Garmin G1000: Cessna Caravan 208/208B Reference guide

Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

p:913.397.8200

f:913.397.8282

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

p:503.391.3411

f:503.364.2138

Garmin (Europe) Ltd.

Liberty House, Bulls Copse Road

Houndsdown Business Park

Southampton, SO40 9RB, U.K.

p:44/0870.8501241

f:44/0870.8501251

Garmin Corporation

No. 68, Jangshu 2nd Road

Shijr, Taipei County, Taiwan

p:886/02.2642.9199

f:886/02.2642.9099

www.garmin.com

Cessna Caravan

G1000

®

Integrated Flight Deck

Pilot’s Guide

G1000

®

Pilot’s Guide

Cessna Caravan

190-00749-02

Revision 1TP

Caravan Cover.indd 1 11/2/2009 3:15:01 PM

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM (EIS)

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

Garmin G1000 Pilot’s Guide for the Cessna Caravan

190-00749-02 Rev. C

This manual reﬂects the operation of System Software version 0767.05 or later for the Cessna Caravan. Some differences in operation may

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

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: 503/391.3411 Fax 503/364.2138

Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9RB, U.K.

Tel: 44/0870.851241 Fax: 44/0870.8501251

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan

Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please

contact Garmin’s AOG Hotline at 913.397.0836.

Web Site 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 per-

sonal 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

®

and G1000

®

are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH

®

, FliteCharts

®

, and SafeTaxi

®

are trademarks of

Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

Bendix/King

®

and Honeywell

®

are registered trademarks of Honeywell International, Inc.; Becker

®

is a registered trademark of Becker

Flugfunkwerk GmbH; NavData

®

is a registered trademark of Jeppesen, Inc.; XM

®

is a registered trademark of XM Satellite Radio, Inc.

July, 2011 190-00749-02 Rev. C Printed in the U.S.A.

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

i

LIMITED WARRANTY

This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this

period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made

at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty

does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED

OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR

PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO

STATE.

IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER

RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not

allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.

Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole

discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.

To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit

the Garmin Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.

Garmin G1000 Pilot’s Guide for the Cessna Caravan

190-00749-02 Rev. Cii

WARNINGS, CAUTIONS, AND NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance

feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance

and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The

terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from

third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

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

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

aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and

could vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data

Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always

use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated

regularly in order to ensure that the information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is

intended only to supplement other approved navigation data sources and should be considered as an aid to

enhance situational awareness.

WARNING: Trafﬁc information shown on system displays is provided as an aid in visually acquiring trafﬁc.

Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conﬂicting

trafﬁc.

WARNING: XM Weather should not be used for hazardous weather penetration. Weather information

provided by the GDL 69 is approved only for weather avoidance, not penetration.

WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent

delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for

short-range weather avoidance.

WARNING: The Garmin G1000, as installed in the Cessna Caravan aircraft, has a very high degree of

functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability

for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous

operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot

to detect such an occurrence by means of cross-checking with all redundant or correlated information

available in the cockpit.

WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

iii

WARNINGS, CAUTIONS, AND NOTES

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

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

and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic

NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be

misused or misinterpreted and, therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000

Pilot’s Guide documentation and the Cessna Caravan Pilot’s Operating Handbook. Thoroughly practice

basic operation prior to actual use. During ﬂight operations, carefully compare indications from the G1000

to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts,

etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate

a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information

Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed as severe or giving an

intense radar echo.

WARNING:

Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of

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

aboutGarmin/environment/disposal.jsp.

WARNING:

Because of variation in the earth’s magnetic ﬁeld, operating the system within the following

areas could result in loss of reliable attitude and heading indications. 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 use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

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

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

in error as displayed.

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very

sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE

ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an

eyeglass lens cleaner that is speciﬁed as safe for anti-reﬂective coatings.

CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by

an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty

and the pilot’s authority to operate this device under FAA/FCC regulations.

Garmin G1000 Pilot’s Guide for the Cessna Caravan

190-00749-02 Rev. Civ

WARNINGS, CAUTIONS, AND NOTES

NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and

displays, are subject to change and may not reﬂect the most current G1000 system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

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

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

including interference that may cause undesired operation.

NOTE: 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

: 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 feet

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.

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

v

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-00749-00 A

B

C

January, 2008

February, 2008

All

Copyright Page

Initial release

Correct system software number

Changed EMER PWR LVR to EMERG PWR LVR.

Changed GENERATR OVRHT to GENERATOR OVHT.

