Garmin SA01535Wi-D Reference Guide
®
G1000
Cockpit Reference Guide for the Beechcraft 300/B300 Series
Integrated Flight Deck
FLIGHT INSTRUMENTS
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2011, 2012 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0985.04 or later for the
Beechcraft 300 and B300. Some differences in operation may be observed when comparing
the information in this manual to earlier or later software versions.
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Tel: 913/397.8200 Fax: 913/397.8282
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Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied,
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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
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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® , G1000®, WATCH®, FliteCharts®, and SafeTaxi® are registered trademarks of Garmin
Ltd. or its subsidiaries. ESP™ 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.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable for any incidental, special or
consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
April, 2012 190-01344-00 Rev. B 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 74B 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 system displays 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: Do not use datalink 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.
190-01344-00 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
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: 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.
WARNING: The Garmin G1000, as installed in the Hawker Beechcraft 300/
B300 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
G1000 Integrated Avionics System and GFC 700 AFCS in Hawker Beechcraft
300 and B300 King Air Airplane Flight Manual Supplement. 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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
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.
190-01344-00 Rev. B
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
Record of Revisions
Part Number Change Summary
190-01344-00
Rev A Initial release
Revision Date of Revision Affected Pages Description
B April, 2012 52 Removed reference to TCAS II
pitch attitude cue.
190-01344-00 Rev. B RR-1
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Record of Revisions
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RR-2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
Table of Contents
FLIGHT INSTRUMENTS ................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting ...................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg) ....................................................1
Change Altimeter Barometric Pressure Setting Units ...................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings ........................................... 1
Synchronize CDI......................................................................................................................... 1
Change Navigation Sources ................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS .................................................... 2
Generic Timer ............................................................................................................................. 2
Configure Vspeed Bugs Individually .....................................................................................2
Turn Vspeed Bugs On or Off by Category ............................................................................ 3
Set Barometric/Radar Altimeter Minimum Descent Altitude ......................................... 3
Testing the Radar Altimeter ................................................................................................... 3
Displaying Wind Data .............................................................................................................. 3
NAV/COM/TRANSPONDER/AUDIO PANEL .........................................................................5
ADF Tuning (Optional) .............................................................................................................. 5
DME Tuning.................................................................................................................................5
Enter a Transponder Code....................................................................................................... 5
Select Transponder Mode ....................................................................................................... 5
Activate ADS-B Transmit (Not available with TCAS II) ..................................................... 6
Selecting a COM Radio ............................................................................................................ 6
Selecting a NAV Radio ............................................................................................................. 6
NAV/COM Tuning ....................................................................................................................... 7
Intercom ...................................................................................................................................... 7
Passenger Address (PA) System ............................................................................................. 7
Clearance Recorder and Player ............................................................................................. 8
AUTOMATIC FLIGHT CONTROL SYSTEM ............................................................................ 9
Flight Director Activation ....................................................................................................... 9
Vertical Modes .........................................................................................................................10
Lateral Modes .......................................................................................................................... 11
GPS NAVIGATION ........................................................................................................................ 13
Direct-to Navigation .............................................................................................................. 13
Activate a Stored Flight Plan ............................................................................................... 14
Activate a Flight Plan Leg ..................................................................................................... 14
Stop Navigating a Flight Plan .............................................................................................. 15
Vertical Navigation (VNAV)................................................................................................... 15
FLIGHT PLANNING ...................................................................................................................... 17
Weight Planning ...................................................................................................................... 17
Trip Planning ............................................................................................................................ 17
Create a User Waypoint Defined by Latitude & Longitude ........................................... 19
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Table of Contents
Create a User Waypoint Defined by Radials from Other Waypoints ........................... 20
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint ..22
Delete a User Waypoint ......................................................................................................... 23
Create a Flight Plan ................................................................................................................ 24
Import a Flight Plan from an SD Card ................................................................................ 25
Insert a Waypoint in the Active Flight Plan ...................................................................... 25
Enter an Airway in a Flight Plan .......................................................................................... 26
Invert An Active Flight Plan .................................................................................................. 27
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 27
Store a Flight Plan .................................................................................................................. 27
Edit a Stored Flight Plan ....................................................................................................... 28
Delete a Waypoint from the Flight Plan ............................................................................ 28
Invert and Activate a Stored Flight Plan ........................................................................... 28
Copy a Flight Plan ................................................................................................................... 29
Delete a Flight Plan ................................................................................................................ 29
Graphical Flight Plan Creation ............................................................................................. 29
Export a Flight Plan to an SD Card ..................................................................................... 30
PROCEDURES ................................................................................................................................. 31
