Garmin G1000 NXi - Beechcraft King Air 200/A200/B200 Reference guide

Type
Reference guide
Beechcraft 200/A200/B200 Series
System Software Version 2286.11 or later
Pilot’s Guide
®
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
Copyright © 2005-2020 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2286.11 or later for the G1000 NXi Beechcraft 200/A200/B200 Series.
Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
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incidental or consequential damages so the above limitations or exclusions may not apply to you.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. A
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK 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 AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to
the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses
related to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. 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 license
Printed in the U.S.A.
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series iii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining
separation from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources
and cannot independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical
information. Displayed aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole means of navigation.
Basemap data is intended only to supplement other approved navigation data sources and should be
considered only an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of
hazardous weather. Information contained within data link weather products may not accurately depict
current weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be older than the indicated weather product age.
WARNING: Do not rely on the displayed minimum safe altitude (MSAs) as the sole source of obstacle
and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum
clearance altitudes.
WARNING: Do not operate this equipment without first obtaining qualified instruction.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not rely on the autopilot to level the aircraft at the MDA/DH when flying an approach with
vertical guidance. The autopilot will not level the aircraft at the MDA/DH even if the MDA/DH is set in the
altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING: Always use traffic information shown on system displays only as an aid to visually acquiring
traffic. Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories , ATC guidance, or positive
visual acquisition of conflicting traffic.
WARNING: Do not rely on information from a lightning detection system display as the sole basis for
hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate
or incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.
Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or
reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
WARNING: Do not use the Garmin SVT runway depiction as the sole means for determining the proximity
of the aircraft to the runway or for maintaining the proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within
the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of
precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color
not representative of the true intensity.
WARNING: Do not assume weather radar transmission is disabled unless all display panes displaying
weather radar are set to Standby Mode, and are displaying ‘STANDBY’ in the center of each weather radar
display. Transmission is also disabled by touching the Radar On Button or pressing the Radar On Softkey to
set the weather radar system to Off Mode, as indicated by a gray annunciator.
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series v
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use SurfaceWatch™ information as the primary method of flight guidance during
airborne or ground operations. SurfaceWatch does not have NOTAM or ATIS information regarding the
current active runway, condition, or information about the position of hold lines.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION: Do not allow repairs to be made by anyone other than an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and affect the airworthiness of the
aircraft.
CAUTION: Never disconnect power to the system when loading a database. Power interruption during the
database loading process could result in maintenance being required to reboot the system.
CAUTION: When downloading updates to the Jeppesen Navigation Database, copy the data to an SD card
other than a Garmin Supplemental Data Card. Otherwise, data corruption can occur.
CAUTION: Avoid areas on the radar display that appear “shadowed” (gray). The accuracy of the intensity
of returns in the shaded areas should be treated as suspect. Exercise extreme caution, making maneuvering
decisions with this information in mind.
CAUTION: In Standby mode, the antenna is parked at the center line. It is always a good idea to put the
radar in Standby mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop
and possibly causing damage to the radar assembly.
NOTE: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear
as a partial symbol.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the system panel
and displays, are subject to change and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: 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 system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
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: 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: 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: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields
can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut
down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no
comparison is possible.
NOTE: The system responds to a terminal procedure based on data coded within that procedure in the
Navigation Database. Differences in system operation may be observed among similar types of procedures
due to differences in the Navigation Database coding specific to each procedure.
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue
of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database
and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.
Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with
established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established
AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed
in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at
www.FlyGarmin.com by selecting ‘Database Exclusions List.
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series vii
WARNINGS, CAUTIONS, AND NOTES
NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their
impact on the intended aircraft operation. The database alerts can be viewed at www.FlyGarmin.com by
selecting ‘Aviation Database Alerts.
NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to www.FlyGarmin.com and select Aviation Data Error Report’.
NOTE: Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC
120 76D as a Type B Electronic Flight Bag (EFB) for FlightCharts and ChartView. The accuracy of the charts
is subject to the chart data provider. Own-ship position on airport surface charts cannot be guaranteed to
meet the accuracy specified in AC 120-76D. Possible additional requirements may make a secondary source
of aeronautical charts, such as traditional paper charts or an additional electronic display, necessary on the
aircraft and available to the pilot. If the secondary source of aeronautical charts is a Portable Electronic
Device (PED), its use must be consistent with the guidance in AC 120-76D.
