Garmin Beechcraft 58, G58 Reference Guide

TM

G1000

Cockpit Reference Guide

for the Beechcraft 58/G58

Copyright © 2005 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0500.00 or later for the Beechcraft 58/G58. Some differences in opera

-

tion 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., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K.
Tel: [phone] Fax: [phone]

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

Web Site Address: www.garmin.com

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

Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000™ is a trademark of Garmin Ltd. or its subsidiaries.
These trademarks may not be used without the express permission of Garmin.

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

October 2005 190-00526-00 Rev. A Printed in the U.S.A.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

WARNINGS,

CAUTIONS, & NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function.
The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain
Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications
requiring a certified terrain awareness system. Terrain data is obtained from third party sources. Garmin is
not able to independently verify the accuracy of the terrain data.

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

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

WARNING: The Jeppesen database used in the G1000 system must be updated regularly in order to ensure
that its information remains current. Updates are released every 28 days. A database information packet is
included in the G1000 package. Pilots using an outdated database do so entirely at their own risk.

WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non­navigational situational awareness. Any basemap indication should be compared with other navigation
sources.

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 interface for hazardous weather penetration (thunderstorm penetration)
is prohibited. Weather information on the G1000 MFD is approved only for weather avoidance, not
penetration.

WARNING: Use of the GDL 69 Weather Interface for hazardous weather penetration is prohibited. Weather
information provided by the GDL 69 is approved only for weather avoidance, not penetration.

ii

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

WARNINGS,

CAUTIONS, & NOTES

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

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

WARNING: The 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 58/G58 Pilot’s Operating Handbook. 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.

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 Airman’s Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense
radar echo.”

CAUTION: The GDU 1040 PFD and GDU 1043 MFD displays use a lens coated with a special anti-reflective
coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA
WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth
and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

iii

WARNINGS,

CAUTIONS, & NOTES

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.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge
points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has
been cleared.

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

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

iv

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

RECORD OF REVISIONS

Part Number Change Summary

190-00526-00 Initial release.

Revision Date of Revision Affected Pages Description

A 10/3/05 i-Index-4 Initial release

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

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RECORD OF REVISIONS

This page intentionally left blank.

