Garmin G1000 NXi: Beechcraft King Air 200/B200 Reference guide

Type
Reference guide

This manual is also suitable for

Beechcraft 200/B200 Series
Pilot’s Guide
®
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
Copyright © 2005-2018 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2286.06 or later for the G1000 NXi Beechcraft 200/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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Garmin Corporation
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Contact Garmin Product Support at www.flygarmin.com.
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
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a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
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and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
,
G1000
®
NXi, WATCH
®
, Flitecharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries.
Garmin ESP
, Garmin SVT
, SurfaceWatch
, and Connext
are trademarks of Garmin International, Inc. or its subsidiaries. These
trademarks may not be used without the express permission of Garmin.
Skywatch
®
and Stormscope
®
are registered trademarks of L-3 Communications. AC-U-KWIK
®
is a registered trademark of Penton Business
Media Inc. Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc. NavData
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is a registered trademark
of Jeppesen. Inc. Wi-Fi
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is a registered trademark of the Wi-Fi Alliance. SiriusXM Weather and SiriusXM Satellite Radio are provided by
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Garmin is under license.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-01 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 licensee.
Printed in the U.S.A.
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/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.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-01 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
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.
WARNING: Do not rely on information from the reactive wind shear detection system display as the sole
basis for detecting wind shear conditions. The system cannot predict the conditions in which wind shear is
likely to develop.
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/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.
C
AUTION: 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.
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
: Steep approaches are not supported by Landing Data calculations.
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.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-01 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
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.
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 FlyGarmin.com and select Aviation Data Error Report’.
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
vii
WARNINGS, CAUTIONS, AND NOTES
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 89º North latitude and south of 89º 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 using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
that can cause isolated discharge points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after
the screen has been cleared.
NOTE: 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: 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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-01 Rev. Aviii
WARNINGS, CAUTIONS, AND NOTES
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190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/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/B200 Series
190-02041-01 Rev. Ax
SOFTWARE LICENSE AGREEMENT
Blank Page
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
xi
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02041-01 A 7/20/18 i – I-6 Initial Release for GDU 20.82
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-01 Rev. Axii
REVISION INFORMATION
Blank Page
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/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
PFD/MFD Controller ...................................................... 6
Secure Digital Cards ...................................................... 8
1.3 System Operation .................................................... 9
System Power-up .......................................................... 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 ....................................................................... 28
MFD Page Groups ....................................................... 29
Split Screen Functionality ............................................ 32
System Settings .......................................................... 33
System Utilities ........................................................... 44
1.5 Display Backlighting ............................................. 48
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 52
Airspeed Indicator ...................................................... 52
Attitude Indicator ....................................................... 55
Altimeter ................................................................... 56
Vertical Speed Indicator (VSI) ....................................... 62
Vertical Deviation ....................................................... 62
Horizontal Situation Indicator (HSI) .............................. 65
Directional Gyro (DG) Mode (GRS 7800 Installations Only) .
68
Course Deviation Indicator (CDI) .................................. 71
2.2 Garmin SVT (Synthetic Vision Technology) ......... 78
SVT Operation ............................................................ 79
SVT Features .............................................................. 81
Field of View .............................................................. 89
2.3 Supplemental Flight Data .................................... 91
Temperature Displays .................................................. 91
Wind Data ................................................................. 92
Vertical Navigation (VNV) Indications ........................... 93
2.4 PFD Annunciations and Alerting Functions ........ 94
Marker Beacon Annunciations...................................... 94
Altitude Alerting ......................................................... 94
Low Altitude Annunciation .......................................... 95
Minimum Descent Altitude/Decision Height Alerting ...... 95
Radar Altimeter .......................................................... 97
2.5 Abnormal Operations ........................................... 99
Abnormal GPS Conditions ........................................... 99
Comparator Annunciations ........................................ 100
Reversionary Sensor Annunciations ............................ 101
Unusual Attitudes ..................................................... 102
SVT Unusual Attitudes ............................................... 103
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display ............................................................ 106
3.2 EIS Display in Reversionary Mode ..................... 109
Reversionary Display ................................................. 110
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 111
Audio Panel Volume Control ...................................... 111
PFD Controls and Frequency Display ........................... 112
Audio Panel Controls ................................................ 114
PFD/MFD Controller .................................................. 116
4.2 COM Operation .................................................... 119
COM Tuning Boxes .................................................... 119
COM Transceiver Manual Tuning ................................ 120
Quick-TuningandActivating121.500MHz .................. 120
Auto-Tuning the COM Frequency ................................ 121
Frequency Spacing .................................................... 123
4.3 NAV Operation ..................................................... 125
NAV Tuning Boxes..................................................... 125
NAV Radio Selection and Activation ........................... 126
