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
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
Copyright © 2005-2017 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0636.07 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.
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, G1000
®
, WATCH
®
, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin
ESP
, and Garmin SVT
are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the
express permission of Garmin.
Skywatch
®
and Stormscope
®
are registered trademarks of L-3 Communications. Ryan
®
, TCAD
®
and Avidyne
®
are registered trademarks of
Avidyne Corporation. AC-U-KWIK
®
is a registered trademark of Penton Business Media Inc. Bendix/King
®
and Honeywell
®
are registered
trademarks of Honeywell International, Inc. Becker
®
is a registered trademark of Becker Flugfunkwerk GmbH. NavData
®
is a registered
trademark of Jeppesen, Inc.; Sirius, XM, and all related marks and logos are trademarks of Sirius XM Radio, Inc. and its subsidiaries. .
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.
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-04 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
Printed in the U.S.A.
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation
from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot
independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical
information. Displayed aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap
data is intended only to supplement other approved navigation data sources and should be considered only
an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be older than the indicated weather product age.
WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied
upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: Always obtain qualified instruction prior to operational use of this equipment.
WARNING
:
Do not use a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-04 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.
WARNING: When using the autopilot to fly an approach with vertical guidance, the autopilot will not level
the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING
:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications in the following geographic areas: North of 72° North latitude at all longitudes; South
of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W.
(Northern Canada); North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada);
North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South
latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).
WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous
weather avoidance. Range limitations and interference may cause the system to display inaccurate or
incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
WARNING:
Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.
Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or
reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
WARNING:
Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may
appear as a partial symbol.
WARNING:
Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of
the aircraft to the runway or for maintaining the proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within
the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of
precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color
not representative of the true intensity.
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
v
WARNINGS, CAUTIONS, AND NOTES
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION:
Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or
modifications could void both the warranty and affect the airworthiness of the aircraft.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the system panel
and displays, are subject to change and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System and is solely responsible for
its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
NOTE
: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE
: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards
away from the source of the interference should alleviate the condition.
NOTE
: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE
: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields
can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut
down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no
comparison is possible.
NOTE: The system responds to a terminal procedure based on data coded within that procedure in the
Navigation Database. Differences in system operation may be observed among similar types of procedures
due to differences in the Navigation Database coding specific to each procedure.
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-04 Rev. Avi
REVISION INFORMATION
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen that have a Type 2 Letter of Authorization (LOA) from the FAA are assured
compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable
database and can be viewed at http://fly.garmin.com by selecting Aviation Database Declarations.
Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with
established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established
AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE
: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in
SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at
www.flygarmin.com by selecting ‘Database Exclusions List.
NOTE
: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their
impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by
selecting ‘Aviation Database Alerts.
NOTE
: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to FlyGarmin.com and select Aviation Data Error Report’.
NOTE: Lamp(s) inside this product 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
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: Operate G1000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
NOTE: The system supports approval of AC 120-76C Hardware Class 3, Software Type B Electronic Flight Bag
(EFB) electronic aeronautical chart applications. Possible additional requirements may make a secondary
source (traditional paper or additional electronic display) necessary onboard the aircraft. If the secondary
source is a Portable Electronic Device (PED), its use must be consistent with guidance in AC 120-76C.