Changed L, R, L-R FUEL LO to L, R, L-R FUEL LOW.

Removed A-ICE LF annunciation.

Added Message Advisory Alerts

190-00749-01 A September, 2008 All Removed gradient background.

Added Synthetic Vision System

Added GDU 9.04 parameters

190-00749-02 A

B

C

January, 2010

July, 2011

All Added Flight Plan Import/Export

Added AOPA Airport Directory

Added temporary user waypoints

Added CDI availability during Dead Reckoning mode

Added new MFD page navigation

Added dual navigation database capability

Added database synchronization

Added Flight Data Logging

Added other GDU 10.01 parameters

Added Dual GMA support

Updated SiriusXM product references

Added MV DB update procedures

Rescind Rev. B changes

Garmin G1000 Pilot’s Guide for the Cessna Caravan

190-00749-02 Rev. Cvi

REVISION INFORMATION

Blank Page

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

vii

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

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

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

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

PFD/MFD Controls ........................................................ 7

AFCS Controls .............................................................. 9

Audio Panel Controls .................................................. 11

Softkey Function ......................................................... 13

1.4 Secure Digital Cards.............................................. 20

1.5 System Power-up ................................................... 21

1.6 System Operation .................................................. 22

Normal Operation ....................................................... 22

Reversionary Mode ..................................................... 22

AHRS Operation ......................................................... 23

G1000 System Annunciations ...................................... 25

GPS Receiver Operation .............................................. 26

1.7 Accessing G1000 Functionality............................ 31

Menus ....................................................................... 31

MFD Page Groups ....................................................... 31

MFD System Pages...................................................... 36

1.8 Display Backlighting ............................................. 45

Automatic Adjustment ................................................ 45

Manual Adjustment .................................................... 45

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 50

Airspeed Indicator ...................................................... 50

Attitude Indicator ....................................................... 52

Altimeter ................................................................... 53

Vertical Speed Indicator (VSI) ....................................... 57

Vertical Deviation ....................................................... 57

Horizontal Situation Indicator (HSI) .............................. 58

Course Deviation Indicator (CDI) .................................. 63

2.2 Supplemental Flight Data .................................... 71

Temperature Displays .................................................. 71

Wind Data ................................................................. 72

Vertical Navigation (VNV) Indications ........................... 73

2.3 PFD Annunciations and Alerting Functions ........ 74

System Alerting .......................................................... 74

Marker Beacon Annunciations...................................... 75

Trafﬁc Annunciation .................................................... 75

TAWS Annunciations ................................................... 76

Altitude Alerting ......................................................... 77

Low Altitude Annunciation .......................................... 77

Minimum Descent Altitude/Decision Height Alerting ...... 78

2.4 Abnormal Operations ........................................... 80

Abnormal GPS Conditions ........................................... 80

Unusual Attitudes ....................................................... 81

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 Engine Display ....................................................... 86