Load and Activate a Departure Procedure ....................................................................... 31
Activate A Departure Leg ..................................................................................................... 31
Load An Arrival Procedure .................................................................................................... 31
Activate An Arrival Leg ......................................................................................................... 32
Load and/or Activate an Approach Procedure ................................................................. 32
Activate An Approach in the Active Flight Plan ............................................................... 33
Activate a Vector to Final Approach Fix ............................................................................ 33
Activate A Missed Approach in the Active Flight Plan ................................................... 33
HAZARD AVOIDANCE ................................................................................................................ 35
Customizing the Hazard Displays on the Navigation Map ............................................ 35
STORMSCOPE® (Optional) ..................................................................................................... 35
XM WX Satellite Weather (Optional) .................................................................................. 37
Worldwide Weather ................................................................................................................ 39
Traffic Avoidance Systems .................................................................................................... 49
Traffic Collision Avoidance System (TCAS II) (Optional) ................................................ 51
Terrain Awareness & Warning System ............................................................................... 53
Airborne Color Weather Radar ............................................................................................ 56
ADDITIONAL FEATURES ........................................................................................................... 61
Synthetic Vision ....................................................................................................................... 61
Terminal Procedure Charts ................................................................................................... 62
AOPA Airport Directory ......................................................................................................... 64
Satellite Telephone and Data Link Services ..................................................................... 65
ii
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
Table of Contents
WI-FI Connections ................................................................................................................... 78
System Data Logging ............................................................................................................. 81
SiriusXM Radio Entertainment ............................................................................................ 83
Electronic Stability & Protection (ESP™) ............................................................................ 85
ANNUNCIATIONS & ALERTS ................................................................................................... 87
WARNING Annunciation ........................................................................................................ 87
Advisory Annunciations......................................................................................................... 87
Message Advisory Alerts ....................................................................................................... 87
Comparator Annunciations ................................................................................................... 88
Reversionary Sensor Annunciations ................................................................................... 88
AFCS Alerts ............................................................................................................................... 89
TAWS-A Alerts .......................................................................................................................... 90
TAWS-B Alerts .......................................................................................................................... 93
Additional Aural Alerts .......................................................................................................... 96
MFD & PFD Message Advisories .......................................................................................... 97
Database Message Advisories ............................................................................................. 98
GMA 1347D Message Advisories ....................................................................................... 102
GIA 63W Message Advisories ............................................................................................. 103
GEA 71 Message Advisories ................................................................................................ 106
GTX 33 Message Advisories ................................................................................................ 106
GRS 77 Message Advisories ................................................................................................ 107
GMU 44 Message Advisories .............................................................................................. 108
GSR 56 Message Advisories ................................................................................................ 108
GDL 59 Message Advisories ................................................................................................ 109
GDL 69A Message Advisories ............................................................................................. 109
GWX 68 Alert Messages ....................................................................................................... 110
GDC 74B Message Advisories ............................................................................................. 110
GCU 477 Message Advisories ............................................................................................. 111
GMC 710 Message Advisories ............................................................................................ 111
Miscellaneous Message Advisories ................................................................................... 112
Flight Plan Import/Export Messages ................................................................................ 116
APPENDIX ..................................................................................................................................... 119
PFD Softkey Map .................................................................................................................. 119
MFD Navigation Page Softkey Map ................................................................................. 128
Loading Updated Databases .............................................................................................. 130
INDEX .........................................................................................................................................Index-1
190-01344-00 Rev. B iii
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
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)
Push the BARO Knob to select standard 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.
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
Instruments
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION
Window.
4)
Turn the
small
FMS Knob clockwise to ON or counterclockwise to OFF.
SYNCHRONIZE CDI
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the
190-01344-00 Rev. B 1
small
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Additional
Features Annun/Alerts Appendix Index
Flight Instruments
CHANGE NAVIGATION SOURCES
Flight
1)
Instruments
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This changes
the NAV1 standby frequency in the upper left corner of the PFD to light
blue, indicating this is the frequency selected for tuning.
2)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or
LOC2. This changes the NAV2 standby frequency in the upper left corner of
the PFD to light blue, indicating this is the frequency selected for tuning.
3)
Press the CDI Softkey a third time to return to GPS.
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.
Flight
PlanningProcedures
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.
Hazard
2)
Avoidance
FeaturesAnnun/AlertsAppendixIndex
Additional
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 will start 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
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
2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
large
FMS Knob to highlight the desired Vspeed.
190-01344-00 Rev. B
Flight Instruments
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
TURN VSPEED BUGS ON OR OFF BY CATEGORY
1)
Press the TMR/REF Softkey.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Press the TMR/REF Softkey to remove the window.
SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE
1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the
right of ‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to select BARO or RAD ALT.
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.
Instruments
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
TESTING THE RADAR ALTIMETER
1)
Select the AUX-SYSTEM STATUS Page on the MFD.
