Garmin G1000: Beechcraft King Air 200/B200 User guide

Type
User guide

This manual is also suitable for

Beechcraft 200/B200 Series
G1000
®
Integrated Flight Deck
Pilot’s Guide
Untitled-1 1 11/13/2007 9:15:37 AM
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
Copyright © 2008-2011 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0985.03 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
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
Website Address: www.garmin.com
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®
and G1000
®
are registered trademarks of Garmin Ltd. or its subsidiaries, and ESP
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
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®
is a registered trademark of Jeppesen, 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.
August 2011 Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-03 Rev. Aii
LIMITED WARRANTY
LIMITED WARRANTY
Within the warranty period, Garmin will, at its sole discretion, 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/or labor incidental to the direct repair of said product. Garmin may,
at its discretion with prior approval, reimburse an authorized Garmin Service Center for associated labor costs incurred for removal and
replacement of the panel mount product installed in an aircraft. The customer shall be responsible for any transportation or other cost. This
warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product
damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or
other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider
of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin
reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any
country.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS,
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 in every case.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or 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 the nearest Service Center, call
Garmin Customer Service at one of the numbers listed below.
Products sold through online auctions are not eligible for warranty coverage or rebates or other special offers from Garmin. Online auction
confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original
retailer is required. Garmin will not replace missing components from any package purchased through an online auction.
Garmin International Inc.
1200 East 151st Street, Olathe, Kansas 66062
Telephone: (913)397-8200
Telephone Toll Free: (888)606-5482
Facsimile: (913)397-8282
Facsimile Toll Free: (800)801-4670
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road, Southampton, SO40
9RB, UK
Telephone: ++44 (0) 870-8501243
Telephone Toll Free: ++44 (0) 0808 238 0000
(option 5)
Facsimile: ++44 (0) 238052004
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
iii
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: Do not use datalink weather products (e.g., XM WX Satellite Weather, GFDS World Wide Weather,
or FIS-B) for hazardous weather penetration. Weather information provided by these products is aged by up
to several minutes and may not depict actual weather conditions as they currently appear.
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.
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-03 Rev. Aiv
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:
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 variation 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 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 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.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
v
WARNINGS, CAUTIONS, AND NOTES
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.
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.
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-03 Rev. Avi
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00928-00 A 12/3/08 i – I-6 Initial Release for GDU 9.12
190-00928-01 A 7/24/09 i – I-6 Added GDU 10.00 changes
Added TAWS A functionality
Added radar altimeter functionality
190-00928-02 A 10/20/10 i – I-6 Added GDU 11.12 changes
Added GTS 820/850
Added GDL 59/GSR 56
Added Worldwide Weather
Added Profile View
Added Selected Altitude Arc
Added Electronic Stabilization & Protection (ESP
)
190-00928-03 A 8/30/11 i – I-6 Added GDU 12.01 changes
Added EGNOS
Added WX LGND Softkey on PFD
Removed DB SYNC Softkey
Changed Altitude to GSL Altitude on GPS Status Page
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
vii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................... 1
1.2 Line Replaceable Units (LRU) ................................... 2
1.3 G1000 Controls ......................................................... 8
PFD Controls ................................................................ 8
Controls Associated With the MFD ............................... 10
AFCS Controls ............................................................ 12
Audio Panel Controls .................................................. 14
1.4 Secure Digital Cards ............................................... 16
1.5 System Power-up ..................................................... 17
1.6 System Operation ................................................... 18
Normal Operation ....................................................... 18
Reversionary Mode ..................................................... 18
AHRS Operation ......................................................... 20
G1000 System Annunciations ...................................... 22
Softkey Function ......................................................... 22
GPS Receiver Operation .............................................. 29
1.7 Accessing G1000 Functionality ............................. 34
Menus ....................................................................... 34
MFD Page Groups ....................................................... 34
MFD System Pages...................................................... 38
1.8 Display Backlighting ............................................... 52
