Garmin G1000: Beechcraft King Air 200/B200 User guide

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User guide

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Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
Garmin AT, Inc.
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Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
Garmin Corporation
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Shijr, Taipei County, Taiwan
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www.garmin.com
Beechcraft 200/B200 Series
G1000
®
Integrated Flight Deck
Pilot’s Guide
G1000
®
Pilot’s Guide
Beechcraft 200/
B200 Series
190-00928-00
Revision A
System Software 0985.00 or later
Untitled-1 1 11/13/2007 9:15:37 AM
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-00 Rev. A
Copyright © 2008 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0985.00 or later for the Hawker Beechctaft 200/B200 Series. Some
differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax: 503/364.2138
Garmin (Europe) Ltd., Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K
Tel: 44/0870.8501241 Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
Website 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
®
is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000
®
is a trademark of Garmin Ltd. or its subsidiaries. These
trademarks may not be used without the express permission of Garmin.
Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc.; Becker
®
is a registered trademark of Becker
Flugfunkwerk GmbH; NavData
®
is a registered trademark of Jeppesen, Inc.; and XM
®
is a registered trademark of XM Satellite Radio,
Inc..
December 2008 Printed in the U.S.A.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
i
LIMITED WARRANTY
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made
at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty
does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED
OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR
PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole
discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit
the Garmin Website at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-00 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance
feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from
third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be
relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting
traffic.
WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm
penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather
avoidance, not penetration.
WARNING: GDL 69 Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69 is approved only for weather avoidance, not penetration.
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent
delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for
short-range weather avoidance.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
The Garmin G1000, as installed in this aircraft, has a very high degree of functional integrity.
However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable
system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur
without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such
an occurrence by means of cross-checking with all redundant or correlated information available in the
cockpit.
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING:
The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy
and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
WARNING:
To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the G1000 Integrated Avionics System in the Airplane Flight Manual.
Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications
from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual
sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
WARNING
: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an
intense radar echo.
WARNING
:
Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING
:
Because of anomalies in the earth’s magnetic field, operating the G1000 within the following
areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south
of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An
area south of 55° South latitude between longitude 120º East and 165º East.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-00 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
CAUTION:
The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty
and the pilot’s authority to operate this device under FAA/FCC regulations.
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: All visual depictions contained within this document, including screen images of the G1000 panel and
displays, are subject to change and may not reflect the most current G1000 system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE
: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions:
(1) this device may not cause harmful interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE
: 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.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00928-00 A 12/3/08 i – I-6 Initial Release
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-00 Rev. Avi
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 7
PFD Controls ................................................................ 7
Controls Associated With the MFD ................................. 9
AFCS Controls ............................................................ 11
Audio Panel Controls .................................................. 13
1.4 Secure Digital Cards.............................................. 15
1.5 System Power-up ................................................... 15
1.6 System Operation .................................................. 17
Normal Operation ....................................................... 17
Reversionary Mode ..................................................... 17
AHRS Operation ......................................................... 18
G1000 System Annunciations ...................................... 20
Softkey Function ......................................................... 21
GPS Receiver Operation .............................................. 27
1.7 Accessing G1000 Functionality............................ 31
Menus ....................................................................... 31
MFD Page Groups ....................................................... 32
MFD System Pages...................................................... 36
1.8 Display Backlighting ............................................. 50
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 54
Airspeed Indicator ...................................................... 54
Attitude Indicator ....................................................... 57
Altimeter ................................................................... 59
Vertical Speed Indicator (VSI) ....................................... 61
Vertical Deviation ....................................................... 62
Horizontal Situation Indicator (HSI) .............................. 63
Course Deviation Indicator (CDI) .................................. 68
2.2 Supplemental Flight Data .................................... 76
Temperature Displays .................................................. 76
Wind Data ................................................................. 77
Vertical Navigation (VNV) Indications ........................... 78
2.3 PFD Annunciations and Alerting Functions ........ 79
G1000 Alerting system ................................................ 79
Marker Beacon Annunciations...................................... 81
Traffic Annunciation .................................................... 81
TAWS Annunciations ...................................................82
Altitude Alerting .........................................................82
Low Altitude Annunciation .......................................... 83
Minimum Descent Altitude/Decision Height Alerting ......83
2.4 Abnormal Operations ........................................... 85
Abnormal GPS Conditions ........................................... 85
Unusual Attitudes ....................................................... 86
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display .............................................................. 88
Interstage Turbine Temperature .................................... 90
Torque ....................................................................... 90
