Garmin G1000 NXi - Beechcraft King Air 200/A200/B200 Reference guide

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Reference guide

This manual is also suitable for

Beechcraft 200/B200 Series
Pilot’s Guide
®
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
Copyright © 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2286.00 or later for the G1000 NXi Beechcraft 200/B200 Series. Some
differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
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Fax: 913.397.8282
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Tel: 34-93-357-2608
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Website Address: www.garmin.com
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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
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and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, G1000
®
NXi,
WATCH
®
, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries.
Garmin ESP
, Garmin SVT
, SurfaceWatch
, and Connext
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. Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance. SiriusXM Weather and SiriusXM Satellite Radio are
provided by SiriusXM Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-00 Rev. A
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.
September 2016 Printed in the U.S.A.
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
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.
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 Beechcraft 200/B200 Series
190-02041-00 Rev. Aiv
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.
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: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories , ATC guidance, or positive visual
acquisition of conflicting traffic.
WARNING
:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications (GRS 77 installations only) 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.
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
v
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
WARNING: Do not use SurfaceWatch
information as the primary method of flight guidance during airborne
or ground operations. SurfaceWatch does not have NOTAM or ATIS information regarding the current active
runway, condition, or information about the position of hold lines.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-00 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
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.
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: Operate G1000NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
vii
WARNINGS, CAUTIONS, AND NOTES
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: When operating the system with the magnetic sensor uncoupled from the AHRS, the displayed
heading and heading information used by some system components (e.g. traffic system, AFCS, and weather
radar) will be different from the heading calculated by the AHRS. The difference is an amount equal to the
difference between the current Magnetic Field Variation Database (MV DB) value, and the MV DB value
when the magnetic sensor was uncoupled. Due to the convergence of isogonic lines, this condition is most
noticeable at or near the north and south magnetic poles.
NOTE
: System navigation utilities may not reliably calculate range and bearing information when the
aircraft is operating north of 80° North latitude or south of 80° South latitude. This may result in the system
displaying small gaps in racetrack holding pattern depictions (GRS 7800 installations only).
NOTE
: The Terrain Awareness and Warning System (TAWS) may not operate reliably north of 89º North
latitude and south of 89º South latitude. This is due to limitations present within the Terrain database and
the system’s ability to process the data representing the affected areas (GRS 7800 installations only).
NOTE: 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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-00 Rev. Aviii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02041-00 A 9/15/16 i – I-6 Initial Release for GDU 20.01
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
ix
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................... 1
1.2 Line Replaceable Units (LRU) ................................... 2
1.3 System Controls ........................................................ 5
PFD Controls ................................................................ 5
Controls Associated With the MFD ................................. 7
AFCS Controls .............................................................. 9
Additional AFCS Controls ............................................ 10
Audio Panel Controls .................................................. 11
1.4 Secure Digital Cards ............................................... 13
1.5 System Power-up ..................................................... 14
1.6 System Operation ................................................... 15
Normal Operation ....................................................... 15
Reversionary Mode ..................................................... 15
ADAHRS Operation ..................................................... 16
AHRS Operation ......................................................... 18
System Annunciations ................................................. 21
Softkey Function ......................................................... 22
GPS Receiver Operation .............................................. 34
1.7 Accessing System Functionality ............................ 39
Menus ....................................................................... 39
MFD Page Groups ....................................................... 40
MFD System Pages...................................................... 44
1.8 Display Backlighting ............................................... 59
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................... 64
Airspeed Indicator ...................................................... 64
Attitude Indicator ....................................................... 67
Altimeter ................................................................... 70
Vertical Speed Indicator (VSI) ....................................... 74
Vertical Deviation ....................................................... 74
Horizontal Situation Indicator (HSI) .............................. 76
Directional Gyro (DG) Mode (GRS 7800 Only) ................ 78
Course Deviation Indicator (CDI) .................................. 81
2.2 Garmin SVT (Synthetic Vision Technology) ........... 89
SVT Operation ............................................................ 90
2.3 Supplemental Flight Data ...................................... 97
Temperature Displays .................................................. 97
Wind Data ................................................................. 99
Vertical Navigation (VNV) Indications ......................... 100
