Garmin G1000 - Beechcraft King Air C90A/C90GT/C90GTi Reference guide

Type
Reference guide

This manual is also suitable for

Beechcraft C90A/GT/GTi
G1000
®
Integrated Avionics System
Pilot’s Guide
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
Copyright © 2008, 2009, 2012, 2014 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0636.06 or later for the Beechcraft C90A/GT/GTi. Some differences in
operation may be observed when comparing the information in this manual to earlier or later software versions.
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Tel: 913/397.8200 Fax: 913/397.8282
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For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
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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
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®
is a registered trademark of Jeppesen, Inc. SiriusXM Weather and SiriusXM Satellite Radio are provided
by SiriusXM Satellite Radio, 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
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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.
December 2014 Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-03 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 74 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: 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: 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 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: 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 significantly older than the indicated weather product age.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING:
The Garmin system, 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.
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: Do not use the system to attempt to penetrate a thunderstorm. The illustrations in this guide are
only examples. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding any thunderstorm identified as severe of giving intense radar echo by
at least 20 miles.
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 system within the following
areas could result in loss of reliable attitude and heading indications (GRS 77 installations only). 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
:
Because of variation in the earth’s magnetic field, operating the system within the following
areas could result in loss of reliable attitude and heading indications (GRS 7800 installations only). North
of 84° North latitude at all longitudes; South of 70° South latitude at all longitudes; South of 55° South
latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand)
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.
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-03 Rev. Aiv
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.
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: 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 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.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
v
WARNINGS, CAUTIONS, AND NOTES
NOTE
: When operating the G1000 in DG Free Mode (GRS 7800 installations only), the heading information
used by some system components (e.g. GTS 8000, AFCS, and GWX) will be different from the heading
displayed on the GDU by an amount equal to the difference between the current Magnetic Field Variation
Database (MV DB) value, and the MV DB value when DG Free Mode was activated. Due to the convergence
of isogonic lines, this condition is most noticeable at or near the North and South poles.
NOTE
: System navigation utilities may not reliably calculate range and bearing information when the
aircraft is operating north of 80° North latitude or south of 80° South latitude. This may result in the system
displaying small gaps in racetrack holding pattern depictions (GRS 7800 installations only).
NOTE
: The Terrain Awareness and Warning System (TAWS) may not operate reliably north of 89º North
latitude and south of 89º South latitude. This is due to limitations present within the Terrain database and
the system’s ability to process the data representing the affected areas (GRS 7800 installations only).
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 ‘Report An Aviation Data Error Report.’
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-03 Rev. Avi
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00663-00 A 9/21/07 i – I-6 Initial Release at GDU SW 8.10
190-00663-01 A 3/11/09 i – I-6 Initial Release
- Added SVS
- Updated to GDU SW 9.14
- Added optional ADS-B
- Added Audio Panel with Cabin Button
190-00663-02 A 10/25/12 i – I-6 Initial Release for GDU SW 12.03
- Added ESP
- Updated to GDU SW 12.03
190-00663-02 B 10/31/12 i – I-6 Added VNAV Note and explanatory paragraphs on page 234
190-00663-03 A 12/8/14 i – I-6 Initial Release for GDU SW 13.09
- Added optional GRS 7800
- Replaced GWX 68 with GWX 70
- Updated to GDU SW 13.08
- Added pilot profile import/export
- Added user-defined holding patterns
- Added temperature compensated minimums
- Added RNAV LP approach service level
- Added AC-U-KWIK airport directory
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
vii
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 ............................................................ 10
Audio Panel Controls .................................................. 12
1.4 Secure Digital Cards.............................................. 14
1.5 System Power-up ................................................... 15
1.6 System Operation .................................................. 16
Normal Operation ....................................................... 16
Reversionary Mode ..................................................... 17
AHRS Operation ......................................................... 18
G1000 System Annunciations ...................................... 21
Softkey Function ......................................................... 21
GPS Receiver Operation .............................................. 28
1.7 Accessing G1000 Functionality............................ 33
Menus ....................................................................... 33
MFD Page Groups ....................................................... 33
MFD System Pages...................................................... 37
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) ....................................... 63
Vertical Deviation ....................................................... 64