NOTE: The navigation databases used in Garmin navigation systems contain Special Procedures. Prior
to flying these procedures, pilots must have specific FAA authorization, training, and possession of the
corresponding current, and legitimately sourced chart (approach plate, etc.). Inclusion of the Special
Procedure in the navigation database DOES NOT imply specific FAA authorization to fly the procedure.
NOTE: Terrain and obstacle alerting is not available north of 89° North latitude and south 89° South latitude.
This is due to limitations present within the Terrain database and the system’s ability to process the data
representing the affected areas.
NOTE: When operating the system with the magnetic sensor uncoupled from the AHRS, the displayed
heading and heading information used by some system components (e.g. traffic system, AFCS, and weather
radar) will be different from the heading calculated by the AHRS. The difference is an amount equal to the
difference between the current Magnetic Field Variation Database (MV DB) value, and the MV DB value
when the magnetic sensor was uncoupled. Due to the convergence of isogonic lines, this condition is most
noticeable at or near the north and south magnetic poles.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Aviii
WARNINGS, CAUTIONS, AND NOTES
NOTE: Operate G1000 NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
NOTE: The nose of the ‘own ship’ symbol represents the location of the aircraft. The center of any traffic
symbol represents the location of that traffic. The traffic and own ship symbols are an abstract representation
and do not reflect the physical extent of the aircraft/traffic, and should not replace other methods for
identifying traffic.
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series ix
SOFTWARE LICENSE AGREEMENT
SOFTWARE LICENSE AGREEMENT
BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN (“THE GARMIN PRODUCT”), YOU
AGREE TO BE BOUND BY THE TERMS AND CONDITIONS OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ
THIS AGREEMENT CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the software
embedded in the Garmin Product (the “Software”) in binary executable form in the normal operation of the Garmin Product. Title,
ownership rights, and intellectual property rights in and to the Software remain with Garmin and/or its third-party providers. You
acknowledge that the Software is the property of Garmin and/or its third-party providers and is protected under the United States of
America copyright laws and international copyright treaties. You further acknowledge that the structure, organization, and code of
the Software are valuable trade secrets of Garmin and/or its third-party providers and that the Software in source code form remains
a valuable trade secret of Garmin and/or its third-party providers. You agree not to reproduce, decompile, disassemble, modify,
reverse assemble, reverse engineer, or reduce to human readable form the Software or any part thereof or create any derivative
works based on the Software. You agree not to export or re-export the Software to any country in violation of the export control
laws of the United States of America.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Ax
SOFTWARE LICENSE AGREEMENT
Blank Page
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series xi
RECORD OF REVISIONS
Record of Revisions
Part Number Revision Date Page Range Description
190-02041-00 A
B
9/14/16
3/24/17
All
All
Initial Release for GDU 20.01
Revision
- Added Visual Approach
- Added Glidepath Preview
- Added SurfaceWatch Setup user interface
- Added ChartView section
- Added phone contacts
- Corrected comparator annunciations
190-02041-01 A
B
C
7/20/18
5/02/19
5/13/19
All
All
All
- Software update to GDU 20.82
- Editorial updates
Revision
- Software update to GDU 20.84
- Editorial updates
- Clerical updates
190-02041-02 A 10/29/20 All - Software update to GDU 20.84
- Added A200
- Editorial updates
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Axii
RECORD OF REVISIONS
Blank Page
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series xiii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ..............................................1
Line Replaceable Units ........................................................ 1
1.2 System Controls ...................................................4
PFD Controls .......................................................................4
Secure Digital Cards ............................................................ 8
1.3 System Operation ................................................9
System Power-on ................................................................9
Normal Operation .............................................................10
Reversionary Mode ...........................................................10
System Annunciations .......................................................11
ADAHRS Operation ...........................................................14
GPS Receiver Operation ....................................................17
1.4 Accessing System Functionality .........................22
Softkey Function ...............................................................22
Menus ............................................................................... 29
MFD Page Groups .............................................................30
Split Screen Functionality .................................................. 33
System Settings .................................................................35
System Utilities .................................................................45
1.5 Display Backlighting ..........................................49
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ..............................................54
Airspeed Indicator ............................................................. 54
Attitude Indicator ..............................................................57
Altimeter ........................................................................... 59
Vertical Speed Indicator (VSI) ............................................65
Vertical Deviation ..............................................................65
Horizontal Situation Indicator (HSI) ...................................68
Directional Gyro (DG) Mode (GRS 7800 Installations Only) ..