2.4 PFD Annunciations and Alerting Functions ........ 101
Alerting System ........................................................ 101
Marker Beacon Annunciations.................................... 102
Altitude Alerting ....................................................... 102
Low Altitude Annunciation ........................................ 103
Minimum Descent Altitude/Decision Height Alerting .... 103
Radar Altimeter ........................................................ 105
2.5 Abnormal Operations ........................................... 107
Abnormal GPS Conditions ......................................... 107
Comparator Annunciations ........................................ 108
Unusual Attitudes ..................................................... 108
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display ............................................................. 112
Interstage Turbine Temperature .................................. 114
Torque ..................................................................... 114
Tachometer (RPM) .................................................... 115
Turbine Speed .......................................................... 116
Fuel Flow ................................................................. 116
Oil Pressure .............................................................. 117
Oil Temperature ........................................................ 117
3.2 EIS Display in Reversionary Mode ...................... 118
Reversionary Display ................................................. 119
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 121
Audio Panel Volume Control ...................................... 121
PFD Controls and Frequency Display ........................... 122
Audio Panel Controls ................................................ 124
Control Unit ............................................................. 126
4.2 COM Operation...................................................... 128
COM Transceiver Selection and Activation ................... 128
COM Transceiver Manual Tuning ................................ 129
Quick-Tuning and Activating 121.500 MHz .................. 131
Auto-Tuning the COM Frequency ................................ 131
Frequency Spacing .................................................... 135
Automatic Squelch .................................................... 136
Volume .................................................................... 137
4.3 NAV Operation....................................................... 138
NAV Radio Selection and Activation ........................... 138
NAV Receiver Manual Tuning ..................................... 139
Auto-Tuning a NAV Frequency from the MFD............... 141
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-00 Rev. Ax
TABLE OF CONTENTS
Marker Beacon Receiver ............................................ 145
DME Tuning ............................................................. 146
4.4 Mode S Transponders ........................................... 147
GTX 335/345/3000 Transponder Controls .................... 147
GTX 335/345/3000 Transponder Mode Selection .......... 148
TCAS II Transponder Controls (optional) ...................... 150
TCAS II Transponder Mode Selection (optional) ............ 151
Entering a Transponder Code ..................................... 153
IDENT Function ........................................................ 155
4.5 Additional Audio Panel Functions ....................... 156
Power-Up ................................................................. 156
Mono/Stereo Headsets .............................................. 156
Speaker ................................................................... 156
Unmuted Inputs ....................................................... 156
Intercom .................................................................. 157
Passenger Address (PA) System .................................. 158
Simultaneous COM Operation .................................... 158
Clearance Recorder and Player ................................... 159
4.6 Audio Panels Preflight Procedure ....................... 160
4.7 Abnormal Operation ............................................. 162
Stuck Microphone ..................................................... 162
COM Tuning Failure ................................................... 162
PFD Failure, Dual System ...........................................163
Audio Panel Fail-Safe Operation ................................. 164
Reversionary Mode ................................................... 164
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ........................................................... 165
Navigation Status Box ............................................... 167
5.2 Using Map Displays .............................................. 169
Map Orientation ....................................................... 169
Map Range .............................................................. 171
Map Panning ............................................................ 173
Measuring Bearing and Distance ................................ 179
Topography .............................................................. 180
Map Symbols ........................................................... 184
Airways ................................................................... 189
Track Vector ............................................................. 191
Wind Vector ............................................................. 192
Fuel Range Ring ....................................................... 193
Field of View (SVT) .................................................... 194
Selected Altitude Intercept Arc ................................... 195
IFR/VFR Charts ......................................................... 196
5.3 Waypoints .............................................................. 199
Airports ................................................................... 200
Intersections ............................................................ 207
NDBs ....................................................................... 209
VORs ....................................................................... 211
VRPs ....................................................................... 213
User Waypoints ........................................................ 215
5.4 Airspaces ................................................................ 221
5.5 Direct-to-Navigation ........................................... 226
5.6 Flight Planning ...................................................... 232
Flight Plan Creation .................................................. 233
Adding Waypoints to an Existing Flight Plan ................ 243
Adding Airways to a Flight Plan ................................. 245
Adding Procedures to a Stored Flight Plan .................. 248
Flight Plan Storage ................................................... 255
Flight Plan Editing .................................................... 257
