Garmin G950 Reference guide

Vulcanair P68

G950

®

Integrated Flight Deck

Pilot’s Guide

G950

®

Pilot’s Guide

Vulcanair P68

190-01325-01

Revision A

Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

Tel: 913.397.8200

Fax: 913.397.8282

AOG Hotline: 913.397.0836

Aviation Dealer

Technical Support: 888.606.5482

www.garmin.com

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Tel: 503.581.8101

Fax: 503.364.2138

Garmin (Europe) Ltd.

Liberty House,Houndsdown Business Park

Southampton, Hampshire, SO40 9LR, U.K.

Tel: +44 (0) 238 052 4000

Fax: +44 (0) 238 052 4004

Aviation Support: +44 (0) 370 850 1243

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District,

New Taipei City, Taiwan

Tel: 34-93-357-2608

Fax: 34-93-429-4484

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AUTOMATIC FLIGHT CONTROL SYSTEM

ADDITIONAL FEATURES

APPENDICES

INDEX

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. A

This manual reﬂects the operation of System Software version 0935.37 or later for the Vulcanair P68 Some differences in operation may

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

Garmin International, Inc.

1200 East 151st Street

Olathe, Kansas 66062, U.S.A.

Tel: 913.397.8200

Fax: 913.397.8282

Aircraft On Ground (AOG) Hotline: 913.397.0836

Aviation Dealer Technical Support: 888.606.5482

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Tel: 44.(0).23.8052.4000

Fax: 44.(0).23.8052.4004

Aviation Support: 44.(0).37.0850.1243

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Tel: 503.581.8101

Fax 503.364.2138

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District, New Taipei City, Taiwan

Tel: 34.93.357.2608

Fax: 34.93.429.4484

Website Address: www.garmin.com

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

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

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

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

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

Garmin

®

is a registered trademark of Garmin Ltd. or its subsidiaries, and G950

®

is a trademark of Garmin Ltd. or its subsidiaries. These

trademarks may not be used without the express permission of Garmin.

Honeywell

®

is a registered trademark of Honeywell International, Inc. Stormscope

®

is a registered trademark of L-3 Communications.

Avidyne

®

is a registered trademark of Avidyne Corporation. AC-U-KWIK

®

is a registered trademark of Penton Business Media Inc. 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.

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.

May 2016 Printed in the U.S.A

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

i

WARNINGS, CAUTIONS, AND NOTES

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

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

independently verify the accuracy of the information.

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

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

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

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

requirements, instructions, and clearances.

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

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

an aid to enhance situational awareness.

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

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

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

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

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

weather conditions.

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

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

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

may be signiﬁcantly 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 G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. Aii

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

:

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

to enhance situational awareness.

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

iii

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.

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. Aiv

WARNINGS, CAUTIONS, AND NOTES

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

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

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

NOTE

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

following:

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

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

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

obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue

of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database

and can be viewed at http://ﬂy.garmin.com by selecting ‘Type 2 LOA Status.’

• 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 to

coordinate the revised DQRs.

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.

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

v

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-01325-00 A 12/20/11 i – I-6 Initial release for 12.01 software.

190-01325-01 A 5/12/2016 ALL Added support for GWX 70 Weather Radar

Added support for GDL 69A SXM

Added support for GRA 55 Radar Altimeter

Added support for GSR 56 Iridium Transceiver

Added support for GTS 825 Trafﬁc Advisory System (TAS)

