Garmin Embraer Prodigy 100 User guide

Type
User guide
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
www.garmin.com
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
Embraer Phenom 100
System Software 0734.19 or later
Embraer Prodigy
Flight Deck 100
Pilot’s Guide
Embraer Prodigy
Flight Deck 100
Embraer
Phenom 100
190-00728-02
Revision A
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE & AIRFRAME SYSTEMS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
190-00728-02 Rev. A
Copyright © 2008, 2009 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0734.19 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, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K.
Tel: 44/0870.8501241 Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
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 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.
September, 2009 190-00728-02 Rev. A Printed in the U.S.A.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
i
LIMITED WARRANTY
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made
at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty
does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED
OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR
PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole
discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit
the Garmin Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
190-00728-02 Rev. Aii
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: XM Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69 is approved only for weather avoidance, not penetration.
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent
delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for
short-range weather avoidance.
WARNING: The 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.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING: The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the 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).
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.
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.
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
190-00728-02 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
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.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-00728-00
190-00728-01
190-00728-02
A
A
A
July, 2008
March, 2009
September, 2009
All
All
Production release
Added ADF
Added ChartView and FliteCharts
Added TAS
Added flight plan import/export
Added other GDU 9.14 parameters
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
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
190-00728-02 Rev. Avi
REVISION INFORMATION
Bl a n k Pa g e
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
vii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 Prodigy
Controls ................................................... 7
MFD/PFD Controls ........................................................ 7
MFD Control Unit ......................................................... 9
AFCS Controls ............................................................ 10
Audio Panel Controls .................................................. 12
Softkey Function ......................................................... 14
1.4 Secure Digital Cards.............................................. 24
1.5 System Power-up ................................................... 25
1.6 System Operation .................................................. 26
Normal Operation ....................................................... 26
Reversionary Mode ..................................................... 27
AHRS Operation ......................................................... 28
Prodigy
System Annunciations ................................... 29
GPS Receiver Operation .............................................. 30
1.7 Accessing System Functionality .......................... 34
Menus ....................................................................... 34
MFD Page Groups ....................................................... 35
MFD System Pages...................................................... 39
1.8 Display Backlighting ............................................. 53
Automatic Adjustment ................................................ 53
Manual Adjustment .................................................... 53
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 58
Airspeed Indicator ...................................................... 58
Attitude Indicator ....................................................... 61
Altimeter ................................................................... 63
Vertical Speed Indicator (VSI) ....................................... 67
Vertical Deviation ....................................................... 67
Horizontal Situation Indicator (HSI) .............................. 68
Course Deviation Indicator (CDI) .................................. 73
2.2 Supplemental Flight Data .................................... 81
Temperature Displays .................................................. 81
Wind Data ................................................................. 82
Vertical Navigation (VNV) Indications ........................... 83
2.3 PFD Annunciations and Alerting Functions ........ 84
Prodigy
tm
System Annunciations ................................... 84
Marker Beacon Annunciations...................................... 85
Traffic Annunciations................................................... 85
TAWS Annunciations ................................................... 86
Altitude Alerting ......................................................... 86
Low Altitude Annunciation .......................................... 87
Minimum Descent Altitude/Decision Height Alerting ...... 87
Radar Altimeter .......................................................... 89
2.4 Abnormal Operations ........................................... 91
Altitude Alerting ......................................................... 91
Abnormal GPS Conditions ........................................... 91
Unusual Attitudes ....................................................... 92
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
3.1 Engine Indication System (EIS) ............................ 96
Takeoff Data Set Window ............................................97
Engine Indications ...................................................... 98
Fuel and Electrical Indications .................................... 100
Cabin Pressurization ................................................. 101
Landing Gear ........................................................... 102
Flaps and Trim .......................................................... 102
3.2 Synoptics .............................................................. 103
System Status ........................................................... 103
Environmental Control System (ECS) .......................... 104