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................... 56
Airspeed Indicator ...................................................... 56
Attitude Indicator ....................................................... 59
Altimeter ................................................................... 61
Vertical Speed Indicator (VSI) ....................................... 64
Vertical Deviation ....................................................... 64
Horizontal Situation Indicator (HSI) .............................. 65
Course Deviation Indicator (CDI) .................................. 70
2.2 Supplemental Flight Data ...................................... 78
Temperature Displays .................................................. 78
Wind Data ................................................................. 79
Vertical Navigation (VNV) Indications ........................... 80
2.3 PFD Annunciations and Alerting Functions .......... 81
G1000 Alerting system ................................................ 81
Marker Beacon Annunciations...................................... 83
Traffic Annunciation .................................................... 83
TAWS Annunciations ................................................... 84
Altitude Alerting ......................................................... 84
Low Altitude Annunciation .......................................... 85
Minimum Descent Altitude/Decision Height Alerting ...... 85
Radar Altimeter .......................................................... 86
2.4 Abnormal Operations ............................................. 88
Abnormal GPS Conditions ........................................... 88
Unusual Attitudes ....................................................... 89
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display ............................................................... 92
Interstage Turbine Temperature .................................... 94
Torque ....................................................................... 94
Tachometer (RPM) ...................................................... 95
Turbine Speed ............................................................ 96
Fuel Flow ................................................................... 96
Oil Pressure ................................................................ 97
Oil Temperature .......................................................... 97
3.2 EIS Display in Reversionary Mode ........................ 98
Reversionary Display ................................................... 99
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 101
Audio Panel Volume Control ...................................... 101
PFD Controls and Frequency Display ........................... 102
Audio Panel Controls ................................................ 104
Control Unit ............................................................. 106
4.2 COM Operation...................................................... 108
COM Transceiver Selection and Activation ................... 108
COM Transceiver Manual Tuning ................................ 109
Quick-Tuning and Activating 121.500 MHz .................. 111
Auto-Tuning the COM Frequency ................................ 112
Frequency Spacing .................................................... 116
Automatic Squelch .................................................... 117
Volume .................................................................... 117
4.3 NAV Operation....................................................... 118
NAV Radio Selection and Activation ........................... 118
NAV Receiver Manual Tuning ..................................... 119
Auto-Tuning a NAV Frequency from the MFD............... 122
Marker Beacon Receiver ............................................ 127
DME Tuning ............................................................. 128
4.4 GTX 33 Mode S Transponders .............................. 129
Transponder Controls ................................................ 129
Transponder Mode Selection ...................................... 130
Entering a Transponder Code ..................................... 133
IDENT Function ........................................................ 135
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-03 Rev. Aviii
TABLE OF CONTENTS
4.5 Additional Audio Panel Functions ....................... 136
Power-Up ................................................................. 136
Mono/Stereo Headsets .............................................. 136
Speaker ................................................................... 136
Unmuted Inputs ....................................................... 136
Intercom .................................................................. 137
Passenger Address (PA) System .................................. 138
Simultaneous COM Operation .................................... 138
Clearance Recorder and Player ................................... 139
4.6 Audio Panels Preflight Procedure ....................... 140
4.7 Abnormal Operation ............................................. 142
Stuck Microphone ..................................................... 142
COM Tuning Failure ................................................... 142
PFD Failure, Dual System ...........................................143
Audio Panel Fail-Safe Operation ................................. 144
Reversionary Mode ................................................... 144
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ........................................................... 145
Navigation Status Box ............................................... 146
5.2 Using Map Displays .............................................. 148
Map Orientation ....................................................... 148
Map Range .............................................................. 150
Map Panning ............................................................ 152
Measuring Bearing and Distance ................................ 157
