Garmin G5000 NG - Beechcraft Model 400A (Beechjet) Reference guide

Type
Reference guide
Beechjet 400A &
Hawker 400XP (Model 400A)
G5000
®
Integrated Avionics System
Pilot’s Guide
190-02014-01 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
Copyright © 2016, 2018 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2091.03 or later for the Beechjet 400A & Hawker 400XP (Model 400A).
Some differences in operation may be observed when comparing the information in this manual to later software versions.
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Garmin Corporation
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Xizhi District, New Taipei City, Taiwan
Web Site Address: 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
®
, G5000
®
, WATCH
®
,
FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin Ltd. or its subsidiaries. Garmin SVT
and
Connext
®
are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the express permission
of Garmin.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
Skywatch
®
and Stormscope
®
are registered trademarks of L-3 Communications. AC-U-KWIK
®
is a registered trademark of Penton Business
Media Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
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.
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ii
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 a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
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WARNINGS, CAUTIONS, AND NOTES
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.
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 the accuracy of attitude and heading indications in the following geographic
areas (due to variations in the earth’s magnetic field): North of 72° North latitude at all longitudes; South
of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W
(Northern Canada); North of 70° North latitude between longitude 70° W and 128° W (Northern Canada);
North of 70° North latitude between longitude 85° E and 114° E (Northern Russia); South of 55° South
latitude between longitude 120° E and 165° E (Region south of Australia and New Zealand).
WARNING: Do not 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.
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WARNINGS, CAUTIONS, AND NOTES
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
: 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 use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
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.
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: 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.
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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 that have a Type 2 Letter of Authorization (LOA) from the FAA are assured
compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable
database and can be viewed at http://fly.garmin.com by selecting Aviation Database Declarations.
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.
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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 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 FliteCharts 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 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: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear as
a partial symbol.
NOTE: Operate G5000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
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Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
SOFTWARE LICENSE AGREEMENT
vii
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.
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SOFTWARE LICENSE AGREEMENT
viii
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REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02014-00 A 08/12/2016 All Production release at GDU 6.56
190-02014-01 A 07/24/2018 All Production release at GDU 20.82
Added HSI Map
Added IFR/VFR Charts
Added Transition to Approach
Added Visual Approach
Added support for Williams Engine
Removed Connext Info
Removed Satellite Telephone
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REVISION INFORMATION
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TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 System Controls....................................................... 4
PFD Controls ................................................................ 4
Touchscreen Controller ................................................ 12
PFD Controller ............................................................ 34
Secure Digital Cards .................................................... 35
1.3 System Operation .................................................. 36
System Power-up ........................................................ 36
Normal Operation ....................................................... 37
Reversionary Display Operation ................................... 38
AHRS Operation ......................................................... 40
GPS Receiver Operation .............................................. 42
Annunciations ............................................................ 46
1.4 FMS Initialization .................................................. 48
1.5 System Management ............................................ 50
Avionics Settings ........................................................ 50
Avionics Status ........................................................... 57
Additional Setup Features ............................................ 58
1.6 Utilities ................................................................... 59
Trip Stats ................................................................... 59
Timer ......................................................................... 60
Scheduled Messages ................................................... 61
Screen Cleaning .......................................................... 63
Crew Profiles .............................................................. 63
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 70
Attitude Indicator ....................................................... 70
Airspeed Indicator ...................................................... 72
Altimeter ................................................................... 75
Altimeter Setting ........................................................ 75
Selected Altitude ........................................................ 77
Altitude Display Units ................................................. 77
Barometric Transition Altitude Alert .............................. 78
Vertical Speed Indicator (VSI) ....................................... 78
Vertical Deviation ....................................................... 79
Horizontal Situation Indicator (HSI) .............................. 81
Turn Rate Indicator ..................................................... 84
Bearing Pointers and Information Windows ................... 84
Course Deviation Indicator (CDI) .................................. 86
FMS CDI Scaling ......................................................... 88
OBS Mode ................................................................. 91
2.2 Garmin SVT (Synthetic Vision Technology) ......... 93
SVT Operation ............................................................ 94
SVT Features .............................................................. 95
Flight Path Marker ...................................................... 96
Zero Pitch Line ........................................................... 96
Horizon Heading ......................................................... 96
Traffic ........................................................................ 97
Airport Signs .............................................................. 97
Runways .................................................................... 98
Terrain Alerting ........................................................... 99
Field of View ............................................................100