71
Course Deviation Indicator (CDI) .......................................74
2.2 Garmin SVT (Synthetic Vision Technology) .........81
SVT Operation ................................................................... 82
SVT Features .....................................................................84
Field of View .....................................................................93
2.3 Supplemental Flight Data ..................................94
Temperature Displays ........................................................ 94
Wind Data ......................................................................... 95
Vertical Navigation (VNV) Indications ............................... 96
2.4 PFD Annunciations and Alerting Functions ........97
Marker Beacon Annunciations ..........................................97
Altitude Alerting ................................................................97
Low Altitude Annunciation ................................................ 98
Minimum Altitude Alerting ................................................98
Radar Altimeter ............................................................... 100
2.5 Abnormal Operations .......................................102
Abnormal GPS Conditions ...............................................102
Comparator Annunciations .............................................103
Reversionary Sensor Annunciations ................................104
SVT Troubleshooting .......................................................105
Reversionary Mode .........................................................105
Unusual Attitudes ...........................................................105
SVT Unusual Attitudes ....................................................106
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display .......................................................108
3.2 EIS Display in Reversionary Mode ...................111
Reversionary Display ....................................................... 112
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .......................................................... 113
PFD Controls and Frequency Display ............................... 114
Audio Panel Controls ......................................................116
PFD/MFD Controller ........................................................120
4.2 COM Operation ................................................122
COM Tuning Boxes .......................................................... 122
COM Transceiver Manual Tuning ..................................... 123
Quick-Tuning and Activating 121.500 MHz .....................124
Auto-Tuning the COM Frequency ....................................124
Frequency Spacing ..........................................................127
4.3 NAV Operation .................................................128
NAV Tuning Boxes ...........................................................128
NAV Radio Selection and Activation................................129
NAV Receiver Manual Tuning ..........................................129
Auto-Tuning a NAV Frequency from the MFD .................130
Marker Beacon Receiver .................................................132
ADF/DME Tuning .............................................................133
4.4 Mode S Transponders .......................................136
Transponder Controls ......................................................136
Transponder Mode Selection ........................................... 137
GTX 3000 TCAS II Transponder Controls (optional) .........139
GTX 3000 TCAS II Transponder Mode Selection (opt) ......140
Entering a Transponder Code ..........................................142
IDENT Function ...............................................................144
4.5 Additional Audio Panel Functions ....................145
Power Application ...........................................................145
Mono/Stereo Headsets .................................................... 145
Speaker ...........................................................................145
Passenger Address System ..............................................145
Intercom System (GMA 1360D) ......................................147
Simultaneous COM Operation ........................................148
3D Audio (GMA 1360D) ..................................................149
Clearance Recorder and Player .......................................150
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Axiv
TABLE OF CONTENTS
Entertainment Inputs (GMA 1347D) ...............................151
Entertainment Inputs (GMA 1360D) ...............................152
Blue Select Mode (GMA 1360D) .....................................152
Bluetooth
®
Setup (GMA 1360D) .....................................153
4.6 Audio Panels Preflight Procedure ....................155
4.7 Abnormal Operation ........................................156
Stuck Microphone ...........................................................156
COM Tuning Failure ......................................................... 156
PFD Failure, Dual System ................................................. 156
Audio Panel Fail-Safe Operation ......................................156
Reversionary Mode .........................................................156
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction .....................................................157
Navigation Status Box and Data Bar ............................... 159
5.2 Using Map Displays ..........................................161
Map Orientation .............................................................161
Map Range .....................................................................163
Map Panning ...................................................................165
Measuring Bearing and Distance ....................................167
Topography .....................................................................168
Map Symbols ..................................................................171
Airways ...........................................................................175
Additional Navigation Map Items ...................................177
5.3 Waypoints ........................................................180
Airports ...........................................................................181
Non-Airport Waypoints ...................................................187
5.4 Airspaces .......................................................... 197
Nearest Airspace .............................................................198
Smart Airspace ................................................................201
5.5 Direct-to-Navigation ........................................202
5.6 Flight Planning .................................................206
Introduction ....................................................................206
Flight Plan Views .............................................................209
