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

Beechcraft C90A/GT/GTi

G1000

®

Integrated Avionics System

Pilot’s Guide

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

This manual reﬂects the operation of System Software version 0636.07 or later for the Beechcraft C90A/GT/GTi. Some differences in

operation may be observed when comparing the information in this manual to earlier or later software versions.

Garmin International, Inc.

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Tel: 913.397.8200

Fax: 913.397.8282

Aircraft On Ground (AOG) Hotline: 913.397.0836

Aviation Dealer Technical Support: 888.606.5482

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Fax: +44 (0) 238 052 4004

Aviation Support: +44 (0) 370 850 1243

Garmin AT, Inc.

2345 Turner Road SE

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Tel: 503.581.8101

Fax 503.364.2138

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District, New Taipei City, Taiwan

Tel: 34-93-357-2608

Fax: 34-93-429-4484

Website Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored

in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download

a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for

personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice

and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin

®

, G1000

®

, WATCH

®

, FliteCharts

®

, and SafeTaxi

®

are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin

ESP

™

, and Garmin SVT

™

are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the

express permission of Garmin.

Skywatch

®

and Stormscope

®

are registered trademarks of L-3 Communications. Ryan

®

, TCAD

®

and Avidyne

®

are registered trademarks of

Avidyne Corporation. AC-U-KWIK

®

is a registered trademark of Penton Business Media Inc. Bendix/King

®

and Honeywell

®

are registered

trademarks of Honeywell International, Inc. Becker

®

is a registered trademark of Becker Flugfunkwerk GmbH. NavData

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is a registered

trademark of Jeppesen, Inc.; Sirius, XM, and all related marks and logos are trademarks of Sirius XM Radio, Inc. and its subsidiaries. .

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,

with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties

of merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any

representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any

incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if

AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to

the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual

or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for

incidental or consequential damages so the above limitations or exclusions may not apply to you.

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

190-00663-04 Rev. Aii

WARNINGS, CAUTIONS, AND NOTES

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with

respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of

merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or

make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the

maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related

to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions

do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations

or exclusions may not apply to licensee.

Printed in the U.S.A.

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

iii

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation

from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot

independently verify the accuracy of the information.

WARNING: Always refer to current aeronautical charts and NOTAMs for veriﬁcation of displayed aeronautical

information. Displayed aeronautical data may not incorporate the latest NOTAM information.

WARNING: Do not use geometric altitude for compliance with air trafﬁc control altitude requirements. The

primary barometric altimeter must be used for compliance with all air trafﬁc control altitude regulations,

requirements, instructions, and clearances.

WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap

data is intended only to supplement other approved navigation data sources and should be considered only

an aid to enhance situational awareness.

WARNING: Do not rely solely upon the display of trafﬁc information to accurately depict all of the trafﬁc

within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information

from aircraft or ground stations, trafﬁc may be present that is not represented on the display.

WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous

weather. Information contained within data link weather products may not accurately depict current

weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather

information shown by the data link weather product. Due to time delays inherent in gathering and processing

weather data for data link transmission, the weather information shown by the data link weather product

may be older than the indicated weather product age.

WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied

upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical

charts for appropriate minimum clearance altitudes.

WARNING: Always obtain qualiﬁed instruction prior to operational use of this equipment.

WARNING

:

Do not use a QFE altimeter setting with this system. System functions will not operate properly

with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the

standard pressure setting, as applicable.

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

190-00663-04 Rev. Aiv

WARNINGS, CAUTIONS, AND NOTES

WARNING

:

Do not use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that

may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned

in error as displayed.

WARNING: When using the autopilot to ﬂy an approach with vertical guidance, the autopilot will not level

the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.

WARNING: Do not rely solely upon the display of trafﬁc information for collision avoidance maneuvering.

The trafﬁc display does not provide collision avoidance resolution advisories and does not under any

circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.

WARNING

:

Because of variation in the earth’s magnetic ﬁeld, do not rely on the accuracy of attitude and

heading indications in the following geographic areas: North of 72° North latitude at all longitudes; South

of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W.

