Garmin G1000 NXi - Cessna 182T/T182T/J182T Nav III Reference guide

Type
Reference guide
Pilot’s Guide
190-02177-00
Revision B
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 AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
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 Corporation
No. 68, Zhangshu 2nd Road
Xizhi District,
New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
Cirrus SR2x
G1000
®
NXi Pilot’s Guide Cessna Nav III
Cessna Nav III
®
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
EIS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AFCS
ADDITIONAL FEATURES
APPENDICES
INDEX
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
Copyright © 2017 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2501.00 or later for Cessna 172R, 172S, 182T, T182T, 206H, and T206H
aircraft. Some differences in operation may be observed when comparing the information in this manual to earlier or later software
versions.
NOTE: Cessna Nav III aircraft include the Cessna 172R, the Cessna 172S, the normally aspirated Cessna 182 (182),
the turbocharged Cessna 182 (T182), the normally aspirated Cessna 206 (206), and the turbocharged Cessna 206
(T206). Unless otherwise indicated, information in the G1000 Cockpit Reference Guide pertains to all Cessna Nav
III aircraft.
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
®
NXi, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin
SVT
is a trademark of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the express permission
of Garmin.
Stormscope
®
is registered trademarks of L-3 Communications. CO Guardian is a trademark of CO Guardian, Inc. AC-U-KWIK
®
is a
registered trademark of Penton Business Media Inc. Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International,
Inc. NavData
®
is a registered trademark of Jeppesen, Inc.; Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance. SiriusXM Weather and
SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc. The Bluetooth
®
word mark and logos are owned by the Bluetooth
SIG, Inc. and any use of such marks by Garmin is under license.
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 NXi Pilot’s Guide for the Cessna Nav III
190-02177-00 Rev. B
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.
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
i
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.
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.
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
190-02177-00 Rev. Bii
WARNINGS, CAUTIONS, AND NOTES
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.
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 use 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.
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
iii
WARNINGS, CAUTIONS, AND NOTES
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.
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
POHs 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: 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.
NOTE: Operate G1000 NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
190-02177-00 Rev. Biv
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02177-00 A January 2017 All Production release with GDU software version 20.05.
190-02177-00 B May 2017 All HSI Map information added
SurfaceWatch information added
VSD information added
Updated to fix clerical errors
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
v
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
Line Replaceable Units (LRU) ......................................... 1
1.2 System Controls....................................................... 4
PFD/MFD Controls ........................................................ 4
Secure Digital Cards ...................................................... 7
1.3 System Operation .................................................... 8
System Power-up .......................................................... 8
Normal Operation ......................................................... 9
Reversionary Mode ..................................................... 10
System Annunciations ................................................. 11
System Status ............................................................. 13
ADAHRS Operation ..................................................... 14
AHRS Operation ......................................................... 15
GPS Receiver Operation .............................................. 16
1.4 Accessing System Functionality .......................... 22
Softkey Function ......................................................... 22
Menus ....................................................................... 27
MFD Page Groups ....................................................... 28
System Settings .......................................................... 31
System Utilities ........................................................... 37
1.5 Display Backlighting ............................................. 42
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 46
Airspeed Indicator ...................................................... 46
Attitude Indicator ....................................................... 48
Altimeter ................................................................... 49
Vertical Speed Indicator (VSI) ....................................... 51
Vertical Deviation ....................................................... 51
Horizontal Situation Indicator (HSI) .............................. 53
Course Deviation Indicator (CDI) .................................. 57
2.2 Supplemental Flight Data .................................... 64
Temperature Display ................................................... 64
Wind Data ................................................................. 64
Generic Timer ............................................................. 65
Vertical Navigation (VNV) Indications ........................... 66
2.3 PFD Annunciations and Alerting Functions ........ 67
Marker Beacon Annunciations...................................... 67
Altitude Alerting ......................................................... 67
Low Altitude Annunciation .......................................... 68
Minimum Descent Altitude/Decision Height Alerting ...... 68
2.4 Abnormal Operations ........................................... 70
Abnormal GPS Conditions ........................................... 70
Unusual Attitudes ....................................................... 71
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Display ....................................................... 74
Engine Page ............................................................... 86
3.2 EIS Display (Reversionary Mode) ........................ 91
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 93
PFD Controls and Frequency Display ............................. 94
Audio Panel Controls .................................................. 96
4.2 COM Operation ...................................................... 98
COM Tuning Boxes ...................................................... 98