Horizontal Situation Indicator (HSI) .............................. 65
Course Deviation Indicator (CDI) .................................. 71
2.2 Supplemental Flight Data .................................... 79
Temperature Displays .................................................. 79
Wind Data ................................................................. 80
Vertical Navigation (VNV) Indications ........................... 81
2.3 PFD Annunciations and Alerting Functions ........ 82
G1000 Alerting system ................................................ 82
Marker Beacon Annunciations...................................... 83
Traffic Annunciation .................................................... 84
TAWS Annunciations ................................................... 84
Altitude Alerting ......................................................... 85
Low Altitude Annunciation .......................................... 85
Minimum Descent Altitude/Decision Height Alerting ...... 86
2.4 Abnormal Operations ........................................... 88
Abnormal GPS Conditions ........................................... 88
GRS 7800 Directional Gyro (DG) Modes ........................ 89
Unusual Attitudes ....................................................... 90
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display .............................................................. 94
Interstage Turbine Temperature .................................... 96
Torque ....................................................................... 96
Tachometer (rpm) ....................................................... 97
Turbine Speed ............................................................ 98
Fuel Flow ................................................................... 98
Oil Pressure ................................................................ 99
Oil Temperature .......................................................... 99
3.2 EIS Display in Reversionary Mode ..................... 100
Reversionary Display ................................................. 101
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 103
Audio Panel Volume Control ...................................... 103
PFD Controls and Frequency Display ........................... 104
Audio Panel Controls ................................................ 106
4.2 COM Operation .................................................... 108
COM Transceiver Selection and Activation ................... 108
COM Transceiver Manual Tuning ................................ 109
Quick-Tuning and Activating 121.500 MHz .................. 110
Auto-Tuning the COM Frequency ................................ 111
Frequency Spacing .................................................... 115
Automatic Squelch .................................................... 116
Volume .................................................................... 116
4.3 NAV Operation ..................................................... 117
NAV Radio Selection and Activation ........................... 117
NAV Receiver Manual Tuning ..................................... 118
Auto-Tuning a NAV Frequency from the MFD............... 120
Marker Beacon Receiver ............................................ 125
DME Tuning ............................................................. 126
4.4 GTX 33 Mode S Transponders ............................ 127
Transponder Controls ................................................ 127
Transponder Mode Selection ...................................... 128
Entering a Transponder Code ..................................... 130
IDENT Function ........................................................ 132
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-03 Rev. Aviii
TABLE OF CONTENTS
4.5 Additional Audio Panel Functions ..................... 133
Power-Up ................................................................. 133
Mono/Stereo Headsets .............................................. 133
Speaker ................................................................... 133
Unmuted Inputs ....................................................... 133
Intercom .................................................................. 134
Passenger Address (PA) System .................................. 135
Simultaneous COM Operation .................................... 135
Clearance Recorder and Player ................................... 136
4.6 Audio Panels Preflight Procedure ......................137
4.7 Abnormal Operation ........................................... 139
Stuck Microphone ..................................................... 139
COM Tuning Failure ................................................... 139
PFD Failure, Dual System ........................................... 140
Audio Panel Fail-Safe Operation ................................. 141
Reversionary Mode ................................................... 141
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 143
Navigation Status Box ............................................... 144
5.2 Using Map Displays ............................................. 146
Map Orientation ....................................................... 146
Map Range .............................................................. 148
Map Panning ............................................................ 150
Measuring Bearing and Distance ................................ 155
Topography .............................................................. 156
Map Symbols ........................................................... 159
Airways ................................................................... 165
Track Vector ............................................................. 167
Wind Vector ............................................................. 168
Nav Range Ring........................................................ 169
Fuel Range Ring ....................................................... 170
Field of View (SVT) .................................................... 171
Selected Altitude Intercept Arc ................................... 172
5.3 Waypoints ............................................................. 173
Airports ................................................................... 174
Intersections ............................................................ 181
NDBs ....................................................................... 183
VORs ....................................................................... 185