Added other GDU 15.02 parameters

Added support for Auxiliary Video

Added User Deﬁned Holds

Added Temperature Compensated Altitudes

Updated Engine Parameter Displays

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. Avi

REVISION INFORMATION

Blank Page

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

vii

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

1.1 Line Replaceable Units ........................................... 2

1.2 Secure Digital (SD) Cards .......................................8

1.3 System Power-up ..................................................... 9

1.4 System Operation .................................................. 10

Display Operation ....................................................... 10

G950 System Annunciations ........................................ 11

System Status ............................................................. 12

AHRS Operation ......................................................... 14

GPS Receiver Operation .............................................. 15

1.5 G950 Controls ........................................................ 20

PFD/MFD Controls ...................................................... 20

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

1.6 Accessing G950 Functionality .............................. 29

Menus ....................................................................... 29

Data Entry.................................................................. 29

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

System Settings .......................................................... 35

System Utilities ........................................................... 45

1.7 Display Backlighting ............................................. 49

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 54

Airspeed Indicator ...................................................... 54

Attitude Indicator ....................................................... 55

Altimeter ................................................................... 56

Vertical Speed Indicator (VSI) ....................................... 58

Vertical Deviation ....................................................... 59

Horizontal Situation Indicator (HSI) .............................. 60

Course Deviation Indicator (CDI) .................................. 65

2.2 Supplemental Flight Data .................................... 72

Temperature Displays .................................................. 72

Wind Data ................................................................. 73

Vertical Navigation (VNV) Indications ........................... 74

2.3 PFD Annunciations and Alerting Functions ........ 75

System Alerting .......................................................... 75

Marker Beacon Annunciations...................................... 76

Trafﬁc Annunciation .................................................... 77

TAWS Annunciations ................................................... 78

Altitude Alerting ......................................................... 79

Low Altitude Annunciation .......................................... 79

Minimum Descent Altitude/Decision Height Alerting ...... 80

Radar Altimeter .......................................................... 81

2.4 Abnormal Operations ........................................... 83

Abnormal GPS Conditions ........................................... 83

Unusual Attitudes ....................................................... 84

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 Engine Display ....................................................... 87

Manifold Pressure Gauges ........................................... 88

Tachometers ............................................................... 88

Fuel Flow Indicators .............................................................

88

Cylinder Head Temperatures ........................................ 88

Oil Pressure and Temperature Gauges ........................... 89

Electrical Information .................................................. 89

Fuel Quantity Gauge ................................................... 89

3.2 Engine Page............................................................ 90

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 95

PFD Controls and Frequency Display ............................. 96

GMA 1347 Audio Panel Controls .................................. 98

4.2 COM Operation .................................................... 100

COM Transceiver Selection and Activation ................... 100

COM Transceiver Manual Tuning ................................ 101

Quick-tuning and Activating 121.500 MHz .................. 102

Auto-tuning the COM Frequency ................................ 103

Auto-tuning from the MFD ........................................ 104

Frequency Spacing .................................................... 107

Automatic Squelch .................................................... 108

Volume .................................................................... 108

4.3 NAV Operation ..................................................... 109

NAV Radio Selection and Activation ........................... 109

NAV Receiver Manual Tuning ..................................... 110

Auto-tuning a NAV Frequency from the MFD ............... 112

Auto-tuning NAV Frequencies on Approach Activation . 116

Marker Beacon Receiver ............................................ 117

4.4 GTX 33 Mode S Transponders ............................ 118

Transponder Controls ................................................ 118

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

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. Aviii

TABLE OF CONTENTS

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

Split COM Operation ................................................. 128

Entertainment Inputs ................................................ 129

4.6 Audio Panel Preﬂight Procedure ....................... 130

4.7 Abnormal Operation ........................................... 131

Stuck Microphone ..................................................... 131

COM Tuning Failure ................................................... 131

Audio Panel Fail-safe Operation ................................. 131

PFD Failure (Reversionary Mode) ............................... 131

SECTION 5 FLIGHT MANAGEMENT

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

Navigation Status Box ............................................... 134

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

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

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

Map Panning ............................................................ 140

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 (SVT) .................................................... 161