NAV Receiver Manual Tuning ..................................... 126
Auto-Tuning a NAV Frequency from the MFD............... 127
Marker Beacon Receiver ............................................ 130
DME Tuning ............................................................. 130
4.4 Mode S Transponders .......................................... 132
GTX 335/345/3000 Transponder Controls .................... 132
GTX 335/345/3000 Transponder Mode Selection .......... 133
TCAS II Transponder Controls (optional) ...................... 135
TCAS II Transponder Mode Selection (optional) ............ 136
Entering a Transponder Code ..................................... 138
IDENT Function ........................................................ 139
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
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TABLE OF CONTENTS
4.5 Additional Audio Panel Functions ..................... 140
Power-Up ................................................................. 140
Mono/Stereo Headsets .............................................. 140
Speaker ................................................................... 140
Unmuted Inputs ....................................................... 140
Intercom System (ICS) ............................................... 140
Passenger Address (PA) System .................................. 142
Simultaneous COM Operation .................................... 142
Clearance Recorder and Player ................................... 143
3D Audio ................................................................. 143
Telephone/Entertainment Inputs ................................. 145
Bluetooth
®
Setup ...................................................... 147
4.6 Audio Panels Preflight Procedure ...................... 148
4.7 Abnormal Operation ........................................... 149
Stuck Microphone ..................................................... 149
COM Tuning Failure ................................................... 149
PFD Failure, Dual System ...........................................149
Audio Panel Fail-Safe Operation ................................. 149
Reversionary Mode ................................................... 149
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 151
Navigation Status Box AND Data Bar .......................... 153
5.2 Using Map Displays ............................................. 155
Map Orientation ....................................................... 155
Map Range .............................................................. 157
Map Panning ............................................................ 159
Measuring Bearing and Distance ................................ 162
Topography .............................................................. 163
Map Symbols ........................................................... 166
Airways ................................................................... 170
Additional Navigation Map Items ............................... 173
5.3 Waypoints ............................................................. 176
Airports ................................................................... 177
Non-Airport Waypoints .............................................. 184
5.4 Airspaces .............................................................. 193
Nearest Airspace ...................................................... 194
Smart Airspace ......................................................... 196
5.5 Direct-to-Navigation .......................................... 197
5.6 Flight Planning ..................................................... 202
Introduction ............................................................. 202
Flight Plan Views ...................................................... 205
Creating a Flight Plan ............................................... 208
Flight Plan Waypoint and Airway Modifications ........... 209
Flight Plan Operations ............................................... 218
Closest Point of FPL .................................................. 223
User-Defined Holding Patterns ................................... 224
Managing Flight Plans .............................................. 227
5.7 Vertical Navigation ............................................. 236
Altitude Constraints .................................................. 238
Vertical Situation Display (VSD) .................................. 240
5.8 Procedures ...........................................................244
Departures ............................................................... 245
Arrivals ................................................................... 249
Approaches ............................................................. 252
5.9 Trip Planning ........................................................ 263
Trip Planning ............................................................ 263
Weight Planning ....................................................... 267
5.10 Abnormal Operation ........................................... 270
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ............................................... 274
Activating Data Link Weather Services ........................ 275
Weather Product Age ................................................ 278
Displaying Data Link Weather Products ....................... 283
Connext Data Requests ............................................. 293
Weather Product Overview ........................................ 296
FIS-B Weather Status................................................. 332
Abnormal Operations for Garmin Connext Weather ..... 334
6.2 Stormscope Lightning Detection System ......... 336
Using the Stormscope Page ....................................... 337
Additional Stormscope Displays ................................. 338
Stormscope Abnormal Operations .............................. 339
6.3 Airborne Color Weather Radar .......................... 340
System Description ................................................... 340
Safe Operating Distance ............................................ 345
Basic Antenna Tilt Setup ............................................ 346
Practical Application Using the Basic Tilt Setup ............ 347
Weather Mapping and Interpretation ......................... 349
Ground Mapping and Interpretation ........................... 362
Additional Weather Radar Displays ............................. 362
System Status ........................................................... 365
6.4 TAWS-B ................................................................. 367
Relative Terrain Symbology ........................................ 368
TAWS-B Alerts .......................................................... 372
System Status ........................................................... 379
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TABLE OF CONTENTS
6.5 Vertical Situation Display (VSD) Terrain ........... 380
VSD Display ............................................................. 380
6.6 TAWS-A ................................................................. 384
Relative Terrain Symbology ........................................ 385
TAWS-A Page ........................................................... 389
TAWS-A Alerts .......................................................... 390
System Status ........................................................... 403
TAWS-A Abnormal operations .................................... 403
6.7 TAS/TCAS I Traffic ................................................ 405
TAS Theory of Operation ............................................ 406
Traffic Alerts ............................................................. 410
System Test .............................................................. 411
Operation ................................................................ 412
6.8 ADS-B Traffic ........................................................ 420
ADS-B System Overview ............................................ 420
ADS-B with TAS/TCAS I .............................................. 422
Conflict Situational Awareness & Alerting ................... 422
Airborne and Surface Applications .............................. 425
Traffic Description ..................................................... 426