2.3 Supplemental Flight Data .................................. 101
Temperature Displays ................................................ 101
Wind Data ............................................................... 102
Vertical Navigation (VNAV) Indications ....................... 102
2.4 PFD Annunciations and Alerting Functions ...... 104
Marker Beacon Annunciations.................................... 104
Altitude Alerting ....................................................... 104
Low Altitude Annunciation ........................................ 105
Minimum Descent Altitude/Decision Height Alerting .... 106
Radar Altimeter ........................................................ 108
2.5 Abnormal Operations ......................................... 109
Abnormal GPS Conditions ......................................... 109
Comparator Annunciations ........................................ 110
Reversionary Annunciations ....................................... 111
Unusual Attitudes ..................................................... 112
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
3.1 Engine Indication System (EIS) .......................... 116
Engine Indications .................................................... 118
3.2 Aircraft Systems ..................................................124
Engine Vibration (Pratt and Whitney Engine only) ........ 124
Fuel Used Reset ........................................................ 124
System Tests ............................................................. 124
3.3 Reversionary Mode ............................................. 126
SECTION 4 AUDIO AND CNS
4.1 Overview .............................................................. 127
Touchscreen Controller Audio and CNS Controls .......... 128
PFD COM/NAV display and Controls ........................... 130
4.2 COM Operation .................................................... 132
COM Transceiver Selection and Activation ................... 132
COM Frequency Tuning .............................................. 134
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TABLE OF CONTENTS
Frequency Spacing .................................................... 140
Automatic Squelch .................................................... 142
Volume .................................................................... 143
4.3 NAV Operation ..................................................... 144
NAV Radio Selection and Activation ........................... 144
NAV Receiver Tuning ................................................. 145
Marker Beacon Receiver ............................................ 154
ADF/DME Tuning ...................................................... 155
4.4 Mode S Transponder ........................................... 161
Transponder Controls ................................................ 161
Transponder Mode Selection ...................................... 161
Entering a Transponder Code ..................................... 164
IDENT Function ........................................................ 166
Flight ID Reporting.................................................... 167
4.5 Additional Audio Functions ................................ 168
Mono/Stereo Headsets .............................................. 168
Speaker ................................................................... 168
Intercom .................................................................. 169
Passenger Address (PA) System .................................. 171
Clearance Recorder and Player ................................... 172
Simultaneous COM Operation .................................... 173
Entertainment .......................................................... 173
Audio Feedback (Clicks) ............................................ 175
4.6 Abnormal Operation ........................................... 177
Stuck Microphone ..................................................... 177
COM Tuning Failure ................................................... 177
Audio Controller Fail-Safe Operation .......................... 177
Touchscreen Controller Failure ................................... 177
Amber COM Frequency Digits .................................... 177
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 187
Navigation Status Bar ............................................... 189
5.2 Using Map Displays ............................................. 191
Map Settings Synchronization .................................... 191
Map Orientation ....................................................... 192
Map Range .............................................................. 194
Map Panning ............................................................ 196
Measuring Bearing and Distance ................................ 200
Absolute Terrain ....................................................... 202
Map Symbols ........................................................... 205
Airways ................................................................... 212
Additional Navigation Map Items ............................... 214
5.3 Waypoints ............................................................. 218
Airports ................................................................... 219
Non-Airport Waypoints .............................................. 225
5.4 Airspaces .............................................................. 234
Nearest Airspace ...................................................... 235
Smart Airspace ......................................................... 238
5.5 Direct-to-Navigation .......................................... 239
5.6 Flight Planning ..................................................... 246
Introduction ............................................................. 246
Creating a Flight Plan ............................................... 250
Flight Plan Waypoint and Airway Modifications ........... 252
Flight Plan Operations ............................................... 262
Managing Flight Plans .............................................. 277
5.7 Vertical Navigation ............................................. 285
Climb/Cruise/Descent ............................................... 287
Constraints .............................................................. 291
Vertical Situation Display ........................................... 300
Vertical Navigation Direct To ...................................... 305
5.8 Procedures ...........................................................306
Departures ............................................................... 309
Arrival ..................................................................... 312
Approaches ............................................................. 315
5.9 Trip Planning ........................................................ 329
Trip Statistics ............................................................ 330
Fuel Statistics ........................................................... 331
Other Statistics ......................................................... 331
5.10 Weight and Fuel Planning .................................. 334
Weight Caution And Warning Conditions .................... 337
5.11 Takeoff and Landing Data .................................. 338
Takeoff Data ............................................................. 338
Landing Data ........................................................... 339
5.12 Abnormal Operation ........................................... 341
FMS Degradation ...................................................... 341
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ............................................... 346
Activating Data Link Weather Services ........................ 346
Weather Product Age ................................................ 348
Displaying Data Link Weather Products ....................... 350
Weather Product Overview ........................................ 357
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6.2 Airborne Color Weather Radar .......................... 386
