Garmin Embraer Phenom 100 Reference Guide

Embraer Prodigy™ Flight Deck 100

Cockpit Reference Guide

Embraer Phenom 100

System Software 0743.06 or later

FLIGHT INSTRUMENTS

ENGINE & AIRFRAME SYSTEMS

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2008 Garmin Ltd. or its subsidiaries. All rights reserved.

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.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: [phone] Fax: [phone]

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone] Fax [phone]

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: [phone] Fax: [phone]

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone] Fax: [phone]

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.

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.

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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 Number Change Summary

190-00685-00 Initial release

Revision Date of Revision Affected Pages Description

A July, 2008 Production 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

190-00685-00 Rev. A

Table of Contents

FLIGHT INSTRUMENTS ................................................................................................................ 1

Selecting the Altimeter Barometric Pressure Setting ...................................................... 1

Selecting Standard Barometric Pressure ............................................................................. 1

Change Altimeter Barometric Pressure Setting Units ...................................................... 1

Synchronizing the Altimeter Barometric Pressure Settings ........................................... 1

Synchronize CDI......................................................................................................................... 1

Change Navigation Sources ................................................................................................... 2

Enable/Disable OBS Mode While Navigating with GPS ....................................................2

Generic Timer ............................................................................................................................. 2

Configure Vspeed Bugs Individually ..................................................................................... 2

Turn Vspeed Bugs On or Off by Category ............................................................................ 3

Set Barometric Minimum Descent Altitude ........................................................................ 3

Displaying Wind Data ..............................................................................................................3

ENGINE & AIRFRAME SYSTEMS ............................................................................................. 5

Engine Indication System ....................................................................................................... 5

Synoptics .................................................................................................................................. 10

NAV/COM/TRANSPONDER/AUDIO PANEL ....................................................................... 19

Enter or Change Flight ID ..................................................................................................... 19

DME Tuning............................................................................................................................... 19

Enter a Transponder Code..................................................................................................... 19

Selecting a COM Radio .......................................................................................................... 20

Selecting a NAV Radio ........................................................................................................... 20

NAV/COM Tuning ..................................................................................................................... 20

Intercom .................................................................................................................................... 20

Passenger Address (PA) System ........................................................................................... 21

Clearance Recorder and Player ...........................................................................................21

AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................................... 23

Flight Director Activation ..................................................................................................... 23

Vertical Modes ......................................................................................................................... 24

Lateral Modes .......................................................................................................................... 25

GPS NAVIGATION ........................................................................................................................ 27

Direct-to Navigation .............................................................................................................. 27

Activate a Stored Flight Plan ............................................................................................... 28

Activate a Flight Plan Leg ..................................................................................................... 28

Stop Navigating a Flight Plan .............................................................................................. 29

Vertical Navigation (VNAV)................................................................................................... 29

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i

Table of Contents

FLIGHT PLANNING ...................................................................................................................... 31

Weight Planning ...................................................................................................................... 31

Trip Planning ............................................................................................................................ 31

Create a New User Waypoint ............................................................................................... 33

Delete a User Waypoint ......................................................................................................... 34

Create a New Flight Plan ...................................................................................................... 34

Insert a Waypoint in the Active Flight Plan ...................................................................... 36

Enter an Airway in a Flight Plan .......................................................................................... 36

Invert An Active Flight Plan .................................................................................................. 37

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 37

Store a Flight Plan .................................................................................................................. 38

Edit a Stored Flight Plan ....................................................................................................... 38

Delete a Waypoint from the Flight Plan ............................................................................ 38

Invert and Activate a Stored Flight Plan ...........................................................................39

Copy a Flight Plan ................................................................................................................... 39

Delete a Flight Plan ................................................................................................................ 39

Graphical Flight Plan Creation .............................................................................................40

PROCEDURES ................................................................................................................................. 41

Load and Activate a Departure Procedure ....................................................................... 41

Activate A Departure Leg ..................................................................................................... 41

Load An Arrival Procedure .................................................................................................... 41

Activate An Arrival Leg ......................................................................................................... 42

Load and/or Activate an Approach Procedure ................................................................. 42

Activate An Approach in the Active Flight Plan ............................................................... 43

Activate a Vector to Final Approach Fix ............................................................................ 43

Activate A Missed Approach in the Active Flight Plan ................................................... 44

HAZARD AVOIDANCE ................................................................................................................45

Customizing the Hazard Displays on the Navigation Map ............................................ 45

XM Weather (Optional) .......................................................................................................... 45

Traffic Information Service (TIS) ......................................................................................... 47

Terrain Awareness & Warning System (TAWS) Display ................................................... 48

Airborne Color Weather Radar ............................................................................................ 50

ADDITIONAL FEATURES ........................................................................................................... 53

SafeTaxi® ...................................................................................................................................53

XM® Radio Entertainment..................................................................................................... 53

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

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Table of Contents

ABNORMAL OPERATION..........................................................................................................57

Engine ........................................................................................................................................ 57

Cabin pressurization .............................................................................................................. 57

Flaps ........................................................................................................................................... 58

Trim ............................................................................................................................................ 58

Reversionary Mode ................................................................................................................ 58

Abnormal COM Operation .................................................................................................... 59

Hazard Displays with Loss of GPS Position ....................................................................... 59

Unusual Attitudes ................................................................................................................... 60

Dead Reckoning ...................................................................................................................... 60

ANNUNCIATIONS & ALERTS ................................................................................................... 63

CAS Messages .......................................................................................................................... 63

Aural Alerts .............................................................................................................................. 68

Other Prodigy™ Aural Alerts ................................................................................................. 68

Comparator Annunciations ................................................................................................... 69

Reversionary Sensor Annunciations ................................................................................... 69

TAWS Alerts .............................................................................................................................. 70

MFD & PFD Message Advisories .......................................................................................... 72

Database Message Advisories ............................................................................................. 73

GMA 1347D Message Advisories ......................................................................................... 76

GIA 63W Message Advisories ............................................................................................... 77

GSD 41 Message Advisories.................................................................................................. 80

GEA 71 Message Advisories .................................................................................................. 80

GTX 33/33D Message Advisories .......................................................................................... 81

GRS 77 Message Advisories ..................................................................................................81

GMU 44 Message Advisories ................................................................................................ 83

GDL 69A Message Advisories ............................................................................................... 83

GWX 68 Alert Messages ......................................................................................................... 84

GDC 74B Message Advisories ............................................................................................... 84

GCU 475 Message Advisories ............................................................................................... 85

GMC 715 Message Advisories .............................................................................................. 85

Miscellaneous Message Advisories ..................................................................................... 86

APPENDIX ....................................................................................................................................... 91

PFD Softkey Map .................................................................................................................... 91

MFD Softkey Map ................................................................................................................... 96

INDEX .........................................................................................................................................Index-1

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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

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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/

Alerts Appendix Index

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.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

Operation

Abnormal

Annun/

Alerts Appendix Index

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

Instruments EAS

Flight

11

1

2

1

XPDR/Audio AFCS GPS Nav

Nav/Com/

2

3

3

4

4

5

Planning Procedures

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/

Alerts Appendix Index

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.

Indication Thrust Rating

CRZ Cruise
CLB Climb

CON Continuous

TO Takeoff

GA Go 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

AlertsAppendixIndex

Annun/

in both engines.

Disabling/enabling Automatic Thrust Reserve (ATR):

1)

Select the SYSTEM Softkey.

2)

Select the ENG SET Softkey to display the Takeoff Data Set Window.

6

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

ATR ATR enabled in both engines

ATR ATR armed in both engines, but inactive

TO - RSV ATR activated in at least one engine

Automatic Thrust Reserve (ATR) Status

190-00685-00 Rev. A

Engine & Airframe Systems

3)

To disable ATR, select the ATR OFF Softkey;

Or

:

To enable ATR, select the ATR ON Softkey.

4)

If desired, change the OAT while the Takeoff Data Set Window is displayed.

5)

To confirm the selected takeoff settings and close the Takeoff Data Set
Window, select the ACCEPT Softkey,

Or

:

To cancel the operation, select the BACK Softkey.