COM Transceiver Manual Tuning .................................. 99
Auto-Tuning the COM Frequency .................................. 99
Frequency Spacing .................................................... 102
4.3 NAV Operation ..................................................... 103
NAV Tuning Boxes..................................................... 103
NAV Radio Selection and Activation ........................... 104
NAV Receiver Manual Tuning ..................................... 104
Auto-Tuning a NAV Frequency from the MFD............... 105
Marker Beacon Receiver ............................................ 107
DME Tuning ............................................................. 108
4.4 Mode S Transponder ........................................... 109
Transponder Controls ................................................ 109
Transponder Mode Selection ...................................... 110
Entering a Transponder Code ..................................... 112
IDENT Function ........................................................ 113
Flight ID Reporting.................................................... 113
4.5 Additional Audio Panel Functions ..................... 114
Power-Up ................................................................. 114
Mono/Stereo Headsets .............................................. 114
Speaker ................................................................... 114
Intercom .................................................................. 114
Clearance Recorder and Player ................................... 116
Entertainment Inputs ................................................ 116
4.6 Audio Panels Preflight Procedure ...................... 118
4.7 Abnormal Operation ........................................... 119
Stuck Microphone ..................................................... 119
COM Tuning Failure ................................................... 119
Audio Panel Fail-Safe Operation ................................. 119
Reversionary Mode ................................................... 119
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
190-02177-00 Rev. Bvi
TABLE OF CONTENTS
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 121
Navigation Status Box and Data Bar ........................... 123
5.2 Using Map Displays ............................................. 125
Map Orientation ....................................................... 125
Map Range .............................................................. 127
Map Panning ............................................................ 129
Measuring Bearing and Distance ................................ 132
Topography .............................................................. 133
Map Symbols ........................................................... 136
Airways ................................................................... 141
Additional Navigation Map Items ............................... 143
IFR/VFR Charts ......................................................... 146
5.3 Waypoints ............................................................. 149
Airports ................................................................... 150
Intersections ............................................................ 157
NDBs ....................................................................... 159
VORs ....................................................................... 161
VRPs ....................................................................... 163
User Waypoints ........................................................ 165
5.4 Airspaces .............................................................. 170
5.5 Direct-to-Navigation .......................................... 174
5.6 Flight Planning ..................................................... 179
Flight Plan Creation .................................................. 180
Flight Plan Import/Export........................................... 184
Adding Waypoints to an Existing Flight Plan ................ 189
Adding Airways to a Flight Plan ................................. 190
Adding Procedures to a Stored Flight Plan .................. 192
Flight Plan Storage ................................................... 197
Flight Plan Editing .................................................... 199
Along Track Offsets ................................................... 203
Parallel Track ............................................................ 204
Activating a Flight Plan Leg ....................................... 206
Inverting a Flight Plan ............................................... 206
Flight Plan Views ......................................................206
Closest Point of FPL .................................................. 208
User-Defined Holding Patterns ................................... 208
5.7 Vertical Navigation ............................................. 212
Altitude Constraints .................................................. 214
Vertical Situation Display (VSD) .................................. 217
5.8 Procedures ...........................................................220
Departures ............................................................... 222
Arrivals ................................................................... 224
Approaches ............................................................. 226
5.9 Trip Planning ........................................................ 236
Trip Planning ............................................................ 236
5.10 Abnormal Operation ........................................... 240
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ............................................... 244
Activating Data Link Weather Services ........................ 244
Weather Product Age ................................................ 246
Displaying Data Link Weather Products ....................... 248
Weather Product Overview ........................................ 256
FIS-B Weather Status................................................. 288
6.2 Stormscope Lightning Detection System ......... 290
Using the Stormscope Page ....................................... 290
Setting Up Stormscope on the Navigation Map ........... 292
6.3 Terrain Displays ................................................... 294
Relative Terrain Symbology ........................................ 295
Terrain-SVT and TAWS-B Alerting Displays ................... 300
Forward Looking Terrain Avoidance ............................ 302
Additional TAWS-B Alerting ....................................... 303
System Status ........................................................... 305
6.4 Traffic Information Service (TIS) ........................ 308
Displaying Traffic Data .............................................. 309
Traffic Map Page ....................................................... 310
TIS Alerts ................................................................. 311
System Status ........................................................... 313