User Waypoints ........................................................ 187
5.4 Airspaces .............................................................. 193
5.5 Direct-to-Navigation .......................................... 198
5.6 Flight Planning ..................................................... 204
Flight Plan Creation .................................................. 205
Adding Waypoints to an Existing Flight Plan ................210
Adding Airways to a Flight Plan ................................. 212
Adding Procedures to a Stored Flight Plan .................. 215
Flight Plan Storage ................................................... 222
Flight Plan Editing .................................................... 224
Along Track Offsets ................................................... 228
Parallel Track ............................................................ 229
Activating a Flight Plan Leg ....................................... 232
Inverting a Flight Plan ............................................... 233
Flight Plan Views ...................................................... 234
Closest Point of FPL .................................................. 237
User-Defined Holding Patterns ................................... 237
5.7 Vertical Navigation ............................................. 242
Altitude Constraints .................................................. 244
5.8 Procedures ...........................................................248
Departures ............................................................... 249
Arrivals ................................................................... 252
Approaches ............................................................. 255
5.9 Trip Planning ........................................................ 264
Trip Planning ............................................................ 264
Weight Planning ....................................................... 268
Weight Caution And Warning Conditions .................... 270
5.10 RAIM Prediction................................................... 271
5.11 Navigating a Flight Plan ..................................... 275
5.12 Abnormal Operation ........................................... 304
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 308
Activating Services .................................................... 308
Using SiriusXM Weather Products .............................. 309
Weather Softkeys on the Weather Data Link (XM) Page 313
6.2 Airborne Color Weather Radar .......................... 342
System Description ................................................... 342
Principles of Pulsed Airborne Weather Radar ............... 342
Safe Operating Distance ............................................ 346
Basic Antenna Tilt Setup ............................................ 347
Practical Application Using the Basic Tilt Setup ............ 347
Weather Mapping and Interpretation ......................... 348
Ground Mapping and Interpretation ........................... 360
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
ix
TABLE OF CONTENTS
6.3 Stormscope .......................................................... 361
Setting Up Stormscope on the Navigation Map ........... 362
Selecting the Stormscope Page .................................. 365
6.4 TAWS-B ................................................................. 367
Displaying TAWS-B Data ............................................ 368
TAWS-B Alerts .......................................................... 372
System Status ........................................................... 378
6.5 Profile View Terrain ............................................. 380
Profile View Display .................................................. 381
6.6 Traffic Information Service (TIS) ........................ 384
Traffic Map Page ....................................................... 387
TIS Alerts ................................................................. 388
System Status ........................................................... 390
6.7 L-3 Skywatch Traffic ............................................ 393
TAS Symbology ......................................................... 393
Operation ................................................................ 394
Altitude Display ........................................................ 397
Traffic Map Page Display Range ................................. 397
TAS Alerts ................................................................ 399
System Status ........................................................... 399
6.8 Honeywell KTA 870 Traffic .................................. 401
TAS Symbology ......................................................... 401
Operation ................................................................ 402
Altitude Display ........................................................ 405
Traffic Map Page Display Range ................................. 405
TAS Alerts ................................................................ 407
System Status ........................................................... 408
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................... 409
Additional AFCS Controls .......................................... 411
Basic Autopilot Operation .......................................... 412
7.2 Flight Director Operation ................................... 413
Activating the Flight Director ..................................... 413
AFCS Status Box ....................................................... 414
Flight Director Modes ................................................ 415
Switching Flight Directors .......................................... 415
Command Bars ......................................................... 416
Underspeed Protection .............................................. 417
7.3 Vertical Modes ..................................................... 419
Pitch Hold Mode (PIT) ............................................... 420
Selected Altitude Capture Mode (ALTS) ....................... 421
Altitude Hold Mode (ALT) .......................................... 422
Vertical Speed Mode (VS) .......................................... 423
Flight Level Change Mode (FLC) ................................. 424
Vertical Navigation Modes (VPTH, ALTV) ..................... 426
Glidepath Mode (GP) ................................................ 431