Selected Altitude Intercept Arc ................................... 162

5.3 Waypoints ............................................................. 163

Airports ................................................................... 164

Intersections ............................................................ 171

NDBs ....................................................................... 173

VORs ....................................................................... 175

User Waypoints ........................................................ 177

5.4 Airspaces .............................................................. 183

5.5 Direct-to-Navigation .......................................... 187

5.6 Flight Planning ..................................................... 193

Flight Plan Creation .................................................. 194

Adding Waypoints to an Existing Flight Plan ................ 199

Adding Airways to a Flight Plan ................................. 201

Adding Procedures to a Stored Flight Plan .................. 204

Flight Plan Storage ................................................... 211

Flight Plan Editing .................................................... 213

Along Track Offsets ................................................... 216

Parallel Track ............................................................ 217

Activating a Flight Plan Leg ....................................... 220

Inverting a Flight Plan ............................................... 222

Flight Plan Views ...................................................... 223

Closest Point of FPL .................................................. 225

User-Deﬁned Holding Patterns ................................... 225

5.7 Vertical Navigation ............................................. 230

Altitude Constraints .................................................. 232

5.8 Procedures ...........................................................236

Departures ............................................................... 237

Arrivals ................................................................... 240

Approaches ............................................................. 243

5.9 Trip Planning ........................................................ 251

Trip Planning ............................................................ 251

Weight Planning ....................................................... 255

Weight Caution And Warning Conditions .................... 257

5.10 RAIM Prediction................................................... 258

5.11 Navigating a Flight Plan ..................................... 262

5.12 Abnormal Operation ........................................... 290

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather ................................................ 294

Activating Services .................................................... 294

Using SiriusXM Weather Products .............................. 295

6.2 Garmin Connext Weather ................................... 327

Registering the Iridium Satellite System ...................... 327

Registering the system for Garmin Connext Weather .... 328

Accessing Garmin Connext Weather Products .............. 330

Connext Data Requests ............................................. 336

Garmin Connext Weather Products ............................. 340

Abnormal Operations ................................................ 355

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

ix

TABLE OF CONTENTS

6.3 Airborne Color Weather Radar .......................... 357

System Description ................................................... 357

Principles of Pulsed Airborne Weather Radar ............... 357

Safe Operating Distance ............................................ 361

Basic Antenna Tilt Setup ............................................ 362

Weather Mapping and Interpretation ......................... 363

Ground Mapping and Interpretation ........................... 376

Weather Radar Overlay on the Navigation Map Page ... 376

System Status ........................................................... 378

6.4 WX-500 Stormscope ........................................... 380

Setting Up Stormscope on the Navigation Map ........... 380

Selecting the Stormscope Page .................................. 384

6.5 Terrain Proximity ................................................. 386

Displaying Terrain Proximity Data ............................... 386

6.6 Proﬁle View Terrain ............................................. 391

Proﬁle View Display .................................................. 392

6.7 Terrain-SVS ........................................................... 395

Displaying Terrain-SVS Data ....................................... 396

Terrain-SVS Page ...................................................... 398

Terrain-SVS Alerts ..................................................... 400

System Status ........................................................... 403

6.8 TAWS-B ................................................................. 404

Displaying TAWS-B Data ............................................ 405

TAWS-B Page ........................................................... 408

TAWS-B Alerts .......................................................... 410

System Status ........................................................... 416

6.9 Trafﬁc Information Service (TIS) ........................ 418

Displaying Trafﬁc Data .............................................. 419

Trafﬁc Map Page ....................................................... 421

TIS Alerts ................................................................. 422

System Status ........................................................... 423

6.10 TAS Trafﬁc ............................................................. 426

Theory of operation .................................................. 426

TAS Alerts ................................................................ 429

System Test .............................................................. 430

Operation ................................................................ 431

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 S-TEC Fifty Five X Autopilot (Optional) ............ 439

Flight Director Mode Annunciation ............................. 439

Altitude Preselect ..................................................... 439

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology (SVT) ..................... 442