Along Track Offsets ................................................... 261
Parallel Track ............................................................ 262
Activating a Flight Plan Leg ....................................... 265
Inverting a Flight Plan ............................................... 266
Flight Plan Views ...................................................... 267
Closest Point of FPL .................................................. 269
User-Defined Holding Patterns ................................... 270
5.7 Vertical Navigation ............................................... 275
Altitude Constraints .................................................. 277
5.8 Procedures ............................................................. 281
Departures ............................................................... 281
Arrivals ................................................................... 285
Approaches ............................................................. 288
5.9 Trip Planning .......................................................... 296
Trip Planning ............................................................ 296
Weight Planning ....................................................... 300
Weight Caution And Warning Conditions .................... 302
5.10 RAIM Prediction .................................................... 303
5.11 Navigating a Flight Plan ....................................... 306
5.12 Abnormal Operation ............................................. 333
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather .................................................. 336
Activating Services .................................................... 336
Using SiriusXM Weather Products .............................. 338
Weather Softkeys on the Weather Data Link (XM) Page 342
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
xi
TABLE OF CONTENTS
6.2 Garmin Connext Weather ..................................... 372
Connext Data Requests ............................................. 379
Garmin Connext Weather Products ............................. 383
Abnormal Operations ................................................ 399
6.3 FIS-B Weather ........................................................ 401
Using FIS-B Weather Products .................................... 401
FIS-B Weather Status................................................. 423
6.4 Airborne Color Weather Radar ............................ 425
System Description ................................................... 425
Principles of Pulsed Airborne Weather Radar ............... 425
Safe Operating Distance ............................................ 429
Basic Antenna Tilt Setup ............................................ 430
Practical Application Using the Basic Tilt Setup ............ 430
Weather Mapping and Interpretation ......................... 431
Ground Mapping and Interpretation ........................... 443
Additional Weather Radar Displays ............................. 444
System Status ........................................................... 447
6.5 Stormscope ............................................................ 450
Setting Up Stormscope on the Navigation Map ........... 451
Using the Stormscope Page ....................................... 454
6.6 TAWS-B ................................................................... 456
Relative Terrain Symbology ........................................ 457
TAWS-B Alerts .......................................................... 461
System Status ........................................................... 467
6.7 Vertical Situation Display (VSD) Terrain ............. 469
VSD Display ............................................................. 469
6.8 TAWS-A ................................................................... 473
Relative Terrain Symbology ........................................ 474
TAWS-A Page ........................................................... 478
TAWS-A Alerts .......................................................... 479
System Status ........................................................... 492
TAWS-A Abnormal operations .................................... 493
6.9 Garmin TAS/TCAS I Traffic ..................................... 495
Theory of Operation .................................................. 495
Traffic Alerts ............................................................. 499
System Test .............................................................. 500
Operation ................................................................ 501
6.10 L-3 Skywatch Traffic .............................................. 508
TAS Symbology ......................................................... 508
Operation ................................................................ 509
Altitude Display ........................................................ 512
Traffic Map Page Display Range ................................. 512
TAS Alerts ................................................................ 514
System Status ........................................................... 514
6.11 Honeywell KTA 870 Traffic ................................... 516
TAS Symbology ......................................................... 516
Operation ................................................................ 517
Altitude Display ........................................................ 519
Traffic Map Page Display Range ................................. 520
TAS Alerts ................................................................ 522
System Status ........................................................... 523
6.12 ADS-B Traffic .......................................................... 524
ADS-B System Overview ............................................ 524
ADS-B with TAS/TCAS I .............................................. 526
Conflict Situational Awareness & Alerting ................... 526
Airborne and Surface Applications .............................. 529
Traffic Description ..................................................... 530
Operation ................................................................ 530
ADS-B System Status ................................................ 536
6.13 TCAS II Traffic ......................................................... 539
Theory of Operation .................................................. 539
TCAS II Alerts ........................................................... 540
System Test .............................................................. 545
Operation ................................................................ 546
System Status ........................................................... 552
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview ...................................................... 555
Additional AFCS Controls .......................................... 557
Basic Autopilot Operation .......................................... 558