Fuel and Electrical Indications

Engine Fuel Flow

Tank Fuel Quantity

Fuel Temperature

Fuel Display

Total Fuel Quantity

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Cabin Pressurization

Pressure Altitude

Pressure Differential

Oxygen System Pressure

190-00685-00 Rev. A

Electrical Display

High Landing Field Elevation

Pressure Change Rate

Landing Field Elevation

Cabin Pressure Display

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

7

Engine & Airframe Systems

Setting the displayed landing field elevation:

Flight

InstrumentsEAS

Select the

2)

Select the

3)

Select the FMS LFE Softkey to set the LFE to the value for the destination

SYSTEM

LFE

Softkey.

1)

airport in the current flight plan.

Or

:

Nav/Com/

XPDR/AudioAFCSGPS Nav

Use the ±500 and ±50 FT softkeys to set the desired elevation.

4)

To confirm the new LFE value, select the ACCEPT Softkey.

Speed Brakes and Landing Gear

Speed Brake Status

Flight

PlanningProcedures

Main Landing Gear

Left-side Landing

Softkey.

Gear

Right-side Landing
Gear

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Speed Brake and Landing Gear

Indications

Indication Description

CLOSED Speed brakes retracted

OPEN Speed brakes deployed

NOT AVAIL Invalid information

Speed Brake Indications

8

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Engine & Airframe Systems

Indication Description

Landing Gear Down

Instruments EAS

Flight

Flaps and Trim

Landing Gear Up

Landing Gear Transitioning
(Normal)

Landing Gear Locked Down

Landing Gear Locked Up

Landing Gear Transitioning
(Abnormal)

Landing Gear Position Indications

Flap Position

Flap Selected Bug

Flap Lever Setting

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00685-00 Rev. A

Flap and Trim Indications

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

Annun/

Alerts Appendix Index

9

Engine & Airframe Systems

SYNOPTICS

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

10

9

Flight

PlanningProcedures

31 42 5 6 7

8

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

System Clock

1

Static Air Temperature (SAT)

2

3

Total Air Temperature (TAT)

4

True Airspeed (TAS)

Aircraft Gross Weight

5

10

6

Hrdraulic Pressure

7

Oxygen

Emergency Brake Accumulator Pressure

8

Door Status

9

Electrical

10

System Status Synoptics Page

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Engine & Airframe Systems

Environmental Control System (ECS)

1

2 5

7

9

10

13

15

17

19

Cockpit Temperature Setting

1

Actual Cockpit Temperature

2

3

4

6

8

11

12

14

16

18

20

Outflow Valve (OFV) Status*

11

Heat Exchanger Pack Cooling Circuit

12

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

3

Cockpit Evaporator Fan

4

Cabin Temperature Setting

Actual Cabin Temperature

5

6

Cabin Evaporator Fan

7

Flow Control Shutoff Valve (FCV) 1

Flow Control Shutoff Valve (FCV) 2

8

Ram Air Valve (RAV)

9

Ram Air Duct

10

* Outflow valve (OFV) status is displayed only while the aircraft is parked or taxiing.

Environmental Control System Synoptics Page

190-00685-00 Rev. A

Bleed Line 1 (Left) Pressure

13

Bleed Line 2 (Right) Pressure

14

Cockpit Duct Temperature Setting

15

Cabin Duct Temperature Setting

16

Pressure Regulating Shutoff Valve (PRSOV) 1

17

Pressure Regulating Shutoff Valve (PRSOV) 2

18

Ground Cooling Fan (GCF)

19

Vapor Cycle System (VCS)

20

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

11

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

Unit Icons and Descriptions

Flight

InstrumentsEAS

Fan

On

Off

Heat Exchanger

Nav/Com/

XPDR/AudioAFCSGPS Nav

Vapor Cycle System

PRSOV

Flight

PlanningProcedures

Ram Air Duct From
NACA Scoop

Hazard

Avoidance

Ram Air Valve

Features

Additional

On

Off

On

Open with flow

Open, no flow Closed

Off

Airborne

Closed

Environmental Control System Unit Status Indications

Open, airborne

On ground

Open, on ground

Abnormal

Operation

AlertsAppendixIndex

Annun/

12

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Engine & Airframe Systems

Electrical

Generator

Bus

Battery

Ground Power Unit

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Unit Icons and Descriptions

Generator

Bus

Battery

190-00685-00 Rev. A

Electrical Synoptics Page

On

Off Bus

Normal

Abnormal

Normal

Electrical System Unit Status Indications

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

Abnormal

Additional

Features

Operation

Abnormal

Off

Annun/

Alerts Appendix Index

13

Engine & Airframe Systems

Fuel

Flight

InstrumentsEAS

1

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

2

4

6

8

10

12 13

14 15

Fuel Transfer SOV

1

Left Tank Fuel Quantity

2

3

Right Tank Fuel Quantity

4

Left DC Pump

Fuel 2 SOV

9

Total Fuel

10

Fuel Used

11

LH Pressure Switch

12

3

5

7

9

11

Abnormal

Operation

AlertsAppendixIndex

Annun/

14

Right DC Pump

5

6

Left Feed Ejector

7

Right Feed Ejector

Fuel 1 SOV

8

RH Pressure Switch

13

Left Engine Feed Line

14

Right Engine Feed Line

15

Fuel Synoptics Page

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Engine & Airframe Systems

Unit Icons and Descriptions

Instruments EAS

Flight

Fuel Line

Feed Ejector

Fuel Pressure
Switch

Valve

DC Pump

Fuel Transfer Valve

Operating

Operating

Not operating

Not operating

Operating

Not operation

Open with flow Open, no flow In transit

Operating

Open with flow

Fuel System Unit Status Indications

In transit

Not operating

XPDR/Audio AFCS GPS Nav

Nav/Com/

Closed

Planning Procedures

Flight

Closed

Avoidance

Hazard

Additional

Features

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

15

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

Ice Protection System

Flight

InstrumentsEAS

1

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

2

3

5

7

11

Windshield Heaters

1

Boot Lines and Valves

2

3

Inboard Ejector Flow Control Valve

4

Outboard Ejector Flow Control Valve

Engine Anti-ice 1 Bleed Duct and Lip Skin

5

6

Engine Anti-ice 2 Bleed Duct and Lip Skin

Ice Protection Synoptics Page

Blank Page

2

7

EAI 1 Valve and Bleed Line

EAI 2 Valve and Bleed Line

8

Pressure Regulating Shut-Off Valve 1

9

(PRSOV 1)
Pressure Regulating Shut-Off Valve 2

10

(PRSOV 2)
Ice Protection Bleed Duct

11

STAB EFCV

12

2

4

6

8

109

12

AlertsAppendixIndex

Annun/

16

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Engine & Airframe Systems

Unit Icons and Descriptions

Inboard/Outboard
EFCV and PRSOV

Open with flow Open, no flow

STB EFCV and, EAI
Valve

Open with flow Open, no flow

Ice Protection System Unit Status Indications

Closed

Closed

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

17

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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18

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ENTER OR CHANGE FLIGHT ID

1)

Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.

2)

Turn the small FMS Knob to enter the first character.

3)

Turn the large FMS Knob to select the next field.

4)

Turn the small FMS Knob to enter the next desired character.

5)

Repeat steps 3 and 4 until the desired Flight ID is entered.

6)

Press the ENT Key to update the Flight ID.

Nav/Com/XPDR/Audio Panel

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

DME TUNING

1)

Press the DME Softkey.

2)

If two DMEs are installed, turn the large FMS to select the DME source
field.

3)

Turn the small FMS Knob to select the desired Nav radio.

4)

Press the ENT Key to complete the selection.

ENTER A TRANSPONDER CODE

1)

Press the XPDR Softkey to display the transponder mode selection softkeys.

2)

If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder.

3)

Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.

4)

Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

19

Nav/Com/XPDR/Audio Panel

SELECTING A COM RADIO

Flight

InstrumentsEAS

Transmit/Receive

Press the COM1 MIC, COM2 MIC
the audio panel.

Receive Only

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the COM1, COM2

SELECTING A NAV RADIO

1)

Press the CDI Softkey to select NAV1 (VOR1/LOC1) or NAV2 (VOR2/LOC2).

2)

Pressing the NAV1, NAV2, DME, or ADF Key on the audio panel selects
and deselects the navigation radio audio source. All radio keys can be
selected individually or together.

Flight

PlanningProcedures

NAV/COM TUNING

1)

Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.

2)

Turn the respective tuning knobs to enter the desired frequency into the

Hazard

Avoidance

Features

Additional

standby frequency field. The large knob enters MHz and the small knob
enters kHz.