(Northern Canada); North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada);

North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South

latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).

WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous

weather avoidance. Range limitations and interference may cause the system to display inaccurate or

incomplete information. Refer to documentation from the lightning detection system manufacturer for

detailed information about the system.

WARNING:

Use appropriate primary systems for navigation, and for terrain, obstacle, and trafﬁc avoidance.

Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or

reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or trafﬁc.

WARNING:

Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may

appear as a partial symbol.

WARNING:

Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of

the aircraft to the runway or for maintaining the proper approach path angle during landing.

WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within

the MPEL boundary.

WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of

precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color

not representative of the true intensity.

WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only

to enhance situational awareness.

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

v

WARNINGS, CAUTIONS, AND NOTES

CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will

harm the anti-reﬂective coating.

CAUTION:

Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or

modiﬁcations could void both the warranty and affect the airworthiness of the aircraft.

NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.

Always conﬁrm TFR information through ofﬁcial sources such as Flight Service Stations or Air Trafﬁc Control.

NOTE: All visual depictions contained within this document, including screen images of the system panel

and displays, are subject to change and may not reﬂect the most current system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

NOTE: The United States government operates the Global Positioning System and is solely responsible for

its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and

performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation

AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or

misinterpreted and, therefore, become unsafe.

NOTE

: This device complies with part 15 of the FCC Rules. Operation is subject to the following two

conditions: (1) this device may not cause harmful interference, and (2) this device must accept any

interference received, including interference that may cause undesired operation.

NOTE

: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards

away from the source of the interference should alleviate the condition.

NOTE

: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

NOTE

: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with

California’s Proposition 65. If you have any questions or would like additional information, please refer to

our web site at www.garmin.com/prop65.

NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic ﬁelds

can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut

down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no

comparison is possible.

NOTE: The system responds to a terminal procedure based on data coded within that procedure in the

Navigation Database. Differences in system operation may be observed among similar types of procedures

due to differences in the Navigation Database coding speciﬁc to each procedure.

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

190-00663-04 Rev. Avi

REVISION INFORMATION

NOTE

: The FAA has asked Garmin to remind pilots who ﬂy with Garmin database-dependent avionics of the

following:

• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information

related to the use of databases in the National Airspace System.

• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases

obtained from Garmin or Jeppesen that have a Type 2 Letter of Authorization (LOA) from the FAA are assured

compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable

database and can be viewed at http://ﬂy.garmin.com by selecting ‘Aviation Database Declarations.’

• Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with

established FAA regulatory guidance, but does not constitute authorization to ﬂy any and all terminal procedures

that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established

AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

NOTE

: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in

SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at

www.ﬂygarmin.com by selecting ‘Database Exclusions List.’

NOTE

: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their

impact on the intended aircraft operation. The database alerts can be viewed at www.ﬂygarmin.com by

selecting ‘Aviation Database Alerts.’

NOTE

: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support.

NOTE: Garmin requests the ﬂight crew report any observed discrepancies related to database information.

These discrepancies could come in the form of an incorrect procedure; incorrectly identiﬁed terrain, obstacles

and ﬁxes; or any other displayed item used for navigation or communication in the air or on the ground. Go

to FlyGarmin.com and select ‘Aviation Data Error Report’.

NOTE: Lamp(s) inside this product contain mercury (HG) and must be recycled or disposed of according to

local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/

environment/disposal.jsp

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms

that can cause isolated discharge points in the strike display mode. However, clusters of two or more

discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after

the screen has been cleared.

NOTE: Operate G1000 system power through at least one cycle in a period of four days of continuous

operation to avoid an autonomous system reboot.

NOTE: The system supports approval of AC 120-76C Hardware Class 3, Software Type B Electronic Flight Bag

(EFB) electronic aeronautical chart applications. Possible additional requirements may make a secondary

source (traditional paper or additional electronic display) necessary onboard the aircraft. If the secondary

source is a Portable Electronic Device (PED), its use must be consistent with guidance in AC 120-76C.