System Description ................................................... 386
Principles of Airborne Weather Radar .......................... 386
Safe Operating Distance ............................................ 391
Basic Antenna Tilt Setup ............................................ 391
Weather Display And Interpretation ............................ 393
Weather Radar Operation .......................................... 397
System Status ........................................................... 412
6.3 Stormscope Lightning ......................................... 414
Using the Stormscope Pane ....................................... 415
Stormscope Information on Navigation Maps .............. 416
Abnormal Operations ................................................ 419
6.4 TAWS-B ................................................................. 420
Relative Terrain Symbology ........................................ 421
Displaying Relative Terrain Information ....................... 423
System Status ........................................................... 432
TAWS-B Abnormal Operations ................................... 433
6.5 TAWS-A ................................................................. 434
Relative Terrain Symbology ........................................ 435
TAWS Pane .............................................................. 437
Forward Looking Terrain Avoidance (FLTA) ................... 441
Premature Descent Alerting ....................................... 442
Inhibiting FLTA and PDA Alerts ................................... 442
Inhibiting GPWS Alerts (EDR, ECR, FIT, and NCR) .......... 450
Excessive below Glideslope/Glidepath Deviation Alert .. 451
Inhibiting GSD Alerts ................................................. 452
Altitude Voice Callout (VCO) ...................................... 453
System Status ........................................................... 453
TAWS-A Abnormal Operations ................................... 453
6.6 TCAS II Traffic ....................................................... 455
TCAS II Alerts ........................................................... 456
Resolution advisories ................................................ 457
Displaying TCAS II Traffic ........................................... 459
Additional Traffic Displays ......................................... 460
Operation ................................................................ 462
System Status ........................................................... 466
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 468
Basic Autopilot Operation .......................................... 470
7.2 Flight Director Operation ................................... 471
Activating the Flight Director ..................................... 471
AFCS Status Box ....................................................... 472
Command Bars ......................................................... 472
Flight Director Modes ................................................ 474
Flight Director Selection ............................................ 474
7.3 AFCS Modes ......................................................... 475
Vertical Modes (PIT, ALT, VS, FLC) ................................ 475
Lateral Modes (ROL, BANK, HDG, NAV) ....................... 483
Combination Modes (VNAV, APPR, NAV, BC, TO, GA) .... 488
7.4 Autopilot Operation ............................................ 502
Engaging the Autopilot ............................................. 502
Control Wheel Steering ............................................. 503
Disengaging the Autopilot ......................................... 503
7.5 AFCS Annunciations and Alerts ......................... 504
Underspeed Protection (optional) ............................... 504
Overspeed Protection ................................................ 505
AFCS CAS Messages ................................................. 506
7.6 Abnormal Operation ........................................... 507
Overpowering Autopilot Servos .................................. 507
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi ................................................................ 510
8.2 Charts .................................................................... 512
ChartView (Optional) ................................................ 512
FliteCharts ............................................................... 519
IFR/VFR Charts ........................................................ 525
8.3 Airport Directory ................................................. 528
8.4 Database Cycle Number and Revisions ............ 529
Cycle Number and Revision ....................................... 529
8.5 SurfaceWatch ....................................................... 531
Information Display .................................................. 532
Alerts ...................................................................... 533
8.6 SiriusXM Satellite Radio ..................................... 534
Activating SiriusXM Satellite Services ......................... 534
Using SiriusXM Radio ................................................ 535
8.7 Electronic Documents ......................................... 539
Installed Documents ................................................. 539
User Documents ....................................................... 539
Viewing Electronic Documents ................................... 540
8.8 Electronic Checklists ........................................... 546
8.9 Flight Data Logging ............................................ 549
8.10 Abnormal Operation ........................................... 551
GDL 69A SXM Data Link Receiver Troubleshooting ....... 551
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TABLE OF CONTENTS
APPENDICES
Annunciations and Alerts ............................................. 553
CAS Messages .......................................................... 553
System Annunciations ............................................... 555
System Message Advisories ....................................... 557
G5000 Aural Alerts ................................................... 571
Database Management ................................................ 573
Loading Updated Databases ...................................... 574
Database Updates Using a Supplemental Data Card .... 575
Database Synchronization feature .............................. 578
Database Deletion feature ......................................... 579
Magnetic Field Variation Database Update .................. 580
Aviation Terms and Acronyms ...................................... 583
Frequently Asked Questions ........................................ 593
Map Symbols ................................................................. 597
INDEX
Index ................................................................................ I-1
190-02014-01 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G5000
®
Integrated Avionics System as installed in the Beechjet 400A
& Hawker 400XP (Model 400A) aircraft. The G5000 is an integrated flight control system that presents flight
instrumentation, position, navigation, communication, and identification information to the flight crew using
flat-panel color displays and Touchscreen Controllers. The system consists of the following Line Replaceable
Units (LRUs):
GDU 1250W (3) – Each GDU (display unit) features a 12-inch light emitting diode (LED) backlit widescreen
display with a 1280 x 800 resolution. The unit installed on the left/pilot side is designated as PFD1. In normal
operations, it shows a Primary Flight Display (PFD), and may also show a Display Pane. The center unit is
designated as the MFD. In normal operations it shows the Engine Indication and Crew Alerting System (EICAS)
display, in addition to one or two Display Panes. The unit installed on the right/copilot side is designated as
PFD2. Both PFDs may be displayed in full screen format, or in a 60/40 split format. The GDUs communicate
with each other, the Touchscreen Controllers, and with the on-side GIA Integrated Avionics Unit (IAU).
