Garmin G5000® for Beechjet Reference guide

Type
Reference guide
Beechjet 400A &
HawkerXP (Model 400A)
G5000
®
Integrated Avionics System
Pilot’s Guide
190-02014-00 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
Copyright © 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2091.00 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.
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, 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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Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
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: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied
upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: Always obtain qualified instruction prior to operational use of this equipment.
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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iii
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: When using the autopilot to fly 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: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories , ATC guidance, or positive visual
acquisition of conflicting traffic.
WARNING:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications (GRS 77 installations only) in the following geographic areas: 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:
Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may
appear as a partial symbol.
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.
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iv
WARNINGS, CAUTIONS, AND NOTES
WARNING
: Do not operate the weather radar in a transmitting mode when personnel or objects are within
the MPEL boundary.
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:
Repairs should only be made by 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.
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Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
v
WARNINGS, CAUTIONS, AND NOTES
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.
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.
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vi
WARNINGS, CAUTIONS, AND NOTES
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 to
coordinate the revised DQRs.
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: Operate the 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)
vii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02014-00 A 8/12/16 All Production release at GDU 6.56
190-02014-00 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
viii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 System Power-up ..................................................... 4
1.3 G5000 Controls ........................................................ 6
PFD Controls ................................................................ 6
Touchscreen Controller ................................................ 15
GDU Controllers ......................................................... 37
1.4 System Operation .................................................. 39
Normal Operation ....................................................... 39
Reversionary Display Operation ................................... 40
AHRS Operation ......................................................... 41
GPS Receiver Operation .............................................. 42
Annunciations ............................................................ 46
1.5 FMS Initialization .................................................. 48
1.6 System Management ............................................ 50
Avionics Settings ........................................................ 50
Crew Profiles .............................................................. 59
Avionics Status ........................................................... 61
SiriusXM Information .................................................. 62
System Tests ............................................................... 63
Screen Cleaning .......................................................... 64
1.7 Utilities ................................................................... 65
Timer ......................................................................... 65
Trip Stats ................................................................... 66
1.8 Secure Digital Cards.............................................. 71
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 76
Airspeed Indicator ...................................................... 76
Attitude Indicator ....................................................... 79
Altimeter ................................................................... 80
Vertical Speed Indicator (VSI) ....................................... 84
Vertical Deviation ....................................................... 84
Horizontal Situation Indicator (HSI) .............................. 86
Course Deviation Indicator (CDI) .................................. 90
2.2 Garmin SVT (Synthetic Vision Technology) ......... 97
SVT Operation ............................................................ 98
SVT Features .............................................................. 99
Field of View ............................................................104
2.3 Supplemental Flight Data .................................. 105
Temperature Displays ................................................ 105
Wind Data ............................................................... 106
Vertical Navigation (VNV) Indications ......................... 107
2.4 PFD Annunciations and Alerting Functions ...... 108
Marker Beacon Annunciations.................................... 108
Traffic Annunciation .................................................. 108
Terrain Annunciations ............................................... 109
Altitude Alerting ....................................................... 110
Low Altitude Annunciation ........................................ 110
Minimum Descent Altitude/Decision Height Alerting .... 111
Radar Altimeter ........................................................ 112
2.5 Abnormal Operations ......................................... 114
Abnormal GPS Conditions ......................................... 114
Comparator Annunciations ........................................ 115
Unusual Attitudes ..................................................... 116
SECTION 3 ENGINE INDICATION & CREW ALERTING
SYSTEM (EICAS)
3.1 Engine Indication System (EIS) .......................... 119
Engine Indications .................................................... 121
3.2 Aircraft Systems ..................................................131
Engine Vibration ....................................................... 131
Fuel Used Reset ........................................................ 131
System Tests ............................................................. 132
3.3 Crew Alerting System (CAS) ............................... 133
SECTION 4 AUDIO AND CNS
4.1 Overview .............................................................. 135
Touchscreen Controller Audio and CNS Controls .......... 136
PFD COM/NAV display and Controls ........................... 138
4.2 COM Operation .................................................... 140
COM Transceiver Selection and Activation ................... 140
COM Frequency Tuning .............................................. 142
Frequency Spacing .................................................... 148
Automatic Squelch .................................................... 150
Volume .................................................................... 151
4.3 NAV Operation ..................................................... 152
NAV Radio Selection and Activation ........................... 152
NAV Receiver Tuning ................................................. 153
Marker Beacon Receiver ............................................ 161