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

vii

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-00663-00 A 9/21/07 i – I-6 Initial Release at GDU SW 8.10

190-00663-01 A 3/11/09 i – I-6 Initial Release

- Added SVS

- Updated to GDU SW 9.14

- Added optional ADS-B

- Added Audio Panel with Cabin Button

190-00663-02 A 10/25/12 i – I-6 Initial Release for GDU SW 12.03

- Added ESP

- Updated to GDU SW 12.03

190-00663-02 B 10/31/12 i – I-6 Added VNAV Note and explanatory paragraphs on page 234

190-00663-03 A 12/8/14 i – I-6 Initial Release for GDU SW 13.09

- Added optional GRS 7800

- Replaced GWX 68 with GWX 70

- Updated to GDU SW 13.08

- Added pilot proﬁle import/export

- Added user-deﬁned holding patterns

- Added temperature compensated minimums

- Added RNAV LP approach service level

- Added AC-U-KWIK airport directory

190-00663-04 A 2/21/16 i – I-6 Initial Release for GDU SW 13.31

- Added optional GTX 33D

- Added optional GDL 69A SXM

- Added

auto-nomination of arrival and approach altitude constraints

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

190-00663-04 Rev. Aviii

REVISION INFORMATION

Blank Page

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

ix

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

1.1 System Description ................................................. 1

1.2 Line Replaceable Units (LRU) ................................. 2

1.3 G1000 Controls ........................................................ 7

PFD Controls ................................................................ 7

Controls Associated With the MFD ................................. 9

AFCS Controls ............................................................ 10

Audio Panel Controls .................................................. 12

1.4 Secure Digital Cards.............................................. 14

1.5 System Power-up ................................................... 15

1.6 System Operation .................................................. 16

Normal Operation ....................................................... 16

Reversionary Mode ..................................................... 17

AHRS Operation ......................................................... 18

G1000 System Annunciations ...................................... 21

Softkey Function ......................................................... 22

GPS Receiver Operation .............................................. 28

1.7 Accessing G1000 Functionality............................ 33

Menus ....................................................................... 33

MFD Page Groups ....................................................... 34

MFD System Pages...................................................... 38

1.8 Display Backlighting ............................................. 54

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 58

Airspeed Indicator ...................................................... 58

Attitude Indicator ....................................................... 61

Altimeter ................................................................... 63

Vertical Speed Indicator (VSI) ....................................... 65

Horizontal Situation Indicator (HSI) .............................. 67

GRS 7800 Directional Gyro (DG) Modes ........................ 71

Course Deviation Indicator (CDI) .................................. 74

2.2 Supplemental Flight Data .................................... 82

Temperature Displays .................................................. 82

Wind Data ................................................................. 83

Vertical Navigation (VNV) Indications ........................... 84

2.3 PFD Annunciations and Alerting Functions ........ 85

G1000 Alerting system ................................................ 85

Marker Beacon Annunciations...................................... 86

Trafﬁc Annunciation .................................................... 87

TAWS Annunciations ................................................... 88

Altitude Alerting ......................................................... 88

Low Altitude Annunciation .......................................... 89

Minimum Descent Altitude/Decision Height Alerting ...... 89

2.4 Abnormal Operations ........................................... 91

Abnormal GPS Conditions ........................................... 91

Unusual Attitudes ....................................................... 92

SECTION 3 ENGINE INDICATION SYSTEM

3.1 EIS Display .............................................................. 94

Interstage turbine temperature .................................... 96

Torque ....................................................................... 96

Tachometer (rpm) ....................................................... 97

Turbine speed ............................................................. 98

Fuel ﬂow ................................................................... 98

Oil pressure ................................................................ 99

Oil temperature .......................................................... 99

3.2 EIS Display in Reversionary Mode ..................... 100

Reversionary Display ................................................. 101

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview .............................................................. 103