7.2 Flight Director Operation ..................................... 559
Activating the Flight Director ..................................... 559
AFCS Status Box ....................................................... 560
Flight Director Modes ................................................ 561
Switching Flight Directors .......................................... 561
Command Bars ......................................................... 562
7.3 AFCS Modes ........................................................... 563
Vertical Modes ......................................................... 563
Lateral Modes .......................................................... 570
Combination modes (VNV, APR, NAV, BC, GA) ............. 575
7.4 Autopilot and Yaw Damper Operation ............... 587
Flight Control ........................................................... 587
Engagement ............................................................. 588
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
190-02041-00 Rev. Axii
TABLE OF CONTENTS
Control Wheel Steering ............................................. 588
Disengagement ........................................................ 589
Underspeed Protection .............................................. 590
7.5 Example Flight Plan .............................................. 592
Departure ................................................................ 593
Intercepting a VOR Radial .......................................... 595
Flying a Flight Plan/GPS Course ................................. 596
Descent ................................................................... 597
Approach ................................................................. 602
Go Around/Missed Approach ..................................... 606
7.6 AFCS Annunciations and Alerts ........................... 608
Overspeed Protection ................................................ 608
7.7 Abnormal Operation ............................................. 609
Suspected Autopilot malfunction ................................ 609
Overpowering Autopilot Servos .................................. 609
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ...................... 612
SVT Operation .......................................................... 613
SVT Features ............................................................ 615
Field of View ............................................................ 624
8.2 SafeTaxi .................................................................. 626
SafeTaxi Cycle Number and Revision .......................... 629
8.3 FliteCharts .............................................................. 632
FliteCharts Softkeys .................................................. 634
Terminal Procedures Charts ....................................... 635
Chart Options ........................................................... 638
Day/Night View ........................................................ 639
FliteCharts Cycle Number and Expiration Date ............. 639
8.4 Airport Directory ................................................... 642
Airport Directory Database Cycle Number and Revision 642
8.5 Satellite Telephone ............................................... 645
Registering with Garmin Connext
®
............................ 645
Disable/Enable Iridium Transceiver.............................. 645
Telephone Communication ........................................ 647
Text Messaging (SMS) ............................................... 654
8.6 WIFI Connections .................................................. 665
8.7 SiriusXM Radio Entertainment ............................ 668
Activating SiriusXM Satellite Radio Services ................ 668
Using SiriusXM Radio ................................................ 669
8.8 Scheduler ............................................................... 673
8.9 SurfaceWatch ......................................................... 675
Information Box ....................................................... 675
Alerts ...................................................................... 676
8.10 Flight Data Logging .............................................. 680
8.11 Electronic Stability & Protection (ESP
) ............ 682
Roll Engagement ...................................................... 683
Pitch Engagement..................................................... 685
Angle of Attack Protection ......................................... 686
High Airspeed Protection ........................................... 686
8.12 Abnormal Operation ............................................. 687
SVT Troubleshooting ................................................. 687
Reversionary Mode ................................................... 687
Unusual Attitudes ..................................................... 687
GSR 56 & GDL 59/69/69A Troubleshooting .................. 687
APPENDICES
Annunciations and Alerts ............................................... 691
Alert Level Definitions ............................................... 692
Aircraft Alerts ........................................................... 693
Comparator Annunciations ........................................ 696
Reversionary Sensor Annunciations ............................ 697
System Annunciations ............................................... 698
System Message Advisories ....................................... 701
AFCS Alerts .............................................................. 716
TAWS Alerts ............................................................. 717
Flight plan Import/Export Messages ........................... 720
Pilot Profile Import/Export Messages .......................... 720
GDL 69/69A SXM Data Link Receiver Messages ........... 721
SurfaceWatch Alert Annunciations .............................. 721
Database Management .................................................. 723
Loading Updated Databases ...................................... 723
Magnetic Field Variation Database Update .................. 732
Garmin Aviation Glossary .............................................. 735
Frequently Asked Questions .......................................... 745
Map Symbols ................................................................... 749
INDEX
Index .................................................................................. I-1
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 NXi Integrated Avionics System as installed in the Beechcraft
200/B200 Series. The system is an integrated system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays.
In the Beechcraft 200/B200 Series, the Garmin Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the system.
NOTE: Refer to the AFCS section for details on the Garmin AFCS.
The optional Flight Stream 510 device provides a Bluetooth
®
connection between the system and a mobile
device. GPS, ADAHRS, ADS-B, traffic, Sirius XM audio, and FIS-B 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 also
be performed using the Flight Stream 510 WiFi link.