Tachometer (RPM) ...................................................... 91
Turbine Speed ............................................................ 92
Fuel Flow ................................................................... 92
Oil Pressure ................................................................ 93
Oil Temperature .......................................................... 93
3.2 EIS Display in Reversionary Mode ....................... 94
Reversionary Display ................................................... 95
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 97
Audio Panel Volume Control ........................................ 97
PFD Controls and Frequency Display ............................. 98
Audio Panel Controls ................................................ 100
Control Unit ............................................................. 102
4.2 COM Operation .................................................... 104
COM Transceiver Selection and Activation ................... 104
COM Transceiver Manual Tuning ................................ 105
Quick-Tuning and Activating 121.500 MHz .................. 107
Auto-Tuning the COM Frequency ................................ 108
Frequency Spacing .................................................... 112
Automatic Squelch .................................................... 113
Volume .................................................................... 113
4.3 NAV Operation ..................................................... 114
NAV Radio Selection and Activation ........................... 114
NAV Receiver Manual Tuning ..................................... 115
Auto-Tuning a NAV Frequency from the MFD............... 118
Marker Beacon Receiver ............................................ 123
DME Tuning ............................................................. 124
4.4 GTX 33 Mode S Transponders ............................ 125
Transponder Controls ................................................ 125
Transponder Mode Selection ...................................... 126
Entering a Transponder Code ..................................... 129
IDENT Function ........................................................ 131
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
vii
TABLE OF CONTENTS
4.5 Additional Audio Panel Functions ..................... 132
Power-Up ................................................................. 132
Mono/Stereo Headsets .............................................. 132
Speaker ................................................................... 132
Unmuted Inputs ....................................................... 132
Intercom .................................................................. 133
Passenger Address (PA) System .................................. 134
Simultaneous COM Operation .................................... 134
Clearance Recorder and Player ................................... 135
4.6 Audio Panels Preflight Procedure ...................... 136
4.7 Abnormal Operation ........................................... 138
Stuck Microphone ..................................................... 138
COM Tuning Failure ................................................... 138
PFD Failure, Dual System ........................................... 139
Audio Panel Fail-Safe Operation ................................. 140
Reversionary Mode ................................................... 140
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 141
Navigation Status Box ............................................... 143
5.2 Using Map Displays ............................................. 144
Map Orientation ....................................................... 144
Map Range .............................................................. 146
Map Panning ............................................................ 149
Measuring Bearing and Distance ................................ 154
Topography .............................................................. 155
Map Symbols ........................................................... 158
Airways ................................................................... 164
Track Vector ............................................................. 166
Wind Vector ............................................................. 167
Nav Range Ring........................................................ 168
Fuel Range Ring ....................................................... 169
Field of View (SVS) .................................................... 170
5.3 Waypoints ............................................................. 171
Airports ................................................................... 172
Intersections ............................................................ 178
NDBs ....................................................................... 180
VORs ....................................................................... 182
User Waypoints ........................................................ 184
5.4 Airspaces .............................................................. 190
5.5 Direct-to-Navigation .......................................... 195
5.6 Flight Planning ..................................................... 202
Flight Plan Creation .................................................. 203
Adding Waypoints to an Existing Flight Plan ................ 207
Adding Airways to a Flight Plan ................................. 209
Adding Procedures to a Stored Flight Plan .................. 212
Flight Plan Storage ................................................... 219
Flight Plan Editing .................................................... 221
Along Track Offsets ................................................... 225
Parallel Track ............................................................ 226
Activating a Flight Plan Leg ....................................... 229
Inverting a Flight Plan ............................................... 230
Flight Plan Views ...................................................... 231
Closest Point of FPL .................................................. 233
5.7 Vertical Navigation ............................................. 234
Altitude Constraints .................................................. 236
5.8 Procedures ........................................................... 240
Departures ............................................................... 240
Arrivals ................................................................... 243
Approaches ............................................................. 245
5.9 Trip Planning ........................................................ 251
Trip Planning ............................................................ 251
Weight Planning ....................................................... 255
Weight Caution And Warning Conditions .................... 257
5.10 RAIM Prediction................................................... 258
5.11 Navigating a Flight Plan ..................................... 262
5.12 Abnormal Operation ........................................... 291
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 293
Activating Services .................................................... 293
Using XM Satellite Weather Products .......................... 295
Weather Softkeys on the Weather Data Link Page ........ 298
6.2 Airborne Color Weather Radar .......................... 323
System Description ................................................... 323
Principles of Pulsed Airborne Weather Radar ............... 323
Safe Operating Distance ............................................ 327
Basic Antenna Tilt Setup ............................................ 328
Practical Application Using the Basic Tilt Setup ............ 328
Weather Mapping and Interpretation ......................... 329
Ground Mapping and Interpretation ........................... 342
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-00 Rev. Aviii
TABLE OF CONTENTS
6.3 Stormscope Weather Mapping Sensor ............. 343
Setting Up Stormscope on the Navigation Map ........... 344
Selecting the Stormscope Page .................................. 347
6.4 Terrain Awareness and Warning System ........... 350
TAWS-B Alerts .......................................................... 355
System Status ........................................................... 360