Audio Panel Volume Control ...................................... 103

PFD Controls and Frequency Display ........................... 104

Audio Panel Controls ................................................ 106

4.2 COM Operation .................................................... 108

COM Transceiver Selection and Activation ................... 108

COM Transceiver Manual Tuning ................................ 109

Quick-Tuning and Activating 121.500 MHz .................. 110

Auto-Tuning the COM Frequency ................................ 111

Frequency Spacing .................................................... 115

Automatic Squelch .................................................... 116

Volume .................................................................... 116

4.3 NAV Operation .....................................................117

NAV Radio Selection and Activation ........................... 117

NAV Receiver Manual Tuning ..................................... 118

Auto-Tuning a NAV Frequency from the MFD............... 120

Marker Beacon Receiver ............................................ 125

DME Tuning ............................................................. 126

4.4 GTX 33 Mode S Transponders ............................ 127

Transponder Controls ................................................ 127

Transponder Mode Selection ...................................... 128

Entering a Transponder Code ..................................... 130

IDENT Function ........................................................ 132

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

190-00663-04 Rev. Ax

TABLE OF CONTENTS

4.5 Additional Audio Panel Functions ..................... 133

Power-Up ................................................................. 133

Mono/Stereo Headsets .............................................. 133

Speaker ................................................................... 133

Unmuted Inputs ....................................................... 133

Intercom .................................................................. 134

Passenger Address (PA) System .................................. 135

Simultaneous COM Operation .................................... 135

Clearance Recorder and Player ................................... 136

4.6 Audio Panels Preﬂight Procedure ...................... 137

4.7 Abnormal Operation ........................................... 139

Stuck Microphone ..................................................... 139

COM Tuning Failure ................................................... 139

PFD Failure, Dual System ........................................... 140

Audio Panel Fail-Safe Operation ................................. 141

Reversionary Mode ................................................... 141

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 143

Navigation Status Box ............................................... 144

5.2 Using Map Displays ............................................. 146

Map Orientation ....................................................... 146

Map Range .............................................................. 148

Map Panning ............................................................ 150

Measuring Bearing and Distance ................................ 155

Topography .............................................................. 156

Map Symbols ........................................................... 159

Airways ................................................................... 166

Track Vector ............................................................. 168

Wind Vector ............................................................. 169

Nav Range Ring........................................................ 170

Fuel Range Ring ....................................................... 171

Field of View (SVT) .................................................... 172

Selected Altitude Intercept Arc ................................... 173

5.3 Waypoints ............................................................. 174

Airports ................................................................... 175

Intersections ............................................................ 182

NDBs ....................................................................... 184

VORs ....................................................................... 186

User Waypoints ........................................................ 188

5.4 Airspaces .............................................................. 194

5.5 Direct-to-Navigation .......................................... 198

5.6 Flight Planning ..................................................... 204

Flight Plan Creation .................................................. 205

Adding Waypoints to an Existing Flight Plan ................ 210

Adding Airways to a Flight Plan ................................. 212

Adding Procedures to a Stored Flight Plan .................. 216

Flight Plan Storage ................................................... 223

Flight Plan Editing .................................................... 225

Along Track Offsets ................................................... 229

Parallel Track ............................................................ 230

Activating a Flight Plan Leg ....................................... 233

Inverting a Flight Plan ............................................... 234

Flight Plan Views ...................................................... 235

Closest Point of FPL .................................................. 237

User-Deﬁned Holding Patterns ................................... 238

5.7 Vertical Navigation ............................................. 243

Altitude Constraints .................................................. 245

5.8 Procedures ...........................................................249

Departures ............................................................... 250

Arrivals ................................................................... 253

Approaches ............................................................. 256

5.9 Trip Planning ........................................................ 265

Trip Planning ............................................................ 265

Weight Planning ....................................................... 269

Weight Caution And Warning Conditions .................... 271

5.10 RAIM Prediction................................................... 272

5.11 Navigating a Flight Plan ..................................... 276

5.12 Abnormal Operation ........................................... 305

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather ................................................ 308