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
vii
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
190-00663-04 A 2/21/16 i – I-6 Initial Release for GDU SW 13.31
- Added optional GTX 33D
- Added optional GDL 69A SXM
- Added
auto-nomination of arrival and approach altitude constraints
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-04 Rev. Aviii
REVISION INFORMATION
Blank Page
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
ix
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 ......................................................... 22
GPS Receiver Operation .............................................. 28
1.7 Accessing G1000 Functionality............................ 33
Menus ....................................................................... 33
MFD Page Groups ....................................................... 34
MFD System Pages...................................................... 38
1.8 Display Backlighting ............................................. 54
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 58
Airspeed Indicator ...................................................... 58
Attitude Indicator ....................................................... 61
Altimeter ................................................................... 63
Vertical Speed Indicator (VSI) ....................................... 65
Horizontal Situation Indicator (HSI) .............................. 67
GRS 7800 Directional Gyro (DG) Modes ........................ 71
Course Deviation Indicator (CDI) .................................. 74
2.2 Supplemental Flight Data .................................... 82
Temperature Displays .................................................. 82
Wind Data ................................................................. 83
Vertical Navigation (VNV) Indications ........................... 84
2.3 PFD Annunciations and Alerting Functions ........ 85
G1000 Alerting system ................................................ 85
Marker Beacon Annunciations...................................... 86
Traffic Annunciation .................................................... 87
TAWS Annunciations ................................................... 88
Altitude Alerting ......................................................... 88
Low Altitude Annunciation .......................................... 89
Minimum Descent Altitude/Decision Height Alerting ...... 89
2.4 Abnormal Operations ........................................... 91
Abnormal GPS Conditions ........................................... 91
Unusual Attitudes ....................................................... 92
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
190-00663-04 Rev. Ax
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 ................................................................... 166
Track Vector ............................................................. 168
Wind Vector ............................................................. 169
Nav Range Ring........................................................ 170
Fuel Range Ring ....................................................... 171
Field of View (SVT) .................................................... 172
Selected Altitude Intercept Arc ................................... 173
5.3 Waypoints ............................................................. 174
Airports ................................................................... 175
Intersections ............................................................ 182
NDBs ....................................................................... 184
VORs ....................................................................... 186
User Waypoints ........................................................ 188
5.4 Airspaces .............................................................. 194
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 .................. 216
Flight Plan Storage ................................................... 223
Flight Plan Editing .................................................... 225
Along Track Offsets ................................................... 229
Parallel Track ............................................................ 230
Activating a Flight Plan Leg ....................................... 233
Inverting a Flight Plan ............................................... 234
Flight Plan Views ...................................................... 235
Closest Point of FPL .................................................. 237
User-Defined Holding Patterns ................................... 238
5.7 Vertical Navigation ............................................. 243
Altitude Constraints .................................................. 245
5.8 Procedures ...........................................................249
Departures ............................................................... 250
Arrivals ................................................................... 253
Approaches ............................................................. 256
5.9 Trip Planning ........................................................ 265
Trip Planning ............................................................ 265
Weight Planning ....................................................... 269
Weight Caution And Warning Conditions .................... 271
5.10 RAIM Prediction................................................... 272
5.11 Navigating a Flight Plan ..................................... 276
5.12 Abnormal Operation ........................................... 305
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 ............................................ 346
Practical Application Using the Basic Tilt Setup ............ 346
Weather Mapping and Interpretation ......................... 347
Ground Mapping and Interpretation ........................... 358
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
xi
TABLE OF CONTENTS
6.3 Stormscope .......................................................... 359
Setting Up Stormscope on the Navigation Map ........... 360
Selecting the Stormscope Page .................................. 363
6.4 TAWS-B ................................................................. 365
Displaying TAWS-B Data ............................................ 366
TAWS-B Alerts .......................................................... 370
System Status ........................................................... 376
6.5 Profile View Terrain ............................................. 378
Profile View Display .................................................. 379
6.6 Traffic Information Service (TIS) ........................ 382
Traffic Map Page ....................................................... 385
TIS Alerts ................................................................. 386
System Status ........................................................... 388
6.7 L-3 Skywatch Traffic ............................................ 390
TAS Symbology ......................................................... 390
Operation ................................................................ 391
Altitude Display ........................................................ 394
Traffic Map Page Display Range ................................. 394
TAS Alerts ................................................................ 396
System Status ........................................................... 396
6.8 Honeywell KTA 870 Traffic .................................. 398
TAS Symbology ......................................................... 398
Operation ................................................................ 399
Altitude Display ........................................................ 402
Traffic Map Page Display Range ................................. 402