SVT Operation .......................................................... 443

SVT Features ............................................................ 445

Field of View ............................................................ 454

8.2 SafeTaxi ................................................................ 456

SafeTaxi Cycle Number and Revision .......................... 459

8.3 ChartView ............................................................. 462

ChartView Softkeys ................................................... 462

Terminal Procedures Charts ....................................... 463

Chart Options ........................................................... 471

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

ChartView Cycle Number and Expiration Date ............. 479

8.4 FliteCharts ............................................................ 482

FliteCharts Softkeys .................................................. 482

Terminal Procedures Charts ....................................... 483

Chart Options ........................................................... 490

Day/Night View ........................................................ 494

FliteCharts Cycle Number and Expiration Date ............. 496

8.5 AOPA Airport Directory ....................................... 499

AOPA Database Cycle Number and Revision ............... 500

8.5 Satellite Telephone and SMS Messaging .......... 502

Registering With Garmin Connext .............................. 502

Telephone Communication ........................................ 503

Text Messaging (SMS) ............................................... 517

8.6 SiriusXM Radio Entertainment .......................... 529

Activating SiriusXM Satellite Radio Services ................ 529

Using SiriusXM Radio ................................................ 531

8.7 Scheduler .............................................................. 535

8.8 Flight Data Logging ............................................ 537

8.9 Auxiliary Video (Optional) .................................. 539

Video Setup .............................................................540

Display Selection ...................................................... 540

Zoom/Range ............................................................ 541

8.10 Abnormal Operation ........................................... 542

SVT Troubleshooting ................................................. 542

Reversionary Mode ................................................... 542

Unusual Attitudes ..................................................... 543

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. Ax

TABLE OF CONTENTS

APPENDICES

Annunciations and Alerts ............................................. 547

G950 System Message Advisories .............................. 554

Flight Plan Import/Export Messages ........................... 564

TAS Alerts and Annunciations .................................... 566

TIS Alerts and Annunciations...................................... 567

TAWS-B ALERTS and Annunciations ............................ 568

SVS Terrain Alerts ...................................................... 570

Weather Radar Alerts and Annunciations .................... 571

GDL 69A/GDL 69A SXM Data Link Receiver Messages .. 572

Database Management ............................................. 573

Navigation Databases ............................................... 573

Garmin Databases/Jeppesen Chartview Database ........ 578

Garmin Aviation Glossary ............................................ 585

Frequently Asked Questions ........................................ 595

General TIS Information ............................................... 599

Map Symbols ................................................................. 601

INDEX

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

1

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

SECTION 1 SYSTEM OVERVIEW

NOTE: This document provides a complete description of all existing features of the Garmin G950 system.

Not all of those are available on P68 series aircraft. The Aircraft Owner/Operator shall refer only to the

sections of this document relevant to the current aircraft conﬁguration.

The G950 Integrated Flight Deck System presents ﬂight instrumentation, position, navigation, communication,

and identiﬁcation information to the pilot using ﬂat-panel color displays. The system is distributed across the

following Line Replaceable Units (LRUs):

•

GDU 1040A

Primary Flight Display (PFD)

•

GDU 1040A

Multi Function Display (MFD)

•

GMA 1347

Audio Panel with Integrated Marker

Beacon Receiver

•

GEA 71

Engine/Airframe Unit

•

GIA 63W

Integrated Avionics Units (IAU)

•

GRS 77

Attitude and Heading Reference System

(AHRS)

•

GMU 44

Magnetometer

•

GDC 74A

Air Data Computer (ADC)

•

GTX 33

ES Mode S Transponder with Extended

Squitter

•

GTP 59

Outside Air Temperature (OAT) Probe

Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2. The

G950 is capable of interfacing with the following optional equipment:

•

GDL 69A

/GDL 69A SXM Satellite Data Link

Receiver

•

GWX 68

and GWX 70 Weather Radar

•

GTS 800/820/825

Trafﬁc Advisory System

•

GRA 5500

Radar Altimeter– Provides altitude above

the ground to the PFD, through the GIA 63W, via

HSDB connection.

•

GSR 56

Iridium Transceiver (optional)

• S-TEC 55X Autopilot

• KN 63 DME

• KR 87 ADF

•

WX 500

Lightning Detection System

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. A2

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.1 LINE REPLACEABLE UNITS

• GDU 1040 (2) – The left-hand GDU is conﬁgured as a Primary Flight Display (PFD) and the right-hand GDU

as a Multi Function Display (MFD). Both feature 10.4-inch LCD screens with 1024 x 768 resolution. The

displays communicate with each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each

display is also paired with an Ethernet connection to an IAU.

•

GMA 1347

(1) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,

intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual

control of display reversionary mode (red

DISPLAY BACKUP

Button; see Section 1.5, System Operation) and

communicates with both IAUs using an RS-232 digital interface.