Topography .............................................................. 158
Map Symbols ........................................................... 161
Airways ................................................................... 167
Track Vector ............................................................. 169
Wind Vector ............................................................. 170
Nav Range Ring........................................................ 171
Fuel Range Ring ....................................................... 172
Field of View (SVS) .................................................... 173
Selected Altitude Intercept Arc ................................... 174
5.3 Waypoints .............................................................. 175
Airports ................................................................... 176
Intersections ............................................................ 183
NDBs ....................................................................... 185
VORs ....................................................................... 187
User Waypoints ........................................................ 189
5.4 Airspaces ................................................................ 195
5.5 Direct-to-Navigation ........................................... 200
5.6 Flight Planning ...................................................... 207
Flight Plan Creation .................................................. 208
Adding Waypoints to an Existing Flight Plan ................ 213
Adding Airways to a Flight Plan ................................. 215
Adding Procedures to a Stored Flight Plan .................. 218
Flight Plan Storage ................................................... 225
Flight Plan Editing .................................................... 227
Along Track Offsets ................................................... 231
Parallel Track ............................................................ 232
Activating a Flight Plan Leg ....................................... 235
Inverting a Flight Plan ............................................... 236
Flight Plan Views ...................................................... 237
Closest Point of FPL .................................................. 239
5.7 Vertical Navigation ............................................... 240
Altitude Constraints .................................................. 242
5.8 Procedures ............................................................. 246
Departures ............................................................... 246
Arrivals ................................................................... 249
Approaches ............................................................. 251
5.9 Trip Planning .......................................................... 257
Trip Planning ............................................................ 257
Weight Planning ....................................................... 261
Weight Caution And Warning Conditions .................... 263
5.10 RAIM Prediction .................................................... 264
5.11 Navigating a Flight Plan ....................................... 268
5.12 Abnormal Operation ............................................. 297
SECTION 6 HAZARD AVOIDANCE
6.1 XM WX Satellite Weather ..................................... 300
Activating Services .................................................... 300
Using XM WX Satellite Weather Products .................... 301
Weather Softkeys on the Weather Data Link (XM) Page 305
6.2 GFDS Worldwide Weather .................................... 334
GFDS Weather Data Requests .................................... 342
Worldwide Weather Products ..................................... 346
Abnormal Operations ................................................ 363
6.3 Airborne Color Weather Radar ............................ 365
System Description ................................................... 365
Principles of Pulsed Airborne Weather Radar ............... 365
Safe Operating Distance ............................................ 369
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
ix
TABLE OF CONTENTS
Basic Antenna Tilt Setup ............................................ 370
Practical Application Using the Basic Tilt Setup ............ 370
Weather Mapping and Interpretation ......................... 371
Ground Mapping and Interpretation ........................... 382
6.4 Stormscope ............................................................ 383
Setting Up Stormscope on the Navigation Map ........... 384
Selecting the Stormscope Page .................................. 387
6.5 TAWS-B ................................................................... 389
Displaying TAWS-B Data ............................................ 390
TAWS-B Alerts .......................................................... 394
System Status ........................................................... 400
6.6 Profile View Terrain ............................................... 402
Profile View Display .................................................. 403
6.7 TAWS-A ................................................................... 406
TAWS-A Page ........................................................... 408
TAWS-A Alerts .......................................................... 410
System Status ........................................................... 422
TAWS-A Abnormal Operations ................................... 423
6.8 Traffic Information Service (TIS) .......................... 425
Traffic Map Page ....................................................... 428
TIS Alerts ................................................................. 429
System Status ........................................................... 431
6.9 Garmin GTS Traffic ................................................ 434
Theory of Operation .................................................. 434
Traffic Alerts ............................................................. 437