6.5 Traffic Information Service (TIS) ........................ 362
Traffic Map Page ....................................................... 365
TIS Alerts ................................................................. 366
System Status ........................................................... 367
6.6 L-3 Skywatch Traffic Advisory System .............. 370
TAS Symbology ......................................................... 370
Operation ................................................................ 371
Altitude Display ........................................................ 374
Traffic Map Page Display Range ................................. 374
TAS Alerts ................................................................ 376
System Status ........................................................... 376
6.7 Honeywell KTA 870 Traffic Advisory System .... 378
TAS Symbology ......................................................... 378
Operation ................................................................ 379
Altitude Display ........................................................ 382
Traffic Map Page Display Range ................................. 382
TAS Alerts ................................................................ 384
System Status ........................................................... 385
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................... 387
Additional AFCS Controls .......................................... 389
7.2 Flight Director Operation ................................... 390
Activating the Flight Director ..................................... 390
AFCS Status Box ....................................................... 391
Flight Director Modes ................................................ 392
Switching Flight Directors .......................................... 392
Command Bars ......................................................... 393
7.3 Vertical Modes ..................................................... 394
Pitch Hold Mode (PIT) ............................................... 395
Selected Altitude Capture Mode (ALTS) ....................... 396
Altitude Hold Mode (ALT) .......................................... 397
Vertical Speed Mode (VS) .......................................... 398
Flight Level Change Mode (FLC) ................................. 399
Vertical Navigation Modes (VPTH, ALTV) ..................... 401
Glidepath Mode (GP) ................................................ 406
Glideslope Mode (GS) ............................................... 408
Takeoff (TO) and Go Around (GA) Modes .................... 409
7.4 Lateral Modes ...................................................... 410
Roll Hold Mode (ROL) ............................................... 411
Low Bank Mode ....................................................... 411
Navigation Modes (GPS, VOR, LOC) ............................ 413
Approach Modes (GPS, VAPP, LOC) ............................. 415
Backcourse Mode (BC) .............................................. 417
7.5 Autopilot and Yaw Damper Operation ............. 418
Flight Control ........................................................... 418
Engagement ............................................................. 419
Control Wheel Steering ............................................. 419
Disengagement ........................................................ 420
7.6 Example Flight Plan ............................................ 421
Departure ................................................................ 422
Intercepting a VOR Radial .......................................... 424
Flying a Flight Plan/GPS Course ................................. 425
Descent ................................................................... 426
Approach ................................................................. 430
Go Around/Missed Approach ..................................... 432
7.7 AFCS Annunciations and Alerts .........................434
AFCS Status Alerts .................................................... 434
Overspeed Protection ................................................ 435
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 438
SVS Operation .......................................................... 439
SVS Features ............................................................ 441
Field of View ............................................................ 449
8.2 SafeTaxi ................................................................ 451
SafeTaxi Cycle Number and Revision .......................... 454
8.3 ChartView ............................................................. 457
ChartView Softkeys ................................................... 457
Terminal Procedures Charts ....................................... 458
Chart Options ........................................................... 466
Day/Night View ........................................................ 472
ChartView Cycle Number and Expiration Date ............. 474
8.4 FliteCharts ............................................................ 478
FliteCharts Softkeys .................................................. 478
Terminal Procedures Charts ....................................... 479
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
ix
TABLE OF CONTENTS
Chart Options ........................................................... 486
Day/Night View ........................................................ 490
FliteCharts Cycle Number and Expiration Date ............. 492
8.5 XM Radio Entertainment .................................... 496
Activating XM Satellite Radio Services ........................ 496
Using XM Radio ....................................................... 498
8.6 Scheduler .............................................................. 501
8.7 Abnormal Operation ........................................... 503
SVS Troubleshooting ................................................. 503
Reversionary Mode ................................................... 503
Unusual Attitudes ..................................................... 504
APPENDICES
Annunciations and Alerts ............................................. 507
Comparator Annunciations ........................................ 510
Reversionary Sensor Annunciations ............................ 511
G1000 System Annunciations .................................... 511
G1000 System Message Advisories ............................. 514
AFCS Alerts .............................................................. 525
Terrain-SVS Alerts ..................................................... 526
Terrain-SVS Status Annunciations ............................... 526
TAWS ALERTS ........................................................... 527
Flight plan Import/Export Messages ........................... 528
SD Card Use ................................................................... 529
Jeppesen Databases .................................................. 529
Garmin Databases .................................................... 530
Glossary .......................................................................... 533
Frequently Asked Questions ........................................ 541
Map Symbols ................................................................. 547
INDEX
Index ................................................................................I-1
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-00 Rev. Ax
TABLE OF CONTENTS
Bl a n k Pa g e
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Beechcraft 200/B200
Series. The G1000 system is an integrated flight control system that presents flight instrumentation, position,
navigation, communication, and identification information to the pilot through large-format displays. The system
consists of the following Line Replaceable Units (LRUs):
•
GDU 1040A
Primary Flight Display (PFD)
•
GDU 1500
Multi Function Display (MFD)
•
GIA 63W
Integrated Avionics Unit
•
GDC 74B
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GMA 1347D
Dual Audio System with Integrated
Marker Beacon Receiver
•
GTX 33/33D
Extended Squitter Mode S
Transponder
•
GDL 69A
Satellite Data Link Receiver
•
GWX 68
Weather Radar
•
GCU 477
MFD Control Unit
•
GMC 710
AFCS Control Unit
•
GTP 59
Outside Air Temperature (OAT) Probe
•
GSA 80
AFCS Servos
•
GSM 85A
Servo Gearboxes
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A).