3)

Press the Frequency Transfer Key to place the frequency into the active
frequency field.

, or

COM3 MIC Key (HF, if installed) on

, or

COM3 Key (HF, if installed) on the audio panel.

INTERCOM

Abnormal

Operation

Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may

AlertsAppendixIndex

Annun/

select or deselect the intercom.

The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.

The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.

20

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Nav/Com/XPDR/Audio Panel

During manual squelch operation, pressing the ICS Knob switches between volume
and squelch adjustment, lighting the associated annunciator beneath the knob. When
the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When
the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.

PASSENGER ADDRESS (PA) SYSTEM

A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the headset only if the
PA Key is enabled on both audio panels. PA messages are one way from the flight deck
to the passengers.

CLEARANCE RECORDER AND PLAYER

NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.

Recorded COM audio is stored in separate memory blocks. Once 2.5
minutes of recording time have been reached, the recorder begins recording
over the stored memory blocks, starting from the oldest block.

The PLAY Key controls the play function. The PLAY annunciator is
illuminated to indicate when play is in progress. The PLAY annunciator
extinguishes after playback is finished.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Pressing the PLAY Key once plays the latest recorded memory block and
then returns to normal operation. Pressing the PLAY Key again during play
of a memory block stops play. If a COM input signal is detected during play
of a recorded memory block, play is halted.

Pressing the PLAY Key twice within one-half second while audio is playing
plays the previous block of recorded audio. Each subsequent two presses
of the PLAY Key within one-half second backtracks through the recorded
memory blocks to reach and play any recorded block.

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

21

Operation

Abnormal

Annun/

Alerts Appendix Index

Nav/Com/XPDR/Audio Panel

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

22

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

AUTOMATIC FLIGHT CONTROL SYSTEM

NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.

NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.

FLIGHT DIRECTOR ACTIVATION

An initial press of a key listed in the following table (when the flight director is not

active) activates the pilot-side flight director in the listed modes.

AFCS

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Control Pressed

Flight Director

Activated

Lateral Vertical

Modes Selected

FD Key (pilot-side) Pilot-side Roll Hold (default) ROL Pitch Hold (default) PIT

FD Key (copilot-side) Copilot-side Roll Hold (default) ROL Pitch Hold (default) PIT

AP Key Pilot-side Roll Hold (default) ROL Pitch Hold (default) PIT

CWS Button Pilot-side Roll Hold (default) ROL Pitch Hold (default) PIT

GA Switch Pilot-side

Roll Hold (default)
Roll Hold (default)

ROL

Takeoff (on ground)

ROL

Go Around (in air)TOGA

ALT Key Pilot-side Roll Hold (default) ROL Altitude Hold ALT

VS Key Pilot-side Roll Hold (default) ROL Vertical Speed VS

VNV Key Pilot-side Roll Hold (default) ROL Vertical Path Tracking* VPTH

GPS

NAV Key Pilot-side Navigation**

VOR

Pitch Hold (default) PIT

LOC

BC

APR Key Pilot-side Approach**

Pitch Hold (default)

GPS
VOR
LOC

Glidepath

Glideslope

PIT
GP
GS

HDG Key Pilot-side Heading Select HDG Pitch Hold (default) PIT

*Valid VNV flight plan must be entered before VNV Key press activates flight director.

**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before

or

APR

Key press activates flight director.

NAV

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

23

AFCS

VERTICAL MODES

Flight

InstrumentsEAS

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Nav/Com/

XPDR/AudioAFCSGPS Nav

Selected Altitude
Armed

Altitude Hold Holds the current Altitude Reference ALT Key A LT nnnnn f T

Vertical Speed

Flight Level Change,

Flight

PlanningProcedures

IAS Hold

Flight Level Change,
Mach Hold

VNAV

Hazard

Avoidance

VNAV Target
Altitude Armed

Features

Additional

Glidepath

Abnormal

Operation

Glideslope

AlertsAppendixIndex

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Go Around

* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude

is to be captured instead of VNAV Target Altitude

** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of

Selected Altitude

may be used to climb/descend to the
Selected Altitude

AFCS armed to capture the altitude
displayed in the Selected Altitude
window

Maintains the current aircraft vertical
speed; may be used to climb/descend
to the Selected Altitude

Maintains the current aircraft airspeed
(in IAS or Mach) while the aircraft is
climbing/descending to the Selected
Altitude

Captures and tracks the VNAV flight
path

AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
window

Captures and tracks the WAAS
glidepath on approach

Captures and tracks the ILS glideslope
on approach

Disengages the autopilot and
commands a constant pitch attitude
and wings level

(default) PIT

* ALTS

VS Key VS nnnn f p m

FLC nnn k T

FLC Key

FLC M .nnn

VNV

Key

** ALTV

APR Key

GA

Switch

VPTH

GP

GS

GA

24

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

AFCS

LATERAL MODES

Instruments EAS

Flight

Lateral Mode Description Control Annunciation

Holds the current aircraft roll attitude

Roll Hold

Low Bank

Heading Select

Navigation, GPS
Arm/Capture/Track

or rolls the wings level, depending on
the commanded bank angle

Limits the maximum commanded roll
angle

Captures and tracks the Selected
Heading

(default) ROL

BANK

Key

HDG

Key

*

HDG

GPS

XPDR/Audio AFCS GPS Nav

Nav/Com/

Navigation, VOR
Enroute Arm/
Capture/Track

Captures and tracks the selected
navigation source (GPS, VOR, LOC)

VOR

Planning Procedures

Flight

NAV

Navigation, LOC
Arm/Capture/Track

Key

LOC

(No Glideslope)
Navigation,

Backcourse Arm/
Capture/Track

Approach, GPS
Arm/Capture/Track**

Approach, VOR
Arm/Capture/Track

Approach, ILS Arm/
Capture/Track
(Glideslope Mode
automatically armed)

* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
** Glidepath Mode automatically arms if vertical guidance is available for the selected approach.

Captures and tracks a localizer signal
for backcourse approaches

Captures and tracks the selected
navigation source (GPS, VOR, LOC)

APR Key

BC

GPS

VAPP

LOC

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

25

AFCS

Cruise Speed Control (CSC)

Flight

Cruise Speed Control (CSC) is available while the AFCS Altitude Hold Mode is

InstrumentsEAS

active and the autopilot is engaged. When active, green arcs appear on the N1 gauges,
at values corresponding to the cruise speed selected.

Selecting Cruise Speed Control (CSC):

1)

Enter Altitude Hold Mode and engage the autopilot (see the AFCS Section

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

for details).

2)

Press the CSC Key (on the AFCS Control Unit).

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

26

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation using the MFD

1)

With the MFD selected on the controller, press the Direct-to

2)

Enter the waypoint identifier.

3)

Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.

4)

If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.

5)

Turn the large FMS Knob counterclockwise to place the cursor over the
‘VNV’ altitude field.

6)

Enter the desired altitude.

7)

Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.

8)

Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

9)

Press the ENT Key. The cursor is now flashing in the VNV offset distance field.

10)

Enter the desired offset distance before (-) the waypoint.

11)

Press the ENT Key. The ‘Activate?’ field is highlighted.

12)

Press the ENT Key to activate.

GPS Navigation

( )

Key.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Direct-to Navigation using the PFD

1)

Press the Direct-to Key

2)

Turn the large FMS Knob to place the cursor in the desired selection field.

3)

Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.

4)

Press the ENT Key.

5)

The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.

6)

Turn the large FMS Knob counterclockwise to place the cursor over the
‘ALT’ altitude field.

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

( )

on the PFD or controller.

27

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude constraint.

8)

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

ACTIVATE A STORED FLIGHT PLAN

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.

9)

Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

10)

Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.

11)

Turn the small FMS Knob to enter the desired offset distance (-) from the

selected Direct-to.

12)

Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to

highlight the ‘CRS’ field.

13)

Turn the small FMS Knob to enter the desired course to the waypoint.

14)

Press the ENT Key to highlight ‘ACTIVATE?’.

15)

Press the ENT Key again to activate the Direct-to.

1)

Press the FPL Key and turn the small FMS Knob to display the Flight Plan
Catalog Page.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan

4)

Select the ACTIVE Softkey. The confirmation window is now displayed.

5)

With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.