2)
Select the RA TEST Softkey. ‘RA TEST’ is displayed to the left of the Radar
Altitude window. The Radar Altitude window displays 50 feet, indicating a
properly functioning system.
3)
Selecting the RA TEST Softkey again, or exiting the System Status Page
cancels the test.
DISPLAYING WIND DATA
1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data below the Selected Heading.
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.
190-01344-00 Rev. B 3
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Additional
Features Annun/Alerts Appendix Index
Flight Instruments
Flight
Instruments
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
FeaturesAnnun/AlertsAppendixIndex
Additional
4
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
Nav/Com/XPDR/Audio Panel
NAV/COM/TRANSPONDER/AUDIO PANEL
Instruments
Flight
ADF TUNING (OPTIONAL)
Tune the ADF using the remote ADF control head.
DME TUNING
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 (XPDR/TFC if the TCAS II option is available).
2)
If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder. If these softkeys are not
present, proceed to step 3.
3)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
4)
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.
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features Annun/Alerts Appendix Index
SELECT TRANSPONDER MODE
With TCAS II Option
1)
Press the XPDR/TFC Softkey.
2)
Press the MODE Softkey to display the transponder mode selection
softkeys.
3)
Press the desired transponder mode softkey (STBY, ON, or A LT ).
190-01344-00 Rev. B 5
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Nav/Com/XPDR/Audio Panel
Without TCAS II Option
Flight
1)
Instruments
Press the XPDR Softkey.
2)
If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder.
Nav/Com/
3)
XPDR/AudioAFCSGPS Nav
Press the desired transponder mode softkey (STBY, ON, ALT , or GND).
ACTIVATE ADS-B TRANSMIT (NOT AVAILABLE WITH TCAS II)
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.
SELECTING A COM RADIO
Flight
PlanningProcedures
Transmit/Receive
Press the COM1 MIC, COM2 MIC
installed) on the audio panel.
, or
COM3 MIC Key (optional COM, if
Receive Only
Hazard
Avoidance
Press the COM1, COM2
audio panel.
SELECTING A NAV RADIO
FeaturesAnnun/AlertsAppendixIndex
Additional
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.
6
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
, or
COM3 Key (optional COM, if installed) on the
190-01344-00 Rev. B
Nav/Com/XPDR/Audio Panel
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
Instruments
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
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.
INTERCOM
Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.
Planning Procedures
Flight
The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.
The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.
Avoidance
Hazard
During manual squelch operation, pressing the ICS Knob switches between volume
and squelch adjustment, lighting the associated annunciator beneath the knob. When
the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When
the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.
Additional
Features Annun/Alerts Appendix Index
PASSENGER ADDRESS (PA) SYSTEM
A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the headset only if the
PA Key is enabled on both audio panels. PA messages are one way from the flight deck
to the passengers.
190-01344-00 Rev. B 7
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
Nav/Com/XPDR/Audio Panel
CLEARANCE RECORDER AND PLAYER
Flight
Instruments
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.
Nav/Com/
XPDR/AudioAFCSGPS Nav
Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes
of recording time have been reached, the recorder begins recording over the stored
memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator is illuminated to
indicate when play is in progress. The PLAY annunciator extinguishes after playback
is finished.
Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
Flight
PlanningProcedures
block, play is halted.
Pressing the PLAY Key twice within one-half second while audio is playing plays
the previous block of recorded audio. Each subsequent two presses of the PLAY Key
within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.
Hazard
Avoidance
FeaturesAnnun/AlertsAppendixIndex
Additional
8
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
AFCS
AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
FLIGHT DIRECTOR ACTIVATION
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
Instruments
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Control Pressed
Lateral Vertical
Modes Selected
FD Key Roll Hold (default) ROL Pitch Hold (default) PIT
AP Key Roll Hold (default) ROL Pitch Hold (default) PIT
CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT
GA Switch
Takeoff (on ground)
Go Around (in air)
TO
GA
Takeoff (on ground)
Go Around (in air)
TO
GA
ALT Key Roll Hold (default) ROL Altitude Hold A LT
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
BC Key Backcourse*** BC Pitch Hold (default) PIT
APR Key Approach**
GPS
VAPP
LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT
GP
GS
HDG Key Heading Select HDG Pitch Hold (default) PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV
or
APR
Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features Annun/Alerts Appendix Index
190-01344-00 Rev. B 9
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
AFCS
VERTICAL MODES
Flight
Instruments
Vertical Mode Description Control Annunciation
Holds the current aircraft pitch attitude; may
Pitch Hold
Nav/Com/
XPDR/AudioAFCSGPS Nav
Selected Altitude
Armed
Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn fT
Vertical Speed
Flight Level Change,
IAS Hold
Flight
PlanningProcedures
Flight Level Change,
Mach Hold
VNAV Captures and tracks the VNAV flight path VNV Key VPTH
VNAV Target
Altitude Armed
Hazard
Glidepath
Avoidance
Glideslope
FeaturesAnnun/AlertsAppendixIndex
Additional
Takeoff (on ground)
Go Around (in air)
Level Commands 0° pitch attitude
* ALTS armed automatically when PIT, VS, FLC, TO, 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
be used to climb/descend to the Selected
(default) PIT
Altitude
AFCS armed to capture the altitude displayed in
the Selected Altitude window
Maintains the current aircraft vertical speed;
may be used to climb/descend to the Selected
Altitude
Maintains the current aircraft airspeed (in
IAS or Mach) while the aircraft is climbing/
descending to the Selected Altitude. Press
FLC Key
the SPD Key to switch between IAS and
MACH.
