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Embraer Phenom 100
Embraer Prodigy
®
Flight Deck 100
Pilot’s Guide
190-00728-06 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
Copyright © 2008-2010, 2012-2014 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0734.7A or later for the Embraer Phenom 100. 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 9LR, U.K.
Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004
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
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.
Prodigy
®
is a registered trademark of Embraer-Empresa Brasileira de Aeronautica S.A.
Garmin
®
is a registered trademark 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.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AC-U-KWIK
®
is a registered trademark of Penton Business Media 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.
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. A
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
October, 2014 Printed in the U.S.A.
190-00728-06 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
iii
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 the GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the 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: 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 Prodigy
®
Integrated Flight Deck, as installed in the Embraer Phenom 100 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 system. 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, system operational procedures must be learned on the ground.
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. Aiv
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 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.
WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the Prodigy
®
Pilot’s Guide documentation and the Embraer Phenom 100 Airplane Flight Manual. Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare indications from the system
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 system 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 system 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.
190-00728-06 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
v
WARNINGS, CAUTIONS, AND NOTES
NOTE: All visual depictions contained within this document, including screen images of the panel and
displays, are subject to change and may not reflect the most current system and 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 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
: 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
: 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.’
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
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 ‘Report An Aviation Data Error Report.’
190-00728-06 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
vii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00728-00 A July, 2008 Production release
190-00728-01 A All Added ADF
Added ChartView and FliteCharts
Added TAS
Added flight plan import/export
Added other GDU 9.14 parameters
190-00728-02 A September, 2009 All Added Synthetic Vision System
TAWS-A
TCAS I
TCAS II
ADF Tuning
Radar Altimeter
Added AOPA Airport Directory
Added Iridium Satellite Telephone and Data Link Services
Electronic checklists
Added dual navigation database capability
Added database synchronization
Added other GDU 10.00 parameters
190-00728-02 B September, 2009 Copyright
Page
Changed system software number from 0734.19 to
0734.24
190-00728-03 A November, 2010 All Added METARs to active flight plan and maps
Updated XM Weather product age and icon display
Added SMS texting
Updated database update procedures
Added other GDU 11.12 parameters
190-00728-04 A March, 2012 All Updated CAS messages
Updated SiriusXM Satellite Radio audio mute procedure
Added Pilot Profiles
Updated Database Update procedures
Added optional Spoilers
Added AC-U-KWIK Airport Directory capability
Updated GFDS registration procedure
Added Inset Map WX LGND Softkey
Removed flightplan sorting capability
Added other GDU 12.11 parameters
190-00728-05 A May, 2013 All Added CPDLC
Added User Defined Holds
Added temperature compensated altitude
Updated CAS and voice messages
Added other GDU 13.01 parameters
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. Aviii
REVISION INFORMATION
Record of Revisions
190-00728-06 A October, 2014 All Added support for ADS-B out
Updated MFD Data Bar Field choices
Added Ice Detector Option
Added Wind Speed and Heading Indicator Improvements
Added support for Bottlang Charts
Updated CPDLC discussion
Added Profile View
Added Weather Radar overlay on the Navigation Map
Updated Iridium Telephone Page Displays
Updated CAS messages
Added other GDU 14.02 parameters
190-00728-06 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
ix
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 Prodigy
®
Controls .................................................... 8
MFD/PFD Controls ........................................................ 8
MFD Control Unit ....................................................... 10
AFCS Controls ............................................................ 11
Audio Panel Controls .................................................. 13
Softkey Function ......................................................... 15
1.4 Secure Digital Cards.............................................. 26
1.5 System Power-up ................................................... 27
1.6 System Operation .................................................. 28
Normal Operation ....................................................... 28
Reversionary Mode ..................................................... 29
AHRS Operation ......................................................... 30
Prodigy
®
System Annunciations .................................... 31
GPS Receiver Operation .............................................. 32
1.7 Accessing System Functionality .......................... 37
Menus ....................................................................... 37
MFD Page Groups ....................................................... 37
MFD System Pages...................................................... 43
1.8 Display Backlighting ............................................. 59
Automatic Adjustment ................................................ 59
Manual Adjustment .................................................... 59
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 64
