.

Press the ENT Key to conﬁrm the export.

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Flight Planning

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

Press the PROC Key.

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

Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ ﬁeld with a list of available departures.

Turn the large FMS Knob to highlight the desired departure.

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.

Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ ﬁeld with a list of available transitions.

Turn the large FMS Knob to highlight the desired transition.

Press the ENT Key.

With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when the ﬂight plan is active.

Procedures

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ACTIVATE A DEPARTURE LEG

Press the FPL Key on the MFD to display the active ﬂight plan.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired waypoint within the departure.

Press the ACT LEG Softkey. A conﬁrmation window showing the selected leg is displayed.

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AN ARRIVAL PROCEDURE

Press the PROC Key.

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

Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ ﬁeld with a list of available arrivals.

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Procedures

Turn the large FMS Knob to highlight the desired arrival.

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Press the ENT Key. A list of transitions is displayed for the selected arrival.

Turn either FMS Knob to select the desired transition.

Press the ENT Key. A list of runways may be displayed for the selected arrival.

Turn the large FMS Knob to highlight the desired runway.

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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:

Press the FMS Knob to activate the cursor.

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

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PlanningProcedures

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

ACTIVATE AN ARRIVAL LEG

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Press the FPL Key to display the active ﬂight plan.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to highlight the desired waypoint within the arrival.

Press the ACT LEG Softkey. A conﬁrmation window showing the selected leg is displayed.

With ‘ACTIVATE’ highlighted, press the ENT Key.

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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.

Press the PROC Key.

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

Press the ENT Key. A list of available approaches for the destination airport is displayed.

Turn either FMS Knob to highlight the desired approach.

Press the ENT Key. A list of available transitions for the selected approach procedure is now displayed.

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.

Press the ENT Key. The cursor moves to the MINIMUMS ﬁeld.

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

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Avoidance

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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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Procedures

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

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InstrumentsEIS

Press the PROC Key.

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

Press the ENT Key.

ACTIVATE A VECTOR TO FINAL APPROACH FIX

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Press the PROC Key.

Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.

Press the ENT Key.

The ﬁnal approach course becomes the active leg.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

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Avoidance

Press the PROC Key.

Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.

Press the ENT Key. A conﬁrmation window is displayed.

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the Go-around Button.

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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

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.

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.

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

Press the MAP Softkey.

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

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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

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

Turn either FMS Knob to highlight ‘Map Setup’.

Press the ENT Key.

Turn the small FMS Knob to highlight ‘Weather’.

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Hazard Avoidance

Press the ENT Key.

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Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ ﬁeld.

Turn the small FMS Knob to display the ‘Cell/Strike’ window.

Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.

Push the FMS Knob to return to the Navigation Map Page.

Clear Stormscope Lightning Data from the Navigation Map Page

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

Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ ﬁeld and press the ENT Key.

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PlanningProcedures

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

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Features

Operation

AlertsAppendixIndex

Change the Viewing Mode Between 360˚ and 120˚

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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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

Press the MAP Softkey.

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

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

Turn the small FMS Knob to select the Airport Information Page.

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

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

Turn the small FMS Knob to select the Weather Data Link Page.

Press the available softkeys to select the desired XM weather product.

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

Push in the Joystick to display the panning arrow.

Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs.

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.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Hazard Avoidance

SiriusXM Weather Products and Symbols

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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

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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.

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.

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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)

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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

Operation

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Hazard Avoidance

Displaying Trafﬁc on the Trafﬁc Map Page

Flight

InstrumentsEIS

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

Turn the small FMS Knob to select the Trafﬁc Map Page.

Press the OPERATE Softkey to begin displaying trafﬁc. ‘OPERATING’ is displayed in the Trafﬁc Mode ﬁeld.

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.

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

Press the TNA MUTE Softkey to mute the “Trafﬁc Not Available” aural alert.

Displaying Trafﬁc on the Navigation Map

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

Flight

PlanningProcedures

MAP Softkey.

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

Trafﬁc Advisory System (TAS)(If Installed)

Displaying Trafﬁc on the Trafﬁc Map Page

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Avoidance

Features

Operation

AlertsAppendixIndex

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

Turn the small FMS Knob to select the Trafﬁc Map Page.