TAS Alerts ................................................................ 404
System Status ........................................................... 405
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................... 407
Additional AFCS Controls .......................................... 409
Basic Autopilot Operation .......................................... 410
7.2 Flight Director Operation ................................... 411
Activating the Flight Director ..................................... 411
AFCS Status Box ....................................................... 412
Flight Director Modes ................................................ 413
Switching Flight Directors .......................................... 413
Command Bars ......................................................... 414
Underspeed Protection .............................................. 415
7.3 Vertical Modes ..................................................... 417
Pitch Hold Mode (PIT) ............................................... 418
Selected Altitude Capture Mode (ALTS) ....................... 419
Altitude Hold Mode (ALT) .......................................... 420
Vertical Speed Mode (VS) .......................................... 421
Flight Level Change Mode (FLC) ................................. 422
Vertical Navigation Modes (VPTH, ALTV) ..................... 424
Glidepath Mode (GP) ................................................ 429
Glideslope Mode (GS) ............................................... 431
Takeoff (TO) and Go Around (GA) Modes .................... 432
Level Mode (LVL) ...................................................... 433
7.4 Lateral Modes ...................................................... 434
Roll Hold Mode (ROL) ............................................... 435
Low Bank Mode ....................................................... 435
Heading Select Mode (HDG) ...................................... 436
Navigation Modes (GPS, VOR, LOC) ............................ 437
Approach Modes (GPS, VAPP, LOC) ............................. 439
Backcourse Mode (BC) .............................................. 440
Level Mode (LVL) ...................................................... 441
7.5 Autopilot and Yaw Damper Operation ............. 442
Flight Control ........................................................... 442
Engagement ............................................................. 443
Control Wheel Steering ............................................. 443
Disengagement ........................................................ 444
7.6 Example Flight Plan ............................................ 445
Departure ................................................................ 446
Intercepting a VOR Radial .......................................... 448
Flying a Flight Plan/GPS Course ................................. 449
Descent ................................................................... 450
Approach ................................................................. 453
Go Around/Missed Approach ..................................... 456
7.7 AFCS Annunciations and Alerts ......................... 458
AFCS Status Alerts .................................................... 458
Overspeed Protection ................................................ 459
7.8 Abnormal Operation ........................................... 460
Suspected Autopilot Malfunction ............................... 460
Overpowering Autopilot Servos .................................. 460
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology ............................... 462
SVT Operation .......................................................... 463
SVT Features ............................................................ 465
Field of View ............................................................ 474
8.2 SafeTaxi ................................................................ 476
SafeTaxi Cycle Number and Revision .......................... 479
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
190-00663-04 Rev. Axii
TABLE OF CONTENTS
8.3 ChartView ............................................................. 482
ChartView Softkeys ................................................... 483
Terminal Procedures Charts ....................................... 484
Chart Options ........................................................... 492
Day/Night View ........................................................ 498
ChartView Cycle Number and Expiration Date ............. 500
8.4 FliteCharts ............................................................ 503
FliteCharts Softkeys .................................................. 504
Terminal Procedures Charts ....................................... 505
Chart Options ........................................................... 512
Day/Night View ........................................................ 516
FliteCharts Cycle Number and Expiration Date ............. 518
8.5 Airport Directory ................................................. 521
Airport Directory Database Cycle Number and Revision 522
8.6 SiriusXM Satellite Radio ..................................... 524
Activating SiriusXM Satellite Radio Services ................ 524
Using SiriusXM Satellite Radio ................................... 526
8.7 Electronic Stability and Protection (ESP
) ....... 529
Roll Engagement ...................................................... 530
Pitch Engagement..................................................... 531
High Airspeed Protection ........................................... 532
8.8 Scheduler .............................................................. 533
8.9 Flight Data Logging ............................................ 535
8.10 Abnormal Operation ........................................... 537
SVT Troubleshooting ................................................. 537
Reversionary Mode ................................................... 537
Unusual Attitudes ..................................................... 538
APPENDICES
Annunciations and Alerts ............................................. 541
Comparator Annunciations ........................................ 544
Reversionary Sensor Annunciations ............................ 545
System Annunciations ............................................... 545
System Message Advisories ....................................... 548
AFCS Alerts .............................................................. 562
Terrain-SVS Alerts ..................................................... 563
Terrain-SVS Status Annunciations ............................... 563
TAWS-B ALERTS ........................................................ 564
TAWS-B System Status Annunciations ......................... 565
Flight Plan Import/Export Messages ........................... 566
Pilot Profile Import/Export Messages .......................... 566
Database Management ................................................ 567
Navigation Databases ............................................... 568
Garmin Databases/Jeppesen Chartview Database ........ 572
Frequently Asked Questions ........................................ 589
Map Symbols ................................................................. 593
INDEX
Index ................................................................................ I-1
190-00663-04 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 Avionics System as installed in the Beechcraft
C90A/GT/GTi. The 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)/33D
Extended Squitter Mode S
Transponder
GDL 69A/69A SXM
Satellite Data Link Receiver
GWX 68/70
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/86
Servo Gearboxes
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A/86).