vi

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

TABLE OF CONTENTS

SECTION 1: SYSTEM OVERVIEW .................................... 1-1

1.1 PFD/MFD Controls ................................................... 1-2

1.2 PFD Softkeys ............................................................ 1-4

1.3 MFD Softkeys ..........................................................1-7

1.4 MFD Page Groups ................................................... 1-8

1.5 Backlighting ............................................................. 1-8

SECTION 2: FLIGHT INSTRUMENTS .............................. 2-1

2.1 Airspeed Indicator .................................................. 2-3

Speed Indication .........................................................2-3

Speed Ranges ............................................................. 2-3

Airspeed Trend Vector ................................................. 2-3

Vspeed References ...................................................... 2-3

2.2 Attitude Indicator ..................................................2-3

2.3 Altimeter .................................................................. 2-4

Altitude Reference Bug ................................................ 2-4

Altitude Trend Vector ................................................... 2-4

Barometric Setting Box ................................................ 2-4

2.4 Vertical Deviation/Glideslope Indicator ............ 2-4

2.5 Marker Beacon Annunciations ............................2-4

2.6 Vertical Speed Indicator ....................................... 2-5

2.7 Horizontal Situation Indicator (HSI) ...................2-5

Course Pointer ............................................................ 2-6

Course Deviation Indicator (CDI) ..................................2-6

Bearing Pointers and Information Windows .................. 2-6

DME Radio (optional) .................................................. 2-7

Navigation Source ....................................................... 2-7

SECTION 3: ENGINE INDICATION SYSTEM (EIS) .... 3-1

3.1 Engine Display ......................................................... 3-1

3.2 Lean Engine Display ............................................... 3-1

3.3 Engine System Display .......................................... 3-2

SECTION 4: NAV/COM AND TRANSPONDER .......... 4-1

4.1 Radio Status Indications ....................................... 4-3

4.2 Volume ...................................................................... 4-3

4.3 Automatic Squelch ................................................. 4-3

4.4 Quickly Activating 121.500 MHz .......................... 4-3

4.5 Optional NAV Radios ............................................. 4-3

DME Radio (optional) .................................................. 4-3

4.6 Frequency Auto-tuning ......................................... 4-4

Auto-tuning on the PFD .............................................. 4-4

Auto-tuning on the MFD .............................................4-4

4.7 Transponder ............................................................. 4-4

Mode Selection ...........................................................4-4

Ground Mode (Automatic)
Reply Status
Code Selection

Flight ID Reporting ...................................................... 4-5

........................................................... 4-4

....................................................... 4-4

...................................... 4-4

SECTION 5: AUDIO PANEL ................................................5-1

5.1 COM Radio Selection ............................................. 5-2

5.2 Marker Beacon Receiver ....................................... 5-2

Marker Beacon Signal Sensitivity .................................5-2

5.3 Nav Radio Audio Selection ................................... 5-2

5.4 Intercom System (ICS) Isolation .......................... 5-3

5.5 Intercom Squelch Control ..................................... 5-3

5.6 Digital Clearance Recorder with Playback

Capability ................................................................. 5-4

SECTION 6: AUTOMATIC FLIGHT CONTROL ............. 6-1

6.1 Mode Annunciations .............................................. 6-1

6.2 Overspeed Protection ...........................................6-2

6.3 AP Engagement/Disengagement ........................ 6-2

Automatic Disengagement ..........................................6-3

Manual Disengagement ..............................................6-3

Control Wheel Steering ................................................6-3

Yaw Damper ...............................................................6-3

6.4 Loss of Data ............................................................. 6-3

6.5 Pitch Axis Modes ....................................................6-3

Pitch Hold Mode (PIT) ................................................. 6-4

Altitude Hold Mode (ALT) ............................................ 6-5

Vertical Speed Mode (VS) ............................................ 6-6

Flight Level Change Mode (FLC) ..................................6-7

Go-Around Mode (GA) ................................................ 6-8

Glideslope (GS) ........................................................... 6-8

6.6 Roll Axis Modes ....................................................... 6-9

Roll Hold Mode (ROL) .................................................. 6-9

Heading Select Mode (HDG) ...................................... 6-10

Navigation Mode (GPS, VOR, LOC, or BC) ................... 6-11

Navigation Mode Armed

Approach Mode (GPS, VAPP or LOC) .......................... 6-12

Go Around (GA) ........................................................ 6-12

6.7 Example Procedures Using AFCS ....................... 6-13

Departure .................................................................6-14

Intercepting a VOR Radial ..........................................6-15

Flying a Flight Plan / GPS Course ............................... 6-16

....................................... 6-11

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

vii

TABLE OF CONTENTS

Flight Level Change (Descent) .................................... 6-17

ILS Approach ............................................................. 6-18

Go-Around / Missed Approach ...................................6-19

SECTION 7: NAVIGATION .................................................. 7-1

7.1 Navigation Map Page ............................................ 7-1

Select the MAP Page Group ......................................... 7-1

7.2 Direct-to Navigation .............................................. 7-1

Direct-to Navigation from the MFD .............................. 7-1

Direct-to Navigation from the PFD ............................... 7-2

7.3 Airport Information ............................................... 7-3

Select the Airport Information Page .............................7-3

Enter a Waypoint Facility Name or City Location ........... 7-3

Access Runway Information ......................................... 7-3

Access Frequency Information ...................................... 7-3

7.4 Intersection Information ...................................... 7-4

Select the Intersection Information Page ...................... 7-4

Access Information on an Intersection ......................... 7-4

7.5 NDB Information ..................................................... 7-4

Select the NDB Information Page .................................7-4

View Information on a Specific NDB ............................7-4

7.6 VOR Information ..................................................... 7-5

Select the VOR Information Page ................................. 7-5

Access Information on a VOR ....................................... 7-5

7.7 User Waypoint Information Page .......................7-5

7.8 Nearest Airports ..................................................... 7-5

Nearest Airport Information on the MFD ...................... 7-5

Nearest Airports Information on the PFD ...................... 7-6

7.9 Nearest Intersections ............................................ 7-6

Select the Nearest Intersections Page ........................... 7-6

View Information on the Nearest Intersection ..............7-7

7.10 Nearest NDB ............................................................ 7-7

Select the Nearest NDB Page ....................................... 7-7

Access Information on a Specific NDB .......................... 7-7

7.11 Nearest VOR ............................................................. 7-7

Select the Nearest VOR Page ....................................... 7-7

View Information on the Nearest VOR .......................... 7-7

Select and Load a VOR Frequency ................................ 7-8

7.12 Nearest User Waypoint .......................................... 7-8

Select the Nearest User Waypoint Page ........................ 7-8

Select a Nearest User Waypoint ................................... 7-8

7.13 Nearest Frequencies ..............................................7-8

Select the Nearest Frequencies Page ............................ 7-8

Select and Load the Nearest ARTCC, FSS, or Weather

Frequency ................................................................... 7-9

7.14 Nearest Airspaces ................................................... 7-9

Select the Nearest Airspaces Page ................................ 7-9

Airspace Alerts Box ..................................................... 7-9

View Additional Details for a Listed Airspace ................ 7-9

View and Quickly Load the Frequency for a Controlling

Agency .......................................................................7-9