Airspeed Indicator ...................................................... 64
Attitude Indicator ....................................................... 67
Altimeter ................................................................... 69
Vertical Speed Indicator (VSI) ....................................... 72
Vertical Deviation ....................................................... 73
Horizontal Situation Indicator (HSI) .............................. 74
Course Deviation Indicator (CDI) .................................. 79
2.2 Supplemental Flight Data .................................... 87
Temperature Displays .................................................. 87
Wind Data ................................................................. 88
Vertical Navigation (VNV) Indications ........................... 89
2.3 PFD Annunciations and Alerting Functions ........ 90
System Annunciations ................................................. 90
Marker Beacon Annunciations...................................... 91
Traffic Annunciations................................................... 91
TAWS Annunciations ................................................... 92
Altitude Alerting ......................................................... 92
Low Altitude Annunciation .......................................... 93
Minimum Descent Altitude/Decision Height Alerting ...... 93
Radar Altimeter .......................................................... 95
2.4 Abnormal Operations ........................................... 97
Altitude Alerting ......................................................... 97
Abnormal GPS Conditions ........................................... 97
Heading Failure Modes................................................ 98
Unusual Attitudes ....................................................... 98
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
3.1 Engine Indication System (EIS) .......................... 104
Takeoff Data Set Window .......................................... 105
Engine Indications .................................................... 106
Fuel and Electrical Indications .................................... 108
Cabin Pressurization ................................................. 109
Spoiler and Landing Gear .......................................... 110
Flaps and Trim .......................................................... 110
3.2 Synoptics .............................................................. 111
System Status ........................................................... 111
Environmental Control System (ECS) .......................... 112
Electrical .................................................................. 114
Fuel ......................................................................... 115
Ice Protection System ................................................ 116
Engine Maintenance ................................................. 118
3.3 Abnormal Operations ......................................... 119
Engine ..................................................................... 119
Cabin Pressurization ................................................. 119
Flaps ....................................................................... 120
Trim ......................................................................... 120
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 121
Audio Panel Volume Control ...................................... 121
MFD/PFD Controls and Frequency Display ................... 122
Audio Panel Controls ................................................ 124
4.2 COM Operation .................................................... 126
COM Transceiver Selection and Activation ................... 126
COM Transceiver Manual Tuning ................................ 127
Quick-tuning and Activating 121.500 MHz .................. 128
Auto-tuning the COM Frequency ................................ 129
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. Ax
TABLE OF CONTENTS
Frequency Spacing .................................................... 133
Automatic Squelch .................................................... 134
Volume .................................................................... 134
4.3 Controller Pilot Data Link Communications
(CPDLC) ........................................................................... 135
CPDLC Session Overview ........................................... 135
CPDLC System Status ................................................ 136
CPDLC Message Status Icons ..................................... 137
Connecting to the CPDLC System ............................... 138
Creating a Message .................................................. 140
Responding to an ATC Message ................................. 141
Viewing an ATC Message .......................................... 142
Viewing CPDLC Message Dialogs ............................... 142
Deleting Message Dialogs ......................................... 143
Disconnecting from the CPDLC System ....................... 144
Disabling Data Mode ................................................ 144
CPDLC System Failure ............................................... 144
4.4 NAV Operation ..................................................... 145
NAV Radio Selection and Activation ........................... 145
NAV Receiver Manual Tuning ..................................... 146
Auto-tuning a NAV Frequency from the MFD ............... 148
Marker Beacon Receiver ............................................ 152
ADF/DME Tuning ...................................................... 153
4.5 Mode S Transponder ........................................... 157
GTX 33/33D Transponder Controls .............................. 158
GTX 33/33D Transponder Mode Selection.................... 159
TCAS II Transponder Controls (optional) ...................... 161
TCAS II Transponder Mode Selection (optional) ............ 162
Entering a Transponder Code ..................................... 164
IDENT Function ........................................................ 165
Flight ID Reporting.................................................... 166
4.6 Additional Audio Panel Functions ..................... 167
Power-Up ................................................................. 167
Mono/Stereo Headsets .............................................. 167
Speaker ................................................................... 167
Intercom .................................................................. 168