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.
190-00663-04 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.
190-00663-04 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.
190-00663-04 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)/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/69A SXM
(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. It communicates
with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the
GDL 69A/69A SXM capability.
GWX 68/70
(1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL
69A/69A SXM, via HSDB connection.
190-00663-04 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/86
(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/86 servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo
actuator to the mechanical flight-control surface linkage.
190-00663-04 Rev. A
Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi
6
SYSTEM OVERVIEW
GDU 1040A
(PFD #1)
GDU1040A
(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
GDC74B #1
GTP59#1
GMA 1347D/
GMA 1347D-20
#2
GMA 1347D/
GMA 1347D-20
#1
GTX 33/33(ES)/
GTX 33D
GCU 475
GWX 68/70
GDL 69A/
GDL 69A SXM
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
GTX 33/33(ES)/
GTX 33D #1
GTX 33/33(ES)/
GTX 33D
GTX 33/33(ES)/
GTX 33D #2
Figure 1-1 G1000 System (LRU Configuration)
  • Page 1 1
  • Page 2 2
  • Page 3 3
  • Page 4 4
  • Page 5 5
  • Page 6 6
  • Page 7 7
  • Page 8 8
  • Page 9 9
  • Page 10 10
  • Page 11 11
  • Page 12 12
  • Page 13 13
  • Page 14 14
  • Page 15 15
  • Page 16 16
  • Page 17 17
  • Page 18 18
  • Page 19 19
  • Page 20 20
  • Page 21 21
  • Page 22 22
  • Page 23 23
  • Page 24 24
  • Page 25 25
  • Page 26 26
  • Page 27 27
  • Page 28 28
  • Page 29 29
  • Page 30 30
  • Page 31 31
  • Page 32 32
  • Page 33 33
  • Page 34 34
  • Page 35 35
  • Page 36 36
  • Page 37 37
  • Page 38 38
  • Page 39 39
  • Page 40 40
  • Page 41 41
  • Page 42 42
  • Page 43 43
  • Page 44 44
  • Page 45 45
  • Page 46 46
  • Page 47 47
  • Page 48 48
  • Page 49 49
  • Page 50 50
  • Page 51 51
  • Page 52 52
  • Page 53 53
  • Page 54 54
  • Page 55 55
  • Page 56 56
  • Page 57 57
  • Page 58 58
  • Page 59 59
  • Page 60 60
  • Page 61 61
  • Page 62 62
  • Page 63 63
  • Page 64 64
  • Page 65 65
  • Page 66 66
  • Page 67 67
  • Page 68 68
  • Page 69 69
  • Page 70 70
  • Page 71 71
  • Page 72 72
  • Page 73 73
  • Page 74 74
  • Page 75 75
  • Page 76 76
  • Page 77 77
  • Page 78 78
  • Page 79 79
  • Page 80 80
  • Page 81 81
  • Page 82 82
  • Page 83 83
  • Page 84 84
  • Page 85 85
  • Page 86 86
  • Page 87 87
  • Page 88 88
  • Page 89 89
  • Page 90 90
  • Page 91 91
  • Page 92 92
  • Page 93 93
  • Page 94 94
  • Page 95 95
  • Page 96 96
  • Page 97 97
  • Page 98 98
  • Page 99 99
  • Page 100 100
  • Page 101 101
  • Page 102 102
  • Page 103 103
  • Page 104 104
  • Page 105 105
  • Page 106 106
  • Page 107 107
  • Page 108 108
  • Page 109 109