6.5 TAS Traffic ............................................................. 315
TAS Theory of Operation ............................................ 315
TAS Alerts ................................................................ 319
System Test .............................................................. 320
Operation ................................................................ 321
6.6 ADS-B Traffic ........................................................ 327
ADS-B System Overview ............................................ 327
Conflict Situational Awareness & Alerting (CSA) .......... 329
Airborne and Surface Applications .............................. 330
Traffic Description ..................................................... 331
Operation ................................................................ 331
ADS-B System Status ................................................ 337
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
vii
TABLE OF CONTENTS
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................... 341
7.2 Flight Director Operation ................................... 345
Activating the Flight Director ..................................... 345
AFCS Status Box ....................................................... 346
Flight Director Modes ................................................ 347
Command Bars ......................................................... 347
7.3 AFCS MODES ........................................................ 348
Vertical Modes ......................................................... 348
Lateral Modes .......................................................... 354
Combination modes (VNV, APR, NAV, BC, GA) ............. 358
7.4 Autopilot .............................................................. 372
Flight Control ........................................................... 372
Engagement ............................................................. 373
Control Wheel Steering ............................................. 373
Disengagement ........................................................ 374
7.5 AFCS Annunciations and Alerts ......................... 375
Overspeed Protection ................................................ 376
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 378
SVT Operation .......................................................... 379
SVT Features ............................................................ 381
Field of View ............................................................389
8.2 SafeTaxi ................................................................ 391
8.3 Charts .................................................................... 393
ChartView ................................................................ 394
FliteCharts ............................................................... 403
IFR/VFR Charts ......................................................... 408
Airport Directory ....................................................... 409
8.4 SurfaceWatch ....................................................... 410
Information Box ....................................................... 410
Alerts ...................................................................... 411
Surfacewatch Setup .................................................. 414
8.5 Database Cycle Number and Revisions ............ 416
Cycle Number and Revision ....................................... 416
8.6 SiriusXM Radio Entertainment .......................... 418
Activating SiriusXM Satellite Radio Services ................ 418
Using SiriusXM Radio ................................................ 419
8.7 Flight Data Logging ............................................ 422
8.8 Connext Setup ..................................................... 424
8.9 Auxiliary Video (Optional) .................................. 426
Video Setup .............................................................426
Display Selection ...................................................... 426
Zoom/Range ............................................................ 428
8.10 Abnormal Operation ........................................... 429
SiriusXm Data Link Receiver Troubleshooting............... 429
APPENDICES
Annunciations and Alerts ............................................. 431
Alert Level Definitions ............................................... 432
Audio Alerting System Test ........................................ 433
System Message Advisories ....................................... 433
Database Management ................................................ 445
Loading Updated Databases ...................................... 445
Magnetic Field Variation Database Update .................. 454
Garmin Aviation Glossary ............................................ 455
Frequently Asked Questions ........................................ 465
Map Symbols ................................................................. 469
INDEX
Index ................................................................................ I-1
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
190-02177-00 Rev. Bviii
TABLE OF CONTENTS
Blank Page
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 NXi Integrated Avionics System as installed in the Cessna
Nav III. The system presents flight instrumentation, position, navigation, communication, and identification
information to the pilot through large-format displays.
The optional Flight Stream 510 device provides a Bluetooth
®
connection between the system and a mobile
device. GPS, ADAHRS/AHRS, ADS-B, traffic, SiriusXM audio, and weather data can then be shared with the
mobile device, and flight plans can be transferred to or from the mobile device. Also, database updates may be
performed using the Flight Stream 510 WiFi link.
LINE REPLACEABLE UNITS (LRU)
The system consists of the following Line Replaceable Units (LRUs):
GDU 1054B/1050
(2) – The system features two LCD display units. The left display is configured as a
PFD and the right display is configured as an MFD. The displays communicate with each other through a
High-Speed Data Bus (HSDB) connection. Each display is also connected to the onside GIA 63W. Systems
configured with the Garmin Automatic Flight Control System (AFCS) use the GDU 1054B. Systems without
the Garmin AFCS use the GDU 1050.
GIA 63W
(2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. 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 PFD and MFD via HSDB connection. The
GIA 63Ws are not paired together and do not communicate with each other directly.
GSU 75
(1) – Processes data from the pitot/static system as well as the OAT probe to provide pressure
altitude, airspeed, vertical speed and OAT information to the system. This unit also provides aircraft attitude
and heading information via ARINC 429 to the PFD, MFD, and GIA 63W. The GSU 75 contains advanced
sensors (including accelerometers and rate sensors) and interfaces with the GMU 44 to obtain magnetic field
information, and with the GIA 63W to obtain GPS information. ADAHRS/AHRS modes of operation are
discussed later in this document.