Passenger Address (PA) System .................................. 169
Simultaneous COM Operation .................................... 169
Clearance Recorder and Player ................................... 170
Entertainment Inputs ................................................ 171
4.7 Audio Panels Preflight Procedure ......................172
4.8 Abnormal Operation ........................................... 174
Stuck Microphone ..................................................... 174
COM Tuning Failure ................................................... 174
PFD Failure, Dual System ...........................................174
Audio Panel Fail-safe Operation ................................. 175
Reversionary Mode ................................................... 176
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 177
Navigation Status Box ............................................... 178
5.2 Using Map Displays ............................................. 180
Map Orientation ....................................................... 180
Map Range .............................................................. 182
Map Panning ............................................................ 185
Measuring Bearing and Distance ................................ 190
Topography .............................................................. 191
Map Symbols ........................................................... 194
Airways ................................................................... 200
Track Vector ............................................................. 202
Wind Vector ............................................................. 203
Nav Range Ring........................................................ 204
Fuel Range Ring ....................................................... 205
Field of View (SVS) .................................................... 206
Selected Altitude Intercept Arc ................................... 207
5.3 Waypoints ............................................................. 208
Airports ................................................................... 209
Intersections ............................................................ 216
NDBs ....................................................................... 218
VORs ....................................................................... 220
User Waypoints ........................................................ 222
5.4 Airspaces .............................................................. 228
5.5 Direct-to-Navigation .......................................... 232
5.6 Flight Planning ..................................................... 238
Flight Plan Creation .................................................. 239
Adding Waypoints to an Existing Flight Plan ................ 244
Adding Airways to a Flight Plan ................................. 246
Adding Procedures to a Stored Flight Plan .................. 249
Flight Plan Storage ................................................... 256
Flight Plan Editing .................................................... 258
Along Track Offsets ................................................... 262
Parallel Track ............................................................ 263
Activating a Flight Plan Leg ....................................... 266
Inverting a Flight Plan ............................................... 267
Flight Plan Views ...................................................... 268
190-00728-06 Rev. A
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
xi
TABLE OF CONTENTS
Closest Point of FPL .................................................. 270
User-Defined Holding Patterns ................................... 270
5.7 Vertical Navigation ............................................. 275
Altitude Constraints .................................................. 277
5.8 Procedures ...........................................................281
Departures ............................................................... 282
Arrivals ................................................................... 285
Approaches ............................................................. 288
5.9 Trip Planning ........................................................ 296
Trip Planning ............................................................ 296
Weight Planning ....................................................... 300
Weight Caution And Warning Conditions .................... 302
5.10 RAIM Prediction................................................... 303
5.11 Navigating a Flight Plan ..................................... 307
5.12 Abnormal Operation ........................................... 335
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 338
Activating Services ................................................... 338
Using SiriusXM Weather Products .............................. 339
6.2 Garmin Connext Weather ................................... 373
Registering the system for Garmin Connext Weather .... 373
Accessing Garmin Connext Weather Products .............. 375
Connext Weather Data Requests ................................ 381
Garmin Connext Weather Products ............................. 385
Abnormal Operations ................................................ 397
6.3 Airborne Color Weather Radar .......................... 399
System Description ................................................... 399
Principles of Pulsed Airborne Weather Radar ............... 399
NEXRAD and Airborne Weather Radar ....................... 400
Antenna Beam Illumination ....................................... 400
Safe Operating Distance ............................................ 403
Basic Antenna Tilt Setup ............................................ 404
Weather Mapping and Interpretation ......................... 406
Ground Mapping and Interpretation ........................... 418
Weather Radar Overlay on the Navigation Map Page ... 419
System Status ........................................................... 420
6.4 TAWS-B ................................................................. 422
Displaying TAWS-B Data ............................................ 423
TAWS-B Page ........................................................... 426
TAWS-B Alerts .......................................................... 428
System Status ........................................................... 434
6.5 TAWS-A ................................................................. 436
Displaying TAWS-A Data ........................................... 437