• GIA 63W (2) – The Integrated Avionics Units (IAU) function as the main communication hubs, linking all

LRUs with the on-side display. Each IAU contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, and

system integration microprocessors, and is paired with the on-side display via HSDB connection. The IAUs are

not paired together and do not communicate with each other directly.

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

3

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GDC 74A (1)

– The Air Data Computer (ADC) processes data from the pitot/static system and outside air

temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information

to the G950 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429

digital interface.

•

GEA 71

(2) – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors.

This unit communicates with both IAUs using an RS-485 digital interface.

•

GTX 33 ES with Extended Squitter

(1) – Solid-state transponder that provides Modes A, C and S capability.

The transponder can be controlled from the PFD. The transponder communicates with the GIA 63Ws through

an RS-232 digital interface. The GTX 33 with Extended Squitter will also provide 1090 MHz Extended Squitter

(1090ES) transmit capability. The transponder communicates with both IAUs through an RS-232 digital

interface.

•

GRS 77 (1)

– The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading

information via ARINC 429 to both PFDs and the primary IAU. The AHRS contains advanced sensors (including

accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic ﬁeld information,

with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation is discussed

in Section 1.4, System Operation.

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. A4

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

•

GMU 44 (1)

– The Magnetometer measures local magnetic ﬁeld and sends data to the AHRS for processing to

determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with

it via an RS-485 digital interface.

•

GTP 59

(1) – Provides Outside Air Temperature (OAT) data to the GDC 74A.

•

GDL 69A/69A SXM

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

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

The GDL 69A/GDL69A SXM communicates with the MFD via HSDB connection. A subscription to the XM

Satellite Radio service is required to enable the GDL 69A/GDL69A SXM capability.

•

GSR 56

(1)

(optional)

– The Iridium Transceiver operation for voice communication is by means of a telephone

handset. The tranceiver can also send and receive data provided by the GDL 59 through the RS-232 bus.

•

GWX 68/70

(1)

(optional)

– Provides airborne weather and ground mapped radar data to the MFD, through the

GDL 69A or directly linked to the MFD, via HSDB connection.

190-01325-01 Rev. A

Garmin G950 Pilot’s Guide for the Vulcanair P68

5

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GTS 800/820/825

(1)

(optional)

– The GTS 800/820/825 Trafﬁc Advisory System (TAS) uses active interrogations

of Mode S, Mode A, and Mode C transponders to provide Trafﬁc Advisories to the pilot independent of the air

trafﬁc control system.

•

GA 58 (1) (optional)

– The GA 58 is directional antenna for the Trafﬁc Avoidance System. One top-mounted

directional antenna is required when the optional GTRS 800/820 is installed.

•

GA 36

(2) (1 optional with GDL 69A installation) and

GA 37

(1 optional with GDL 69A installation) – The GA 36

is a through-mount GPS/SBAS antenna. The GA 37 is a through-mount GPS/SBAS antenna with XM/Data Link.

GA 36 GA 37

•

GRA 5500

(1)

(optional)

– The optional Radar Altimeter provides altitude above the ground information and

rate of change of radar altitude information.

Garmin G950 Pilot’s Guide for the Vulcanair P68

190-01325-01 Rev. A6

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

GTX 33 ES

Transponder

GDC 74A

Air Data

Computer

OAT

Airspeed

Altitude

Vertical Speed

GMU 44

Magnetometer

Heading

GMA 1347

Audio Panel

G

C

V

e

A

r

ed

No. 2 GIA 63W

Integrated Avionics Unit

System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GPS Output

No. 1 GIA 63W

Integrated Avionics Unit

System Inegration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GPS Output

GRS 77

AHRS

Attitude

Rate of Tu rn

Slip/Skid

GDU 1040

Primary Flight Display

GDU 1040

Multi-Function Display

Reversionary

Control

Reversionary

Control

GEA 71 #1

Engine/Airframe

Unit

GEA 71 #2

Engine/Airframe

Unit

GTS 800/820/825

Traffic Awareness

System

Figure 1-1 Basic G950 Block Diagram

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