3.2 System Display ...................................................... 88

Fuel Calculations ........................................................ 91

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 93

MFD/PFD Controls and Frequency Display ..................... 94

Audio Panel Controls .................................................. 96

4.2 COM Operation ...................................................... 98

COM Transceiver Selection and Activation ..................... 98

COM Transceiver Manual Tuning .................................. 99

Quick-Tuning and Activating 121.500 MHz .................. 100

Auto-Tuning the COM Frequency ................................ 101

Frequency Spacing .................................................... 105

Automatic Squelch .................................................... 106

Volume .................................................................... 106

4.3 NAV Operation ..................................................... 107

NAV Radio Selection and Activation ........................... 107

NAV Receiver Manual Tuning ..................................... 108

Auto-Tuning a NAV Frequency from the MFD............... 110

Marker Beacon Receiver ............................................ 115

DME Tuning ............................................................. 116

4.4 GTX 33 Mode S Transponder .............................. 117

Transponder Controls ................................................ 117

Transponder Mode Selection ...................................... 119

Entering a Transponder Code ..................................... 121

IDENT Function ........................................................ 122

Flight ID Reporting.................................................... 123

4.5 Additional Audio Panel Functions ..................... 124

Power-Up ................................................................. 124

Mono/Stereo Headsets .............................................. 124

Speaker ................................................................... 124

Intercom .................................................................. 125

Passenger Address (PA) System .................................. 127

Clearance Recorder and Player ................................... 127

Entertainment Inputs ................................................ 128

Garmin G1000 Pilot’s Guide for the Cessna Caravan

190-00749-02 Rev. Cviii

TABLE OF CONTENTS

4.6 Audio Panel Preﬂight Procedure ....................... 129

4.7 Abnormal Operation ........................................... 130

Stuck Microphone ..................................................... 130

COM Tuning Failure ................................................... 130

PFD Failure, Dual System ........................................... 130

Audio Panel Fail-Safe Operation ................................. 131

Reversionary Mode ................................................... 131

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 133

Navigation Status Box ............................................... 135

5.2 Using Map Displays ............................................. 136

Map Orientation ....................................................... 136

Map Range .............................................................. 138

Map Panning ............................................................ 141

Measuring Bearing and Distance ................................ 145

Topography .............................................................. 146

Map Symbols ........................................................... 149

Airways ................................................................... 155

Track Vector ............................................................. 157

Wind Vector ............................................................. 158

Nav Range Ring........................................................ 159

Fuel Range Ring ....................................................... 160

Field of View (SVS) .................................................... 161

5.3 Waypoints ............................................................. 162

Airports ................................................................... 163

Intersections ............................................................ 170

NDBs ....................................................................... 172

VORs ....................................................................... 174

User Waypoints ........................................................ 176

5.4 Airspaces .............................................................. 182

5.5 Direct-to-Navigation .......................................... 186

5.6 Flight Planning ..................................................... 191

Flight Plan Creation .................................................. 192

Adding Waypoints to an Existing Flight Plan ................ 197

Adding Airways to a Flight Plan ................................. 199

Adding Procedures to a Stored Flight Plan .................. 201

Flight Plan Storage ................................................... 207

Flight Plan Editing .................................................... 210

Along Track Offsets ................................................... 213

Parallel Track ............................................................ 215

Activating a Flight Plan Leg ....................................... 218

Inverting a Flight Plan ............................................... 219

Flight Plan Views ......................................................220

Closest Point of FPL .................................................. 222

5.7 Vertical Navigation ............................................. 223

Altitude Constraints .................................................. 225

5.8 Procedures ...........................................................229

Departures ............................................................... 229

Arrivals ................................................................... 232

Approaches ............................................................. 234

5.9 Trip Planning ........................................................ 240

Trip Planning ............................................................ 240

5.10 RAIM Prediction................................................... 244

5.11 Navigating a Flight Plan ..................................... 247

5.12 Abnormal Operation ........................................... 275

SECTION 6 HAZARD AVOIDANCE

6.1 XM Satellite Weather .......................................... 277

Activating Services .................................................... 278

Using XM Satellite Weather Products .......................... 279

6.2 Airborne Color Weather Radar .......................... 306

System Description ................................................... 306

Principles of Pulsed Airborne Weather Radar ............... 306

Safe Operating Distance ............................................ 311

Basic Antenna Tilt Setup ............................................ 311

Weather Mapping and Interpretation ......................... 313

Ground Mapping and Interpretation ........................... 326

6.3 WX-500 Stormscope ........................................... 327

Setting Up Stormscope on the Navigation Map ........... 327

6.4 Terrain Proximity ................................................. 333

Displaying Terrain Proximity Data ............................... 334

Terrain Proximity Page ............................................... 336

6.5 Terrain-SVS ........................................................... 339

TERRAIN-SVS Page ................................................... 343

TERRAIN-SVS Alerts .................................................. 345

6.6 TAWS-B ................................................................. 350

Displaying TAWS-B Data ............................................ 351

TAWS-B Page ........................................................... 354

TAWS-B Alerts .......................................................... 356

System Status ........................................................... 362

6.7 Trafﬁc Advisory System (TAS)............................. 364

TAS Symbology ......................................................... 364

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

ix

TABLE OF CONTENTS

Operation ................................................................ 365

Altitude Display ........................................................ 368

Trafﬁc Map Page Display Range ................................. 368

TAS Alerts ................................................................ 370

System Status ........................................................... 370

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Controls ...................................................... 374