Activating Services .................................................... 308

Using SiriusXM Weather Products .............................. 309

Weather Softkeys on the Weather Data Link (XM) Page 313

6.2 Airborne Color Weather Radar .......................... 342

System Description ................................................... 342

Principles of Pulsed Airborne Weather Radar ............... 342

Safe Operating Distance ............................................ 346

Basic Antenna Tilt Setup ............................................ 346

Practical Application Using the Basic Tilt Setup ............ 346

Weather Mapping and Interpretation ......................... 347

Ground Mapping and Interpretation ........................... 358

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Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

xi

TABLE OF CONTENTS

6.3 Stormscope .......................................................... 359

Setting Up Stormscope on the Navigation Map ........... 360

Selecting the Stormscope Page .................................. 363

6.4 TAWS-B ................................................................. 365

Displaying TAWS-B Data ............................................ 366

TAWS-B Alerts .......................................................... 370

System Status ........................................................... 376

6.5 Proﬁle View Terrain ............................................. 378

Proﬁle View Display .................................................. 379

6.6 Trafﬁc Information Service (TIS) ........................ 382

Trafﬁc Map Page ....................................................... 385

TIS Alerts ................................................................. 386

System Status ........................................................... 388

6.7 L-3 Skywatch Trafﬁc ............................................ 390

TAS Symbology ......................................................... 390

Operation ................................................................ 391

Altitude Display ........................................................ 394

Trafﬁc Map Page Display Range ................................. 394

TAS Alerts ................................................................ 396

System Status ........................................................... 396

6.8 Honeywell KTA 870 Trafﬁc .................................. 398

TAS Symbology ......................................................... 398

Operation ................................................................ 399

Altitude Display ........................................................ 402

Trafﬁc Map Page Display Range ................................. 402

TAS Alerts ................................................................ 404

System Status ........................................................... 405

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Overview .................................................... 407

Additional AFCS Controls .......................................... 409

Basic Autopilot Operation .......................................... 410

7.2 Flight Director Operation ................................... 411

Activating the Flight Director ..................................... 411

AFCS Status Box ....................................................... 412

Flight Director Modes ................................................ 413

Switching Flight Directors .......................................... 413

Command Bars ......................................................... 414

Underspeed Protection .............................................. 415

7.3 Vertical Modes ..................................................... 417

Pitch Hold Mode (PIT) ............................................... 418

Selected Altitude Capture Mode (ALTS) ....................... 419

Altitude Hold Mode (ALT) .......................................... 420

Vertical Speed Mode (VS) .......................................... 421

Flight Level Change Mode (FLC) ................................. 422

Vertical Navigation Modes (VPTH, ALTV) ..................... 424

Glidepath Mode (GP) ................................................ 429

Glideslope Mode (GS) ............................................... 431

Takeoff (TO) and Go Around (GA) Modes .................... 432

Level Mode (LVL) ...................................................... 433

7.4 Lateral Modes ...................................................... 434

Roll Hold Mode (ROL) ............................................... 435

Low Bank Mode ....................................................... 435

Heading Select Mode (HDG) ...................................... 436

Navigation Modes (GPS, VOR, LOC) ............................ 437

Approach Modes (GPS, VAPP, LOC) ............................. 439

Backcourse Mode (BC) .............................................. 440

Level Mode (LVL) ...................................................... 441

7.5 Autopilot and Yaw Damper Operation ............. 442

Flight Control ........................................................... 442

Engagement ............................................................. 443

Control Wheel Steering ............................................. 443

Disengagement ........................................................ 444

7.6 Example Flight Plan ............................................ 445

Departure ................................................................ 446

Intercepting a VOR Radial .......................................... 448

Flying a Flight Plan/GPS Course ................................. 449

Descent ................................................................... 450

Approach ................................................................. 453

Go Around/Missed Approach ..................................... 456

7.7 AFCS Annunciations and Alerts ......................... 458

AFCS Status Alerts .................................................... 458

Overspeed Protection ................................................ 459

7.8 Abnormal Operation ........................................... 460

Suspected Autopilot Malfunction ............................... 460

Overpowering Autopilot Servos .................................. 460

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology ............................... 462