ACTIVATE A FLIGHT PLAN LEG

Abnormal

Operation

1)

From the Active Flight Plan Page, press the FMS Knob to activate the cursor

AlertsAppendixIndex

Annun/

and turn the large FMS Knob to highlight the desired waypoint.

2)

Select the ACT LEG Softkey.

OR

Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from

the PFD.

3)

With ‘Activate’ highlighted, press the ENT Key.

28

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)

Press the FPL Key to display the Active Flight Plan Page.

2)

Press the MENU Key to display the Page Menu Window.

3)

Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.

VERTICAL NAVIGATION (VNAV)

The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.

Large White

Text

Large Light

Blue Text

Small Light

Blue Text

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

Altitudes associated with arrival and approach procedures are “auto-designated”.
This means the system will automatically use the altitudes loaded with the arrival

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

29

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

or approach for giving vertical flight path guidance outside the FAF. Note that these
altitudes will be displayed as small light blue text.

Flight

InstrumentsEAS

Altitudes that are designated for use in vertical navigation may also be made “non­designated” by placing the cursor over the desired altitude and pressing the CLR Key.
The altitude is now displayed only as a reference. It will not be used to give vertical
flight path guidance. Other displayed altitudes may change due to re-calculations
or rendered invalid as a result of manually changing an altitude to a non-designated
altitude.

Nav/Com/

XPDR/AudioAFCSGPS Nav

White Text Light Blue Text Light Blue

Subdued Text

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Large Text

Small Text

Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
flight path guidance.

Altitude is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
and is provided as a
reference.

Altitude has been
entered by the pilot.
Altitude is designated
for use in giving
vertical flight path
guidance. Altitude
does not match the
published altitude in
navigation database or
no published altitude
exists.

Altitude is designated
for use in giving vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches
a published altitude
in the navigation
database.

The system cannot
use this altitude in
determining vertical
flight path guidance.

The system cannot
use this altitude in
determining vertical
flight path guidance.

30

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Flight Planning

Instruments EAS

Flight

Entering Weight Parameters

The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large
small

FMS

Knob to select the first rectangular page icon.

1)

Select the EMPTY WT Softkey to place the cursor in the Basic Empty

FMS

Knob to select the ‘AUX’ page group. Turn the

Weight field.

2)

Enter the desired aircraft empty weight.

3)

Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ field.

4)

Enter the desired weight of Pilot & Stores.

5)

Press the ENT Key.

6)

Continue repeating these steps until all desired weights have been entered.

Entering Fuel Parameters

1)

If necessary, press the FMS Knob to activate the cursor.

2)

Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.

3)

Select the FOB SYNC Softkey to enter the fuel on board quantity as read
from the aircraft fuel quantity sensors.

Or:

Manually enter the desired fuel quantity.

4)

Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field.

5)

Enter the desired reserve fuel quantity.

6)

Press the FMS Knob to remove the cursor.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

TRIP PLANNING

1)

Turn the large FMS Knob to select the ‘AUX’ page group.

2)

Turn the small FMS Knob to select the second rectangular page icon.

3)

The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL
Softkey.

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31

Flight Planning

4)

For Direct-to planning:

Flight

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XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

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AlertsAppendixIndex

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a)

b)

c)

d)

Or:

For point-to-point planning:

a)

b)

c)

d)

Or:

For flight plan leg planning:

a)

b)

c)

d)

Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).

If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.

Press the ENT Key and the flashing cursor moves to the ending
waypoint field.

Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.

Enter the identifier of the starting waypoint.

Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.

Again, enter the identifier of the ending waypoint.

Press the ENT Key to accept the waypoint.

Select the FPL Softkey (at the bottom of the display).

Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.

Turn the large FMS Knob to highlight the ‘LEG’ field.

Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ will be an available option to display planning data
for the remainder of the flight plan.

NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.

32

5)

Turn the large FMS Knob to highlight the departure time (DEP TIME) field.

NOTE: The departure time on the Trip Planning Page is used for preflight

planning. Refer to the Utility Page for the actual flight departure time.

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Flight Planning

6)

Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.

7)

Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’
page mode, fuel flow is provided by the system.

8)

The flashing cursor moves to the fuel onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.

9)

The flashing cursor moves to the calibrated airspeed field. Enter a calibrated
airspeed. Press the ENT Key when finished.

CREATE A NEW USER WAYPOINT

1)

Turn the large FMS Knob to select the ‘WPT’ page group.

2)

Turn the small FMS Knob to select the User WPT Information Page.

3)

Select the NEW Softkey. A waypoint is created at the current aircraft
position.

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the
waypoint can be defined by a reference waypoint. Use one of the following
methods to enter the reference waypoint:

a)

Turn the small FMS Knob to the left to display a list of flight plan
waypoints. This list is populated only when there is an active flight
plan.

b)

Turn the large FMS Knob to select the desired waypoint.

c)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘NRST’ waypoints
to the aircraft’s current position.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

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33

Flight Planning

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list

Flight

InstrumentsEAS

7)

Nav/Com/

XPDR/AudioAFCSGPS Nav

8)

9)

10)

11)

Flight

PlanningProcedures

DELETE A USER WAYPOINT

1)

2)

3)

Hazard

Avoidance

4)

5)

Features

Additional

6)

7)

Abnormal

Operation

is displayed.

b)

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

After pressing the ENT Key, the cursor is displayed in the ‘RAD’ (radial)
field. Enter the desired radial from the reference waypoint.

Press the ENT Key.

The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.

Press the ENT Key. The cursor is now placed for entering another reference

waypoint, if desired.

Press the FMS Knob to remove the flashing cursor.

Turn the large FMS Knob to select the ‘WPT’ page group.

Turn the small FMS Knob to select the User WPT Information Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.

Turn the small FMS Knob to highlight the desired waypoint.

Select the DELETE Softkey.

The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.

CREATE A NEW FLIGHT PLAN

AlertsAppendixIndex

Annun/

NOTE: When creating a new flight plan in the Active Flight Plan Window,

the first leg is activated automatically after it is created.

34

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Flight Planning

Using the MFD

1)

Press the FPL Key.

2)

Turn the small FMS Knob to display the Flight Plan Catalog Page.

3)

Select the NEW Softkey to display a blank flight plan for the first empty storage
location.

4)

Turn the small FMS Knob to display the Waypoint Information Window.

5)

Enter the identifier of the departure waypoint.

6)

Press the ENT Key.

7)

Repeat step number 4, 5, and 6 to enter the identifier for each additional
flight plan waypoint.

8)

When all waypoints have been entered, press the FMS Knob to return to the
Flight Plan Catalog Page. The new flight plan is now in the list.

Using the PFD

NOTE: If a flight plan is active, an additional flight plan cannot be entered

using the PFD.

1)

Press the FPL Key.

2)

Turn the small FMS Knob to display the Waypoint Information Page.

3)

Turn the small FMS Knob to enter the first letter of the destination waypoint
identifier.

4)

Turn the large FMS Knob to the right to move the cursor to the next character
position.

5)

Repeat step 3 and 4 to spell out the rest of the waypoint identifier.

6)

Press the ENT Key and the cursor is now ready for entering of the next flight
plan waypoint.

7)

Repeat steps 3 through 6 to enter the identifier for each additional flight plan
waypoint.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

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Planning Procedures

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Avoidance

Hazard

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Operation

Abnormal

Annun/

Alerts Appendix Index

8)

Once all waypoints have been entered, press the FMS Knob to remove the
cursor. The new flight plan is now active.

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

35

Flight Planning

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

1)

Press the FPL Key to display the active flight plan.

2)

If necessary, press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.

4)

Turn the small FMS Knob. The Waypoint Information Window is now
displayed.

5)

Enter the new flight plan waypoint by one of the following:

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

e)

Press the ENT Key again to “accept” the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

AlertsAppendixIndex

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1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor (not required on the PFD).

3)

Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.

36

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Flight Planning

4)

Turn the small FMS Knob one click clockwise and select the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).

5)

Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”

altitude airways, and then high altitude airways.

6)

Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.

7)

Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.

INVERT AN ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the MENU Key to display the Page Menu.

3)

Turn the large FMS Knob to highlight ‘Invert Flight Plan’.

4)

Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.

5)

With ‘OK’ highlighted, press the ENT Key to invert the flight plan.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT

PLAN

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

a)

Press the MFD FPL Key and turn the small FMS Knob to select the
Flight Plan Catalog Page.

b)

Press the FMS Knob to activate the cursor.

c)

Turn the large FMS Knob to highlight the desired flight plan.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.