Additional AFCS Controls .......................................... 375

7.2 Flight Director Operation ................................... 376

Activating the Flight Director ..................................... 376

AFCS Status Box ....................................................... 377

Flight Director Modes ................................................ 378

Switching Flight Directors .......................................... 378

Command Bars ......................................................... 379

7.3 Vertical Modes ..................................................... 380

Pitch Hold Mode (PIT) ............................................... 381

Selected Altitude Capture Mode (ALTS) ....................... 382

Altitude Hold Mode (ALT) .......................................... 383

Vertical Speed Mode (VS) .......................................... 384

Flight Level Change Mode (FLC) ................................. 385

Vertical Navigation Modes (VPTH, ALTV) ..................... 387

Glidepath Mode (GP) (WAAS Only) ............................ 392

Glideslope Mode (GS) ............................................... 394

Takeoff (TO) and Go Around (GA) Modes .................... 395

7.4 Lateral Modes ...................................................... 396

Roll Hold Mode (ROL) ............................................... 397

Low Bank Mode ....................................................... 397

Heading Select Mode (HDG) ...................................... 398

Navigation Modes (GPS, VOR, LOC) ............................ 399

Approach Modes (GPS, VAPP, LOC) ............................. 401

Backcourse Mode (BC) .............................................. 403

7.5 Autopilot and Yaw Damper Operation ............. 404

Flight Control ........................................................... 404

Engagement ............................................................. 405

Control Wheel Steering ............................................. 405

Disengagement ........................................................ 406

7.6 Example Flight Plan ............................................ 407

Departure ................................................................ 408

Intercepting a VOR Radial .......................................... 410

Flying a Flight Plan/GPS Course ................................. 411

Descent ................................................................... 412

Approach ................................................................. 416

Go Around/Missed Approach ..................................... 418

7.7 AFCS Annunciations and Alerts ......................... 420

AFCS Status Alerts .................................................... 420

Overspeed Protection ................................................ 421

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision System (SVS) (Optional) ......... 424

SVS Operation .......................................................... 425

SVS Features ............................................................ 427

Field of View ............................................................ 436

8.2 SafeTaxi ................................................................ 438

8.3 ChartView ............................................................. 444

ChartView Softkeys ................................................... 444

Terminal Procedures Charts ....................................... 445

Chart Options ........................................................... 454

Day/Night View ........................................................ 460

ChartView Cycle Number and Expiration Date ............. 462

8.4 FliteCharts ............................................................ 465

FliteCharts Softkeys .................................................. 465

Terminal Procedures Charts ....................................... 466

Chart Options ........................................................... 473

Day/Night View ........................................................ 477

FliteCharts Cycle Number and Expiration Date ............. 479

8.5 AOPA Airport Directory ....................................... 482

AOPA Database Cycle Number and Revision ............... 483

8.6 XM Radio Entertainment (Optional) ................. 485

Activating XM Satellite Radio Services ........................ 485

Using XM Radio ....................................................... 487

8.7 Scheduler .............................................................. 490

8.8 Flight Data Logging ............................................ 492

8.9 Abnormal Operation ........................................... 494

SVS Troubleshooting ................................................. 494

Reversionary Mode ................................................... 494

Unusual Attitudes ..................................................... 495

APPENDICES

Annunciations and Alerts ............................................. 499

CAS Annunciation Alert Levels ................................... 501

Caravan CAS Annunciations ....................................... 502

Message Advisory Alerts ............................................ 503

Comparator Annunciations ........................................ 504

Garmin G1000 Pilot’s Guide for the Cessna Caravan

190-00749-02 Rev. Cx

TABLE OF CONTENTS

Reversionary Sensor Annunciations ............................ 504

Voice Alerts .............................................................. 505

G1000 System Annunciations .................................... 505

G1000 System Message Advisories ............................. 507

AFCS Alerts .............................................................. 519

Terrain-SVS Alerts ..................................................... 520

TAWS-B ALERTS ........................................................ 521

Database Updates ......................................................... 523

Garmin Databases .................................................... 524

Jeppesen Databases .................................................. 525

Loading Updated Databases ...................................... 526

Glossary .......................................................................... 529

Frequently Asked Questions ........................................ 535

Display Symbols ............................................................ 539

INDEX

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

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

1

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section provides an overview of the G1000 Integrated Flight Deck as installed in the Cessna Caravan. The

G1000 system is an integrated ﬂight control system that presents ﬂight instrumentation, position, navigation,

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

the following Line Replaceable Units (LRUs):

•

GDU 1040A

Primary Flight Display (PFD)

•

GDU 1040A

Multi Function Display (MFD)

•

GIA 63W

Integrated Avionics Unit

•

GDC 74A

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GRS 77

Attitude and Heading Reference System

(AHRS)

•

GMU 44

Magnetometer

•

GSD 41

Data Concentrator

•

GMA 1347

Audio System with Integrated Marker

Beacon Receiver

•

GTX 33

Mode S Transponder

•

GDL 69A

Satellite Data Link Receiver (optional)

•

GWX 68

Weather Radar (optional)

•

GMC 710

AFCS Control Unit

•

GTP 59

Outside Air Temperature (OAT) Probe

•

GSA 80

and

GSA 81

AFCS Servos

•GSM 85 and

GSM 85A

Servo Gearboxes

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

NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.