SECTION 8: FLIGHT PLANNING ...................................... 8-1

8.1 User Defined Waypoints ........................................ 8-1

Select the User WPT Information Page ......................... 8-1

Create a New User Waypoint ....................................... 8-1

Create User Waypoints from the Navigation

Map Page ................................................................... 8-1

Modify a User Waypoint ..............................................8-2

Delete a User Waypoint ............................................... 8-2

8.2 Viewing the Active Flight Plan ............................ 8-2

8.3 Activate a Stored Flight Plan ............................... 8-2

8.4 Activate a Flight Plan Leg ....................................8-2

8.5 Stop Navigating a Flight Plan .............................. 8-3

8.6 Invert Active Flight Plan ....................................... 8-3

8.7 Create a New Flight Plan ...................................... 8-3

8.8 Load a Departure ...................................................8-4

8.9 Load an Arrival ........................................................ 8-4

8.10 Load an Approach .................................................. 8-4

8.11 Remove a Departure, Arrival, or Approach

from a Flight Plan ...................................................8-5

8.12 Store a Flight Plan .................................................. 8-5

8.13 Edit a Stored Flight Plan ....................................... 8-5

8.14 Delete a Waypoint from the Flight Plan ............ 8-5

8.15 Invert and activate a Stored Flight Plan ........... 8-5

8.16 Copy a Flight Plan .................................................. 8-6

8.17 Delete a Flight Plan ............................................... 8-6

8.18 Graphical Flight Plan Creation ............................ 8-6

8.19 Trip Planning ............................................................ 8-6

8.20 Vertical Navigation (VNAV) Page ........................ 8-7

VNAV Page Menu Options ........................................... 8-9

SECTION 9: PROCEDURES ................................................9-1

9.1 Arrivals and Departures ........................................ 9-1

Load and Activate a Departure Procedure ....................9-1

Load and Activate An Arrival Procedure ........................ 9-1

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

TABLE OF CONTENTS

9.2 Approaches .............................................................. 9-2

Load and/or Activate an Approach Procedure ............... 9-2

Activate An Approach in the Active Flight Plan ............. 9-3

SECTION 10: HAZARD AVOIDANCE ...........................10-1

10.1 Customizing the Hazard Displays on the

Navigation Map .................................................... 10-1

10.2 STORMSCOPE® (Optional) .................................. 10-1

Displaying Stormscope Lightning Data on the

Navigation Map Page ................................................ 10-1

Stormscope Page ....................................................... 10-2

10.3 XM Weather (Optional) .......................................10-3

Displaying METAR and TAF information on the

Airport Information Page ........................................... 10-3

Displaying Weather on the Weather Data Link Page ...10-4

NEXRAD Limitations

Map Panning Information – Weather Data Link Page . 10-5

Weather Products and Symbols .................................10-5

Weather Product Age ................................................10-6

10.4 Traffic Information Service (TIS) ....................... 10-7

Displaying Traffic on the Traffic Map Page ................... 10-7

Displaying Traffic on the Navigation Map ...................10-7

TIS Audio Alert ..........................................................10-7

10.5 Skywatch Traffic Advisory System

(TAS)(Optional) ...................................................... 10-8

Displaying Traffic on the Traffic Map Page ................... 10-8

Displaying Traffic on the Navigation Map ...................10-8

10.6 Terrain And Obstacle Proximity ........................10-9

Displaying Terrain and Obstacles on the Terrain

Proximity Page .......................................................... 10-9

Displaying Terrain and Obstacles on the

Navigation Map ........................................................10-9

10.7 Terrain Awareness & Warning System (TAWs)

Display (Optional) ..............................................10-10

Displaying Terrain on the TAWS Page .......................10-10

Enable/Disable Aviation Data ................................... 10-11

TAWS Inhibit ...........................................................10-12

Manual System Test ................................................. 10-12

Forward Looking Terrain Avoidance (FLTA) ................ 10-12

Reduced Required Terrain Clearance (RTC) and
Reduced Required Obstacle Clearance (ROC)
Imminent Terrain Impact (ITI) and Imminent
Obstacle Impact (IOI)