Glideslope Mode (GS) ............................................... 433
Takeoff (TO) and Go Around (GA) Modes .................... 434
Level Mode (LVL) ...................................................... 435
7.4 Lateral Modes ...................................................... 436
Roll Hold Mode (ROL) ............................................... 437
Low Bank Mode ....................................................... 437
Heading Select Mode (HDG) ...................................... 438
Navigation Modes (GPS, VOR, LOC) ............................ 439
Approach Modes (GPS, VAPP, LOC) ............................. 441
Backcourse Mode (BC) .............................................. 442
Level Mode (LVL) ...................................................... 443
7.5 Autopilot and Yaw Damper Operation ............. 444
Flight Control ........................................................... 444
Engagement ............................................................. 445
Control Wheel Steering ............................................. 445
Disengagement ........................................................ 446
7.6 Example Flight Plan ............................................ 447
Departure ................................................................ 448
Intercepting a VOR Radial .......................................... 450
Flying a Flight Plan/GPS Course ................................. 451
Descent ................................................................... 452
Approach ................................................................. 455
Go Around/Missed Approach ..................................... 458
7.7 AFCS Annunciations and Alerts ......................... 460
AFCS Status Alerts .................................................... 460
Overspeed Protection ................................................ 461
7.8 Abnormal Operation ........................................... 462
Suspected Autopilot Malfunction ............................... 462
Overpowering Autopilot Servos .................................. 462
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology ............................... 464
SVT Operation .......................................................... 465
SVT Features ............................................................ 467
Field of View ............................................................ 476
8.2 SafeTaxi ................................................................ 478
SafeTaxi Cycle Number and Revision .......................... 481
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-03 Rev. Ax
TABLE OF CONTENTS
8.3 ChartView ............................................................. 484
ChartView Softkeys ................................................... 485
Terminal Procedures Charts ....................................... 486
Chart Options ........................................................... 494
Day/Night View ........................................................ 500
ChartView Cycle Number and Expiration Date ............. 502
8.4 FliteCharts ............................................................ 505
FliteCharts Softkeys .................................................. 506
Terminal Procedures Charts ....................................... 507
Chart Options ........................................................... 514
Day/Night View ........................................................ 518
FliteCharts Cycle Number and Expiration Date ............. 520
8.5 Airport Directory ................................................. 523
Airport Directory Database Cycle Number and Revision 524
8.6 SiriusXM Satellite Radio ..................................... 526
Activating SiriusXM Satellite Radio Services ................ 526
Using SiriusXM Satellite Radio ................................... 528
8.7 Electronic Stability and Protection (ESP
) ....... 531
Roll Engagement ...................................................... 532
Pitch Engagement..................................................... 533
High Airspeed Protection ........................................... 534
8.8 Scheduler .............................................................. 535
8.9 Flight Data Logging ............................................ 537
8.10 Abnormal Operation ........................................... 539
SVT Troubleshooting ................................................. 539
Reversionary Mode ................................................... 539
Unusual Attitudes ..................................................... 540
APPENDICES
Annunciations and Alerts ............................................. 543
Comparator Annunciations ........................................ 546
Reversionary Sensor Annunciations ............................ 547
G1000 System Annunciations .................................... 547
G1000 System Message Advisories ............................. 550
AFCS Alerts .............................................................. 563
Terrain-SVS Alerts ..................................................... 564
Terrain-SVS Status Annunciations ............................... 564
TAWS-B ALERTS ........................................................ 565
TAWS-B System Status Annunciations ......................... 566
Flight Plan Import/Export Messages ........................... 567
Pilot Profile Import/Export Messages .......................... 568
Database Management ................................................ 569
Jeppesen Databases .................................................. 570
Garmin Databases .................................................... 574
Frequently Asked Questions ........................................ 589
Map Symbols ................................................................. 593
INDEX
Index ................................................................................ I-1
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
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 C90A/
GT/GTi. 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 77/7800
Attitude and Heading Reference
System (AHRS)(GRS 7800 is optional)
GMU 44
Magnetometer
GMA 1347D/1347D-20
Dual Audio System with
Integrated Marker Beacon Receiver
GTX 33/33(ES)
Extended Squitter Mode S
Transponder
GDL 69A
Satellite Data Link Receiver
GWX 70
Weather Radar
GCU 475
MFD Control Unit
GMC 710
AFCS Control Unit
GTP 59
Outside Air Temperature (OAT) Probe
GSA 80/81
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 Garmin AFCS.