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
window
Captures and tracks the SBAS glidepath on
approach
Captures and tracks the ILS glideslope on
APR Key
approach
Disengages the autopilot and commands a
constant pitch angle and wings level in the
air on the ground in preparation for takeoff
Disengages the autopilot and commands a
constant pitch attitude and wings level in
the air
Activated
the ESP
function
* ALTS
VS Key VS nnnn fpm
FLC nnn kT
FLC M .nnn
** ALTV
GA
Switch
only by
GP
GS
TO
GA
LVL
10
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
AFCS
LATERAL MODES
Instruments
Flight
Lateral Mode Description Control Annunciation
Roll Hold
Holds current aircraft roll attitude
or rolls wings level, depending on
(default) ROL
XPDR/Audio AFCS GPS Nav
Nav/Com/
commanded bank angle
Low Bank
Heading Select
Navigation, GPS Arm/
Capture/Track
Navigation, VOR Enroute
Arm/Capture/Track
Navigation, LOC Arm/
Capture/Track
Limits maximum commanded roll
angle
Captures and tracks Selected
Heading
Captures and tracks selected
navigation source (GPS, VOR, LOC)
BANK
Key
*
HDG Key HDG
GPS
NAV Key
VOR
LOC
Planning Procedures
Flight
(No Glideslope)
Backcourse Arm/Capture/
Track
Approach, GPS Arm/Capture/
Track
Approach, VOR Arm/Capture/
Track
Approach, ILS Arm/Capture/
Track
(Glideslope Mode
Captures and tracks a localizer
signal for backcourse approaches
Captures and tracks selected
navigation source (GPS, VOR, LOC)
BC Key BC
VAPP
APR Key
GPS
LOC
Avoidance
Hazard
Additional
Features Annun/Alerts Appendix Index
automatically armed)
Disengages autopilot and commands
Takeoff (on ground)
Go Around (in air)
a constant pitch angle and wings
level in preparation for takeoff
Disengages autopilot and
commands a constant pitch angle
TO
GA
Switch
GA
and wings level in the air
Activated
Level Commands wings level attitude
only by
the ESP
LVL
function
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
190-01344-00 Rev. B 11
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
AFCS
Flight
Instruments
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
FeaturesAnnun/AlertsAppendixIndex
Additional
12
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
GPS NAVIGATION
GPS Navigation
Instruments
Flight
DIRECT-TO NAVIGATION
Direct-to Navigation from the MFD
1)
Press the Direct-to
2)
Enter the waypoint identifier.
3)
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
4)
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
5)
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
6)
Enter the desired altitude.
7)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
8)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
9)
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
10)
Enter the desired offset distance before (-) or after (+) the waypoint.
11)
Press the ENT Key. The ‘Activate?’ field is highlighted.
12)
Press the ENT Key to activate.
( )
Key on the Control Unit.
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features Annun/Alerts Appendix Index
Direct-to Navigation from the PFD
1)
Press the Direct-to Key
2)
Turn the large FMS Knob to place the cursor in the desired selection field.
3)
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
4)
Press the ENT Key.
5)
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
6)
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
190-01344-00 Rev. B 13
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
( )
on the PFD.
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Flight
Instruments
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
10)
Press the ENT Key. The cursor is placed in the ‘OFFSET’ offset distance field.
11)
Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
12)
Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
13)
Turn the small FMS Knob to enter the desired course to the waypoint.
14)
Press the ENT Key to highlight ‘ACTIVATE?’.
15)
Press the ENT again to activate the Direct-to.
Flight
PlanningProcedures
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key on the Control Unit and turn the small FMS Knob to display
the Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Hazard
Avoidance
Select the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
FeaturesAnnun/AlertsAppendixIndex
Additional
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
14
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
Select the ACT LEG Softkey.
OR
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
3)
With ‘Activate’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B
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