Select the OPERATE or NORMAL Softkey to begin displaying trafﬁc. ‘OPERATING’ is displayed in the Trafﬁc Mode ﬁeld.

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.

Select the STANDBY Softkey to place the system in the Standby Mode. ‘STANDBY’ is displayed in the Trafﬁc Mode ﬁeld.

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

Select the

FLT ID

Softkey to enable or disable Flight ID displayed with the

intruder information (GTS 820 only).

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Hazard Avoidance

System Self Test

With the Trafﬁc Map Page displayed, set the range to 2/6 nm.

Select the STANDBY Softkey.

Select the TEST Softkey.

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

Ensure TAS is operating.

With the Navigation Map displayed, select the MAP Softkey.

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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Planning Procedures

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Hazard

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

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

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

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

Turn the small FMS Knob to select the TAWS-B Page.

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.

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

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Additional

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Annun/

Alerts Appendix Index

Hazard Avoidance

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Enable/Disable Aviation Data

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

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

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.

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Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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Inhibit TAWS

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

Press the MENU Key.

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

Press the ENT Key.

Enable TAWS

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

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

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

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.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

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

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

Turn the small FMS Knob to select the Weather Radar Page.

Press the MODE Softkey.

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.

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.

Turn the Joystick to select the desired range.

If desired, press the VERTICAL Softkey for vertical scanning.

Instruments EIS

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Planning Procedures

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Avoidance

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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:

Press the MENU Key

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

Press the ENT Key.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Alerts Appendix Index

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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:

Press the MENU Key

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

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.

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

Flight

PlanningProcedures

displayed.

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

Turn the Joystick to adjust the range.

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

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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.

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

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.

Press the FMS Knob to remove the cursor.

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

Press the MODE Softkey.

Press the GROUND Softkey to place the radar in Ground Map Mode.

Press the BACK Softkey.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to place the cursor in the ‘TILT’ ﬁeld.

Adjust the antenna tilt angle by turning the small FMS Knob to position the ground returns as desired.

Press the FMS Knob to remove the cursor.

Sector Scan

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.

Press the FMS Knob to display the cursor.

Turn the large FMS Knob to place the cursor in the SECTOR SCAN ﬁeld.

Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.

If desired, readjust the Bearing Line with the Joystick to change the center of the Sector Scan.

Press the FMS Knob to remove the cursor.

Instruments EIS

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Planning Procedures

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Avoidance

Hazard

Antenna Stabilization

To activate or deactivate the antenna stabilization, press the MODE Softkey.

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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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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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.

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XPDR/AudioAFCSGPS Nav

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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

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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

Press the PFD Softkey.

Press the SYN VIS Softkey.

Press the SYN TERR Softkey.

Press the BACK Softkey to return to the previous page.

Planning Procedures

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Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Additional Features

Displaying Pathways

Flight

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Flight

Hazard

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XPDR/AudioAFCSGPS Nav

PlanningProcedures

Avoidance

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the PATHWAY Softkey.

Press the BACK Softkey to return to the previous page.

Displaying Heading on the Horizon

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the HRZN HDG Softkey.

Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the APTSIGNS Softkey.

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

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

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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

Press the SHW CHRT Softkey when displayed.

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

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.

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

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Alerts Appendix Index

Additional Features

View Charts from the Active Flight Plan Page

Flight

InstrumentsEIS

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

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

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

Change Day/Night View

While viewing a chart press the MENU Key to display the Page Menu OPTIONS.

Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and press the ENT Key.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR SCHEME’ Options.

Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen Options.

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

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.

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

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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.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

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

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

Turn the small FMS Knob to select the displayed AUX - XM Information

Nav/Com/

Page.

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

Press the CATGRY Softkey on the XM Radio Page.

Press the CAT + and CAT - Softkeys to cycle through the categories.

Turn the small FMS Knob to display the ‘Categories’ list. Highlight the

Hazard

Additional

Features

desired category with the small FMS Knob.

Operation

Press the ENT Key.

Abnormal

Select an Available Channel within the Selected Category

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

Press the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey.

Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels.

With the desired channel highlighted, press the ENT Key.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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Additional Features

Entering a Channel Directly

Flight

InstrumentsEIS

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

Press the DIR CH Softkey. The channel number in the Active Channel Box is highlighted.