TAWS-A Alerts .......................................................... 442
System Status ........................................................... 454
TAWS-A Abnormal operations .................................... 455
6.8 Profile View Terrain ............................................. 457
Profile View Display .................................................. 457
Profile Path .............................................................. 458
6.7 Traffic Information Service (TIS) ........................ 461
Displaying TRAFFIC Data ........................................... 462
Traffic Map Page ....................................................... 464
TIS Alerts ................................................................. 465
System Status ........................................................... 467
6.8 Garmin TCAS I Traffic .......................................... 469
Theory of operation .................................................. 469
TCAS I Alerts ............................................................ 472
System Test .............................................................. 473
Operation ................................................................ 474
6.9 TCAS II Traffic ....................................................... 483
TCAS II Symbology .................................................... 483
TCAS II Alerts ........................................................... 484
System Test .............................................................. 487
Operation ................................................................ 488
System Status ........................................................... 494
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 498
7.2 Flight Director Operation ................................... 500
Activating the Flight Director ..................................... 500
AFCS Status Box ....................................................... 501
Flight Director Modes ................................................ 502
Flight Director Selection ............................................ 502
Command Bars ......................................................... 503
7.3 Vertical Modes ..................................................... 504
Pitch Hold Mode (PIT) ............................................... 505
Selected Altitude Capture Mode (ALTS) ....................... 506
Altitude Hold Mode (ALT) .......................................... 506
Vertical Speed Mode (VS) .......................................... 508
Flight Level Change Mode (FLC) ................................. 509
Vertical Navigation Modes (VPTH, ALTV) ..................... 511
Glidepath Mode (GP) (sbas Only) ............................... 516
Glideslope Mode (GS) ............................................... 518
Takeoff (TO) and Go Around (GA) Modes .................... 519
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. Axii
TABLE OF CONTENTS
7.4 Lateral Modes ...................................................... 520
Roll Hold Mode (ROL) ............................................... 521
Low Bank Mode ....................................................... 521
Heading Select Mode (HDG) ...................................... 522
Navigation Modes (GPS, VOR, LOC, BC) ......................523
Approach Modes (GPS, VAPP, LOC) ............................. 525
7.5 Autopilot and Yaw Damper Operation ............. 527
Flight Control ........................................................... 527
Engaging the Autopilot and Yaw Damper .................... 528
Control Wheel Steering ............................................. 528
Disengaging the Autopilot and Yaw Damper ................ 529
7.6 Example Flight Plan ............................................ 530
Departure ................................................................ 531
Intercepting a VOR Radial .......................................... 533
Flying a Flight Plan/GPS Course ................................. 534
Descent ................................................................... 535
Approach ................................................................. 539
Go Around/Missed Approach ..................................... 542
7.7 AFCS Annunciations and Alerts ......................... 544
AFCS CAS Messages ................................................. 544
AFCS Voice Alerts ...................................................... 545
Overspeed Protection ................................................ 545
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 548
SVT Operation .......................................................... 549
SVT Features ............................................................ 551
Field of View ............................................................ 560
8.2 SafeTaxi ................................................................ 562
SafeTaxi Database Cycle Number and Revision ............ 565
8.3 ChartView ............................................................. 568
ChartView Softkeys ................................................... 569
Terminal Procedures Charts ....................................... 570
Chart Options ........................................................... 578
Day/Night View ........................................................ 584
ChartView Cycle Number and Expiration Date ............. 586
8.4 FliteCharts ............................................................ 589
FliteCharts Softkeys .................................................. 590
Terminal Procedures Charts ....................................... 591
Chart Options ........................................................... 598
Day/Night View ........................................................ 602
FliteCharts Cycle Number and Expiration Date ............. 604
8.5 Airport Directory ................................................. 607
Airport Directory Database Cycle Number and Revision 608
8.6 Satellite Telephone and SMS Messaging .......... 610
Registering With Garmin Connext .............................. 610
Telephone Communication ........................................ 611
Text Messaging (SMS) ............................................... 626
8.7 Wi-Fi Connections ............................................... 638
8.8 Maintenance Logs ............................................... 643
8.9 SiriusXM Satellite Radio Entertainment ........... 645
Activating SiriusXM Satellite Radio Services ................ 645