Creating a Flight Plan .....................................................213
Flight Plan Waypoint and Airway Modifications .............. 214
Flight Plan Operations ....................................................223
Closest Point of FPL.........................................................225
User-Defined Holding Patterns ........................................228
Managing Flight Plans ....................................................231
5.7 Vertical Navigation ..........................................241
Constraints ......................................................................242
Vertical Situation Display (VSD) ......................................246
Vertical Navigation Direct To ........................................... 250
5.8 Procedures .......................................................251
Departures ......................................................................252
Arrivals ...........................................................................255
Approaches ....................................................................259
5.9 Trip Planning ....................................................271
Trip Planning ...................................................................271
Weight Planning .............................................................275
5.10 Abnormal Operation ........................................278
Dead Reckoning Navigation ............................................278
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather............................................282
Activating Data Link Weather Services ............................ 283
Weather Product Age ......................................................286
Displaying Data Link Weather Products ..........................291
Customizing the Weather Data Link Page .......................296
Connext Data Requests ...................................................301
Weather Product Overview .............................................304
Datalink Weather Product Overlays .................................318
FIS-B Weather Status .......................................................341
Abnormal Operations for Garmin Connext Weather .......343
6.2 Stormscope Lightning Detection System ......... 345
Using the Stormscope Page .............................................346
Additional Stormscope Displays ...................................... 347
Stormscope Abnormal Operations ...................................348
6.3 Airborne Color Weather Radar .........................349
System Description ..........................................................349
Principles of Airborne Weather Radar..............................350
NEXRAD and Airborne Weather Radar ...........................350
Antenna Beam Illumination ............................................351
Safe Operating Distance .................................................356
Basic Antenna Tilt and Range Setup ............................... 356
Weather Mapping and Interpretation .............................360
Ground Mapping and Interpretation ............................... 375
Additional Weather Radar Displays ................................. 376
System Status..................................................................380
6.4 TAWS-B .............................................................382
Relative Terrain Symbology .............................................383
TAWS-B Alerts .................................................................387
System Status..................................................................394
6.5 Vertical Situation Display (VSD) Terrain ........... 396
VSD Display .....................................................................396
6.6 TAWS-A .............................................................400
Relative Terrain Symbology .............................................401
Displaying TAWS-A Data .................................................402
190-02041-02 Rev. A Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series xv
TABLE OF CONTENTS
TAWS-A Page ..................................................................405
TAWS-A Alerts .................................................................406
System Status..................................................................420
TAWS-A Abnormal operations .........................................421
6.7 TAS/TCAS I Traffic .............................................423
TAS Theory of Operation .................................................424
Traffic Alerts ....................................................................428
System Test .....................................................................430
Operation ........................................................................ 431
6.8 ADS-B Traffic ....................................................439
ADS-B System Overview .................................................439
ADS-B with TAS/TCAS I ...................................................441
Conflict Situational Awareness & Alerting .......................441
Airborne and Surface Applications ..................................444
Traffic Description ...........................................................445
Operation ........................................................................ 446
ADS-B System Status.......................................................452
6.9 TCAS II Traffic ...................................................455
Theory of Operation ........................................................455
TCAS II Alerts ..................................................................458
System Test .....................................................................463
Operation ........................................................................ 464
System Status..................................................................470
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 Overview .......................................................... 473
Basic Autopilot Operation ...............................................473
7.2 AFCS Controls ..................................................475
AFCS Controller ...............................................................475
Additional AFCS Controls ................................................ 476
7.3 Flight Director Operation ................................. 477
Activating the Flight Director ..........................................477
AFCS Status Box..............................................................478
Flight Director Modes......................................................478
Flight Director Selection .................................................. 479
Command Bars ...............................................................479
7.4 AFCS Modes .....................................................481
Vertical Modes ................................................................481
Lateral Modes .................................................................487