System Test .............................................................. 438
Operation ................................................................ 439
6.10 L-3 Skywatch Traffic .............................................. 448
TAS Symbology ......................................................... 448
Operation ................................................................ 449
Altitude Display ........................................................ 452
Traffic Map Page Display Range ................................. 452
TAS Alerts ................................................................ 454
System Status ........................................................... 454
6.11 Honeywell KTA 870 Traffic ................................... 456
TAS Symbology ......................................................... 456
Operation ................................................................ 457
Altitude Display ........................................................ 460
Traffic Map Page Display Range ................................. 460
TAS Alerts ................................................................ 462
System Status ........................................................... 463
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview ...................................................... 465
Additional AFCS Controls .......................................... 467
7.2 Flight Director Operation ..................................... 468
Activating the Flight Director ..................................... 468
AFCS Status Box ....................................................... 469
Flight Director Modes ................................................ 470
Switching Flight Directors .......................................... 470
Command Bars ......................................................... 471
Underspeed Protection .............................................. 472
7.3 Vertical Modes ....................................................... 474
Pitch Hold Mode (PIT) ............................................... 475
Selected Altitude Capture Mode (ALTS) ....................... 476
Altitude Hold Mode (ALT) .......................................... 477
Vertical Speed Mode (VS) .......................................... 478
Flight Level Change Mode (FLC) ................................. 479
Vertical Navigation Modes (VPTH, ALTV) ..................... 481
Glidepath Mode (GP) ................................................ 486
Glideslope Mode (GS) ............................................... 488
Takeoff (TO) and Go Around (GA) Modes .................... 489
Level Mode (LVL) ...................................................... 490
7.4 Lateral Modes ........................................................ 491
Roll Hold Mode (ROL) ............................................... 492
Low Bank Mode ....................................................... 492
Heading Select Mode (HDG) ...................................... 493
Navigation Modes (GPS, VOR, LOC) ............................ 494
Approach Modes (GPS, VAPP, LOC) ............................. 496
Backcourse Mode (BC) .............................................. 498
Level Mode (LVL) ...................................................... 499
7.5 Autopilot and Yaw Damper Operation ............... 500
Flight Control ........................................................... 500
Engagement ............................................................. 501
Control Wheel Steering ............................................. 501
Disengagement ........................................................ 502
7.6 Example Flight Plan .............................................. 503
Departure ................................................................ 504
Intercepting a VOR Radial .......................................... 506
Flying a Flight Plan/GPS Course ................................. 507
Descent ................................................................... 508
Approach ................................................................. 514
Go Around/Missed Approach ..................................... 518
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
190-00928-03 Rev. Ax
TABLE OF CONTENTS
7.7 AFCS Annunciations and Alerts ........................... 520
AFCS Status Alerts .................................................... 520
Overspeed Protection ................................................ 521
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ............................. 524
SVS Operation .......................................................... 525
SVS Features ............................................................ 527
Field of View ............................................................ 535
8.2 SafeTaxi .................................................................. 537
SafeTaxi Cycle Number and Revision .......................... 540
8.3 ChartView .............................................................. 543
ChartView Softkeys ................................................... 543
Terminal Procedures Charts ....................................... 544
Chart Options ........................................................... 552
Day/Night View ........................................................ 558
ChartView Cycle Number and Expiration Date ............. 560
8.4 FliteCharts .............................................................. 563
FliteCharts Softkeys .................................................. 563
Terminal Procedures Charts ....................................... 564
Chart Options ........................................................... 571
Day/Night View ........................................................ 575
FliteCharts Cycle Number and Expiration Date ............. 577
8.5 AOPA Airport Directory ........................................ 580
AOPA Database Cycle Number and Revision ............... 581
8.6 Satellite Telephone and Data Link Services ....... 583
Registering with garmin flight data Services ................ 583