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
In the Beechcraft 200/B200 Series, the GFC 700 Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
2
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.2 LINE REPLACEABLE UNITS (LRU)
•
GDU 1040A
(2) – Each unit is configured as a PFD that features a 10.4-inch LCD with 1024 x 768 resolution.
The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side
is designated as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W
Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.
•
GDU 1500
(1) – Features a 15-inch LCD with 1024 x 768 resolution and is configured as an MFD. This unit
is linked to both PFDs via HSDB connection.
•
GIA 63W
(2) Functions as the main communication hub, linking all LRUs with the on-side PFD. Each
GIA 63W contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system
integration microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA
63Ws are not paired together and do not communicate with each other directly.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
3
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GDC 74B
(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 G1000 system, and it communicates
with the on-side GIA 63W, on-side GDU 1040A, GDU 1040A MFD, and on-side GRS 77, using an ARINC 429
digital interface (it also interfaces directly with the on-side GTP 59). The GDC 74B is designed to operate in
Reduced Vertical Separation Minimum (RVSM) airspace.
•
GEA 71
(2) Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws using an RS-485 digital interface.
•
GRS 77
(2) Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU
1040A, the GDU 1040A MFD, and the on-side GIA 63W. The GRS 77 contains advanced sensors (including
accelerometers and rate sensors) and interfaces with the on-side GMU 44 to obtain magnetic field information,
with the GDC 74B to obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS modes of
operation are discussed later in this document.
•
GMU 44
(2) Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft
magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77,
using an RS-485 digital interface.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
•
GMA 1347D
(2) Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is
installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual
control of the display reversionary mode (red
DISPLAY BACKUP
button) and communicates with the on-side
GIA 63W, using an RS-232 digital interface.
•
GTX 33/33D
(2) Solid-state transponders that provide Modes A, C, S and ADS-B capability. Both transponders
can be controlled from either PFD, and only one transponder can be active at a time. Each transponder
communicates with the on-side GIA 63W through an RS-232 digital interface.
•
GDL 69A
(1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and,
indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates
with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the
GDL 69A capability.
•
GWX 68
(1) Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A,
via HSDB connection.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GCU 477
(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
•
GMC 710
(1) Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing
communication with both PFDs.
•
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.
•
GSA 80
(4), and
GSM 85A
(4) – The GSA 80 servos are used for the automatic control of roll, pitch, and yaw,
and pitch trim. These units interface with each GIA 63W.
The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80 servo actuator to
the mechanical flight-control surface linkage.
190-00928-00 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
6
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
GDU 1040A
(PFD #1)
GDU 1040A
(PFD #2)
GDU1500
(MFD)
GIA63W #2
GSA80
(Yaw)
GSA80
(Roll)
GSA 80
(Pitch)
GSA 80
(Pitch Trim)
GRS77#1
GIA 63W #1
GMC710
GMU44#1
GEA71#2
GEA71#1
GDC 74B #1
GTP59#1
GMA1347D
#2
GMA 1347D
#1
GTX 33/33D GTX 33/33D
GCU 477
GWX68
GDL 69A
GRS77#2
GMU44#2
GDC74B #2
GTP59#2
VHF COM
VHF NAV/LOC
GPS/WAAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
VHF COM
VHF NAV/LOC
GPS/WAAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
Figure 1-1 G1000 System (LRU Configuration)
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Garmin G1000: Beechcraft King Air 200/B200 User guide

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User guide
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