Electrical .................................................................. 106
Fuel ......................................................................... 107
Ice Protection System ................................................ 108
Engine Maintenance ................................................. 110
3.3 Crew Alerting System (CAS) ............................... 111
CAS Message Prioritization ........................................ 111
CAS Messages .......................................................... 112
3.4 Abnormal Operations ......................................... 117
Engine ..................................................................... 117
Cabin Pressurization ................................................. 117
Flaps ....................................................................... 118
Trim ......................................................................... 118
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 119
Audio Panel Volume Control ...................................... 119
MFD/PFD Controls and Frequency Display ................... 120
Audio Panel Controls ................................................ 122
4.2 COM Operation .................................................... 124
COM Transceiver Selection and Activation ................... 124
COM Transceiver Manual Tuning ................................ 125
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
190-00728-02 Rev. Aviii
TABLE OF CONTENTS
Quick-tuning and Activating 121.500 MHz .................. 126
Auto-tuning the COM Frequency ................................ 127
Frequency Spacing .................................................... 131
Automatic Squelch .................................................... 132
Volume .................................................................... 132
4.3 NAV Operation ..................................................... 133
NAV Radio Selection and Activation ........................... 133
NAV Receiver Manual Tuning ..................................... 134
Auto-tuning a NAV Frequency from the MFD ............... 136
Marker Beacon Receiver ............................................ 141
ADF/DME Tuning ...................................................... 142
4.4 Mode S Transponder ........................................... 146
GTX 33/33D Transponder Controls .............................. 147
GTX 33/33D Transponder Mode Selection.................... 148
TCAS II Transponder Controls (optional) ...................... 150
TCAS II Transponder Mode Selection (optional) ............ 150
Entering a Transponder Code ..................................... 152
IDENT Function ........................................................ 153
Flight ID Reporting.................................................... 154
4.5 Additional Audio Panel Functions ..................... 155
Power-Up ................................................................. 155
Mono/Stereo Headsets .............................................. 155
Speaker ................................................................... 155
Intercom .................................................................. 156
Passenger Address (PA) System .................................. 157
Simultaneous COM Operation .................................... 157
Clearance Recorder and Player ................................... 158
Entertainment Inputs ................................................ 159
4.6 Audio Panels Preflight Procedure ...................... 160
4.7 Abnormal Operation ........................................... 162
Stuck Microphone ..................................................... 162
COM Tuning Failure ................................................... 162
PFD Failure, Dual System ........................................... 163
Audio Panel Fail-safe Operation ................................. 164
Reversionary Mode ................................................... 164
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 165
Navigation Status Box ............................................... 167
5.2 Using Map Displays ............................................. 168
Map Orientation ....................................................... 168
Map Range .............................................................. 170
Map Panning ............................................................ 173
Measuring Bearing and Distance ................................ 178
Topography .............................................................. 179
Map Symbols ........................................................... 182
Airways ................................................................... 188
Track Vector ............................................................. 190
Wind Vector ............................................................. 191
Nav Range Ring........................................................ 192
Fuel Range Ring ....................................................... 193
Field of View (SVS) .................................................... 194
5.3 Waypoints ............................................................. 195
Airports ................................................................... 196
Intersections ............................................................ 203
NDBs ....................................................................... 205
VORs ....................................................................... 207
User Waypoints ........................................................ 209
5.4 Airspaces .............................................................. 215
5.5 Direct-to-Navigation .......................................... 220
5.6 Flight Planning ..................................................... 226
Flight Plan Creation .................................................. 227
Adding Waypoints to an Existing Flight Plan ................ 232
Adding Airways to a Flight Plan ................................. 234
Adding Procedures to a Stored Flight Plan .................. 236
Flight Plan Storage ................................................... 243
Flight Plan Editing .................................................... 245
Along Track Offsets ................................................... 249
Parallel Track ............................................................ 250
Activating a Flight Plan Leg ....................................... 253
Inverting a Flight Plan ............................................... 254
Flight Plan Views ...................................................... 255
Closest Point of FPL .................................................. 257
5.7 Vertical Navigation ............................................. 258
Altitude Constraints .................................................. 260
5.8 Procedures ........................................................... 264
Departures ............................................................... 264