GTC 575 (2)
– The GTC Touchscreen Controller provides GDU Display Pane control, in addition to Flight
Management System (FMS) functions, data entry capability, and communications control to the system. The
unit installed on the left/pilot side is designated as GTC1, and the unit installed on the right/copilot side is
designated as GTC2. Each touchscreen controller communicates with its respective on-side PFD, as well as the
MFD.
GCU 275 (2)
– The GCU PFD Controller is a panel-mounted user interface which enables the flight crew to
control both PFDs. Each unit is connected to the on-side PFD, and to the MFD.
GMA 36B (2)
– The GMA Audio Controller integrates navigation/communication radio (NAV/COM) digital
audio, intercom, and marker beacon audio. The units are connected to their respective Touchscreen Controllers.
GIA 64E
(2) – The GIA Integrated Avionics Units (IAU) function as the main communications hubs, linking
several LRUs with each on-side PFD/MFD. Each IAU contains a GPS Satellite-Based Augmentation System
(SBAS) receiver, a very high frequency (VHF) communication/navigation/glideslope (COM/NAV/GS) receiver, a
Flight Director (FD) and system integration microprocessors.
GDC 7400
(2) – The GDC Air Data Computer (ADC) processes data from the pitot/static system as well as the
Outside Air Temperature (OAT) probe. This unit provides pressure altitude, airspeed, vertical speed and OAT
information to the system, and it communicates with both IAUs, the on-side PFD/MFD and the on-side AHRS.
The ADC is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace.
GEA 7100 (2)
– The GEA Engine Airframe Unit receives and processes signals from the engine and airframe
sensors, and it communicates with both IAUs.
GTX 3000
(2) – The GTX Transponder provides Modes A/C/S capability, 1090 MHz Extended Squitter Automatic
Dependent Surveillance - Broadcast (ADS-B) transmission, and communicates with both IAUs.
GRS 79
(2) – The GRS Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 protocol to the on-side and cross-side IAU, the on-side PFD, and to the MFD.
An RS-232 backup path connects each AHRS to each IAU. The AHRS contains advanced sensors (including
accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field information,
with the ADC to obtain air data, and with both IAUs to obtain GPS information.
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
190-02014-01 Rev. A
2
SYSTEM OVERVIEW
GMU 44
(2) – The GMU Magnetometer measures local magnetic field and sends data to the AHRS for processing
to determine aircraft magnetic heading. The magnetometer receives power directly from, and communicates
with the AHRS.
GDL 69A SXM
(1) – The SiriusXM Data Link Receiver receives weather information, as well as digital audio
entertainment. The unit communicates with the MFD. A subscription to SiriusXM Weather and/or SiriusXM
Satellite Radio service is required to enable the services.
GMC 7250
– The GMC AFCS Controller provides AFCS control, and connects the PFDs.
GSA 9000
(3) and
GTA 82 (1)
– The GSA Servos are used for automatic control of pitch, roll, and yaw via the
AFCS. The GTA Pitch Trim Adapter works with the existing motor to provide automatic pitch trim. These units
interface with each IAU.
GSM 9100 (3)
The GSM Servo Gearboxes are responsible for transferring the output torque of the servo
actuators to the mechanical flight-control surface linkages.
GWX 70
(1) – The GWX Airborne Weather Radar provides airborne real-time weather and ground mapped
radar data to each PFD/MFD. The unit is connected to the #2 GSD (Data Concentrator).
GSD 41
(2) – The GSD Data Concentrator is used to expand the input and output capabilities of the system.
