Garmin Beechcraft G58 Reference Guide

G1000® Integrated Flight Deck

Cockpit Reference Guide for the Beechcraft G58

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2005, 2007-2012 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software 0857.09 or later for the Beechcraft G58. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: [phone]	Fax: [phone]
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone]	Fax [phone]
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: [phone]	Fax: [phone]
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone]	Fax: [phone]

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

Web Site Address: www.garmin.com

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

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

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

March, 2012

190-00526-03 Rev. A

Printed in the U.S.A.

Warnings, Cautions & Notes

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

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

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

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

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

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

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

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Warnings, Cautions & Notes

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

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

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

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

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

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

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Warnings, Cautions & Notes

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

WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/ environment/disposal.jsp.

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

WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed.

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

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

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

190-00526-03 Rev. A

Warnings, Cautions & Notes

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

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

NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data.

NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.

NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition.

NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.

NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft.

190-00526-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Beechcraft G58

Warnings, Cautions & Notes

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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.

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	RR-1

Record of Revisions

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RR-2	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

		Table of Contents
FLIGHT INSTRUMENTS.................................................................................................................			1
Selecting the Altimeter Barometric Pressure Setting.......................................................			1
Selecting Standard Barometric Pressure (29.92 in Hg).....................................................			1
Change Altimeter Barometric Pressure Setting Units.......................................................			1
Change Navigation Sources....................................................................................................			1
Enable/Disable OBS Mode While Navigating with GPS....................................................			2
Generic Timer.............................................................................................................................			2
Configure Vspeed Bugs Individually.....................................................................................			2
Set Barometric Minimum Descent Altitude.........................................................................			3
Displaying Wind Data...............................................................................................................			3
Changing HSI Format................................................................................................................			3
ENGINE INDICATION SYSTEM..................................................................................................			5
Engine Display............................................................................................................................			5
Lean Engine Display..................................................................................................................			6
Engine System Display.............................................................................................................			8
NAV/COM/TRANSPONDER/AUDIO PANEL.........................................................................			9
ADF Tuning (Optional)..............................................................................................................			9
DME Tuning (Optional).............................................................................................................			9
Enter a Transponder Code.......................................................................................................			9
Activate ADS-B Transmit..........................................................................................................			9
Selecting a COM Radio...........................................................................................................			10
Selecting a NAV Radio............................................................................................................			10
NAV/COM Tuning......................................................................................................................			10
Split COM..................................................................................................................................			10
Digital Clearance Recorder and Player..............................................................................			11
Intercom System (ICS) Isolation...........................................................................................			11
AUTOMATIC FLIGHT CONTROL SYSTEM...........................................................................			13
Flight Director Activation......................................................................................................			13
Vertical Modes.........................................................................................................................			14
Lateral Modes..........................................................................................................................			15
GPS NAVIGATION.........................................................................................................................			17
Direct-to Navigation...............................................................................................................			17
Activate a Stored Flight Plan................................................................................................			18
Activate a Flight Plan Leg.....................................................................................................			18
Stop Navigating a Flight Plan...............................................................................................			19
Vertical Navigation (VNAV)...................................................................................................			19
FLIGHT PLANNING.......................................................................................................................			21
Trip Planning.............................................................................................................................			21
Create a User Waypoint Defined by Latitude & Longitude...........................................			23
			i
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

ii	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

	Table of Contents
ABNORMAL OPERATION..........................................................................................................	57
Reversionary Mode.................................................................................................................	57
Abnormal COM Operation.....................................................................................................	57
Hazard Displays with Loss of GPS Position.......................................................................	57
Unusual Attitudes....................................................................................................................	58
Dead Reckoning.......................................................................................................................	59
ANNUNCIATIONS & ALERTS...................................................................................................	61
WARNING Annunciation.........................................................................................................	61
CAUTION Annunciation...........................................................................................................	61
ADVISORY Annunciation........................................................................................................	62
Alert Message..........................................................................................................................	62
AFCS ALERTS.............................................................................................................................	62
TAWS-B Alerts...........................................................................................................................	63
TAWS-B System Status Annunciations................................................................................	65
Voice Alerts...............................................................................................................................	66
MFD & PFD Message Advisories...........................................................................................	67
Database Message Advisories..............................................................................................	68
GMA 1347 Message Advisories.............................................................................................	70
GIA 63W Message Advisories................................................................................................	71
GEA 71 Message Advisories..................................................................................................	74
GTX 33 Message Advisories..................................................................................................	74
GRS 77 Message Advisories..................................................................................................	75
GDC 74A Message Advisories...............................................................................................	75
GMU 44 Message Advisories.................................................................................................	76
GDL 69/69A Message Advisories..........................................................................................	76
GWX 68 Message Advisories.................................................................................................	76
GTS 820 Message Advisories.................................................................................................	77
Miscellaneous Message Advisories.....................................................................................	77
Flight Plan Import/Export Messages...................................................................................	81
APPENDIX........................................................................................................................................	83
PFD Softkey Map.....................................................................................................................	83
MFD Softkey Map....................................................................................................................	88
Database Updates...................................................................................................................	90
INDEX..........................................................................................................................................	Index-1

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	iii

Table of Contents

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iv	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

1)Press the PFD Softkey.