Premature Descent Alert (PDA) ................................ 10-12

............................................. 10-4

......10-12

..........................................10-12

Excessive Descent Rate Alert (

Negative Climb Rate After TakeoffAlert (NCR) .......... 10-14

“Five-Hundred” Aural Alert ...................................... 10-14

Displaying Terrain and Obstacles on the

Navigation Map ......................................................10-14

Pop-up Alerts .......................................................... 10-15

TAWS Alerts Summary .............................................10-16

Alert Annunciations ................................................. 10-17

10.8 Airborne Weather Radar ...................................10-18

Displaying Weather on the Weather Radar Page .......10-18

Adjusting Antenna Tilt .............................................10-18

On the Horizontal Scan Display
On the Vertical Scan Display

Vertically Scan a Storm Cell ..................................... 10-19

Adjusting Gain ........................................................ 10-20

Ground Mapping ..................................................... 10-20

Sector Scan ............................................................. 10-20

Antenna Stabilization .............................................. 10-21

Weather Attenuated Color Highlight (WATCH) ......... 10-21

EDR) .......................... 10-13

........................... 10-18

...............................10-19

SECTION 11: ABNORMAL OPERATION ..................... 11-1

11.1 Reversionary Mode .............................................. 11-1

11.2 Abnormal COM Operation .................................. 11-2

11.3 Unusual Attitudes ................................................. 11-2

11.4 Stormscope operation with loss of

Heading Input ........................................................ 11-2

SECTION 12: ANNUNCIATIONS & ALERTS ..............12-1

12.1 Alert Level Definitions ........................................ 12-2

12.2 Beechcraft 58/G58 Annunciations & Alerts .....12-3

WARNING Annunciation ............................................ 12-3

CAUTION Annunciation ............................................. 12-3

ADVISORY Annunciation ............................................ 12-3

Alert Message ........................................................... 12-3

12.3 AFCS Alerts ............................................................. 12-4

System Status Field ...................................................12-4

12.4 TAWS ALERTS ......................................................... 12-5

TAWS System Status Annunciations ........................... 12-6

12.5 G1000 System Annunciations ............................ 12-6

Traffic Voice Alerts ..................................................... 12-6

12.6 G1000 System Alert Messages ........................... 12-8

MFD & PFD Alert Messages ....................................... 12-9

Database Alert Messages ........................................ 12-10

GMA 1347 Alert Messages ...................................... 12-11

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

ix

TABLE OF CONTENTS

GIA 63 Alert Messages ............................................ 12-11

GEA 71 Alert Messages ...........................................12-13

GTX 33 Alert Messages ........................................... 12-14

GRS 77 Alert Messages ........................................... 12-14

GMU 44 Alert Messages .......................................... 12-15

GDL 69 Alert Messages ........................................... 12-15

GDC 74A Alert Messages ........................................ 12-15

GWX 68 Alert Messages .......................................... 12-15

Miscellaneous Alert Messages ................................. 12-16

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

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

SECTION 1

SYSTEM OVERVIEW

SECTION 1: SYSTEM OVERVIEW

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 complete system are found in the
following documents:

• G1000 Primary Flight Display Pilot’s Guide

• G1000 VHF NAV/COM Pilot’s Guide

• G1000 Transponder Pilot’s Guide

• G1000 GMA 1347 Audio Panel Pilot’s Guide

• G1000 Engine Indication System Pilot’s Guide

• G1000 AFCS Pilot’s Guide

• G1000 Multi Function Display Pilot’s Guide

• G1000 Optional Equipment Pilot’s Guide

This guide gives the pilot abbreviated operating
instructions for the Primary Flight Display (PFD), Multi
Function Display (MFD), and the GMA 1347 Audio Panel
System.

NOTE: The pilot should read and thoroughly
understand the Beechcraft 58/G58 Pilot’s
Operating Handbook (POH) for limitations,
procedures and operational information not
contained in this Cockpit Reference Guide. The
Beechcraft 58/G58 POH always takes precedence
over the information found in this guide.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

1-1

1-1

SECTION 1

SYSTEM OVERVIEW

1.1 PFD/MFD CONTROLS

3

421 6

5

7

8

9

1-2

18

19

20

21

22

23

17

MFD Only

Figure 1-3 PFD/MFD Controls

24

25

26

27

28

10

11

12

13

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

14

15

16

SECTION 1

SYSTEM OVERVIEW

Functionality of the PFD and MFD controls are the
same with the exception of the dedicated autopilot keys
located only on the MFD bezel.

(1) NAV VOL/ID Knob – Controls the NAV audio level.
Press to toggle the Morse code identifier ON and OFF.
Volume level is shown in the field as a percentage.
(2) NAV Frequency Toggle Key – Toggles the standby
and active NAV frequencies.
(3) Dual NAV Knob – Tunes the MHz (large knob)
and kHz (small knob) standby frequencies for the NAV
receiver. Press to toggle the tuning cursor (light blue box)
between the NAV1 and NAV2 fields.
(4) Heading Knob – Turn to manually select a heading
on the HSI. When pressed, it synchronizes the heading
bug with the compass lubber line. Selected Heading
provides the heading reference to the Flight Director while
operating in Heading Select mode.
(5) Joystick – Changes the map range when rotated.
Activates the map pointer when pressed.
(6) CRS/BARO Knob – The large knob sets the altimeter
barometric pressure and the

small knob adjusts the
course. The course is only adjustable when the HSI is in
VOR1, VOR2, or OBS/SUSP mode. Pressing this knob
centers the CDI on the currently selected VOR.

Selected
Course provides course reference to the Flight Director
when operating in Navigation and Approach modes.
(7) Dual COM Knob – Tunes the MHz (large knob)
and kHz (small knob) standby frequencies for the COM
transceiver. Pressing this knob toggles the tuning cursor
(light blue box) between the COM1 and COM2 fields.
(8) COM Frequency Toggle Key – Toggles the standby
and active COM frequencies. Pressing and holding this
key for two seconds automatically tunes the emergency
frequency (121.5 MHz) in the active frequency field.
(9) COM VOL/SQ Knob – Controls COM audio level.
Pressing this knob turns the COM automatic squelch ON
and OFF. Audio volume level is shown in the field as a
percentage.

(10) Direct-to Key – Allows the user to enter a destination
waypoint and establish a direct course to the selected
destination (specified by the identifier, chosen from the
active route, or taken from the map cursor position).
(11) FPL Key – Displays the active Flight Plan Page for
creating and editing the active flight plan, or for accessing
stored flight plans.
(12) CLR Key (DFLT MAP) – Erases information,
cancels an entry, or removes page menus. To display the
Navigation Map Page immediately, press and hold CLR
(MFD only).
(13) Dual FMS Knob – Used to select the page to be
viewed (only on the MFD). The large knob selects a page
group (MAP, WPT, AUX, NRST), while the small knob
selects a specific page within the page group. Pressing
the small knob turns the selection cursor ON and OFF.
When the cursor is ON, data may be entered in the
different windows using the small and large knobs. The
large knob is used to move the cursor on the page, while
the small knob is used to select individual characters for
the highlighted cursor location. When the G1000 displays
a list that is too long for the display screen, a scroll bar
appears along the right side of the display, indicating the
availability of additional items within the selected category.
Press the FMS/PUSH CRSR knob to activate the cursor
and turn the large FMS knob to scroll through the list.
(14) MENU Key – Displays a context-sensitive list of
options. This list allows the user to access additional
features, or to make setting changes that relate to certain
pages.
(15) PROC Key – Selects approaches, departures and
arrivals from the flight plan. If a flight plan is used,
available procedures for the departure and/or arrival
airport are automatically suggested. If a flight plan is not
used, the desired airport and the desired procedure may be
selected. This key selects IFR departure procedures (DPs),
arrival procedures (STARs) and approaches (IAPs) from
the database and loads them into the active flight plan.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