  • Page 110 110
  • Page 111 111
  • Page 112 112
  • Page 113 113
  • Page 114 114
  • Page 115 115
  • Page 116 116
  • Page 117 117
  • Page 118 118
  • Page 119 119
  • Page 120 120
  • Page 121 121
  • Page 122 122
  • Page 123 123
  • Page 124 124
  • Page 125 125
  • Page 126 126
  • Page 127 127
  • Page 128 128
  • Page 129 129
  • Page 130 130
  • Page 131 131
  • Page 132 132
  • Page 133 133
  • Page 134 134
  • Page 135 135
  • Page 136 136
  • Page 137 137
  • Page 138 138
  • Page 139 139
  • Page 140 140
  • Page 141 141
  • Page 142 142
  • Page 143 143
  • Page 144 144
  • Page 145 145
  • Page 146 146
  • Page 147 147
  • Page 148 148
  • Page 149 149
  • Page 150 150
  • Page 151 151
  • Page 152 152
  • Page 153 153
  • Page 154 154
  • Page 155 155
  • Page 156 156
  • Page 157 157
  • Page 158 158
  • Page 159 159
  • Page 160 160
  • Page 161 161
  • Page 162 162
  • Page 163 163
  • Page 164 164
  • Page 165 165
  • Page 166 166
  • Page 167 167
  • Page 168 168
  • Page 169 169
  • Page 170 170
  • Page 171 171
  • Page 172 172
  • Page 173 173
  • Page 174 174
  • Page 175 175
  • Page 176 176
  • Page 177 177
  • Page 178 178
  • Page 179 179
  • Page 180 180
  • Page 181 181
  • Page 182 182
  • Page 183 183
  • Page 184 184
  • Page 185 185
  • Page 186 186
  • Page 187 187
  • Page 188 188
  • Page 189 189
  • Page 190 190
  • Page 191 191
  • Page 192 192
  • Page 193 193
  • Page 194 194
  • Page 195 195
  • Page 196 196
  • Page 197 197
  • Page 198 198
  • Page 199 199
  • Page 200 200
  • Page 201 201
  • Page 202 202
  • Page 203 203
  • Page 204 204
  • Page 205 205
  • Page 206 206
  • Page 207 207
  • Page 208 208
  • Page 209 209
  • Page 210 210
  • Page 211 211
  • Page 212 212
  • Page 213 213
  • Page 214 214
  • Page 215 215
  • Page 216 216
  • Page 217 217
  • Page 218 218
  • Page 219 219
  • Page 220 220
  • Page 221 221
  • Page 222 222
  • Page 223 223
  • Page 224 224
  • Page 225 225
  • Page 226 226
  • Page 227 227
  • Page 228 228
  • Page 229 229
  • Page 230 230
  • Page 231 231
  • Page 232 232
  • Page 233 233
  • Page 234 234
  • Page 235 235
  • Page 236 236
  • Page 237 237
  • Page 238 238
  • Page 239 239
  • Page 240 240
  • Page 241 241
  • Page 242 242
  • Page 243 243
  • Page 244 244
  • Page 245 245
  • Page 246 246
  • Page 247 247
  • Page 248 248
  • Page 249 249
  • Page 250 250
  • Page 251 251
  • Page 252 252
  • Page 253 253
  • Page 254 254
  • Page 255 255
  • Page 256 256
  • Page 257 257
  • Page 258 258
  • Page 259 259
  • Page 260 260
  • Page 261 261
  • Page 262 262
  • Page 263 263
  • Page 264 264
  • Page 265 265
  • Page 266 266
  • Page 267 267
  • Page 268 268
  • Page 269 269
  • Page 270 270
  • Page 271 271
  • Page 272 272
  • Page 273 273
  • Page 274 274
  • Page 275 275
  • Page 276 276
  • Page 277 277
  • Page 278 278
  • Page 279 279
  • Page 280 280
  • Page 281 281
  • Page 282 282
  • Page 283 283