Press the numbered softkeys located on the bottom of the display to directly select the desired channel number.

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.

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).

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.

Press the SET Softkey.

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

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On the XM Radio Page, press the RADIO Softkey.

Press the VOL Softkey to access the volume control softkeys.

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

Press the MUTE Softkey to mute the radio audio.

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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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

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Alerts Appendix Index

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

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

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Abnormal

Operation

AlertsAppendixIndex

Annun/

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.

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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

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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.

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Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Abnormal Operation

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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

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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

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

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.

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

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

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

Aural Message

Terrain Ahead, Pull Up; Ter-

rain Ahead, Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

“Caution, Terrain; Caution,

Terrain”

“Terrain Ahead; Terrain

Ahead”

“Terrain Ahead; Terrain

Ahead”

“Caution, Terrain; Caution,

Terrain”

“Caution, Obstacle; Cau-

tion, Obstacle”

“Obstacle Ahead; Obstacle

Ahead”

“Obstacle Ahead; Obstacle

Ahead”

“Caution, Obstacle; Cau-

tion, Obstacle”

“Too Low, Terrain”

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)

“Don’t Sink”

“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

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”

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

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.

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

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

– 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.

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.

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

– 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

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

– 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.

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.

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

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.

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:

– Can’t reach current

Bad parallel track geometry.

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

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.

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

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/

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

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

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

Abnormal

Operation

AlertsAppendixIndex

Annun/

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

190-00526-03 Rev. A

Garmin Beechcraft G58 Reference Guide

Specifications and Main Features

Frequently Asked Questions

User Manual

Flight Instruments

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

CHANGE NAVIGATION SOURCES

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

GENERIC TIMER

CONFIGURE VSPEED BUGS INDIVIDUALLY

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

DISPLAYING WIND DATA

CHANGING HSI FORMAT

Engine Indication System

ENGINE DISPLAY

LEAN ENGINE DISPLAY

ENGINE SYSTEM DISPLAY

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

DME TUNING (OPTIONAL)

ENTER A TRANSPONDER CODE

ACTIVATE ADS-B TRANSMIT

SELECTING A COM RADIO

SELECTING A NAV RADIO

NAV/COM TUNING

SPLIT COM

DIGITAL CLEARANCE RECORDER AND PLAYER

INTERCOM SYSTEM (ICS) ISOLATION

AUTOMATIC FLIGHT CONTROL SYSTEM

FLIGHT DIRECTOR ACTIVATION

VERTICAL MODES

LATERAL MODES

GPS NAVIGATION

DIRECT-TO NAVIGATION

ACTIVATE A STORED FLIGHT PLAN

ACTIVATE A FLIGHT PLAN LEG

STOP NAVIGATING A FLIGHT PLAN

VERTICAL NAVIGATION (VNAV)

TRIP PLANNING

FLIGHT PLANNING

CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS

DELETE A USER WAYPOINT

CREATE A FLIGHT PLAN

IMPORT A FLIGHT PLAN FROM AN SD CARD

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

ENTER AN AIRWAY IN A FLIGHT PLAN

INVERT AN ACTIVE FLIGHT PLAN

STORE A FLIGHT PLAN

EDIT A STORED FLIGHT PLAN

DELETE A WAYPOINT FROM THE FLIGHT PLAN

INVERT AND ACTIVATE A STORED FLIGHT PLAN

COPY A FLIGHT PLAN

DELETE A FLIGHT PLAN

GRAPHICAL FLIGHT PLAN CREATION

EXPORT A FLIGHT PLAN TO AN SD CARD

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

ACTIVATE A DEPARTURE LEG

LOAD AN ARRIVAL PROCEDURE

ACTIVATE AN ARRIVAL LEG

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

ACTIVATE A VECTOR TO FINAL APPROACH FIX

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Hazard Avoidance

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

STORMSCOPE® (OPTIONAL)

SIRIUSXM WEATHER (OPTIONAL)

TRAFFIC SYSTEMS

TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY

AIRBORNE COLOR WEATHER RADAR

SYNTHETIC VISION

Additional Features

TERMINAL PROCEDURE CHARTS

AOPA AIRPORT DIRECTORY

SIRIUSXM RADIO ENTERTAINMENT

Abnormal Operation