GDC 74A
(1)(Optional) – 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 system, and it communicates
with the GIA 63Ws, the displays, and the GRS 77, using an ARINC 429 digital interface (it also interfaces
directly with the GTP 59). The GDC 74A is designed to operate in Reduced Vertical Separation Minimum
(RVSM) airspace.
GRS 77
(1) (Optional) – Provides aircraft attitude and heading information via ARINC 429 to both displays
and both GIA 63Ws. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and
interfaces with the GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data, and
with both GIA 63/63Ws to obtain GPS information. ADAHRS/AHRS modes of operation are discussed later
in this document.
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM OVERVIEW
GEA 71
(1) – Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws using an RS-485 digital interface.
GMU 44
(1) – Measures local magnetic field. Data is sent to the GRS unit for processing to determine aircraft
magnetic heading. The GMU 44 receives power directly from the GRS unit and communicates with the
GRS unit using an RS-485 digital interface.
GMA 1347
(1) – Integrates NAV/COM digital audio, intercom system and marker beacon controls. This
unit also enables the manual control of the display reversionary mode (red
DISPLAY BACKUP
button) and
communicates with the #1 GIA 63(W), using an RS-232 digital interface.
GTX 335R/345R/33ES
(1) – Solid-state transponder that provides Mode A, C, S capability. The optional
GTX 345R also provides ADS-B In/Out. The transponder can be controlled from the PFD. The transponder
communicates with the both GIA 63Ws through an RS-232 digital interface.
GSA 81
(3), and
GSM 85/85A
(3) – The GSA 81 servos are used for the automatic control of roll, pitch, and
pitch trim. These units interface with each GIA 63W.
The GSM 85/85A servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator
to the mechanical flight-control surface linkage.
GDL 69A / GDL 69A SXM
(1) (Optional) – A satellite radio receiver that provides data link weather
information to the MFD and, indirectly, to the PFD map as well as digital audio entertainment. The GDL 69A
SXM communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM
Satellite Radio services are required to enable the GDL 69A SXM capability.
GTS 800
(Optional) – The GTS 800 Traffic Advisory System (TAS) uses active interrogations of Mode S and
Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control system.
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are also shown in Figure
1-1. The system is capable of interfacing with the following optional equipment:
GDL 69A / GDL 69A SXM
Data Link Receiver
GTS 800
Traffic Advisory System
L3 Stormscope Lightning Strike and Thunderstorm
Detection
KN 63 DME
KR 87 ADF Receiver
KTA 870 Traffic Avoidance System
CO Guardian Carbon Monoxide Detection
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM OVERVIEW
Non-Garmin Equipment
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
Garmin Equipment
GTX 345R
Or
#1
GDU
1054B/1050
(PFD)
GDL 69A/ GDL
69A SXM (XM
Weather/
Audio Datalink)
GMA 1347
(Audio
Panel)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2
GDU
1054B/1050
(MFD)
GEA 71
(Engine &
Airframe I/F)
GTX 335R/33
(Transponder)
GSA 81 (3)
(Servos)
GMU 44
(Magnetometer)
GSU 75
(ADAHRS)
GRS 77
(AHRS)
GDC 74A
(Air Data
Computer)
KTA 870
(Traffic
Avoidance)
GTS 800
(TAS)
CO Guardian
(Carbon Monoxide
Detection)
L-3
Stormscope
KN-63
(DME)
KR-87
(ADF Reciever)
ELT
(Emergency Locator
Transmitter)
FS 510
(SD Card
Bluetooth Link)
Figure 1-1 System (LRU Configuration)
NOTE: For information on non-Garmin equipment, consult the applicable optional interface user’s guide.
This document assumes that the reader is already familiar with the operation of this additional equipment.
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
4
SYSTEM OVERVIEW
1.2 SYSTEM CONTROLS
NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section.
The system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and
MFD are discussed within the following pages of this section.
PFD/MFD CONTROLS
Figure 1-2 PFD/MFD Controls
4
2
1
6
5
7
9
8
3
12
16
11
10
15
14
13
20
21
19
18
25
24
22
23
28
27
*Only with Garmin AFCS
17
26
29
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
5
SYSTEM OVERVIEW
1
NAV VOL/ID Knob
Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage).