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Alerts Appendix Index

Flight Planning

3)

Press the CLR Key to display a confirmation window.

4)

Flight

InstrumentsEAS

With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.

STORE A FLIGHT PLAN

1)

After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.

Nav/Com/

XPDR/AudioAFCSGPS Nav

2)

Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.

3)

With ‘OK’ highlighted, press the ENT Key to store the flight plan.

EDIT A STORED FLIGHT PLAN

1)

Press the FPL Key for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.

2)

Press the FMS Knob to activate the cursor.

Flight

PlanningProcedures

3)

Turn the large FMS Knob to highlight the desired flight plan.

4)

Select the EDIT Softkey.

5)

Turn the large FMS Knob to place the cursor in the desired location.

6)

Enter the changes, then press the ENT Key.

7)

Hazard

Avoidance

Press the FMS Knob to return to the Flight Plan Catalog Page.

DELETE A WAYPOINT FROM THE FLIGHT PLAN

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

38

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

a)

Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.

b)

Press the FMS Knob to activate the cursor.

c)

Turn the large FMS Knob to highlight the desired flight plan.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the waypoint to be deleted.

3)

Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Flight Planning

4)

With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.

5)

Once all changes have been made, press the FMS Knob to remove the
cursor.

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Press the FPL Key on the MFD or MFD Control Unit.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the desired flight plan.

5)

Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.

6)

With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.

COPY A FLIGHT PLAN

1)

Press the FPL Key on the MFD or MFD Control Unit.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be copied.

5)

Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.

6)

With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

DELETE A FLIGHT PLAN

1)

Press the FPL Key on the MFD or MFD Control Unit.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be deleted.

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

39

Flight Planning

5)

Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is

Flight

InstrumentsEAS

displayed.

6)

With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

GRAPHICAL FLIGHT PLAN CREATION

1)

Press the FPL Key to display the Active Flight Plan Page on the MFD.

Nav/Com/

XPDR/AudioAFCSGPS Nav

2)

Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.

3)

The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted
the cursor. Turn the large FMS Knob to select the desired insertion point.

4)

Flight

PlanningProcedures

Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.

5)

To change the user waypoint name, follow the procedure for modifying a user
waypoint.

ABOVE

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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40

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.

3)

Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.

4)

Turn the large FMS Knob to highlight the desired departure.

5)

Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.

6)

Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.

7)

Turn the large FMS Knob to highlight the desired transition.

8)

Press the ENT Key.

9)

With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.

Procedures

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key on the MFD or MFD Control Unit to display the active
flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired waypoint within the
departure.

4)

Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AN ARRIVAL PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.

3)

Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.

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41

Avoidance

Hazard

Additional

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Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

Flight

InstrumentsEAS

Press the ENT Key. A list of transitions is displayed for the selected arrival.

6)

Turn either FMS Knob to select the desired transition.

7)

Press the ENT Key. A list of runways may be displayed for the selected
arrival.

8)

Turn the large FMS Knob to highlight the desired runway.

9)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key.

10)

With ‘LOAD?’ highlighted, press the ENT Key.

11)

The arrival becomes part of the active flight plan.

ACTIVATE AN ARRIVAL LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Flight

PlanningProcedures

Turn the large FMS Knob to highlight the desired waypoint within the
arrival.

4)

Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Hazard

Avoidance

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

Features

Additional

NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some

published approach procedures for the desired airport may not be displayed
in the list of available approaches.

Abnormal

Annun/

Operation

AlertsAppendixIndex

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT APPROACH’.

3)

Press the ENT Key. A list of available approaches for the destination airport
is displayed.

4)

Turn either FMS Knob to highlight the desired approach.

5)

Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.

6)

Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of

42

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Procedures

the approach and will provide navigation guidance relative to the final
approach course.

7)

Press the ENT Key. The cursor moves to the MINIMUMS field.

8)

If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small

FMS

Knob in the

direction of the green arrow to change the display from OFF to BARO.

9)

Press the

FMS

ENT

Key. The cursor moves to the altitude field. Turn the small

Knob to enter the published DA/MDA for the selected approach

procedure.

10)

Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’

highlighted.

11)

Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.

Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.

12)

Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.

3)

Press the ENT Key.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

ACTIVATE A VECTOR TO FINAL APPROACH FIX

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.

3)

Press the ENT Key.

4)

The final approach course becomes the active leg.

190-00685-00 Rev. A

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Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.

3)

Press the ENT Key. A confirmation window is displayed.

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the go-around button.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

44

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

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Hazard Avoidance

HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1)

With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.

2)

Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.

3)

Press the small FMS Knob to return to the Navigation Map Page.

XM WEATHER (OPTIONAL)

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

WARNING: Use of XM weather for hazardous weather penetration is not

recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.

Displaying XM Weather on the Navigation Map Page

1)

Select the MAP Softkey.

2)

Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Select the applicable softkey again to remove weather data from the
Navigation Map Page.

Display METAR and TAF information on the Airport Information Page

1)

Turn the large FMS Knob to select the WPT Page Group.

2)

Turn the small FMS Knob to select the Airport Information Page.

3)

Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).

Displaying Weather on the Weather Data Link Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the Weather Data Link Page.

3)

Select the available softkeys to select the desired XM weather product.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

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45

Hazard Avoidance

4)

Select the LEGEND Softkey to view the legends for the selected products.

Flight

InstrumentsEAS

If necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.

Map Panning Information – Weather Data Link Page

1)

Push in the Joystick to display the panning arrow.

2)

Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

or SIGMETs.

3)

Press the ENT Key to display pertinent information for the selected product.

Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.

Weather Products and Symbols

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

NEXRAD

46

Cell Movement

XM Lightning

Cloud Top

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

SIGMETs/AIRMETs

City Forecast

METARs

Freezing Levels

Surface Analysis

Cyclone Warnings

County Warnings

Winds Aloft

190-00685-00 Rev. A

Hazard Avoidance

TRAFFIC INFORMATION SERVICE (TIS)

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.

NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.

Traffic Symbol Description

Non-Threat Traffic

(intruder is beyond 5 nm and greater than 1200’ vertical separation)

Traffic Advisory (TA)

(closing rate, distance, and vertical separation meet TA criteria)

Traffic Advisory Off Scale

Traffic Symbol Description

Displaying Traffic on the Traffic Map Page

1)

Turn the large FMS Knob to select the Map Page Group.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

2)

Turn the small FMS Knob to select the Traffic Map Page.

3)

Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.

4)

Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.

5)

Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.

Displaying Traffic on the Navigation Map

1)

Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.

2)

Select the TRAFFIC Softkey. Traffic is now displayed on the map.

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47

Additional

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Operation

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Annun/

Alerts Appendix Index

Hazard Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

Flight

InstrumentsEAS

WARNING: The TAWS display shows supplemental information only. It should

not be used for navigation.

NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.

Nav/Com/

XPDR/AudioAFCSGPS Nav

NOTE: TAWS operation is only available when the system is configured for

a TAWS-B installation.

Manual System Test

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Test TAWS’.

3)

Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center

Flight

PlanningProcedures

of the TAWS Page.
When all is in working order, “TAWS System Test, OK” is heard.

Display Terrain on the TAWS Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Turn the small FMS Knob to select the TAWS Page.

3)

If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.

4)

Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.

Color Terrain/Obstacle Location

Yellow

Black

Red

Terrain/Obstacle above or within 100’
below current aircraft altitude.

Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.

Terrain/Obstacle is more than 1000’

below aircraft altitude.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Hazard Avoidance

Enable/Disable Aviation Data

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.

3)

Press the ENT Key.

TAWS Inhibit

NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.

Inhibit TAWS

While the TAWS Page is displayed, select the INHIBIT Softkey.

Or

:

1)

Press the MENU Key.

2)

Turn the small FMS Knob to select ‘Inhibit TAWS’.

3)

Press the ENT Key.

Enable TAWS

While the TAWS Page is displayed, select the INHIBIT Softkey.

Or

:

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Enable TAWS’.

3)

Press the ENT Key.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

49

Alerts Appendix Index

Annun/

Hazard Avoidance

AIRBORNE COLOR WEATHER RADAR

Flight

InstrumentsEAS

WARNING: Begin transmitting only when it is safe to do so. If it is desired to

transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.