  • Page 284 284
  • Page 285 285
  • Page 286 286
  • Page 287 287
  • Page 288 288
  • Page 289 289
  • Page 290 290
  • Page 291 291
  • Page 292 292
  • Page 293 293
  • Page 294 294
  • Page 295 295
  • Page 296 296
  • Page 297 297
  • Page 298 298
  • Page 299 299
  • Page 300 300
  • Page 301 301
  • Page 302 302
  • Page 303 303
  • Page 304 304
  • Page 305 305
  • Page 306 306
  • Page 307 307
  • Page 308 308
  • Page 309 309
  • Page 310 310
  • Page 311 311
  • Page 312 312
  • Page 313 313
  • Page 314 314
  • Page 315 315
  • Page 316 316
  • Page 317 317
  • Page 318 318
  • Page 319 319
  • Page 320 320
  • Page 321 321
  • Page 322 322
  • Page 323 323
  • Page 324 324
  • Page 325 325
  • Page 326 326
  • Page 327 327
  • Page 328 328
  • Page 329 329
  • Page 330 330
  • Page 331 331
  • Page 332 332
  • Page 333 333
  • Page 334 334
  • Page 335 335
  • Page 336 336
  • Page 337 337
  • Page 338 338
  • Page 339 339
  • Page 340 340
  • Page 341 341
  • Page 342 342
  • Page 343 343
  • Page 344 344
  • Page 345 345
  • Page 346 346
  • Page 347 347
  • Page 348 348
  • Page 349 349
  • Page 350 350
  • Page 351 351
  • Page 352 352
  • Page 353 353
  • Page 354 354
  • Page 355 355
  • Page 356 356
  • Page 357 357
  • Page 358 358
  • Page 359 359
  • Page 360 360
  • Page 361 361
  • Page 362 362
  • Page 363 363
  • Page 364 364
  • Page 365 365
  • Page 366 366
  • Page 367 367
  • Page 368 368
  • Page 369 369
  • Page 370 370
  • Page 371 371
  • Page 372 372
  • Page 373 373
  • Page 374 374
  • Page 375 375
  • Page 376 376
  • Page 377 377
  • Page 378 378
  • Page 379 379
  • Page 380 380
  • Page 381 381
  • Page 382 382
  • Page 383 383
  • Page 384 384
  • Page 385 385
  • Page 386 386
  • Page 387 387
  • Page 388 388
  • Page 389 389
  • Page 390 390
  • Page 391 391
  • Page 392 392
  • Page 393 393
  • Page 394 394
  • Page 395 395
  • Page 396 396
  • Page 397 397
  • Page 398 398
  • Page 399 399
  • Page 400 400
  • Page 401 401
  • Page 402 402
  • Page 403 403
  • Page 404 404
  • Page 405 405
  • Page 406 406
  • Page 407 407
  • Page 408 408
  • Page 409 409
  • Page 410 410
  • Page 411 411
  • Page 412 412
  • Page 413 413
  • Page 414 414
  • Page 415 415
  • Page 416 416
  • Page 417 417
  • Page 418 418
  • Page 419 419
  • Page 420 420
  • Page 421 421
  • Page 422 422
  • Page 423 423
  • Page 424 424
  • Page 425 425
  • Page 426 426
  • Page 427 427
  • Page 428 428
  • Page 429 429
  • Page 430 430
  • Page 431 431
  • Page 432 432
  • Page 433 433
  • Page 434 434
  • Page 435 435
  • Page 436 436
  • Page 437 437
  • Page 438 438
  • Page 439 439
  • Page 440 440
  • Page 441 441
  • Page 442 442
  • Page 443 443
  • Page 444 444
  • Page 445 445
  • Page 446 446
  • Page 447 447
  • Page 448 448
  • Page 449 449
  • Page 450 450
  • Page 451 451
  • Page 452 452
  • Page 453 453
  • Page 454 454
  • Page 455 455
  • Page 456 456
  • Page 457 457