2)Press the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

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

2)Press the ALT UNIT Softkey.

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

Or:

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

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

CHANGE NAVIGATION SOURCES

1)Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD.

2)Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency.

3)Press the CDI Softkey a third time to return to GPS.

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	1

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

Flight Instruments

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)Press the OBS Softkey to select OBS Mode.

2)Turn a CRS Knob to select the desired course to/from the waypoint. Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint.

3)Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1)Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted.

2)Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted.

3)Press the ENT Key to START, STOP, or RESET the timer (if the timer is counting DOWN, it starts counting UP after reaching zero). Press the CLR Key or the TMR/REF Softkey to remove the window.

CONFIGURE VSPEED BUGS INDIVIDUALLY

1)Press the TMR/REF Softkey.

2)Turn the large FMS Knob to highlight the desired Vspeed.

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

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

5)Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.

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

2	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

Flight Instruments

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)Press the TMR/REF Softkey.

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

3)Turn the small FMS Knob clockwise to BARO.

4)Press the ENT Key.

5)Use the small FMS Knob to enter the desired altitude.

6)Press the ENT Key.

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

DISPLAYING WIND DATA

1)Press the PFD Softkey.

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

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

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

CHANGING HSI FORMAT

1)Press the PFD Softkey.

2)Press the HSI FRMT Softkey.

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

Or:

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

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	3

Flight Instruments

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

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4	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

Engine Indication System

ENGINE INDICATION SYSTEM

ENGINE DISPLAY

In all cases green indicates normal operation, yellow indicates caution, and red indicates warning.

Pressing the ENGINE Softkey makes available the LEAN and SYSTEM softkeys which in turn provide access to the Lean Page and the System Page, respectively.

Manifold

Pressure

Gauge

(Left Engine)

RPM Gauge

(Left Engine) Propeller Sync

Indicator

Fuel Flow

Numeric

Fuel Flow Readout

Indicator

Cylinder Head

Temperature

Oil Temperature Indicator

Indicator

Oil Pressure

Indicator

Ammeter

Fuel Quantity

Indicator

Default Engine Page

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	5

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

Engine Indication System

LEAN ENGINE DISPLAY

								Fuel Flow Leaning
								Marker
								Difference between peak
EGT peak								and current temperature
								of selected cylinder
temperature
								(Right Engine)
(Left Engine)
Exhaust Gas								EGT Readout
Temperature								For Selected
Bar Graphs								Cylinder
(Left Engine)								(Right Engine)
Cylinder Head								CHT Readout
Temperature
								For Selected
Bar Graphs
								Cylinder
(Left Engine)
								(Right Engine)

LEAN Engine Page

1)Press the ENGINE Softkey.

2)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 the CYL SLCT Softkey cycles through the cylinders; the selected cylinder number is displayed in light blue. The CYL SLCT Softkey is disabled during warning or caution conditions or when the ASSIST Softkey is pressed.

6	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

Engine Indication System

Monitoring the desired cylinder’s EGT and CHT:

From the Lean Display, press the CYL SLCT Softkey to cycle through each cylinder and view its EGT and CHT. The selected cylinder is shown in light blue.

When the ASSIST Softkey is selected, the system initially highlights and selects the cylinder number with the hottest EGT and displays its temperature below the EGT bar graph. A readout showing the difference between peak (DPEAK) and the current temperature for the selected cylinder is displayed above the EGT bar graph.

As the mixture is leaned, a light blue line will appear above each cylinder to indicate EGT peak.

When the system detects the first cylinder to peak, the cylinder numbers below the EGT graph disappear, and the letter “R” is annunciated below the first peaked cylinder to indicate the other cylinders are rich of peak. As the mixture is further leaned, the letter “L” is annunciated below the last peaked cylinder indicating all cylinders are lean of peak. Refer to the POH and AFM for the recommended mixture adjustment procedures.

Monitoring of the cylinder continues until the ASSIST Softkey is pressed again which disables lean assist and removes the peak lines from the bar graph and the temperature deviation from peak (DPEAK). The system then returns to seeking the hottest cylinder.

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	7

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

Engine Indication System

ENGINE SYSTEM DISPLAY

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

2)If desired, use the DEC FUEL, INC FUEL, 166 GAL, and 194 GAL softkeys to adjust the amount of fuel remaining for totalizer calculations.

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

System

Information

Fuel Calculation

Information

Electrical

Information

SYSTEM Engine Page

8	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

Nav/Com/XPDR/Audio Panel

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

Tune the ADF using the remote ADF control head.

DME TUNING (OPTIONAL)

1)Press the DME Softkey.

2)Turn the large FMS to select the DME source field.

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

4)Press the ENT Key to complete the selection.