Operation ................................................................ 426
ADS-B System Status ................................................ 432
6.9 TCAS II Traffic ....................................................... 435
Theory of Operation .................................................. 435
TCAS II Alerts ........................................................... 436
System Test .............................................................. 441
Operation ................................................................ 442
System Status ........................................................... 448
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................... 451
Additional AFCS Controls .......................................... 453
Basic Autopilot Operation .......................................... 454
7.2 Flight Director Operation ................................... 455
Activating the Flight Director ..................................... 455
AFCS Status Box ....................................................... 456
Flight Director Modes ................................................ 457
Switching Flight Directors .......................................... 457
Command Bars ......................................................... 458
Underspeed Protection .............................................. 459
7.3 Vertical Modes ..................................................... 461
Pitch Hold Mode (PIT) ............................................... 462
Selected Altitude Capture Mode (ALTS) ....................... 463
Altitude Hold Mode (ALT) .......................................... 464
Vertical Speed Mode (VS) .......................................... 465
Flight Level Change Mode (FLC) ................................. 466
Vertical Navigation Modes (VPTH, ALTV) ..................... 468
Glidepath Mode (GP) ................................................ 473
Glideslope Mode (GS) ............................................... 474
Takeoff (TO) and Go Around (GA) Modes .................... 476
Level Mode (LVL) ...................................................... 477
7.4 Lateral Modes ...................................................... 478
Roll Hold Mode (ROL) ............................................... 479
Low Bank Mode ....................................................... 479
Heading Select Mode (HDG) ...................................... 480
Navigation Modes (GPS, VOR, LOC) ............................ 481
Approach Modes (GPS, VAPP, LOC) ............................. 483
Backcourse Mode (BC) .............................................. 484
Intercepting and Flying a DME Arc ............................. 486
Level Mode (LVL) ...................................................... 486
7.5 Autopilot and Yaw Damper Operation ............. 487
Flight Control ........................................................... 487
Engagement ............................................................. 488
Control Wheel Steering ............................................. 488
Disengagement ........................................................ 489
7.6 AFCS Annunciations and Alerts ......................... 490
AFCS Status Alerts .................................................... 490
Overspeed Protection ................................................ 491
7.7 Abnormal Operation ........................................... 492
Suspected Autopilot malfunction ................................ 492
Overpowering Autopilot Servos .................................. 492
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi ................................................................ 494
8.2 Charts .................................................................... 497
FliteCharts ............................................................... 498
Terminal Procedures Charts ....................................... 500
Chart Options ........................................................... 503
Day/Night View ........................................................ 504
ChartView ................................................................ 505
Airport Directory ....................................................... 513
IFR/VFR Charts ......................................................... 514
8.3 Database Cycle number and revisions .............. 517
Cycle Number and Revision ....................................... 517
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-01 Rev. Axvi
TABLE OF CONTENTS
8.4 Satellite Telephone .............................................. 519
Registering with Garmin Connext
®
............................ 519
Disable/Enable Iridium Transceiver.............................. 519
Telephone Communication ........................................ 520
Text Messaging (SMS) ............................................... 529
8.5 Wifi Connections ................................................. 541
8.6 SiriusXM Radio Entertainment .......................... 544
Activating SiriusXM Satellite Radio Services ................ 544
Using SiriusXM Radio ................................................ 545
8.7 Scheduler .............................................................. 549
8.8 SurfaceWatch ....................................................... 551
Information Box ....................................................... 551
Alerts ...................................................................... 552
Surfacewatch Setup .................................................. 555
8.9 Flight Data Logging ............................................ 557
8.10 Electronic Stability & Protection (ESP
) ........... 559
Roll Engagement ...................................................... 560
Pitch Engagement..................................................... 562
High Airspeed Protection ........................................... 562
8.11 Abnormal Operation ........................................... 563
SVT Troubleshooting ................................................. 563
Reversionary Mode ................................................... 563
Unusual Attitudes ..................................................... 563
GSR 56 & GDL 59/69/69A Troubleshooting .................. 564
APPENDICES
Annunciations and Alerts ............................................. 567
Aircraft Alerts ........................................................... 568
System Message Annunciations ................................. 570
System Messages ..................................................... 571
Database Management ................................................ 587
Loading Updated Databases ...................................... 587
Database Deletion Feature ....................................... 598
Magnetic Field Variation Database Update .................. 599
Aviation Terms and Acronyms ...................................... 601
Frequently Asked Questions ........................................ 611
Miscellaneous
Map Symbols ....................................... 615
INDEX
Index ................................................................................ I-1
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/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/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) – 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) – 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) (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) (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.
190-02041-01 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
2
SYSTEM OVERVIEW
•
GMA 1360D
(2) – 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.
•
GTX 335R / 345R / 3000 (2)
(Optional) – Solid-state transponders that provide Modes A, C, S and ADS-B “In”
capability for the 335R and 3000, and “In/Out” capability for the 345R. 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 (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 MFD, 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 that the reader is already familiar with the operation of this additional equipment.
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Garmin G1000 NXi: Beechcraft King Air 200/B200 Reference guide

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