Combination Modes ........................................................492
7.5 Autopilot and Yaw Damper Operation .............504
Flight Control ..................................................................504
Engaging the Autopilot and Yaw Damper .......................504
Control Wheel Steering (CWS) ........................................505
Disengaging the Autopilot and Yaw Damper ...................505
7.6 AFCS Annunciations and Alerts ........................ 507
AFCS Status Alerts...........................................................507
AFCS Voice Alerts ............................................................507
Overspeed Protection ...................................................... 508
Underspeed Protection ....................................................508
7.7 Abnormal Operation ........................................510
Suspected Autopilot Malfunction .................................... 510
Overpowering Autopilot Servos ......................................510
SECTION 8 ADDITIONAL FEATURES
8.1 Overview .......................................................... 511
8.2 SafeTaxi ............................................................ 512
8.3 Electronic Charts ..............................................515
ChartView (Optional) ......................................................516
FliteCharts .......................................................................523
IFR/VFR Charts ................................................................529
8.4 Database Cycle Number and Revisions ............533
Cycle Number and Revision ............................................533
8.5 Satellite Telephone/Datalink Services (Opt) ....536
Registering the System with Garmin Connext .................536
Disabling/Enabling the Iridium Transceiver ......................537
Contacts ..........................................................................538
Telephone Communication..............................................540
Text Messaging (SMS) ..................................................... 547
8.6 WiFi Connections (Optional) ............................559
8.7 SiriusXM Satellite Radio (Optional) .................562
Activating SiriusXM Satellite Radio Services ...................562
Using SiriusXM Radio ......................................................563
8.8 SurfaceWatch ...................................................567
Information Box ..............................................................567
Alerts ..............................................................................568
SurfaceWatch Setup ........................................................ 571
8.9 Flight Data Logging .........................................573
8.10 Connext Setup (Optional) ................................575
8.11 Auxiliary Video (Optional) ................................ 577
Video Setup .....................................................................577
Display Selection ............................................................. 578
Zoom/Range....................................................................579
8.12 Electronic Stability & Protection (ESP) (Opt) ...581
Roll Engagement .............................................................582
Pitch Engagement ........................................................... 583
Angle of Attack Protection ..............................................584
High Airspeed Protection ................................................585
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
190-02041-02 Rev. Axvi
TABLE OF CONTENTS
8.13 Abnormal Operation ........................................586
Iridium and WiFi Receiver Troubleshooting ......................586
APPENDICES
Annunciations and Alerts .........................................589
Aircraft Alerts .................................................................. 590
System Message Annunciations ......................................592
System Messages ............................................................ 593
Database Management ............................................607
Loading Updated Databases ...........................................607
Database Deletion Feature ............................................ 619
Magnetic Field Variation Database Update .....................620
Aviation Terms and Acronyms...................................623
Frequently Asked Questions .....................................635
Miscellaneous
Map Symbols ....................................639
INDEX
Index ......................................................................... I-1
190-02041-02 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the integrated avionics system as installed in the Beechcraft 200/A200/
B200 Series. The system presents flight instrumentation, position, navigation, communication, and identification
information to the pilot through large-format displays.
LINE REPLACEABLE UNITS
The system consists of the following Line Replaceable Units (LRUs):
- GDU 1050A (2) – Each unit is configured as a PFD that features a 10-inch high resolution LED backlit
display. The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/
copilot side is designated as PFD2. These units communicate with each other, the MFD, and with the on-side
GIA Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.
- GDU 1550 (1) – Features a 15-inch, high resolution LED backlit display configured as an MFD. This unit is
linked to both PFDs via HSDB connection.
- GIA 64E (2) or GIA 63W (2) (Alternate) – Integrated Avionics Units (IAUs) function as the main
communication hub, linking all LRUs with the on-side PFD and MFD. Each GIA contains a GPS SBAS
receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. Each
GIA is paired with the on-side PFD via HSDB connection. The GIAs are not paired together and do not
communicate with each other directly.
- GSU 75B (2) (Alternate to GDC and GRS) – Processes data from the pitot/static system as well as the OAT
probe to provide pressure altitude, airspeed, vertical speed and OAT information to the system. This unit
also provides aircraft attitude and heading information via ARINC 429 to the onside PFD and both GIA units.
The GSU contains advanced sensors (including accelerometers and rate sensors) and interfaces with the GMU
44 to obtain magnetic field information, and with the GIA to obtain GPS information. ADAHRS modes of
operation are discussed later in this document.
- GEA 71B
(2) or
GEA 71 (2) (Alternate) – Receives and processes signals from the engine and airframe
sensors. This unit communicates with both GIAs using an RS-485 digital interface.
- GDC 7400 (2) or GDC 74B (Alternate to GSU) – Processes data from the pitot/static system as well as the
OAT probe. This unit provides pressure altitude, airspeed, vertical speed and OAT information to the system
and communicates with the on-side GIA, PFD, GRS, and GTP. The #1 GDC communicates with the MFD. It
is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace.