Press to toggle Morse code identifier audio ON/OFF.
2
NAV Frequency
Transfer Key
Transfers the standby and active NAV frequencies.
3
NAV Knob
Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz).
Press to toggle cyan tuning box between NAV1 and NAV2.
4
*Heading Knob
Turn to manually select a heading. When operating in Heading Select mode, this knob pro-
vides the heading reference to the flight director.
Press to display a digital heading momentarily to the left of the HSI and synchronize the
Selected Heading to the current heading.
5
Joystick
Turn to change map range.
Press to activate Map Pointer for map panning.
6
CRS/BARO Knob
Turn large knob for altimeter barometric pressure setting. Turn the small knob to set the
pilot-selected course on the HSI when the VOR1, VOR2, or OBS/SUSP mode is selected.
Pressing this knob centers the CDI on the currently selected VOR. The pilot-selected course
provides course reference to the pilot-side flight director when operating in Navigation and
Approach modes. Press to re-center the CDI and return course pointer directly TO bearing
of active waypoint/station.
7
COM Knob
Turn to tune COM transceiver standby frequencies (large knob for MHz; small for kHz).
Press to toggle cyan tuning box between COM1 and COM2.
The selected COM (green) is controlled with the COM MIC Key (Audio Panel).
8
COM Frequency
Transfer Key (EMERG)
Transfers the standby and active COM frequencies.
Press and hold two seconds to tune the emergency frequency (121.5 MHz) automatically
into the active frequency field.
9
COM VOL/SQ Knob
Turn to control COM audio volume level (shown as a percentage in the COM Frequency
Box).
Press to turn the COM automatic squelch ON/OFF.
10
Direct-to Key ( )
Activates the direct-to function and allows the user to enter a destination waypoint and
establish a direct course to the selected destination (specified by identifier, chosen from the
active route).
11
FPL Key
Displays flight plan information.
12
CLR Key
(DFLT MAP)
Erases information, cancels entries, or removes menus.
Press and hold to display the MFD Navigation Map Page (MFD only).
13
MENU Key
Displays a context-sensitive list of options for accessing additional features or making setting
changes.
14
PROC Key
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and approach
procedures (IAPs) for a flight plan or selected airport.
15
ENT Key
Validates/confirms menu selection or data entry.
190-02177-00 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
6
SYSTEM OVERVIEW
16
FMS Knob
(Flight
Management
System Knob)
Press to turn the selection cursor ON/OFF.
Data Entry: With cursor ON, turn to enter data in the highlighted field (large knob moves
cursor location; small knob selects character for highlighted cursor location)
Scrolling: When a list of information is too long for the window/box, a scroll bar appears,
indicating more items to view. With cursor ON, turn large knob to scroll through the list.
Page Selection: Turn knob on MFD to select the page to view (large knob selects a page
group; small knob selects a specific page from the group)
17
*ALT SEL Knob
Sets the selected altitude in the Selected Altitude Box (the large knob selects the thousands,
the small knob selects the hundreds). In addition to providing the standard system altitude
alerter function, selected altitude provides an altitude setting for the Altitude Capture/Hold
mode of the AFCS
18
*AP Key
Engages/disengages the Autopilot and Flight Director in the default vertical and lateral-
modes.
19
*HDG Key
Selects/deselects the Heading Select mode.
20
*NAV Key
Selects/deselects the Navigation mode.
21
*APR Key
Selects/deselects the Approach mode.
22
*VS Key
Selects/deselects the Vertical Speed mode.
23
*FLC Key
Selects/deselects the Flight Level Change mode.
24
*FD Key
Activates/deactivates the Flight Director only. Pressing the FD key turns on the Flight Direc-
tor in the default vertical and lateral modes. Pressing the FD key again deactivates the Flight
Director and removes the command bars, unless the Autopilot is engaged. If the Autopilot
is engaged, the FD key is disabled.
25
*ALT Key
Selects/deselects the Altitude Hold mode.
26
*VNV Key
(if equipped)
Selects/deselects Vertical Navigation mode.
27
*BC Key
Selects/deselects Back Course Mode.
28
*NOSE UP Key
Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level
Change modes.
29
*NOSE DN Key
Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level
Change modes.
*This Key only appears when equped with the Garmin AFCS option.
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Garmin G1000 NXi - Cessna 182T/T182T/J182T Nav III Reference guide

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