CAUTION: In Standby Mode, the antenna is parked at the center line. It

Nav/Com/

XPDR/AudioAFCSGPS Nav

is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.

Displaying Weather on the Weather Radar Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the Weather Radar Page.

3)

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Select the MODE Softkey.

4)

If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.

Or

:

If the aircraft is already airborne, select the WEATHER or GROUND
Softkey. The one-minute warm-up period will be initiated, after which the
radar will begin transmitting. The horizontal scan is initially displayed.

5)

Turn the Joystick to select the desired range.

6)

If desired, select the VERTICAL Softkey for vertical scanning.

Abnormal

Operation

Adjusting Antenna Tilt

Move the

AlertsAppendixIndex

Annun/

tor the displayed tilt value in the TILT field.

Joystick

up or down to adjust the tilt of the antenna up or down. Moni-

When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt

of the antenna. If the Tilt Line is not displayed, perform the following steps:

1)

Press the MENU Key

2)

Turn the large FMS Knob to select ‘Show Tilt Line’.

3)

Press the ENT Key.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Hazard Avoidance

Adjusting Antenna Bearing

Move the

Joystick

right or left to adjust the azimuth position of the antenna right

or left. Monitor the displayed bearing value in the BEARING field.

When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:

1)

Press the MENU Key

2)

Turn the large FMS Knob to select ‘Show Bearing Line’.

3)

Press the ENT Key.

Vertically Scan a Storm Cell

1) While in the Horizontal Scan view, move the Joystick to place the Bearing

Line on the desired storm cell, or other area, to be vertically scanned.

2)

Select the VERTICAL Softkey. A vertical “slice” of the selected area will
now be displayed.

3)

Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.

4)

Turn the Joystick to adjust the range.

5)

To select a new area to be vertically scanned, select the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Adjusting Gain

WARNING: Changing the gain in Weather Mode will cause precipitation
intensity to be displayed as a color not representative of the true intensity.
Remember to return the gain setting to ‘Calibrated’ for viewing the actual
intensity of precipitation.

1)

Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.

2)

Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.

3)

Press the FMS Knob to remove the cursor.

4)

Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.

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51

Additional

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Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Ground Mapping

1)

Flight

InstrumentsEAS

Select the MODE Softkey.

2)

Select the GROUND Softkey to place the radar in Ground Map Mode.

3)

Select the BACK Softkey.

Sector Scan

1)

While in the Horizontal Scan Mode, move the Joystick right or left to place

Nav/Com/

XPDR/AudioAFCSGPS Nav

the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.

2)

Press the FMS Knob to display the cursor.

3)

Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.

4)

Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.

5)

If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.

6)

Flight

PlanningProcedures

Press the FMS Knob to remove the cursor.

Antenna Stabilization

1)

To activate or deactivate the antenna stabilization, select the MODE
Softkey.

2)

Hazard

Avoidance

Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.

Weather Attenuated Color Highlight (WATCH®)

Features

Additional

To activate or deactivate the WATCH® feature, select the WATCH Softkey. This

feature is only available in the Horizontal Scan Mode.

Abnormal

Operation

Weather Alert

To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating

AlertsAppendixIndex

Annun/

and deactivating will also enable or inhibit the alert on the PFD.

Automatic Standby

When the weather radar system is in the Weather or Ground Map Mode, upon

landing the system will automatically switch to Standby Mode.

52

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

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Additional Features

ADDITIONAL FEATURES

Instruments EAS

Flight

SAFETAXI

®

SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.

Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR Softkey again cycles
back to the original map detail.

The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams aid in following ground control instructions by accurately displaying
the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and
services. This database is updated on a 56-day cycle.

XM® RADIO ENTERTAINMENT

The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.

Selecting the XM Radio Page

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

1)

Turn the large FMS Knob to select the Auxiliary Page Group.

2)

Turn the small FMS Knob to select the displayed AUX - XM Information
Page.

3)

Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.

Active Channel and Channel List

The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.

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53

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Selecting a Category

Flight

Nav/Com/

The Category Box of the XM Radio Page displays the currently selected category

InstrumentsEAS

of audio.

1)

Select the CATGRY Softkey on the XM Radio Page.

2)

Select the CAT + and CAT - softkeys to cycle through the categories.

Or

:

XPDR/AudioAFCSGPS Nav

Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.

3)

Press the ENT Key.

Select an Available Channel within the Selected Category

1)

While on the XM Radio Page, select the CHNL Softkey.

2)

Select the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.

Flight

PlanningProcedures

Or

:

Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.

3)

With the desired channel highlighted, press the ENT Key.

Entering a Channel Directly

Hazard

Avoidance

1)

While on the XM Radio Page, select the CHNL Softkey.

2)

Features

Additional

Abnormal

Operation

Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.

3)

Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.

4)

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

AlertsAppendixIndex

Annun/

Up to 15 channels from any category can be assigned a preset number.

1)

On the XM Radio Page, with the desired channel active, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).

2)

Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.

54

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Additional Features

3)

Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.

4)

Select the SET Softkey on the desired channel number to save the channel
as a preset.

Adjusting Volume

1)

With the XM Radio Page displayed, select the VOL Softkey.

2)

Select the VOL – Softkey to reduce volume or select the VOL + Softkey to
increase volume. (Once the VOL Softkey is selected, the volume can also be
adjusted using the small FMS Knob.)

3)

Select the MUTE Softkey to mute the audio. Select the MUTE Softkey
again to unmute the audio.

Radio volume may also be adjusted at each passenger station.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

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Abnormal Operation

ABNORMAL OPERATION

NOTE: The Embraer Phenom 100 Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.

Instruments EAS

Flight

ENGINE

When an engine failure occurs, besides the CAS message corresponding to the
failed engine (“E1 FAIL” or “E2 FAIL”), the corresponding N1 gauge displays the an­nunciation “FAIL” in yellow (Figure 3-21). Detection of an engine fire causes the red
annunciation “FIRE” to be displayed over the ITT gauge.

Engine Failure Indication Engine Fire Indication

CABIN PRESSURIZATION

If low flow or a cabin leak is detected, the cabin pressure change rate readout and
arrow turn red.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00685-00 Rev. A

Cabin Leak Indication

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

57

Alerts Appendix Index

Annun/

Abnormal Operation

FLAPS

Flight

The following denote abnormal flap conditions:

InstrumentsEAS

• Flaps not in position for takeoff – Flap pointer and readout turn red (A and B).

• Flaps have failed or become jammed – Flap pointer and readout turn yellow (C)

• Flaps unavailable – Flap pointer is removed and readout turns light blue (D)

Nav/Com/

XPDR/AudioAFCSGPS Nav

A - Flaps Retracted

at Takeoff

B - Flaps at FULL

(Landing) Position at

C - Flaps Failed D - Flaps Unavailable

Takeoff

TRIM

Aileron or rudder mistrim are denoted with yellow arrows pointing in the direction

Flight

PlanningProcedures

of mistrim on the Roll and Yaw Trim indicators (A).

If takeoff configuration has been selected and the pitch trim position is not within
the green band on the pitch trim scale, the pointers and readout turn red (B). If an
asymmetrical pitch trim condition exists, the pointers and readout turn yellow (C).

Aileron

Hazard

Mistrim

Avoidance

Rudder

Features

Additional

Abnormal

Operation

REVERSIONARY MODE

AlertsAppendixIndex

Annun/

A - Mistrim

Mistrim

B - Pitch Trim

Outside Takeoff

Configuration

C - Asymmetrical

Pitch Trim
Condition

If the system detects a failure in PFD1, reversionary mode is entered
automatically. Reversionary mode must be entered manually in the case of
PFD2 or MFD failure.

. In reversionary mode, critical flight instrumentation is

combined with engine instrumentation on the remaining display.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Abnormal Operation

Manual activation of reversionary display mode is accomplished by pressing the

DISPLAY BACKUP Button on the appropriate audio panel.

• PFD1 – By pressing the DISPLAY BACKUP Button on the left audio panel.

• MFD – By pressing the DISPLAY BACKUP Button on the left or the right

audio panel.

• PFD2 – By pressing the DISPLAY BACKUP Button on the right audio

panel.

ABNORMAL COM OPERATION

When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00685-00 Rev. A

Loss of Hazard Functions with Loss of GPS

Position

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

59

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Abnormal Operation

UNUSUAL ATTITUDES

Flight

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary

InstrumentsEAS

functions are displayed in these situations.