1-3

OBS

TMR/REF

NRST

INSET

IDENT

XPDR

CDI

PFD

ALERTS

DME

(optional)

1-4

SECTION 1

SYSTEM OVERVIEW

(16) ENT Key – Accepts a menu selection or data entry.
This key is used to approve an operation or complete data
entry. It is also used to confirm selections and information
entries.
(17) Dual ALT Knob – Sets the reference altitude in
the box located above the Altimeter. The large knob
selects the thousands, while the small knob selects the
hundreds. Selected altitude provides an altitude setting
for the Altitude Capture/Hold mode, in addition to the
standard G1000 altitude alerter function.
(18) AP Key – Engages/disengages the Autopilot and
Flight Director in the default vertical and lateral modes.
(19) FD Key – Activates/deactivates the Flight Director
only. Pressing the

FD key turns on the Flight Director in
the default vertical and lateral modes. Pressing the FD
key again deactivates the Flight Director and removes the
command bars, unless the Autopilot is engaged. If the
Autopilot is engaged, the FD key is disabled.

(20) NAV Key

– Selects/deselects the Navigation mode.
(21) ALT Key – Selects/deselects the Altitude Hold
mode.

(22) VS Key – Selects/deselects the Vertical Speed mode.
(23) FLC Key – Selects/deselects the Flight Level Change

mode.

(24) YD Key – Engages/disengages the Yaw Damper.
(25) HDG Key – Selects/deselects the Heading Select

mode.

(26) APR Key – Selects/deselects the Approach mode.
(27, 28) NOSE UP/NOSE DN Keys – Controls the

active pitch reference for the Pitch Hold, Vertical Speed,
and Flight Level Change modes.

1.2 PFD SOFTKEYS

Softkey ON

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

Softkey OFF

Figure 1-2 PFD Top Level Softkeys

INSET – Press to display the Inset Map in the lower

left corner of the PFD.

OFF

– Press to remove the Inset Map

DCLTR

(3) – Press momentarily to select the desired
amount of map detail. The declutter level appears
adjacent to the DCLTR softkey.

• No declutter: All map features are visible

• Declutter – 1: Declutters land data

• Declutter – 2: Declutters land and SUA data

• Declutter – 3: Declutters large NAV data remaining
(removes everything except the active flight plan)

TRAFFIC
TOPO

– Press to display TIS traffic on the map.

– Press to display topographical data (i.e.,
coastlines, terrain, rivers, lakes, etc.) and
elevation scale on the inset map.

TERRAIN

– Press to display terrain information on

the inset map.

STRMSCP (optional)

– Press to display the
Stormscope lightning data on the inset map
(within a 200 nm radius of the aircraft).

NEXRAD (optional)

– Press to display NEXRAD

precititation data on the inset map.

XM LTNG (optional)

– Press to display the XM Radio

lightning data on the inset map.

BACK

– Press to return to the previous level softkey

configuration.

PFD – Press to display the additional softkeys for

additional configurations to the PFD.

METRIC

– Press to display the current and reference
altitudes in meters, in addition to feet. Pressing
the metric softkey also changes the barometric
setting to hectopascals.

DFLTS

– Press to reset default settings on the PFD.

DME

(optional) – Press to display the DME

information window.

SECTION 1

INSET

OFF

TOPO

TRAFFIC

TERRAIN

DCLTR

DCLTR-2

DCLTR-3

DCLTR-1

NEXRAD

Press the BACK or OFF softkey
to return to the top level
softkeys

XM LTNG

STRMSCP

BACK

ALERTS

(optional) (optional)(optional)

PFD

Press the STD BARO or BACK softkeys
to return to the top level softkeys

Press the DFLTS softkey to change the PFD
metric values to standard

STD BARO

BACK

ALERTS

BRG2

BRG1

METRIC

DFLTS

DME

(optional)

SYSTEM OVERVIEW

BRG1 (bearing)

– Press to cycle through the

following information:

NAV1

– Displays NAV1 waypoint frequency or
identifier and DME information in the BRG1
information window.

GPS

– Displays GPS waypoint identifier and GPS
distance information in the BRG1 information
window.

OFF

– Remov es the BRG1 information

window.

BRG2 (bearing)

– Press to cycle through the

following information:

NAV2

– Displays NAV2 waypoint frequency or
identifier and DME information in the BRG2
information window.

GPS

– Displays GPS waypoint identifier and GPS
distance information in the BRG2 information
window.