Disable/Enable Iridium Transceiver.............................. 586
Telephone Communication ........................................ 587
Text Messaging (SMS) ............................................... 600
System Data Logging ................................................ 616
8.7 SiriusXM Radio Entertainment ............................ 622
Activating SiriusXM Satellite Radio Services ................ 622
Using SiriusXM Radio ................................................ 624
8.8 Scheduler ............................................................... 627
8.9 Flight Data Logging .............................................. 629
8.10 Electronic Stability & Protection (ESP
) ............ 631
Roll Engagement ...................................................... 632
Pitch Engagement..................................................... 634
Angle of Attack Protection ......................................... 635
High Airspeed Protection ........................................... 635
8.11 Abnormal Operation ............................................. 636
SVS Troubleshooting ................................................. 636
Reversionary Mode ................................................... 636
Unusual Attitudes ..................................................... 637
APPENDICES
Annunciations and Alerts ............................................... 641
Alert Level Definitions ............................................... 642
Aircraft Alerts ........................................................... 643
Comparator Annunciations ........................................ 645
Reversionary Sensor Annunciations ............................ 646
G1000 System Annunciations .................................... 646
G1000 System Message Advisories ............................. 649
AFCS Alerts .............................................................. 662
TAWS ALERTS ........................................................... 663
Database Management .................................................. 667
Jeppesen Databases .................................................. 667
Garmin Databases .................................................... 671
Glossary ............................................................................ 677
Frequently Asked Questions .......................................... 685
Map Symbols ................................................................... 689
INDEX
Index .................................................................................. I-1
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the 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
•
GDL 59
Data Link
•
GSR 56
Iridium Transceiver
•
GTS 820/850
Traffic Avoidance System (optional)
•
GMC 710
AFCS Control Unit
•
GA 58
Directional Antenna
•
GTP 59
Outside Air Temperature (OAT) Probe
•
GSA 80
AFCS Servos
•
GSM 85A/GSM 86
Servo Gearboxes
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A/GSM 86).
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.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
2
SYSTEM OVERVIEW
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 SBAS 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.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
3
SYSTEM OVERVIEW
•
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.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
4
SYSTEM OVERVIEW
•
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.
•
GDL 59
(1) – GDL 59 operation is performed with the MFD through the HSDB. Connectivity with the GSR 56
for the Iridium telephone feature is through the RS-232 bus.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
5
SYSTEM OVERVIEW
•
GSR 56
(1) – The Iridium Transceiver operation for voice communication is by means of a telephone handset in
the cabin and pilot and copilot headsets in the cockpit. The tranceiver can also send and receive data provided
by the GDL 59 through the RS-232 bus.
•
GWX 68
(1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A,
via HSDB connection.
•
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.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
6
SYSTEM OVERVIEW
•
GTS 820/850
– The GTS 820 Traffic Advisory System (TAS) and GTS 850 TCAS I use active interrogations of
Mode S and Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control
system.
•
GA 58
– The GA 58 is directional antenna for the Traffic Avoidance System. One top-mounted directional
antenna is required. Optional bottom mounted antenna offers better threat visibility.
•
GA 36
(1) and
GA 37
(1) – The GA 36 is a through-mount GPS/SBAS antenna. The GA 37 is a through-mount
GPS/SBAS antenna with XM/Data Link.
GA 36 GA 37
•
GSA 80
(4), and
GSM 85A/GSM 86
(4) – The GSA 80 servos are used for the automatic control of roll, pitch,
and yaw, and pitch trim. These units interface with each GIA 63W.
The GSM 85A or GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 80 servo
actuator to the mechanical flight-control surface linkage.
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
7
SYSTEM OVERVIEW
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
GDL 69A
GWX68
GCU 477
GRS77#2
GMU44#2
GDC74B #2
GTP59#2
VHF COM
VHF NAV/LOC
GPS/SBAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
VHF COM
VHF NAV/LOC
GPS/SBAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
GSR 56GDL 59
GTS 820/850
Figure 1-1 G1000 System (LRU Configuration)
190-00928-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft 200/B200 Series
8
SYSTEM OVERVIEW
1.3 G1000 CONTROLS
NOTE: The Audio Panel (GMA 1347D) and AFCS controls (GMC 710) are described in the CNS & Audio Panel
and AFCS sections respectively.
The G1000 system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and
audio panel. The controls for the PFD and MFD are discussed within the following pages of this section.
PFD CONTROLS
Figure 1-2 PFD Controls
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Garmin G1000: Beechcraft King Air 200/B200 User guide

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