High Speed Data Bus (HSDB) communications occur among Garmin LRUs. The ARINC 429 protocol connects
non-Garmin LRUs using the Data Concentrator.
The system is capable of interfacing with the following non-Garmin equipment:
MD302 - Standby Flight Indicator DME 442 - Single or Dual DME Radio (optional)
A100 CVR - Cockpit Voice Recorder TCAS-94/TCAS-4000 TCAS II - TCAS II (optional)
ALT-55B - Radar Altimeter (optional) WX-500/WX-1000E - Lightning Detection (optional)
ALT-1000 - Radar Altimeter (optional)
Cabin Entertainment/Airshow (optional)
ADF 462 - Single or Dual ADF Radio (optional)
NOTE: For information on non-Garmin equipment, consult the applicable user’s guide. This document
assumes that the reader is already familiar with the operation of this additional equipment
The Beechjet 400A & Hawker 400XP (Model 400A) aircraft is also equipped with a Garmin Automated Flight
Control System (AFCS), providing the Flight Director (FD), Autopilot (AP), manual electric trim, and control
wheel steering (CWS) functions of the G5000 Integrated Avionics System.
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.
A top-level G5000 system block diagram is shown in Figure 1-1.
190-02014-01 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
3
SYSTEM OVERVIEW
#1
GDU 1250W
(PFD1)
GDL 69A SXM
(SiriusXM
Weather Datalink)
#1 GMA 36B
(Audio
Processor)
#1 GSA 9000 (Pitch)
#2 GSA 9000 (Yaw)
#3 GSA 9000 (Roll)
#1 GIA 64E
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2 GIA 64E
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#3
GDU 1250W
(PFD2)
Non-Garmin Equipment
#1 GTX 3000
(Transponder)
#2
GDU 1250W
(MFD1)
#1 GCU 275
(GDU
Controller)
GTC 575
(Touchscreen
Controller)
GTC 575
(Touchscreen
Controller)
#2 GCU 275
(GDU
Controller)
#2 GEA 7100 (Engine
& Airframe I/F)
#1 GEA 7100 (Engine
& Airframe I/F)
#1 GSD 41
(Data
Concentrator)
#2 GSD 41
(Data
Concentrator)
#1 GDC 7400
(Air Data
Computer)
#2 GDC 7400
(Air Data
Computer)
#2 GMA 36B
(Audio
Processor)
Radios
CVR
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
#2 GTX 3000
(Transponder)
GMC 7250
(AFCS Mode
Controller)
Garmin Equipment
MD302
Standby
Indicator
Lightning
Detection
System
#1 GMU 44
(Magnetometer)
#1 GRS 79
(Attitude &
Heading)
#2 GRS 79
(Attitude &
Heading)
GTA 82 (Trim Adapter)
ELT
#1 ADF
ALT-55B
(Radar
Altimeter)
ALT-1000
(Radar
Altimeter)
#2 GMU 44
(Magnetometer)
TCAS-94/ TCAS
4000 (TCAS II)
#1 DME
#2 DME
GWX 70
(Weather
Radar)
#2 ADF
Cabin
Entertainment
System
OAT
Probe
Figure 1-1 Basic System Block Diagram
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
190-02014-01 Rev. A
4
SYSTEM OVERVIEW
1.2 SYSTEM CONTROLS
The system controls have been designed to simplify operation of the system and minimize workload and the
time required to access sophisticated functionality. Controls are located on each PFD bezel, the Touchscreen
Controllers, the PFD Controllers, and the AFCS Controller. PFD controls, Touchscreen Controllers, and the PFD
Controllers are discussed in this section. AFCS controls are described in the AFCS section. See the Audio and
CNS Section for more information about NAV/COM controls.
PFD CONTROLS
Figure 1-2 PFD Controls
PFD Softkeys
Selection softkeys are located along the bottom each PFD. The five softkeys on the left are not available when
the PFD is in Split Mode. The softkeys shown depend on the softkey level previously selected. The bezel keys
below the softkey labels can be used to select the appropriate softkey. There are three types of softkeys. One
selects a simple on/off state, indicated by an annunciator on the softkey label displayed as green (on) or gray
(off). The next type of softkey selects among several options, indicated by the softkey label changing (with
the exception of the Map Range keys) to reflect the name of the chosen option. The last type of softkey, when
pressed displays another set of softkeys available for the selected function. Also, these softkeys revert to the
previous level after 45 seconds of inactivity. When a softkey function is disabled, the softkey label is subdued
(dimmed).
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Garmin G5000 NG - Beechcraft Model 400A (Beechjet) Reference guide

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