SVT Operation .......................................................... 463

SVT Features ............................................................ 465

Field of View ............................................................ 474

8.2 SafeTaxi ................................................................ 476

SafeTaxi Cycle Number and Revision .......................... 479

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

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TABLE OF CONTENTS

8.3 ChartView ............................................................. 482

ChartView Softkeys ................................................... 483

Terminal Procedures Charts ....................................... 484

Chart Options ........................................................... 492

Day/Night View ........................................................ 498

ChartView Cycle Number and Expiration Date ............. 500

8.4 FliteCharts ............................................................ 503

FliteCharts Softkeys .................................................. 504

Terminal Procedures Charts ....................................... 505

Chart Options ........................................................... 512

Day/Night View ........................................................ 516

FliteCharts Cycle Number and Expiration Date ............. 518

8.5 Airport Directory ................................................. 521

Airport Directory Database Cycle Number and Revision 522

8.6 SiriusXM Satellite Radio ..................................... 524

Activating SiriusXM Satellite Radio Services ................ 524

Using SiriusXM Satellite Radio ................................... 526

8.7 Electronic Stability and Protection (ESP

™

) ....... 529

Roll Engagement ...................................................... 530

Pitch Engagement..................................................... 531

High Airspeed Protection ........................................... 532

8.8 Scheduler .............................................................. 533

8.9 Flight Data Logging ............................................ 535

8.10 Abnormal Operation ........................................... 537

SVT Troubleshooting ................................................. 537

Reversionary Mode ................................................... 537

Unusual Attitudes ..................................................... 538

APPENDICES

Annunciations and Alerts ............................................. 541

Comparator Annunciations ........................................ 544

Reversionary Sensor Annunciations ............................ 545

System Annunciations ............................................... 545

System Message Advisories ....................................... 548

AFCS Alerts .............................................................. 562

Terrain-SVS Alerts ..................................................... 563

Terrain-SVS Status Annunciations ............................... 563

TAWS-B ALERTS ........................................................ 564

TAWS-B System Status Annunciations ......................... 565

Flight Plan Import/Export Messages ........................... 566

Pilot Proﬁle Import/Export Messages .......................... 566

Database Management ................................................ 567

Navigation Databases ............................................... 568

Garmin Databases/Jeppesen Chartview Database ........ 572

Frequently Asked Questions ........................................ 589

Map Symbols ................................................................. 593

INDEX

Index ................................................................................ I-1

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Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

1

SYSTEM OVERVIEW

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section provides an overview of the G1000 Integrated Avionics System as installed in the Beechcraft

C90A/GT/GTi. The system is an integrated ﬂight control system that presents ﬂight instrumentation, position,

navigation, communication, and identiﬁcation information to the pilot through large-format displays. The system

consists of the following Line Replaceable Units (LRUs):

•

GDU 1040A

Primary Flight Display (PFD)

•

GDU 1500

Multi Function Display (MFD)

•

GIA 63W

Integrated Avionics Unit

•

GDC 74B

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GRS 77/7800

Attitude and Heading Reference

System (AHRS)(GRS 7800 is optional)

•

GMU 44

Magnetometer

•

GMA 1347D/1347D-20

Dual Audio System with

Integrated Marker Beacon Receiver

•

GTX 33/33(ES)/33D

Extended Squitter Mode S

Transponder

•

GDL 69A/69A SXM

Satellite Data Link Receiver

•

GWX 68/70

Weather Radar

•

GCU 475

MFD Control Unit

•

GMC 710

AFCS Control Unit

•

GTP 59

Outside Air Temperature (OAT) Probe

•

GSA 80/81

AFCS Servos

•

GSM 85A/86

Servo Gearboxes

A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A/86).

NOTE: Refer to the AFCS section for details on the Garmin AFCS.

In the Beechcraft C90A/GT/GTi, the Garmin Automated Flight Control System (AFCS) provides the ﬂight

director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.

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Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

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SYSTEM OVERVIEW

1.2 LINE REPLACEABLE UNITS (LRU)

•

GDU 1040A

(2) – Each unit is conﬁgured as a PFD that features a 10.4-inch LCD with 1024 x 768 resolution.

The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side

is designated as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W

Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.

•

GDU 1500

(1) – Features a 15-inch LCD with 1024 x 768 resolution and is conﬁgured as an MFD. This unit

is linked to both PFDs via HSDB connection.