The system consists of the following Line Replaceable Units (LRUs):
GDU 1050A
Primary Flight Display (PFD)
GDU 1550
Multi Function Display (MFD)
GIA 63W
Integrated Avionics Unit
GMU 44
Magnetometer
GSU 75B
Air Data, Attitude and Heading Reference
System (ADAHRS)
GDC 74B/7400
(optional) Air Data Computer
(ADC)
GRS 77/7800
(optional) Attitude and Heading
Reference System (AHRS)
GEA 71
Engine/Airframe Unit
GMA 1347D
Dual Audio System with Integrated
Marker Beacon Receiver
GTX 33D/335R/345R/3000
Extended Squitter
Mode S Transponder
GDL 59
(optional) WiFi Data Link
GWX 68/70
Weather Radar
GCU 477
MFD Control Unit
GDL 69A
SXM Data Link
GSR 56
(optional) Iridium Transceiver
GTS 820/850/8000
(optional) Traffic Avoidance
System/Traffic Alert and Collision Avoidance System
GRA 5500
Radio Altimeter
GMC 710
AFCS Control Unit
GTP 59
Outside Air Temperature (OAT) Probe
GSA 80
AFCS Servos
GSM 85A/86
Servo Gearboxes
A top-level system block diagram is shown in Figure 1-1 (it does not include the GSM 85A/86).
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
2
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS (LRU)
GDU 1050A
(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 1550
(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.
GSU 75B
(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 both GDU 1050A units and the GIA 63W unit. The GSU 75B 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 modes of operation are discussed
later in this document.
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.
GDC 74B/7400
(2) (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 on-side GIA 63W, on-side GDU 1050A, GDU 1550 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/7400 is designed to operate
in Reduced Vertical Separation Minimum (RVSM) airspace.
GRS 77/7800
(2) (Optional) – Provides aircraft attitude and heading information via ARINC 429 to both the on-
side GDU 1050A, the GDU 1550 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/7400 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 and communicates with the
GRS 77/7800, using an RS-485 digital interface.
GMA 1347D
(2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is
installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual
control of the display reversionary mode (red
DISPLAY BACKUP
button) and communicates with the on-side
GIA 63W, using an RS-232 digital interface.
GTX 33D/335R/345R/3000
(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.
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
3
SYSTEM OVERVIEW
GDL 69A SXM / GDL 69A
(1) – A satellite radio receiver that provides data link weather information to
the MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL
69A communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM
Satellite Radio services are required to enable the GDL 69A capability.
GDL 59
(1) (Optional) – GDL 59 operation is performed with the MFD through HSDB. Connectivity with the
GSR 56 for the Iridium telephone feature is through the RS-232 bus.
GSR 56
(1) (Optional) – The Iridium Transceiver operation for voice communication is by means of a telephone
handset in the cabin and pilot and copilot headsets in the cockpit. The transceiver can also send and receive data
provided by the GDL 59 through the RS-232 bus, and provide Garmin Connext Weather and SMS functions.
GWX 68/70
(1) (Optional) – Provides airborne weather and ground mapped radar data to the MFD, through
the GDL 69A, via HSDB connection.
GCU 477
(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
GMC 710
(1) – Provides the controls for the 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 GSU 75B (GDC 74B/7400).
GTS 820/850/8000
(Optional) – The GTS 820 Traffic Advisory System (TAS), GTS 850 Traffic Alert and
Collision Avoidance System I (TCAS I) and GTS 8000 (TCAS II) use active interrogations of Mode S and Mode
C transponders to provide traffic information to the pilot independent of the air traffic control system.
GRA 5500
(1) (Optional) – Provides altitude above the ground (AGL) to the MFD, through the GIA 63W, via
HSDB connection.
GSA 80
(3), and
GSM 85A/GSM 86
(4) – The GSA 80 servos are used for the automatic control of roll, pitch,
and yaw, and pitch trim. These units interface with each GIA 63W. The servo gearboxes are responsible for
transferring the output torque of the servo actuator to the mechanical flight-control surface linkage.