ADF/DME Tuning ...................................................... 163
4.4 Mode S Transponder ........................................... 169
Transponder Controls ................................................ 169
Transponder Mode Selection ...................................... 169
Entering a Transponder Code ..................................... 172
IDENT Function ........................................................ 174
Flight ID Reporting.................................................... 174
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Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
ix
TABLE OF CONTENTS
4.5 Additional Audio Functions ................................ 176
Mono/Stereo Headsets .............................................. 176
Speaker ................................................................... 176
Intercom .................................................................. 177
Passenger Address (PA) System .................................. 179
Clearance Recorder and Player ................................... 180
Simultaneous COM Operation .................................... 181
Entertainment .......................................................... 182
Audio Feedback (Clicks) ............................................ 184
4.6 Abnormal Operation ........................................... 185
Stuck Microphone ..................................................... 185
COM Tuning Failure ................................................... 185
Audio Controller Fail-Safe Operation .......................... 185
Touchscreen Controller Failure ................................... 185
Amber COM Frequency Digits .................................... 185
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 ................................ 202
Absolute Terrain ....................................................... 204
Map Symbols ........................................................... 207
Airways ................................................................... 213
Track Vector ............................................................. 215
Navigation Map Wind Vector .....................................216
Fuel Range Ring ....................................................... 217
Field of View (SVT) .................................................... 218
Selected Altitude Intercept Arc ................................... 219
Latitude/Longitude Lines ........................................... 220
Obstacles ................................................................. 221
5.3 Waypoints ............................................................. 222
Airports ................................................................... 223
Intersections ............................................................ 229
NDBs ....................................................................... 232
VORs ....................................................................... 235
User Waypoints ........................................................ 238
5.4 Airspaces .............................................................. 246
5.5 Direct-to-Navigation .......................................... 250
5.6 Flight Planning ..................................................... 260
Flight Plan Creation .................................................. 261
Adding Waypoints to an Existing Flight Plan ................ 271
Adding Airways to a Flight Plan ................................. 279
Adding Procedures to a Stored Flight Plan .................. 281
Flight Plan Storage ................................................... 289
Flight Plan Editing .................................................... 292
Along Track Offsets ................................................... 295
Parallel Track ............................................................ 300
Activating a Flight Plan Leg ....................................... 303
Inverting a Flight Plan ............................................... 303
Collapsing Airways ................................................... 304
Closest Point of Flight Plan ........................................ 305
User-Defined Holding Patterns ................................... 306
5.7 Vertical Navigation ............................................. 313
Altitude Constraints .................................................. 320
Speed Constraints ..................................................... 326
Flight Path Angle (FPA) Constraints ............................ 329
5.8 Procedures ...........................................................332
Departures ............................................................... 334
Arrivals ................................................................... 337
Approaches ............................................................. 340
5.9 Trip Planning ........................................................ 354
Trip Statistics ............................................................ 355
Fuel Statistics ........................................................... 356
Other Statistics ......................................................... 356
5.10 Weight and Fuel Planning .................................. 358
Weight Caution And Warning Conditions .................... 362
5.11 Takeoff and Landing Data .................................. 363
Takeoff Data ............................................................. 363
Landing Data ........................................................... 364
5.12 Abnormal Operation ........................................... 366
FMS Degradation ...................................................... 366
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 370
Activating Services .................................................... 370
Accessing SiriusXM Weather Products ........................ 372
6.2 Garmin Connext Weather ................................... 404
Registering the system for Garmin Connext Services .... 404
Accessing Garmin Connext Weather Products .............. 405
Connext Weather Data Requests ................................ 411
Garmin Connext Weather Products ............................. 416
Abnormal Operations ................................................ 429
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TABLE OF CONTENTS
6.3 Airborne Color Weather Radar .......................... 430
System Description ................................................... 430
Principles of Airborne Weather Radar .......................... 430
Basic Antenna Tilt Setup ............................................ 434
Ground Mapping and Interpretation ........................... 452
Additional Radar Displays .......................................... 453
System Status ........................................................... 456
6.4 Stormscope Lightning ......................................... 458
Using the Stormscope Pane ....................................... 458
Stormscope Information on Navigation Maps .............. 460
Abnormal Operations ................................................ 463
6.5 TAWS-B ................................................................. 464
Relative Terrain Symbology ........................................ 465
Displaying Relative Terrain Information ....................... 467
System Status ........................................................... 476
TAWS-B Abnormal Operations ................................... 477
6.6 TAWS-A ................................................................. 478
Relative Terrain Symbology ........................................ 479
TAWS Pane .............................................................. 481
System Status ........................................................... 496
TAWS-A Abnormal Operations ................................... 496
6.7 TCAS II TraffiC ...................................................... 498