Using SiriusXM Satellite Radio ................................... 647
8.10 Scheduler .............................................................. 650
8.11 Electronic Checklists ........................................... 652
8.12 Abnormal Operation ........................................... 655
SVT Troubleshooting ................................................. 655
Reversionary Mode ................................................... 655
Unusual Attitudes ..................................................... 656
APPENDICES
Annunciations and Alerts ............................................. 659
CAS Messages .......................................................... 659
Comparator Annunciations ........................................ 663
Reversionary Sensor Annunciations ............................ 664
Prodigy
®
System Annunciations .................................. 665
Prodigy
®
System Message Advisories .......................... 669
TAWS-A Alerts .......................................................... 682
TAWS-B Alerts .......................................................... 684
TCAS I Alerts and Annunciations ................................ 685
TCAS II Alerts and Annunciations ............................... 686
CPDLC ATC Alert ....................................................... 687
Other Prodigy
®
Aural Alerts ........................................ 687
Flight Plan Import/Export Messages ........................... 688
Pilot Profile Import/Export Messages .......................... 688
Database Management ................................................ 689
Jeppesen Databases .................................................. 690
Garmin Databases .................................................... 693
Glossary .......................................................................... 701
Frequently Asked Questions ........................................ 707
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®
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TABLE OF CONTENTS
General TIS Information ............................................... 711
Introduction ............................................................. 711
TIS vs. TAS/TCAS ....................................................... 711
TIS Limitations.......................................................... 711
Display Symbols ............................................................ 713
INDEX
Index ................................................................................ I-1
Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-06 Rev. Axiv
TABLE OF CONTENTS
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®
Flight Deck 100 Pilot’s Guide
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the Prodigy
®
Integrated Flight Deck as installed in the Embraer Phenom
100. 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 1240A
Primary Flight Displays and Multi-
function Display
•
GIA 63W
Integrated Avionics Unit
•
GDC 74B
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GMA 1347D
Dual Audio System with Integrated
Marker Beacon Receiver
•
GTX 33/33D
Mode S Transponder (not used with
TCAS II)
•
GDL 69A
Satellite Data Link Receiver
•
GDL 59
Data Link (optional)
•
GDR 66
VHF Data Link Transceiver (optional)
•
GSR 56
Iridium Transceiver (optional)
•
GWX 68
Weather Radar (optional)
•
GCU 475
MFD Control Unit
•
GMC 715
AFCS Control Unit
•
GSD 41
Data Concentrator
•
GTS 850
TCAS 1 System (optional)
•
GA 36
and
GA 37
GPS/SBAS Antennas
•
GA 58
Traffic Avoidance System Antennas
•
GSA 81
AFCS Servos
•
GSM 86
Servo Gearboxes
A top-level system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, GA 58, or GSM
86).
NOTE: Refer to the AFCS section for details on the Garmin AFCS.
In the Embraer Phenom 100, the Garmin AFCS+ Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the system.
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®
Flight Deck 100 Pilot’s Guide
2
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS (LRU)
•
GDU 1240A
(3) – Each unit is configured as one of two PFDs or one MFD. The GDU 1240A features a 12-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. The unit installed in the center is designated the MFD.
These units communicate with each other and with the on-side GIA 63W Integrated Avionics Unit through a
High-Speed Data Bus (HSDB) connection.
•
GMA 1347D
(2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is
installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual
control of the display reversionary mode (red
DISPLAY BACKUP
button) and communicates with the on-side
GIA 63W, using an RS-232 digital interface.
•
GCU 475
(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
•
GMC 715
(1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing
communication with both PFDs.
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Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
3
SYSTEM OVERVIEW
•
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.
•
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 system, and it communicates with the on-side
GIA 63W, on-side GDU 1240A and on-side GRS 77, using an ARINC 429 digital interface. The GDC 74B is
designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace.
•
GEA 71
(3) – 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
1240A and the on-side GIA 63W. 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.
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®
Flight Deck 100 Pilot’s Guide
4
SYSTEM OVERVIEW
•
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 digital interface.
•
GTX 33
(1)
and GTX 33D
(1) – Solid-state transponders that provide Modes A/C/S capability and optional
1090 MHz Extended Squitter Automatic Dependent Serveillance (ADS-B out) transmission. The GTX 33D
includes Mode S with diversity and is indicated as ‘XPDR2’. The GTX 33 is indicated as ‘XPDR1’. 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. These transponders
are not used when the TCAS II option is installed.
•
GDL 69A
(1) – A satellite radio receiver that provides weather information to the MFD (and, indirectly, to the
inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates with the MFD via
HSDB connection. A subscription to the SiriusXM Satellite Radio service is required to enable the GDL 69A
capability.
•
GDL 59
(1) – Provides system WI-FI connectivity. GDL 59 operation is performed with the MFD through the
HSDB. Connectivity with the GSR 56 is through the RS-232 bus. Computers and/or EFBs (Electronic Flight
Bag) may also be connected through three Ethernet ports.
/