OFF

– Remo ves the BRG 2 information

window.

STD BARO

– Press to set the barometric pressure to

29.92 inches of mercury (1013 hPa by pressing
the METRIC softkey).

BACK

– Press to return to the previous level

softkeys.

Figure 1-3 PFD Softkey Flow Chart – 1

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

Figure 1-4 PFD Softkey Flow Chart – 2

1-5

SECTION 1

NRST

OBS

TMR/REF

IDENT

ALERTS

XPDR

STBY

ON

BACK

VFR

ALT

CODE

IDENT

0

1

6

3

2

4

5

7

IDENT

BACK

BKSP

Press the BACK softkey
to return to the top level
softkeys

Press the BACK
softkey
to return to
the top level
softkeys

ALERTS

ALERTS

DME

(optional)

CDI

CDI (VOR1)

CDI (VOR2)

GPS

SYSTEM OVERVIEW

OBS – Press to select OBS mode on the CDI when

navigating by GPS (only available with active leg).

CDI – Press to change navigation mode on the CDI

between GPS, VOR1 and VOR2.

DME (optional) – Press to display the DME Tuning

window.

XPDR – Press to display the transponder mode

selection softkeys.

STBY

– Press to select standby mode.

ON

– Press to select mode A.

ALT

– Press to select altitude reporting mode.

VFR

– Press to automatically squawk 1200 (only
in the U.S.A., refer to ICAO standards for VFR
codes in other countries).

CODE

– Press to display transponder code selection

softkeys 0-7.

0 through 7

– Press numbers to enter code.

IDENT

– Press to provide special aircraft
position identification to Air Traffic Control
(ATC).

BKSP

– Press to remove numbers entered one

at a time.

BACK

– Press to return to the previous level

softkeys.

IDENT

– Press to provide special aircraft position

identification to Air Traffic Control (ATC).

BACK

– Press to return to the previous level

softkeys.

IDENT – Press to provide special aircraft position

identification to Air Traffic Control (ATC).

TMR/REF – Press to display the Timer/References

window.

NRST – Press to display the Nearest Airports

window.

ALERTS – Press to display the Alerts window.

1-6

Figure 1-5 PFD Softkey Flow Chart – 3

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

SECTION 1

MAP

DCLTR

TRAFFIC

TOPO

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

BACK

Press to return to the
top softkey level

CHKLIST

EXIT

EMERGCY

ENGINE

DCLTR

MAP

ENGINE

CHKLIST

CLR

DONE

The DONE softkey changes to UNDO when the checklist
item is already checke

d

STRMSCP

NEXRAD

XM LTNG

(optional)

(optional)

(optional)

BACK

SYSTEM

ENGINE

LEAN

ENGINE

BACK

SYSTEM

LEAN

ENGINE

ENGINE

LEAN

BACK

SYSTEM

Press the BACK softkey on this level to
return to the top softkey level

ASSIST

CYL SLCT

DEC FUEL

Press the ENGINE or BACK softkey on any level to
return to the default page level

INC FUEL

166 GAL

194 GAL

(optional)

SYSTEM OVERVIEW

1.3 MFD SOFTKEYS

ENGINE – Pressing this softkey makes available the LEAN

and SYSTEM softkeys which in turn access the Lean
Page and the System Page, respectively.

MAP – pressing this softkey enables the following

softkeys:

TRAFFIC – pressing this softkey displays/removes

Traffic on the Navigation Map.

TOPO – pressing this softkey displays or removes

topographic information on the Navigation Map.

TERRAIN – pressing this softkey displays/removes

terrain and obstacle data on the Navigation Map.

STRMSCP (optional) – pressing this softkey displays/

removes Stormscope lightning data on the Navigation
Map.

NEXRAD (optional) – pressing this softkey displays/

removes precipitation data on the Navigation Map.

XM LTNG (optional) – pressing this softkey displays/

removes XM Radio lightning data on the Navigation
Map.

BACK – pressing this softkey displays the ENGINE and

MAP top level softkeys.

DCLTR (declutter) – pressing this softkey removes map

information in three levels.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

Figure 1-6 MFD Softkeys

1-7

SECTION 1

SYSTEM OVERVIEW

1.4 MFD PAGE GROUPS

1. Turn the

large FMS

knob until the desired page

group is selected.

2. Turn the

small FMS

knob to select pages within

the group. See Figure 1-7.

Nearest Group

Auxiliary Page Group

Waypoint Page Group

Map Page Group

1.5 BACKLIGHTING

To manually adjust the backlight for the
PFD and MFD:

1. Press the
PFD Setup Menu window.

MENU key on the PFD to display the

Number of Pages in Current

Figure 1-7 Page Group Icon

Group

Selected Page

1-8

2. Press the small FMS knob to activate the cursor.
‘PFD DSPL > AUTO’ is now highlighted.

3. Turn the small FMS knob to display the
selection window.

4. Turn the FMS knob to select ‘MANUAL’, then
press the ENT key.

5. With the intensity value now highlighted, turn
the small FMS knob to select the desired
backlighting.

6. Turn the large FMS knob to highlight ‘MFD
DSPL > AUTO’ and repeat steps 3 through 5.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

Figure 1-8 PFD Setup Menu Window

SECTION 2: FLIGHT INSTRUMENTS

The following discussions pertain to the Primary Flight

Display, unless otherwise indicated.

