This manual reflects the operation of System Software version 0743.06 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.
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. WATCH®, FliteCharts®, and
SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used
without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; and XM® is a registered trademark of
XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell
International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.
July, 2008 190-00685-00 Rev. A Printed in the U.S.A.
Warnings, Cautions & 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 the multi-function display 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 69A is approved only
for weather avoidance, not penetration.
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
190-00685-00 Rev. A
Warnings, Cautions & Notes
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.
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.”
190-00685-00 Rev. A
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
Warnings, Cautions & Notes
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 anomalies 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 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude between longitude 75º West
and 120º West. An area south of 55° South latitude between longitude 120º
East and 165º East.
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 ANTIREFLECTIVE 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 antireflective 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 aviation databases. Depictions of equipment
may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
190-00685-00 Rev. A
Warnings, Cautions & Notes
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: The purpose of this Cockpit Reference Guide is to provide the pilot
a resource with which to find operating instructions on the major features
of the Prodigy system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the complete system
are found in the Prodigy Flight Deck 100 Pilot’s Guide.
190-00685-00 Rev. A
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
Warnings, Cautions & Notes
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Cockpit Reference Guide for the Prodigy™ Flight Deck 100
190-00685-00 Rev. A
Record of Revisions
Part NumberChange Summary
190-00685-00Initial release
RevisionDate of RevisionAffected PagesDescription
AJuly, 2008Production release
190-00685-00 Rev. A
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
RR-1
Record of Revisions
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Cockpit Reference Guide for the Prodigy™ Flight Deck 100
INDEX .........................................................................................................................................Index-1
190-00685-00 Rev. A
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
iii
Table of Contents
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iv
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
190-00685-00 Rev. A
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE
Press the BARO Knob.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Select the PFD Softkey to display the second-level softkeys.
2)
Select the ALT UNIT Softkey.
3)
Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or
:
Select the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Select the BACK Softkey to return to the top-level softkeys.
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
InstrumentsEAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION
Window.
4)
Turn the
small
SYNCHRONIZE CDI
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the
190-00685-00 Rev. A
small
FMS Knob clockwise to ON or counterclockwise to OFF.
FMS Knob clockwise to ON or counterclockwise to OFF.
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
1
Flight Instruments
CHANGE NAVIGATION SOURCES
Flight
InstrumentsEAS
1)
Select the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
2)
Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
Nav/Com/
XPDR/AudioAFCSGPS Nav
frequency.
3)
Select the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Select the OBS Softkey to select OBS Mode.
2)
Turn the CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to slew the CDI Course Pointer to a course bearing directly
to the waypoint.
Flight
PlanningProcedures
3)
Select the OBS Softkey again to disable OBS Mode.
GENERIC TIMER
1)
Select the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
Hazard
Avoidance
Features
Additional
Abnormal
Operation
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
CONFIGURE VSPEED BUGS INDIVIDUALLY
AlertsAppendixIndex
Annun/
1)
Select the TMR/REF Softkey.
2)
Turn the
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
large
FMS Knob to highlight the desired Vspeed.
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
190-00685-00 Rev. A
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field.
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
TURN VSPEED BUGS ON OR OFF BY CATEGORY
1)
Press the TMR/REF Softkey.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Press the TMR/REF Softkey to remove the window.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to BARO.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
InstrumentsEAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
DISPLAYING WIND DATA
1)
Select the PFD Softkey.
2)
Select the WIND Softkey to display wind data below the Selected Heading.
3)
Select one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, select the OFF Softkey.
190-00685-00 Rev. A
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
Operation
Abnormal
Annun/
AlertsAppendixIndex
3
Flight Instruments
Flight
InstrumentsEAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
4
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
190-00685-00 Rev. A
ENGINE & AIRFRAME SYSTEMS
ENGINE INDICATION SYSTEM
Engine & Airframe Systems
12
InstrumentsEAS
Flight
11
1
2
1
XPDR/AudioAFCSGPS Nav
Nav/Com/
2
3
3
4
4
5
PlanningProcedures
Flight
5
6
6
7
7
Avoidance
Hazard
8
9
Additional
9
10
8
10
Features
Operation
Abnormal
11
EICAS Display (Normal Mode)
Engine Fan Rotation Speed
1
Interstage Turbine Temperature (ITT)
2
Engine High Pressure Compressor
3
Rotation Speed
4
Oil Pressure and Temperature
Fuel Display
5
6
Battery Voltmeter
190-00685-00 Rev. A
EIS Display (Reversionary Mode)
7
Pressurization Display
Speed Brake Status
8
Landing Gear Status
9
Flap Indicator
10
Trim Indicator
11
Thrust Rating Indication(top)/Automatic
12
Thrust Reserve status (bottom)
Cockpit Reference Guide for the Prodigy™ Flight Deck 100
Annun/
AlertsAppendixIndex
5
Engine & Airframe Systems
Thrust Rating
Flight
InstrumentsEAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Selecting a thrust rating:
1)
Select the SYSTEM Softkey.
2)
Flight
PlanningProcedures
Select the ENG SET Softkey
3)
To choose the continuous thrust rating, select the CON Softkey,
Or
:
To choose the maximum climb thrust rating, select the CLB Softkey.
4)
Select the BACK Softkey to return to the previous softkey level.
IndicationThrust Rating
CRZCruise
CLBClimb
CONContinuous
TOTakeoff
GAGo Around
Thrust Rating Indications
Hazard
Automatic Thrust Reserve
Avoidance
Features
Additional
Abnormal
Operation
Indication*Description
* When no indication is shown, ATR has not been enabled or armed