Arrivals ................................................................... 267
Approaches ............................................................. 269
5.9 Trip Planning ........................................................ 275
Trip Planning ............................................................ 275
Weight Planning ....................................................... 279
Weight Caution And Warning Conditions .................... 281
5.10 RAIM Prediction................................................... 282
5.11 Navigating a Flight Plan ..................................... 286
5.12 Abnormal Operation ........................................... 315
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
ix
TABLE OF CONTENTS
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather .......................................... 317
Activating Services .................................................... 318
Using XM Satellite Weather Products .......................... 319
6.2 Airborne Color Weather Radar .......................... 346
System Description ................................................... 346
Principles of Pulsed Airborne Weather Radar ............... 346
NEXRAD and Airborne Weather Radar ....................... 347
Antenna Beam Illumination ....................................... 347
Safe Operating Distance ............................................ 350
Basic Antenna Tilt Setup ............................................ 351
Weather Mapping and Interpretation ......................... 353
Ground Mapping and Interpretation ........................... 365
6.3 TAWS-B ................................................................. 366
Displaying TAWS-B Data ............................................ 367
TAWS-B Page ........................................................... 370
TAWS-B Alerts .......................................................... 372
System Status ........................................................... 378
6.4 TAWS-A ................................................................. 380
TAWS-A Page ........................................................... 382
TAWS-A Alerts .......................................................... 384
System Status ........................................................... 396
TAWS-A Abnormal operations .................................... 397
6.5 Traffic Information Service (TIS) ........................ 400
Displaying TRAFFIC Data ........................................... 401
Traffic Map Page ....................................................... 403
TIS Alerts ................................................................. 404
System Status ........................................................... 406
6.6 TCAS I TRAFFIC .................................................... 408
Theory of operation .................................................. 408
TCAS I Alerts ............................................................ 411
System Test .............................................................. 412
Operation ................................................................ 413
6.7 TCAS II Traffic ....................................................... 420
TCAS II Symbology .................................................... 420
TCAS II Alerts ........................................................... 421
System Test .............................................................. 424
Operation ................................................................ 425
System Status .......................................................... 431
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 434
7.2 Flight Director Operation ................................... 436
Activating the Flight Director ..................................... 436
AFCS Status Box ....................................................... 437
Flight Director Modes ................................................ 438
Flight Director Selection ............................................ 438
Command Bars ......................................................... 439
7.3 Vertical Modes ..................................................... 440
Pitch Hold Mode (PIT) ............................................... 441
Selected Altitude Capture Mode (ALTS) ....................... 442
Altitude Hold Mode (ALT) .......................................... 442
Vertical Speed Mode (VS) .......................................... 444
Flight Level Change Mode (FLC) ................................. 445
Vertical Navigation Modes (VPTH, ALTV) ..................... 447
Glidepath Mode (GP) (WAAS Only) ............................452
Glideslope Mode (GS) ............................................... 454
Takeoff (TO) and Go Around (GA) Modes .................... 455
7.4 Lateral Modes ...................................................... 456
Roll Hold Mode (ROL) ............................................... 457
Low Bank Mode ....................................................... 457
Heading Select Mode (HDG) ...................................... 458
Navigation Modes (GPS, VOR, LOC, BC) ...................... 459
Approach Modes (GPS, VAPP, LOC) ............................. 461
7.5 Autopilot and Yaw Damper Operation ............. 463
Flight Control ........................................................... 463
Engaging the Autopilot and Yaw Damper .................... 464
Control Wheel Steering ............................................. 464
Disengaging the Autopilot and Yaw Damper ................ 465
7.6 Example Flight Plan ............................................ 466
Departure ................................................................ 467
Intercepting a VOR Radial .......................................... 469
Flying a Flight Plan/GPS Course ................................. 470
Descent ................................................................... 471
Approach ................................................................. 475
Go Around/Missed Approach ..................................... 478
7.7 AFCS Annunciations and Alerts ......................... 480
AFCS CAS Messages ................................................. 480
AFCS Voice Alerts ...................................................... 481
Overspeed Protection ................................................ 481
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
190-00728-02 Rev. Ax
TABLE OF CONTENTS
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 484
SVS Operation .......................................................... 485
SVS Features ............................................................ 487
Field of View ............................................................ 495
8.2 SafeTaxi ................................................................ 497
SafeTaxi Database Cycle Number and Revision ............ 500
8.3 ChartView ............................................................. 503
ChartView Softkeys ................................................... 503