TCAS II Alerts ........................................................... 499
Displaying TCAS II Traffic ........................................... 501
Operation ................................................................ 504
System Status ........................................................... 507
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 510
Basic Autopilot Operation .......................................... 512
7.2 Flight Director Operation ................................... 513
Activating the Flight Director ..................................... 513
AFCS Status Box ....................................................... 514
Command Bars ......................................................... 514
Flight Director Modes ................................................ 516
Flight Director Selection ............................................ 516
7.3 AFCS Modes ......................................................... 517
Vertical Modes (PIT, ALT, VS, FLC) ................................ 517
Lateral Modes (ROL, BANK, HDG, NAV) ....................... 525
Combination modes (VNAV, APPR, NAV, BC, TO, GA)..... 530
7.4 Autopilot Operation ............................................ 544
Engaging the Autopilot ............................................. 544
Control wheel Steering .............................................. 545
Disengaging the Autopilot ......................................... 545
7.5 AFCS Annunciations and Alerts ......................... 546
Underspeed Protection (optional) ............................... 546
Overspeed Protection ................................................ 547
7.6 Abnormal Operation ........................................... 548
Overpowering Autopilot Servos .................................. 548
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi ................................................................ 550
SafeTaxi Database Information .................................. 551
8.2 SurfaceWatch ....................................................... 553
Information Display .................................................. 554
Alerts ...................................................................... 555
8.3 ChartView (Optional) .......................................... 556
Chart Selection ......................................................... 557
Day/Night View ........................................................ 560
ChartView Database Information ............................... 562
8.4 Airport Directory ................................................. 564
Airport Directory Database Cycle Number and Revision 564
8.5 Satellite Telephone and Datalink Services ....... 566
Registering the System With Garmin Connext .............. 566
Contacts .................................................................. 567
Telephone Communication (Optional) ......................... 569
Text Messaging (SMS) ............................................... 575
8.6 SiriusXM Satellite Radio ..................................... 585
Activating SiriusXM Satellite Services ......................... 585
Using SiriusXM Radio ................................................ 586
8.7 Scheduled Messages ........................................... 590
8.8 Electronic Documents ......................................... 595
Installed Documents ................................................. 595
User Documents ....................................................... 595
Viewing Electronic Documents ................................... 596
8.9 Electronic Checklists ........................................... 602
8.10 Flight Data Logging ............................................ 605
8.11 Abnormal Operation ........................................... 607
APPENDICES
Annunciations and Alerts ............................................. 609
CAS Messages .......................................................... 609
Comparator Annunciations ........................................ 611
Reversionary Sensor Annunciations ............................ 612
System Annunciations ............................................... 613
System Message Advisories ....................................... 615
AFCS Alerts .............................................................. 630
TAWS-A Alerts and Annunciations .............................. 631
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TABLE OF CONTENTS
TAWS-B ALERTS and Annunciations ............................ 633
TCAS I Alerts and Annunciations ................................ 635
Weather Radar Annunciations .................................... 636
G5000 Aural Alerts ................................................... 637
Pilot Profile Import/Export Messages .......................... 638
Flight Plan Import/Export Messages ........................... 638
GDL 69A SXM Data Link Receiver Messages ............... 639
SurfaceWatch Alerts and Annunciations ...................... 639
Database Management ................................................ 641
Navigation Databases ............................................... 642
Automatic Database Synchronization Feature .............. 647
GarminDatabasesandJeppesenChartViewDatabase .648
Magnetic Field Variation Database Update .................. 652
Garmin Aviation Glossary ............................................ 655
Frequently Asked Questions ........................................ 663
Map Symbols ................................................................. 667
INDEX
Index ................................................................................ I-1
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TABLE OF CONTENTS
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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 1200W (3) – The GDU 1200W 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 displyayed 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 63W Integrated Avionics Unit (IAU).
•
GTC 570 (2)
– The 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 one 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 GDU Controller is a panel-mounted user interface which enables the flight crew to control
the both PFDs. Each unit is connected to the on-side PFD, and to the MFD.
•
GMA 36 (2)
– The Remote Audio Processor integrates navigation/communication radio (NAV/COM) digital
audio, intercom, and marker beacon audio. The units are connected to their respective Touchscreen Controllers.
•
GIA 63W
(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking several
LRUs with each on-side GDU. 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) – 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 G5000 system, and it communicates with
both GIA 63Ws, the on-side GDU 1200W and the on-side GRS 77. The GDC 7400 is designed to operate in
Reduced Vertical Separation Minimum (RVSM) airspace.
•
GEA 7100 (2)
– The Engine Airframe Unit receives and processes signals from the engine and airframe sensors,
and it communicates with both IAUs.
•
GTX 3000
(2) – The solid-state Transponder provides Modes A/C/S capability, 1090 MHz Extended Squitter
Automatic Dependent Surveillance - Broadcast (ADS-B) transmission, and communicates with both IAUs.
•
GRS 77
(2) – The 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 GDU, 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. AHRS operation is discussed
in System Operation, later in this section.
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
190-02014-00 Rev. A2
SYSTEM OVERVIEW
•
GMU 44
(2) – The 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 Satellite Data Link Radio Receiver receives weather information, as well as digital audio
entertainment. The Data Link Receiver communicates with the MFD. A subscription to SiriusXM Weather and/
or SiriusXM Satellite Radio service is required to enable the GDL 69A SXM capability.