SECTION 2

FLIGHT INSTRUMENTS

1

2

3

4

5

6

1

NAV Frequency Window

2

Airspeed Indicator

16

15

9

Turn Rate Indicator

10

Barometric Setting Box

14

13

12

11

10

9

8

7

3

True Airspeed Box

4

Heading Box

5

Horizontal Situation Indicator

6

Outside Air Temperature Box

7

System Time Box

8

Transponder Status Bar

Figure 2-1 Default PFD Information

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

11

Vertical Speed Indicator

12

Altimeter

13

Altitude Reference Box

14

COM Frequency Window

15

Navigation Status Bar

16

Slip/Skid Indicator

2-1

SECTION 2

FLIGHT INSTRUMENTS

1

11

10

9

2

3

4

1

Traffic Annunciation

2

Selected Heading Box

3

Inset Map

4

BRG1 Information Window

5

DME Information Window

6

BRG2 Information Window

5

7

Alerts Window

8

Selected Course Box

9

Annunciation Window

10

Vertical Deviation/

11

Marker Beacon Annunciation

Figure 2-2 Additional PFD Information

6

Glideslope Indicator

8

7

2-2

Distance to Next Waypoint

Next Waypoint

Desired Track to

Next Waypoint

Figure 2-3 PFD Navigation Status Window (default)

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

Current Track

SECTION 2

FLIGHT INSTRUMENTS

2.1 AIRSPEED INDICATOR

Flap Extension

Speed

Airspeed Trend

Actual Airspeed

Speed Range

(flaps 30 speed range)

True Airspeed

Box

Figure 2-4 Airspeed Indicator

Speed Indication

The indicated airspeed is displayed inside the black
pointer. The pointer will become red upon reaching
Vne.

Vector

Vspeed

References

(best glide)

Vspeed References

Vspeed References are turned on or off in the

Timer/References window. Press the

TMR/REF softkey
to display the widow. When active (ON), the Vspeeds are
displayed at their respective locations to the right of the
airspeed scale. To activate the Vspeed References, display
the Timer/Reference window and turn the large FMS
knob to place the cursor in the ON/OFF field. Turn the
small FMS knob to select ON or OFF.

2.2 ATTITUDE INDICATOR

The Slip/Skid Indicator is located under the roll pointer
and moves laterally away from the pointer to indicate
lateral acceleration. One Slip/Skid indicator displacement
is equal to one ball displacement when compared to a
traditional slip/skid indicator.

10

9

1

2

8

Figure 2-5 Red Pointer at Vne

Speed Ranges

The color coded speed range strip denotes flaps
operating range, normal operating range, and never
exceed speed (Vne). A red range is also present for low
speed awareness. Refer to the Pilot’s Operating Handbook
(POH) for airspeed limitations and indicator markings.

Airspeed Trend Vector

The end of the trend vector displays approximately
what the airspeed will be in 6 seconds if the current rate
of acceleration/deceleration is maintained.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

3

4

1

Roll Pointer

2

Roll Scale

3

Horizon Line

4

Aircraft Symbol

5

Land Representation

Figure 2-6 Attitude Indicator

6

Aircraft Wing Tips

7

Pitch Scale

8

Slip/Skid Indicator

9

Sky Representation

10

Roll Index

7

6

5

2-3

SECTION 2

FLIGHT INSTRUMENTS

2.3 ALTIMETER

Altitude Reference

Box

Altitude Trend

Vector

Altitude Reference Bug

Figure 2-7 Altimeter

Altitude Reference Bug

The Altitude Reference Bug can be set to any desired
altitude. The bug acts as a visual reference to indicate the
Altitude Select setting.

To set the altitude reference bug:

ALT

1. Turn the
bug. The
the

large ALT

altitude also appears in the altitude reference
box above the altimeter.

knobs to set the altitude reference

small ALT

knob sets the hundreds and

knob sets the thousands. This

Current Altitude

Barometric Setting

Box

Barometric Setting Box

To set barometric pressure, turn the BARO knob to

select the desired setting.

2.4 VERTICAL DEVIATION/GLIDESLOPE INDICATOR

The Vertical Deviation/Glideslope Indicator appears

when an ILS is tuned in the active NAV field.

2.5 MARKER BEACON ANNUNCIATIONS

Marker Beacon

Annunciation

Vertical

Deviation/Glideslope

Indicator

Figure 2-8 Marker Beacon and Vertical Deviation

2-4

Altitude Trend Vector

The end of the trend vector displays approximately
what the altitude will be in 6 seconds if the current rate of
vertical speed is maintained.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

SECTION 2

FLIGHT INSTRUMENTS

2.6 VERTICAL SPEED INDICATOR

Selected Vertical Speed

Vertical Speed Bug

Vertical Speed Pointer

Figure 2-9 Vertical Speed Indicator

The actual vertical speed is displayed inside the
pointer.

Pressing the VS key will display the Vertical Speed Bug.
Press the NOSE UP or NOSE DN key to adjust.