  • Page 458 458
  • Page 459 459
  • Page 460 460
  • Page 461 461
  • Page 462 462
  • Page 463 463
  • Page 464 464
  • Page 465 465
  • Page 466 466
  • Page 467 467
  • Page 468 468
  • Page 469 469
  • Page 470 470
  • Page 471 471
  • Page 472 472
  • Page 473 473
  • Page 474 474
  • Page 475 475
  • Page 476 476
  • Page 477 477
  • Page 478 478
  • Page 479 479
  • Page 480 480
  • Page 481 481
  • Page 482 482
  • Page 483 483
  • Page 484 484
  • Page 485 485
  • Page 486 486
  • Page 487 487
  • Page 488 488
  • Page 489 489
  • Page 490 490
  • Page 491 491
  • Page 492 492
  • Page 493 493
  • Page 494 494
  • Page 495 495
  • Page 496 496
  • Page 497 497
  • Page 498 498
  • Page 499 499
  • Page 500 500
  • Page 501 501
  • Page 502 502
  • Page 503 503
  • Page 504 504
  • Page 505 505
  • Page 506 506
  • Page 507 507
  • Page 508 508
  • Page 509 509
  • Page 510 510
  • Page 511 511
  • Page 512 512
  • Page 513 513
  • Page 514 514
  • Page 515 515
  • Page 516 516
  • Page 517 517
  • Page 518 518
  • Page 519 519
  • Page 520 520
  • Page 521 521
  • Page 522 522
  • Page 523 523
  • Page 524 524
  • Page 525 525
  • Page 526 526
  • Page 527 527
  • Page 528 528
  • Page 529 529
  • Page 530 530
  • Page 531 531
  • Page 532 532
  • Page 533 533
  • Page 534 534
  • Page 535 535
  • Page 536 536
  • Page 537 537
  • Page 538 538
  • Page 539 539
  • Page 540 540
  • Page 541 541
  • Page 542 542
  • Page 543 543
  • Page 544 544
  • Page 545 545
  • Page 546 546
  • Page 547 547
  • Page 548 548
  • Page 549 549
  • Page 550 550
  • Page 551 551
  • Page 552 552
  • Page 553 553
  • Page 554 554
  • Page 555 555
  • Page 556 556
  • Page 557 557
  • Page 558 558
  • Page 559 559
  • Page 560 560
  • Page 561 561
  • Page 562 562
  • Page 563 563
  • Page 564 564
  • Page 565 565
  • Page 566 566
  • Page 567 567
  • Page 568 568
  • Page 569 569
  • Page 570 570
  • Page 571 571
  • Page 572 572
  • Page 573 573
  • Page 574 574
  • Page 575 575
  • Page 576 576
  • Page 577 577
  • Page 578 578
  • Page 579 579
  • Page 580 580
  • Page 581 581
  • Page 582 582
  • Page 583 583
  • Page 584 584
  • Page 585 585
  • Page 586 586
  • Page 587 587
  • Page 588 588
  • Page 589 589
  • Page 590 590
  • Page 591 591
  • Page 592 592
  • Page 593 593
  • Page 594 594
  • Page 595 595
  • Page 596 596
  • Page 597 597
  • Page 598 598
  • Page 599 599
  • Page 600 600
  • Page 601 601
  • Page 602 602
  • Page 603 603
  • Page 604 604
  • Page 605 605
  • Page 606 606
  • Page 607 607
  • Page 608 608
  • Page 609 609
  • Page 610 610
  • Page 611 611
  • Page 612 612
  • Page 613 613
  • Page 614 614
  • Page 615 615
  • Page 616 616
  • Page 617 617
  • Page 618 618

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

Type
Reference guide
This manual is also suitable for

Ask a question and I''ll find the answer in the document

Finding information in a document is now easier with AI