•
GMC 7250
– The AFCS Mode Controller provides AFCS control, and connects to PFD1 and PFD2.
•
GSA 9000
(3) and
GTA 82 (1)
– The GSA 9000 Servos are used for automatic control of pitch, roll, and yaw
via the AFCS. The GTA 82 Pitch Trim Adapter works with the existing motor to provide automatic pitch trim.
These units interface with each IAU.
•
GSM 9100 (3)
The GSM 9100 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 70 provides airborne real-time weather and ground mapped radar data to the GDUs.
The unit is connected to the #2 GSD.
•
GSR 56
(1) (optional) – The Iridium Transceiver provides telephone voice communication by means of pilot
and copilot headsets. The transceiver can also send and receive short message service (SMS) text messages. The
GSR 56 also receives data link weather products from the Garmin Connext weather service through the Iridium
satellite network. The GSR 56 is connected to the #1 GIA 63W.
•
GSD 41
(2) – The data concentrator is used to expand the input and output capabilities of the system. HSDB
communications occur among Garmin LRUs. The ARINC 429 protocol connects non-Garmin LRUs using the
GSD 41 .
A top-level G5000 system block diagram is shown in Figure 1-1.
The G5000 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.
190-02014-00 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
3
SYSTEM OVERVIEW
#1
GDU 1200W
(PFD1)
GDL 69A SXM
(SiriusXM
Weather Datalink)
#1 GMA 36
(Audio
Processor)
#1 GSA 9000 (Pitch)
#2 GSA 9000 (Yaw)
#3 GSA 9000 (Roll)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#3
GDU 1200W
(PFD2)
Non-Garmin Equipment
#1 GTX 3000
(Transponder)
#2
GDU 1200W
(MFD1)
#1 GCU 275
(GDU
Controller)
GTC 570
(Touchscreen
Controller)
GTC 570
(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 36
(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
#1 GSR 56
(Iridium)
Lightning
Detection
System
#1 GMU 44
(Magnetometer)
#1 GRS 77
(Attitude & Head-
ing)
#2 GRS 77
(Attitude & Head-
ing)
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)
190-02014-00 Rev. A4
SYSTEM OVERVIEW
1.2 SYSTEM POWER-UP
NOTE: See the Airplane Flight Manual (AFM) for specific procedures concerning avionics power application
and emergency power supply operation.
NOTE: Refer to Appendix A for system-specific annunciations and alerts.
The G5000 is integrated with the aircraft electrical system and receives power directly from electrical busses.
The GDUs, Touchscreen Controllers, and supporting sub-systems include both power-on and continuous built-in
test features that exercise the processors, memory, external inputs, and outputs to provide safe operation.
During system power-up, the system displays test annunciations, as shown in Figure 1-2. All system annunciations
should be extinguished typically within the first minute of power-up. Upon power-up, annunciator lights on the
AFCS Controller illuminate momentarily.
On PFD1 and PFD2, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS
should display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align
itself both while taxiing in a straight line and during level flight.
When the MFD powers up, the splash screen (Figure 1-3) displays the following information:
•Systemversion
•Copyright
•Landdatabasenameandversion
•SafeTaxidatabaseinformation
•Terraindatabasenameandversion
•Obstacledatabasenameandversion
•Navigationdatabasename,version,andeffectivedates
•AirportDirectoryname,versionandeffectivedates
•ChartViewdatabaseinformation
Current database information includes database type, cycle number, or valid operating dates. Review the listed
information for currency (to ensure that no databases have expired).
Pressing the right-most softkey on the MFD acknowledges this information, and the MFD then shows the
Engine Indication and Crew Alerting System (EICAS) Display and two Navigation Map Panes in Half Mode.
When the system has acquired a sufficient number of satellites to determine a position, the system displays the
aircraft’s current position on the Navigation Map Pane.
190-02014-00 Rev. A
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
5
SYSTEM OVERVIEW
Figure 1-4 Touchscreen Controller
Initialization Screen
Figure 1-2 PFD1 Power-Up
Figure 1-3 MFD Power-Up
Garmin G5000 Pilot’s Guide for the Beechjet 400A & Hawker 400XP (Model 400A)
190-02014-00 Rev. A6
SYSTEM OVERVIEW
1.3 G5000 CONTROLS
The G5000 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 the PFD1 and PFD2 bezels, the
Touchscreen Controllers, the GDU Controllers and the AFCS Controller. PFD controls, Touchscreen Controllers,
and the GDU 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 1-5 PFD Controls
PFD Softkeys
Selection softkeys are located along the bottom of PFD1 and PFD2. 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® for Beechjet Reference guide

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Reference guide

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