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
4
SYSTEM OVERVIEW
#1
GDU 1050A
(PFD1)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
AFCS Mode
Logic
Flight
Director
Servo
Management
#2 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
AFCS Mode
Logic
Flight
Director
Servo
Management
#2
GDU 1050A
(PFD2)
Non-Garmin Equipment
GSR 56
(Iridium
Transceiver)
GDL 59
(Data Link)
#3
GDU 1550
(MFD)
GEA 71
(Engine & Airframe
1/2)
#1 GMU 44
(Magnetometer)
#2 GMU 44
(Magnetometer)
#1 GDC 74B / 7400
(Air Data
Computer)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
GTS 820/850/8000
(TAS or TCAS I/II)
Garmin Equipment
GCU 477
(Display
Controller)
GMA 1347D
(Audio Panel)
GMA 1347D
(Audio Panel)
GMC 710
(AFCS
Controller)
GDL 69A SXM/
GDL 69A
(SiriusXM
Weather Datalink/
Datalink)
GWX 68/70
(Weather Radar)
#1 GSU 75B
(ADAHRS)
#2 GSU 75B
(ADAHRS)
#1 GRS 77/7800
(Attitude & Heading)
GTP 59
(OAT Probe)
GTP 59
(OAT Probe)
#1 GRS 77/7800
(Attitude & Heading)
#1 GSA 80 (Pitch)
#2 GSA 80 (Yaw)
#3 GSA 80 (Roll)
#1 GTX 33D/
335R/345R/3000
(Transponder)
#2 GTX 33D/
335R/345R/3000
(Transponder)
GRA 5500
Radar Altimiter
#2 GDC 74B / 7400
(Air Data
Computer)
ADF
60A
DME
42
Radar
Altimeter
Stormscope
WX 500
Traffic
System
Figure 1-1 System (LRU Configuration)
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
5
SYSTEM OVERVIEW
1.3 SYSTEM CONTROLS
NOTE: The Audio Panel (GMA 1347D) and AFCS controls (GMC 710) are described in the CNS & Audio Panel
and AFCS sections respectively.
The system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio
panel. The controls for the PFD and MFD are discussed within the following pages of this section.
PFD CONTROLS
Figure 1-2 PFD Controls
21 5
4
6
8
7
3
11
12
10
9
15
14
13
190-02041-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Beechcraft 200/B200 Series
6
SYSTEM OVERVIEW
The following list provides an overview of the controls located on the PFD bezel (see Figure 1-2).
1
NAV VOL/ID Knob
– Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON
and OFF. Volume level is shown in the NAV frequency field as a percentage.
2
NAV Frequency Transfer Key
– Toggles the standby and active NAV frequencies.
3
Dual
NAV Knob
– Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for
kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2.
4
Joystick
– Changes the map range when rotated. Activates the map pointer when pressed.
5
BARO Knob
– Sets the altimeter barometric pressure. Press to enter standard pressure (29.92).
6
Dual COM Knob
– Tunes the standby frequencies for the COM transceiver (large knob for MHz; small
knob for kHz). Press to switch the tuning box (cyan box) between COM1 and COM2.
7
COM Frequency Transfer Key
– Toggles the standby and active COM frequencies. Press and hold this
key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency
field.
8
COM
VOL/SQ Knob
– Controls COM audio volume level. Volume level is shown in the COM frequency
field as a percentage. Press to turn the COM automatic squelch ON and OFF.
9
Direct-to Key ( )
– Allows the user to enter a destination waypoint and establish a direct course to the
selected destination (the destination is either specified by the identifier, chosen from the active route, or
taken from the map pointer position).
10
FPL Key
– Displays the active Flight Plan Page for creating and editing the active flight plan.
11
CLR
Key
– Erases information, cancels entries, or removes page menus.
12
Dual FMS Knob
– Flight Management System Knob. Press the
FMS
Knob to turn the selection cursor
ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small
and large
knobs. The large
knob moves the cursor on the page, while the small
knob selects individual
characters for the highlighted cursor location.
13
MENU Key
– Displays a context-sensitive list of options. This list allows the user to access additional
features or make setting changes that relate to particular pages.
14
PROC Key
– Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach
procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or
arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan.
If a flight plan is not used, both the desired airport and the desired procedure may be selected.
15
ENT Key
– Validates or confirms a menu selection or data entry.
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Garmin G1000 NXi - Beechcraft King Air 200/A200/B200 Reference guide

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