In the Beechcraft C90A/GT/GTi, the Garmin Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
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.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
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 77/7800, 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 77/7800
(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 77/7800 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 77/7800 for processing to determine
aircraft magnetic heading. This unit receives power directly from the GRS 77/7800 and communicates with the
GRS 77/7800, using an RS-485 digital interface.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
4
SYSTEM OVERVIEW
GMA 1347D/1347D-20
(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 33/33(ES)
(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 70
(1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A,
via HSDB connection.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
5
SYSTEM OVERVIEW
GCU 475
(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 Garmin AFCS through an RS-232 digital interface allowing
communication with both PFDs.
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.
GSA 80
(3),
GSA 81
(1), and
GSM 85A
(4) – The GSA 80 servos are used for the automatic control of roll,
pitch, and yaw. The GSA 81 servo is used for the automatic control of pitch trim. These units interface with
each GIA 63W.
The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator
to the mechanical flight-control surface linkage.
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
6
SYSTEM OVERVIEW
GDU 1040A
(PFD #1)
GDU 1040A
(PFD #2)
GDU1500
(MFD)
GIA63W #2
GSA80
(Yaw)
GSA80
(Roll)
GSA 80
(Pitch)
GSA 81
(Pitch Trim)
GRS 77/7800
#1
GIA 63W #1
GMC710
GMU44#1
GEA71#2
GEA71#1
GDC 74B #1
GTP59#1
GMA 1347D/
GMA 1347D-20
#2
GMA 1347D/
GMA 1347D-20
#1
GTX 33/33ES GTX 33/33ES
GCU 475GWX 70
GDL 69A
GRS 77/7800
#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
Figure 1-1 G1000 System (LRU Configuration)
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
7
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
21 5
4
6
8
7
3
11
12
10
9
15
14
13
190-00663-03 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
8
SYSTEM OVERVIEW
The following list provides an overview of the controls located on the PFD bezel (see Figure 1-2).
1
NAV VOL/ID Knob
– Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON
and OFF. Volume level is shown in the NAV frequency field as a percentage.
2
NAV Frequency Transfer Key
– Toggles the standby and active NAV frequencies.
3
Dual
NAV Knob
– Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for
kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2.
4
Joystick
– Changes the map range when rotated. Activates the map pointer when pressed.
5
BARO Knob
– Sets the altimeter barometric pressure. Press to enter standard pressure (29.92).
6
Dual COM Knob
– Tunes the standby frequencies for the COM transceiver (large knob for MHz; small
knob for kHz). Press to switch the tuning box (cyan box) between COM1 and COM2.
7
COM Frequency Transfer Key
– Toggles the standby and active COM frequencies. Press and hold this
key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency
field.
8
COM
VOL/SQ Knob
– Controls COM audio volume level. Volume level is shown in the COM frequency
field as a percentage. Press to turn the COM automatic squelch ON and OFF.
9
Direct-to Key ( )
– Allows the user to enter a destination waypoint and establish a direct course to the
selected destination (the destination is either specified by the identifier, chosen from the active route, or
taken from the map pointer position).
10
FPL Key
– Displays the active Flight Plan Page for creating and editing the active flight plan.
11
CLR
Key
– Erases information, cancels entries, or removes page menus. Pressing and holding this key
displays the Navigation Map Page automatically.
12
Dual FMS Knob
– Flight Management System Knob. Press the
FMS
Knob to turn the selection cursor
ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small
and large
knobs. The large
knob moves the cursor on the page, while the small
knob selects individual
characters for the highlighted cursor location.
13
MENU Key
– Displays a context-sensitive list of options. This list allows the user to access additional
features or make setting changes that relate to particular pages.
14
PROC Key
– Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach
procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or
arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan.
If a flight plan is not used, both the desired airport and the desired procedure may be selected.
15
ENT Key
– Validates or confirms a menu selection or data entry.
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Garmin G1000 - Beechcraft King Air C90A/C90GT/C90GTi Reference guide

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