2.7 HORIZONTAL SITUATION INDICATOR (HSI)

14

13

1

2

3

4

5

6

1

Turn Rate Indicator

2

Lateral Deviation Scale

3

Navigation Source

4

Aircraft Symbol

5

Course Deviation Indicator

6

Rotating Compass Rose

7

OBS Mode

8

TO/FROM Indicator

9

Heading Bug

10

Course Pointer

11

Flight Phase

12

Turn Rate and Heading Trend Vector

13

Heading

14

Lubber Line

12

11

10

9

8

7

Figure 2-10 Horizontal Situation Indicator

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

2-5

SECTION 2

FLIGHT INSTRUMENTS

Turn Rate Indicator and Heading Trend Vector

Each tick mark is at 9 (half standard rate tick mark)
and 18 (standard rate tick mark) degrees to the left and
right of the lubber line. A wide magenta line displays the

Bearing Pointers and Information Windows

Pressing the PFD softkey provides access to the BRG1
and BRG2 softkeys. The BRG1 pointer is a single line
pointer. The BRG2 pointer is a double line pointer.

current turn rate, up to 24 degrees. A magenta arrowhead
appears at 25 degrees. This trend vector provides the pilot
with a prediction of what the heading will be in 6 seconds
at the present turn rate.

Figure 2-14 Turn Rate Indicator and Heading Trend Vector

Course Pointer

The course pointer is a single line arrow (GPS, VOR1
and LOC1) or double line arrow (VOR2 and LOC2) which
points in the direction of the set course.

DME

Information

Window

Bearing 1

Information

Figure 2-14 HSI with Bearing Information

Bearing 1

Pointer

Window

Bearing 2

Pointer

CDI

Bearing 2

Information

Window

2-6

Figure 2-15 Course Pointer

Course Deviation Indicator (CDI)

The CDI scale automatically adjusts to the current
phase of flight (enroute 5.0 nm, terminal area 1.0 nm,
or approach 0.3 nm). Scaling may be selected manually
from the MFD System Setup Page. See the MFD Pilot’s
Guide for more detail.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

Distance to

Bearing Source

Waypoint
Identifier

Bearing

Source

Figure 2-15 BRG1 Information Window

Figure 2-16 BRG2 Information Window

Pointer

Icon

Distance to

Bearing Source

Pointer

Icon

Waypoint

Identifier

Bearing

Source

DME Radio (optional)

To display the DME Information Window, press the
PFD softkey followed by the DME softkey.

Figure 2-17 DME Information Window

Navigation Source

To change between navigation sources:

SECTION 2

FLIGHT INSTRUMENTS

1. Press the

CDI softkey to change from GPS to

VOR1/LOC1.

2. Press the

CDI softkey again to change from

VOR1/LOC1 to VOR2/LOC2.

CDI

3. Press the

softkey a third time to return to

GPS.

When using GPS as the navigation source, the following
may appear:

• INTEG – RAIM is not available

• WARN – GPS detects a position error

• SUSP – Displayed when in OBS Mode indicating
GPS navigation is suspended.

Figure 2-18 GPS INTEG, GPS SUSP, LOC1 and VOR2

To enable/disable OBS mode while navigating
with GPS:

1. Press the

OBS softkey to select OBS Mode.

2. Turn the CRS knob to select the desired course

TO/FROM the waypoint.

3. Press the OBS softkey again to return to normal

operation.

NOTE: The OBS softkey is only displayed when

navigating an active leg.

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

2-7

SECTION 2

FLIGHT INSTRUMENTS

.

This page intentionally left blank.

2-8

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

SECTION 3 – ENGINE

INDICATION SYSTEM (EIS)

SECTION 3: ENGINE INDICATION

SYSTEM (EIS)

3.1 ENGINE DISPLAY

In all cases green indicates normal operation, yellow

indicates caution, and red indicates warning.

Pressing 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

ENGINE softkey makes available the

Propeller Sync

Indicator

Fuel Flow

Numeric
Readout

Cylinder Head

Temperature

Indicator

Oil Pressure

Indicator

Fuel Quantity

Indicator

3.2 LEAN ENGINE DISPLAY

Difference between peak

Cylinder peak

temperature

(Left Engine)

Exhaust Gas
Temperature

Bar Graphs

(Left Engine)

Cylinder Head

Temperature

Bar Graphs

(Left Engine)

Figure 3-2 LEAN Engine Page

Press the CYL SLCT softkey to select the desired

cylinder for monitoring.

The CYL SLCT softkey becomes disabled when the

ASSIST softkey is pressed.

Pressing the ASSIST softkey causes the first cylinder
that peaks to become highlighted and information for that
cylinder to be displayed.

and current temperature

of selected cylinder

(Right Engine)

EGT Readout

For Selected

Cylinder

(Right Engine)

CHT Readout

For Selected

Cylinder

(Right Engine)

Figure 3-1 Default Engine Page

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58

3-1

SECTION 3 – ENGINE

INDICATION SYSTEM (EIS)

3.3 ENGINE SYSTEM DISPLAY

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.

3-2

System

Information

Fuel Calculation

Information

Electrical

Information

Figure 3-3 SYSTEM Engine Page

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58