The following information is removed from the PFD (and corresponding softkeys

are disabled) when the aircraft experiences unusual attitudes:

• TrafcAnnunciations

• AFCSAnnunciations

Nav/Com/

XPDR/AudioAFCSGPS Nav

• FlightdirectorCom­mand Bars

• InsetMap

• Temperatures

• DMEInformation

Window

• WindData

• SelectedHeadingBox

Flight

PlanningProcedures

• SelectedCourseBox

• TransponderStatus

Box

Hazard

Avoidance

• SystemTime

• PFDSetupMenu

• Windowsdisplayedin

the lower right corner

of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
– ADF/DME Tuning

• BarometricMinimum

Descent Altitude Box

• Glideslope,Glide­path, and Vertical
Deviation Indicators

• AltimeterBarometric

Setting

• SelectedAltitude

• VNV Target Altitude

Features

Additional

Extreme Pitch Indication

Abnormal

Operation

DEAD RECKONING

AlertsAppendixIndex

Annun/

While in Enroute or Oceanic phase of flight, if the system detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the system uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

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Abnormal Operation

NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the system stops
navigating in GPS Mode.

DR Mode is indicated by the appearance of the letters ‘DR’ superimposed in yellow
over the ‘own aircraft’ symbol as shown in the following figure. In addition, ‘DR’ is
prominently displayed, also in yellow, on the HSI slightly above and to the right of the
aircraft symbol on the CDI as shown in the following figure. Also, the CDI deviation
bar is removed from the display. Lastly, but at the same time, a ‘GPS NAV LOST’ alert
message appears on the PFD.

Normal navigation using GPS/WAAS source data resumes automatically once a
valid GPS solution is restored.

It is important to note that estimated navigation data supplied by the system in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function is not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the system through
DR while there is no heading and/or airspeed data available should not be used for
navigation.

DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00685-00 Rev. A

CDI ‘DR’ Indication on PFD

Dead Reckoning Indications

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

Symbolic Aircraft

(Map pages and Inset Map)

61

Alerts Appendix Index

Annun/

Abnormal Operation

As a result of operating in DR Mode, all GPS-derived data is computed based upon

an estimated position and is displayed as yellow text on the display to denote degraded

Flight

InstrumentsEAS

navigation source information. This data includes the following:

• NavigationStatusBoxeldsexceptActiveLeg,TAS,andDTK

• GPSBearingPointer

• WinddataandpointersintheWindDataBoxonthePFD

• TrackBug

Nav/Com/

• AllBearingPointerDistances

XPDR/AudioAFCSGPS Nav

• ActiveFlightPlandistances,bearings,andETEvalues

Also, while the system is in DR Mode, the autopilot will not couple to GPS, and
both TAWS and Terrain Proximity are disabled. Additionally, the accuracy of all nearest
information (airports, airspaces, and waypoints) is questionable. Finally, airspace
alerts continue to function, but with degraded accuracy.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

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CAS MESSAGES

Warning Messages

Annunciations & Alerts

ANNUNCIATIONS & ALERTS

Instruments EAS

Flight

See the Airplane Flight Manual (AFM) for recommended pilot actions.

Message Description

CAB ALTITUDE HI

DOOR EMER OPEN

DOOR PAX OPEN

E1 FIRE

E2 FIRE
E1 OIL LO PRES
E2 OIL LO PRES

ELEC EMERGENCY

ELEC XFR FAIL

LG LEVER DISAG

NO TO CONFIG

Cabin altitude pressure altitude high
Emergency door open
Passenger door open
Fire in engine 1
Fire in engine 2
Low oil pressure in engine 1
Low oil pressure in engine 2
Generators offline
Generators offline and electrical emergency transfer has failed
Landing gear position and control lever disagreement
No takeoff configuration

Caution Messages

See the Airplane Flight Manual (AFM) for recommended pilot actions.

Message Description

ADS 1 FAIL

ADS 2 FAIL
ADS 1 HTR FAIL
ADS 2 HTR FAIL

AHRS 1 FAIL
AHRS 2 FAIL

A-I E1 FAIL

A-I E2 FAIL

ANTI-SKID FAIL

AP FAIL

AP PITCH MISTRIM

AP ROLL MISTRIM

AUDIO PNL 1 FAIL
AUDIO PNL 2 FAIL

ADS 1 offline or failed
ADS 2 offline or failed
Pitot heater 1 offline or heater element failed
Pitot heater 2 offline or heater element failed
AHRS 1 failure
AHRS 2 failure
Anti-ice system failue in engine 1
Anti-ice system failue in engine 2
Anti-skid function lost; main brake still available
Loss of autopilot function
Airplane mistrimmed in pitch axis when autopilot is engaged
Airplane mistrimmed in roll axis when autopilot is engaged
Audio panel 1 is offline
Audio panel 2 is offline

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

63

Annunciations & Alerts

Message Description

Flight

Nav/Com/

Flight

Hazard

Additional

Abnormal

Annun/

AURAL WRN FAIL

InstrumentsEAS

AUTO PTRIM FAIL

BATT DISCHARG

BATT 1 OFF BUS
BATT 2 OFF BUS

BATT EXCEEDANCE

BLEED 1 FAIL

XPDR/AudioAFCSGPS Nav

BLEED 2 FAIL
BLEED 1 LEAK
BLEED 2 LEAK

BRK FAIL

CAB DELTA-P FAIL

CLUTCH PIT FAIL

CLUTCH ROL FAIL
CLUTCH YAW FAIL
CONFIG MDL FAIL

PlanningProcedures

D-I WINGSTB FAIL

DOORBAG AFT OPEN

DOORBAG FWD OPEN

DUCT 1 OVERTEMP
DUCT 2 OVERTEMP

E1 CTRL FAULT

Avoidance

E2 CTRL FAULT

E1 FAIL
E2 FAIL

Features

E1 FIRE DET FAIL
E2 FIRE DET FAIL

E1 FIREX FAIL

Operation

E2 FIREX FAIL
E1 FUEL IMP BYP
E2 FUEL IMP BYP

AlertsAppendixIndex

E1 TLA FAIL

E2 TLA FAIL
E1 TT0 HTR FAIL
E2 TT0 HTR FAIL

EBAY OVHT

EMER BRK LO PRES

ENG EXCEEDANCE

Aural warning system failure due to non-communicating LRUs
Auto pitch trim failure; other pitch trim functions still available
Battery discharging under normal operation
Battery 1 offline
Battery 2 offline
Battery voltage has exceeded 29 VDC
Bleed 1 system not under control
Bleed 2 system not under control
Bleed 1 hot air leakage at some region of the ducting
Bleed 2 hot air leakage at some region of the ducting
Main brake system lost
Excessive cabin pressure differential
Slip clutch maintenance test failed
Slip clutch maintenance test failed
Slip clutch maintenance test failed
Master Configuration Module failed or non-communicative
Deice system in wings and tail failure
Crew baggage door open
Forward baggage door open
Duct 1 temperature over specified safe value
Duct 2 temperature over specified safe value
Engine 1 responds slowly or not at all to thrust commands
Engine 2 responds slowly or not at all to thrust commands
Uncommanded shutdown detected for engine 1
Uncommanded shutdown detected for engine 2
Fire detection system failure in engine 1
Fire detection system failure in engine 2
Fire extinguisher failure in engine 1
Fire extinguisher failure in engine 2
Fuel filter impending bypass condition for engine 1
Fuel filter impending bypass condition for engine 2
Thrust Lever Angle failure for engine 1
Thrust Lever Angle failure for engine 2
Heater failue in engine 1
Heater failue in engine 2
Electrical bay over temperature
Few emergency brake functions available
Limit exceeded in engine(s) during flight