- GRS 7800 (2) or GRS 77 (2) (Alternate to GSU) – Provides aircraft attitude and heading information to the
on-side PFD, GIA, and GMU. The GRS contains advanced sensors (including accelerometers and rate sensors)
and interfaces with the on-side GMU to obtain magnetic field information, the GDC to obtain air data, and
both GIAs to obtain GPS information. AHRS modes of operation are discussed later in this document.
- GMU 44 (2) – Measures and sends local magnetic field data to the GRS for processing to determine aircraft
magnetic heading. This unit receives power directly from the GRS and communicates with the GRS using an
RS-485 digital interface.
- GMA 1360D (2) or GMA 1347D (2) (Alternate) – Integrates NAV/COM digital audio, intercom system and
marker beacon controls, and is installed in dual configuration on the outboard side of PFD1 and PFD2. This
unit also enables the manual control of the display reversionary mode (red DISPLAY BACKUP Button) and
communicates with the on-side GIA.
190-02041-02 Rev. AGarmin G1000 NXi Pilot’s Guide for the Beechcraft 200/A200/B200 Series2
SYSTEM OVERVIEW
- GTX 335R / 345R / 3000 / 33 / 33D
(2)
(Optional) – Solid-state transponders that provide Modes A, C,
S and ADS-B “Out” capability for the 33. 33D, 335R and 3000, and “In/Out” capability for the 345R. The
GTX 33D transponder features diversity. Both transponders can be controlled from either PFD, and only one
transponder can be active at a time. Each transponder communicates with the on-side GIA through an RS-
232 digital interface. If a GTX 345R is installed, the second transponder will not be another GTX 345R. If
the GTX 3000 is installed, both transponders will be the GTX 3000 model.
- Flight Stream 510
(1)
(Optional) – Bluetooth® transceiver that provides wireless connectivity between a
compatible tablet/mobile device and the avionics system.
- GDL 69A SXM (1) (Optional) – A satellite radio receiver that provides datalink weather information to the
MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A SXM
communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM
Satellite Radio services are required to enable the GDL 69A SXM capability.
- GDL 59 (1) (Optional) – GDL 59 datalink operations are performed through the GDL 69A via an HSDB
connection. If the GDL 69A is not installed, operations go through the MFD. Connectivity with the GSR 56
for the Iridium telephone feature is through the RS-232 bus.
- GSR 56 (1) (Optional) – The Iridium Transceiver operation for voice communication is by means of a
telephone handset in the cabin and pilot and copilot headsets in the cockpit. The transceiver can also send
and receive data provided by the GDL 59 through the RS-232 bus, and provide Garmin Connext Weather
and SMS functions.
- GWX 75 / 68 / 70 (1) – Provides airborne weather and ground mapped radar data to the MFD, through the
XM datalink, via HSDB connection. If the GDL 69A is not installed, operations go through the MFD.
- GCU 477 (1) – Provides the Flight Management System (FMS) controls for the PFD1 and MFD through an
RS-232 digital interface.
- GMC 710 (1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing
communication with both PFDs.
- GTP 59 (2) – Provides Outside Air Temperature (OAT) data to the on-side GSU or GDC.
- GTS 825 / 855 / 8000 (1) (Optional) – The GTS 825 Traffic Advisory System (TAS), GTS 855 Traffic Alert
and Collision Avoidance System I (TCAS I) and GTS 8000 (TCAS II) use active interrogations of Mode S and
Mode C transponders to provide traffic information to the pilot independent of the ATC system.
- GRA 5500 (1) (Optional) – Provides altitude above the ground (AGL) to the G1000 system, through the GIA.
- GSA 80 (4) and GSM 85A / GSM 86 (4) – The GSA 80 servos are used for the automatic control of roll, pitch,
and yaw, and pitch trim. These units interface with each GIA. The GSM servo gearboxes are responsible for
transferring the output torque of the servo actuator to the mechanical flight-control surface linkage.
NOTE: For information on non-Garmin equipment, consult the applicable optional interface user’s guide.
This document assumes the reader is already familiar with the operation of this additional equipment.
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Garmin G1000 NXi - Beechcraft King Air 200/A200/B200 Reference guide

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