•

GIA 63W

(2) – Functions as the main communication hub, linking all LRUs with the on-side PFD. Each

GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a ﬂight director (FD) and system

integration microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA

63Ws are not paired together and do not communicate with each other directly.

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

3

SYSTEM OVERVIEW

•

GDC 74B

(2) – Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure

altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates with the on-

side GIA 63W, on-side GDU 1040A, GDU 1040A MFD, and on-side GRS 77/7800, using an ARINC 429 digital

interface (it also interfaces directly with the on-side GTP 59). The GDC 74B is designed to operate in Reduced

Vertical Separation Minimum (RVSM) airspace.

•

GEA 71

(2) – Receives and processes signals from the engine and airframe sensors. This unit communicates

with both GIA 63Ws using an RS-485 digital interface.

•

GRS 77/7800

(2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side

GDU 1040A, the GDU 1040A MFD, and the on-side GIA 63W. The GRS 77/7800 contains advanced sensors

(including accelerometers and rate sensors) and interfaces with the on-side GMU 44 to obtain magnetic ﬁeld

information, with the GDC 74B to obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS

modes of operation are discussed later in this document.

•

GMU 44

(2) – Measures local magnetic ﬁeld. Data is sent to the GRS 77/7800 for processing to determine

aircraft magnetic heading. This unit receives power directly from the GRS 77/7800 and communicates with the

GRS 77/7800, using an RS-485 digital interface.

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Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

4

SYSTEM OVERVIEW

•

GMA 1347D/1347D-20

(2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls,

and is installed in dual conﬁguration on the outboard side of PFD1 and PFD2. This unit also enables the

manual control of the display reversionary mode (red

DISPLAY BACKUP

button) and communicates with the

on-side GIA 63W, using an RS-232 digital interface.

•

GTX 33/33(ES)/33D

(2) – Solid-state transponders that provide Modes A, C, S and ADS-B capability. Both

transponders can be controlled from either PFD, and only one transponder can be active at a time. Each

transponder communicates with the on-side GIA 63W through an RS-232 digital interface.

•

GDL 69A/69A SXM

(1) – A satellite radio receiver that provides real-time weather information to the G1000

MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. It communicates

with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the

GDL 69A/69A SXM capability.

•

GWX 68/70

(1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL

69A/69A SXM, via HSDB connection.

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Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

5

SYSTEM OVERVIEW

•

GCU 475

(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital

interface.

•

GMC 710

(1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing

communication with both PFDs.

•

GTP 59

(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.

•

GSA 80

(3),

GSA 81

(1), and

GSM 85A/86

(4) – The GSA 80 servos are used for the automatic control of roll,

pitch, and yaw. The GSA 81 servo is used for the automatic control of pitch trim. These units interface with

each GIA 63W.

The GSM 85A/86 servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo

actuator to the mechanical ﬂight-control surface linkage.

190-00663-04 Rev. A

Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT/GTi

6

SYSTEM OVERVIEW

GDU 1040A

(PFD #1)

GDU1040A

(PFD #2)

GDU1500

(MFD)

GIA63W #2

GSA80

(Yaw)

GSA80

(Roll)

GSA 80

(Pitch)

GSA 81

(Pitch Trim)

GRS 77/7800

#1

GIA 63W #1

GMC710

GMU44#1

GEA71#2

GEA71#1

GDC74B #1

GTP59#1

GMA 1347D/

GMA 1347D-20

#2

GMA 1347D/

GMA 1347D-20

#1

GTX 33/33(ES)/

GTX 33D

GCU 475

GWX 68/70

GDL 69A/

GDL 69A SXM

GRS 77/7800

#2

GMU44#2

GDC74B #2

GTP59#2

VHF COM

VHF NAV/LOC

GPS/SBAS

G/S

AFCS Mode Logic

Flight Director

Servo Management

VHF COM

VHF NAV/LOC

GPS/SBAS

G/S

AFCS Mode Logic

Flight Director

Servo Management

GTX 33/33(ES)/

GTX 33D #1

GTX 33/33(ES)/

GTX 33D

GTX 33/33(ES)/

GTX 33D #2

Figure 1-1 G1000 System (LRU Conﬁguration)

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