ENTER A TRANSPONDER CODE

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

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

3)Press the digit softkeys to enter the code in the code field. When entering the code, the next key in sequence must be pressed within 10 seconds, or the entry is cancelled and restored to the previous code. Five seconds after the fourth digit has been entered, the transponder code becomes active.

ACTIVATE ADS-B TRANSMIT

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

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

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

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	9

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

Nav/Com/XPDR/Audio Panel

SELECTING A COM RADIO Transmit/Receive

Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if installed) on the audio panel.

Receive Only

Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the audio panel.

SELECTING A NAV RADIO

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

2)Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or deselect the navigation radio audio source. All radio keys can be selected individually or together.

NAV/COM TUNING

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

2)Turn the respective tuning knobs to enter the desired frequency into the standby frequency field. The large knob enters MHz and the small knob enters kHz.

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

SPLIT COM

During Split COM operation, both the pilot and the copilot can transmit simultaneously over separate radios. The pilot can still monitor NAV1, NAV2, ADF, DME, and MKR Audio as selected, but the copilot is only able to monitor COM2.

When Split COM operation is selected, COM1 is used by the pilot and COM2 is used by the copilot. The COM1 MIC Annunciator flashes when the pilot’s microphone PTT is pressed. The COM2 MIC Annunciator flashes when the copilot’s microphone PTT is pressed.

Pressing the COM 1/2 Key selects Split COM operation. The COM 1/2 Annunciator is illuminated indicating Split COM operation. COM1 and COM2 frequencies are displayed in green indicating that both transceivers are active. Split COM operation is cancelled by pressing the COM 1/2 Key again, at which time the annunciator is extinguished.

10	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 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	COPLT KEY	Pilot Hears	Copilot	Passenger
		ANNUNCIATOR	ANNUNCIATOR		Hears	Hears
				Selected	Selected	Selected
				radios; pilot;	radios; pilot;	radios; pilot;
	ALL	OFF	OFF	copilot;	copilot;	copilot;
				passengers;	passengers;	passengers;
				music	music	music
				Selected	Copilot;	Copilot;
	PILOT	ON	OFF		passengers;	passengers;
				radios; pilot
					music	music
				Selected		Selected
	COPILOT	OFF	ON	radios; pilot;	Copilot	radios; pilot;
				passengers;		passengers;
				music		music
				Selected	Selected	Passengers;
	CREW	ON	ON	radios; pilot;	radios; pilot;
						music
				copilot	copilot

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	11

Nav/Com/XPDR/Audio Panel

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

Blank Page

12	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A

AFCS

AUTOMATIC FLIGHT CONTROL SYSTEM

NOTE: If sensor information (other than attitude) required for a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis.

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

FLIGHT DIRECTOR ACTIVATION

An initial press of a key listed in the following table (when the flight director is not active) activates the pilot-side flight director in the listed modes.

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
		GPS	Pitch Hold (default)	PIT
APR Key	Approach**	VAPP	Glidepath	GP
		LOC	Glideslope	GS
HDG Key	Heading Select	HDG	Pitch Hold (default)	PIT

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

**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director.

Instruments	Flight
EIS
XPDR/Audio	Nav/Com/
AFCS
Nav GPS
Planning	Flight
Procedures
Avoidance	Hazard
Features	Additional
Operation	Abnormal
Alerts	Annun/
Appendix
Index

190-00526-03 Rev. A	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	13

Flight	Instruments
	EIS
Nav/Com/	XPDR/Audio
	AFCS
	GPS Nav
Flight	Planning
	Procedures
Hazard	Avoidance
Additional	Features
Abnormal	Operation
Annun/	Alerts
	Appendix
	Index

AFCS

VERTICAL MODES

Vertical Mode			Description				Control	Annunciation
	Holds the current aircraft pitch
Pitch Hold	attitude; may be used to climb/						(default)		PIT
	descend to the Selected Altitude
Selected Altitude	AFCS armed to capture the altitude
	displayed in the Selected Altitude						*		ALTS
Armed
	window
Altitude Hold	Holds	the		current	Altitude		ALT Key	ALT	nnnnn ft
	Reference
	Maintains		the	current	aircraft
Vertical Speed	vertical speed; may be used to climb/						VS Key	VS	nnnn fpm
	descend to the Selected Altitude
	Maintains		the	current	aircraft
Flight Level Change	airspeed in IAS while the aircraft is						FLC Key	FLC	nnn kt
	climbing/descending to the Selected
	Altitude
VNAV	Captures and tracks the VNAV flight						VNV Key		VPTH
	path
VNAV Target Altitude	AFCS armed to capture the altitude
Armed (GDU 1045	displayed in the VNAV Target						**		ALTV
only)	Altitude window
Glidepath	Captures		and	tracks the		SBAS			GP
	glidepath on approach
							APR Key
Glideslope	Captures		and	tracks	the	ILS			GS
	glideslope on approach
	Disengages the autopilot					and	GA
Go Around	commands a constant pitch attitude								GA
							Switch
	and wings level

*ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude

**ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude

14	Garmin G1000 Cockpit Reference Guide for the Beechcraft G58	190-00526-03 Rev. A