Terminal Procedures Charts ....................................... 504
Chart Options ........................................................... 512
Day/Night View ........................................................ 517
ChartView Cycle Number and Expiration Date ............. 520
8.4 FliteCharts ............................................................ 523
FliteCharts Softkeys .................................................. 523
Terminal Procedures Charts ....................................... 524
Chart Options ........................................................... 531
Day/Night View ........................................................ 535
FliteCharts Cycle Number and Expiration Date ............. 537
8.5 AOPA Airport Directory ....................................... 540
AOPA Database Cycle Number and Revision ............... 541
8.6 Satellite Telephone and Data Link Services ..... 543
Registering the Iridium Satellite System ...................... 543
Disable/Enable Iridium Transceiver.............................. 546
Telephone Communication ........................................ 547
WI-FI Connections .................................................... 560
System Data Logging ................................................ 565
8.7 XM Radio Entertainment .................................... 568
Activating XM Satellite Radio Services ........................ 568
Using XM Radio ....................................................... 570
8.8 Scheduler .............................................................. 573
8.9 Electronic Checklists ........................................... 575
8.10 Abnormal Operation ........................................... 578
SVS Troubleshooting ................................................. 578
Reversionary Mode ................................................... 578
Unusual Attitudes ..................................................... 579
APPENDICES
Annunciations and Alerts ............................................. 583
CAS Messages .......................................................... 583
Comparator Annunciations ........................................ 588
Reversionary Sensor Annunciations ............................ 589
Prodigy
System Annunciations ................................. 590
Prodigy
System Message Advisories ......................... 592
TAWS-A Alerts .......................................................... 605
TAWS-B Alerts .......................................................... 607
TCAS I Alerts and Annunciations ................................ 608
TCAS II Alerts and Annunciations ............................... 609
Other Prodigy
Aural Alerts ....................................... 610
Flight Plan Import/Export Messages ........................... 610
SD Card Use ................................................................... 613
Jeppesen Databases .................................................. 613
Garmin Databases .................................................... 616
Glossary .......................................................................... 623
Frequently Asked Questions ........................................ 629
General TIS Information ............................................... 633
Introduction ............................................................. 633
TIS vs. TAS/TCAS ....................................................... 633
TIS Limitations.......................................................... 633
Display Symbols ............................................................ 635
INDEX
Index ................................................................................I-1
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the 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
•
GSR 56
Iridium Transceiver
•
GWX 68
Weather Radar
•
GCU 475
MFD Control Unit
•
GMC 715
AFCS Control Unit
•
GSD 41
Data Concentrator
•
GA 36
and
GA 37
GPS/WAAS 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, or GSM 86).
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
In the Embraer Phenom 100, the GFC 700 Automated Flight Control System (AFCS) provides the flight director
(FD), autopilot (AP), and yaw damper (YD) functions of the system.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
2
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
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.
•
GIA 63W
(2) Functions as the main communication hub, linking all LRUs with the on-side PFD. Each
GIA 63W contains a GPS WAAS 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.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
3
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
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.
•
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.
•
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.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
•
GTX 33
(1)
and GTX 33D
(1) – Solid-state transponders that provide Modes A, C and S capability. 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 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 communicates with the MFD
via HSDB connection. A subscription to the XM 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.
•
GSR 56
(1) – 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.
•
GCU 475
(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GMC 715
(1) Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing
communication with both PFDs.
•
GWX 68
(1) – Provides airborne weather and ground mapped radar data to the MFD, through the GSD 41, via
HSDB connection.
•
GSD 41
(1) – This unit is a data concentrator used to expand the input and output capabilities of the system.
Communication is through the High Speed Data Bus.
•
GSA 81
(3) and
GSM 86
(3) The GSA 81 servos are used for the automatic control of pitch, roll, and yaw.
These units interface with each GIA 63W.
The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the
mechanical flight-control surface linkage.
•
GA 36
(1) and
GA 37
(1) The GA 36 is a through-mount GPS/WAAS antenna. The GA 37 is a through-mount
GPS/WAAS antenna with XM/Data Link.
GA 36 GA 37
190-00728-02 Rev. A
Embraer Prodigy
Flight Deck 100 Pilot’s Guide
6
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
GDU 1240A
(PFD #1)
GDU 1240A
(PFD #2)
GDU 1240A
(MFD)
GIA 63W #2
GSA 81
(Yaw)
GSA 81
(Roll)
GSA 81
(Pitch)
GRS 77 #1
GIA 63W #1
GMC 715
GMU 44 #1
GEA 71 #3
GEA 71 #1
GDC 74B #1
GMA 1347D
#2
GMA 1347D
#1
GTX 33 GTX 33D
GCU 475
GWX 68
GDL 69A
GRS 77 #2
GMU 44 #2
GDC 74B #2
VHF COM
VHF NAV/LOC
GPS/WAAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
VHF COM
VHF NAV/LOC
GPS/WAAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
GEA 71 #2
GSD 41
HSDB Rev
Switch*
* External to the G1000 system
Normal Mode
MFD Failed Mode
Hi
g
h Speed Data Bus
GSR 56
GDL 59
Figure 1-1 System LRU Configuration
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Garmin Embraer Prodigy 100 User guide

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