In the Cessna Caravan, the GFC 700 Automated Flight Control System (AFCS) provides the ﬂight director (FD),

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

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

2

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.2 LINE REPLACEABLE UNITS (LRU)

•

GDU 1040A

(3) – Each of the PFDs and the MFD feature a 10.4-inch LCD with 1024 x 768 resolution. The unit

installed on the left/pilot side is designated as PFD1. The unit installed on the right/co-pilot side is designated

as PFD2. The unit installed in the center of the panel is designated as the MFD. These units communicate

with each other and with the GIA 63W Integrated Avionics Units through a High-Speed Data Bus (HSDB)

connection.

•

GIA 63W

(2) – Functions as the main communication hub, linking all LRUs with the displays via HSDB

connections. Each GIA 63W contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, a ﬂight director

(FD) and system integration microprocessors. The GIA 63Ws are not paired together and do not communicate

with each other directly.

•

GDC 74A

(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, on-side GTP59, and on-side GRS 77, using an ARINC 429 digital interface

(the pilot’s side GDC 74A also interfaces directly with the MFD).

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

3

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GEA 71

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

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

•

GRS 77

(2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU 1040A

and the on-side GIA 63W (the pilot-side GRS 77 also interfaces with the MFD). The GRS 77 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 for processing to determine aircraft

magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77,

using an RS-485 and RS-232 digital interface.

•

GSD 41

(1) – This unit is a data concentrator used to expand the input and output capabilities of the system.

Communication is through the High Speed Data Bus.

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

4

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

•

GMA 1347 (1)

– Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is

installed between PFD1 and the MFD. This unit also enables the manual control of the display reversionary

mode (red

DISPLAY BACKUP

button) and communicates with both GIA 63Ws, using an RS-232 digital

interface.

•

GTX 33

(1 or 2) – Solid-state transponders that provide Modes A, C and S capability. Both transponders can be

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

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

•

GDL 69A

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

MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A

communicates with the displays via HSDB connection through PFD2. A subscription to the XM Satellite Radio

service is required to enable the GDL 69A capability.

•

GWX 68

(1, optional) – Provides airborne weather and ground mapped radar data to the MFD, via HSDB

connection.

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

5

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GMC 710

(1) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing

communication with the displays.

•

GSD 41

(1, optional) – This unit is a data concentrator used to expand the input and output capabilities of the

system. Communication is through the High Speed Data Bus.

•

GTP 59

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

•

GSA 80

(2),

GSA 81

(2), GSM 85 (1) and

GSM 85A

(3) – The GSA 80 servos are used for the automatic control

of roll and yaw, while the GSA 81 servos are used for the automatic control of pitch and pitch trim. These units

interface with each GIA 63W via an RS-485 interface.

The GSM 85 and GSM 85A servo gearboxes are responsible for transferring the output torque of the GSA 80/81

servo actuator to the mechanical ﬂight-control surface linkage. The GSM 85A servo gearboxes are used when

installed in areas that could experience ice or other contamination. The GSM 85 servo gearbox is used for the

pitch-trim axis, which is installed in a benign enviroment.

190-00749-02 Rev. C

Garmin G1000 Pilot’s Guide for the Cessna Caravan

6

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

G D U 1 0 4 0 A

( PF D # 1 )

G D U 1 0 4 0 A

( P F D # 2 )

( M F D )

G I A 6 3 W # 2

G S A 8 0

( Y a w )

G S A 8 0

( R o l l )

G S A 8 1

( P i t c h )

G S A 8 1

( P i t c h T r i m )

G R S 7 7 # 1

G I A 6 3 W # 1

GMC710

G M U 4 4 # 1

GTX 33 #2

G D C 7 4 A# 1

G T P 5 9 # 1

GMA1347

# 1

G R S 7 7 # 2

G M U 4 4 # 2

G D C 7 4 A# 2

G T P 5 9 # 2

VHF COM

VHF NAV/LOC

GPS/WAAS

G/S

AFCS Mode Logic

Flight Director

Servo Management

VHF COM

VHF NAV/LOC

GPS/WAAS

G/S

AFCS Mode Logic

Flight Director

Servo Management

GDU1040A

GWX68

GDL 69A

(OPTIONAL)

GTX 33 #1

(OPTIONAL)

GEA71

GSD41

(OPTIONAL)

Figure 1-1 G1000 System (LRU Conﬁguration)

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