64

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

Message Description

ENG NO DISPATCH

ENG NO TO DATA

FLAP FAIL
FUEL 1 LO LEVEL
FUEL 2 LO LEVEL

FUEL 1 LO PRES

FUEL 2 LO PRES
FUEL 1 SOV FAIL
FUEL 2 SOV FAIL

FUEL IMBALANCE

FUEL OVERFILL

FUEL XFR FAIL
GEN 1 OFF BUS
GEN 2 OFF BUS

GEN OVLD

GEN START FAULT

GIA 1 FAIL

GIA 2 FAIL

GIA 1 OVHT
GIA 2 OVHT

HYD HI TEMP
HYD LO PRES

LG WOW SYS FAIL

MFD CONFIG

MFD FAULT

MFD OVHT

OXY LO PRES

PARK BRK NOT REL

PAX OXY NO PRES

PFD 1 CONFIG
PFD 2 CONFIG

PFD 1 FAULT
PFD 2 FAULT

PFD 1 OVHT
PFD 2 OVHT

PRESN AUTO FAIL

PTRIM BKP FAIL

PTRIM NML FAIL

FADEC detected no dispatch fault condition in engine(s)
No takeoff data entered
Loss of flaps deployment or retraction
Low fuel level in tank 1
Low fuel level in tank 2
Fuel pressure low in engine 1 feed line
Fuel pressure low in engine 2 feed line
Fuel feed SOV 1 closed or unavilable
Fuel feed SOV 2 closed or unavilable
Fuel is imbalanced between the tanks
Fuel tank overfilled
Fuel transfer failure
Generator 1 offline
Generator 2 offline
Generator(s) overload
Generator start fault
Failure of GIA 1
Failure of GIA 2
GIA 1 over temperature
GIA 2 over temperature
Hydraulic temperature high
Hydraulic pressure low
Landing gear weight-on-wheels system failure
MFD configuration error
Fault with the MFD
MFD over temperature
Oxygen system pressure low
Parking brake not released
Cabin altitude high and passenger oxygen system pressure low
PFD 1 configuration error
PFD 2 configuration error
Fault with PFD 1
Fault with PFD 2
PFD 1 over temperature
PFD 2 over temperature
Pressurization controller failure
Loss of backup pitch trim actuator
Loss of normally-operating pitch trim actuator

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

65

Annunciations & Alerts

Message Description

Flight

InstrumentsEAS

PUSHER FAIL

PUSHER OFF

STBY HTR FAIL

SWPS FAIL

SWPS FAULT

SWPS HTR 1 FAIL

Nav/Com/

XPDR/AudioAFCSGPS Nav

SWPS HTR 2 FAIL

SWPS UNTESTED
WSHLD 1 HTR FAIL
WSHLD 2 HTR FAIL

YD FAIL

YD MISTRIM

Advisory Messages

Stall Warning & Protection System pusher has failed
Stall Warning Pusher is off
Failure of standby heater
Stall Warning & Protection System inoperative
Stall Warning & Protection System activation angles anticipated to
conservative settings
Stall Warning & Protection System heater 1 failure
Stall Warning & Protection System heater 2 failure
Stall Warning & Protection System has not been tested
Windshield 1 heater failure
Windshield 2 heater failure
Loss of yaw damper function
Airplane mistrimmed in yaw axis when YD is engaged

Flight

See the Airplane Flight Manual (AFM) for recommended pilot actions.

PlanningProcedures

A-I E1 ON

A-I E2 ON
ADS 1 HTR FAULT
ADS 2 HTR FAULT

Hazard

ADS-AOA HTR ON

Avoidance

AHRS 1 FAULT
AHRS 2 FAULT

AUDIO PNL 1 FAULT

Features

Additional

AUDIO PNL 2 FAULT

AURAL WRN FAULT

Operation

AVNX FAN FAIL

BLEED 1 OFF

Abnormal

BLEED 2 OFF

CLUTCH PIT PASS

AlertsAppendixIndex

Annun/

CLUTCH PIT PROG
CLUTCH ROL PASS

CLUTCH ROL PROG

CLUTCH YAW PASS

CLUTCH YAW PROG

DC BUS 1 OFF
DC BUS 2 OFF

Message Description

De-ice system on in engine 1
De-ice system on in engine 2
Fault in ADS 1 heater
Fault in ADS 2 heater
ADS - Angle-of-attack heater on
Fault with AHRS 1
Fault with AHRS 2
Fault with audio panel 1
Fault with audio panel 2
Partial loss of aural warning function
Avionics fan failure
Bleed pressure regulator 1 and shut-off valve closed
Bleed pressure regulator 2 and shut-off valve closed
Pitch slip clutch maintenance test passed
Pitch slip clutch maintenance test in progress
Roll slip clutch maintenance test passed
Roll slip clutch maintenance test in progress
Yaw slip clutch maintenance test passed
Yaw slip clutch maintenance test in progress
DC bus 1 offline
DC bus 2 offline

66

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

Message Description

D-I WINGSTB ON
E1 CHIP DETECTED
E2 CHIP DETECTED

E1 FADEC FAULT

E2 FADEC FAULT
E1 SHORT DSPTCH
E2 SHORT DSPTCH

ELEC SYS FAULT

EMER BUS OFF

ENG FIREX DISCH

FLAP NOT AVAIL

FUEL EQUAL
FUEL 1 FEED FAULT
FUEL 2 FEED FAULT

FUEL 1 PSW FAIL

FUEL 2 PSW FAIL
FUEL PUMP 1 FAIL
FUEL PUMP 2 FAIL

GEA 1 FAIL
GEA 2 FAIL
GEA 3 FAIL

GSD FAIL

HSDB FAULT

HSDB SW REV POS

MACH TRIM FAIL

MFD FAN FAIL

OXY SW NOT AUTO

PFD 1 FAN FAIL
PFD 2 FAN FAIL

PTRIM DISCONNECT

PTRIM SW1 FAIL

PTRIM SW2 FAIL

RAM AIR FAIL

SHED BUS OFF

SWPS ICE SPEED

Deice system in wings and tail ON
Chip detected by engine 1 oil chip detector
Chip detected by engine 2 oil chip detector
FADEC fault in engine 1
FADEC fault in engine 2
Engine 1 in short dispatch condition
Engine 2 in short dispatch condition
Electrical system fault
Emergency bus OFF
Engine fire extinguisher discharge
Flaps not available
Fuel quantity asymmetry corrected; XFEED SOV is open
DC pump on due to low fuel pressure
DC pump on due to low fuel pressure
Fuel pressure switch stuck in “high” position
Fuel pressure switch stuck in “high” position
Fuel pump 1 failure
Fuel pump 2 failure
Failure of GEA 1
Failure of GEA 2
Failure of GEA 3
GSD non-communicative
An LRU has stopped communicating over an HSDB
HSDB switch in reversionary position
Mach trim failure; other pitch trim functions still available
Failure of MFD fan
Oxygen system switch in manual mode
Failure of PFD 1 fan
Failure of PFD 2 fan
Pitch trim disconnected
Failure of pilot pitch trim switch
Failure of copilot pitch trim switch
Ram air valve failure
Shed bus off
Stall Warning System activation angles anticipated due to ice conditions

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

67

Annunciations & Alerts

AURAL ALERTS

Flight

InstrumentsEAS

Message Priority Description
“Cabin”

High cabin altitude

“Fire, Fire” Engine fire

“High Speed” Maximum operating speed exceeded

“Landing Gear” Gear up in landing condition

“No Takeoff Brakes” No Takeoff Configuration due to brake status

“No Takeoff Flap” No Takeoff Configuration due to flap status

Nav/Com/

XPDR/AudioAFCSGPS Nav

Warning

“No Takeoff Trim” No Takeoff Configuration due to trim status

“Stall, Stall” Airplane in stall condition
“Flight Director” Flight director has reverted to pitch or roll default mode
“Timer Expired” Countdown timer on the PFD has reached zero
“Trim Trim Trim” Advisory Trim switch malfunction

“Aural Warning OK”
“Aural Warning One

Channel”

Flight

“Takeoff OK” Takeoff configuration test passed

PlanningProcedures

Aural warning system test passes

Status

Aural warning system test detects failure in one channel

OTHER PRODIGY™ AURAL ALERTS

Aural Alert Description

“Minimums, minimums” The aircraft has descended below the preset barometric minimum descent

Hazard

Avoidance

Features

Additional

“Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical

“Traffic” The Traffic Information Service (TIS) has issued a Traffic Advisory alert.

“TIS not available” The aircraft is outside the Traffic Information Service (TIS) coverage area.

altitude.

navigation is enabled.

Abnormal

Operation

AlertsAppendixIndex

Annun/

68

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

COMPARATOR ANNUNCIATIONS

Comparator

Window Text

ALT MISCOMP

Difference in altitude sensors is > 200 ft.

If both airspeed sensors detect < 35 knots, this is inhibited.

IAS MISCOMP

If either airspeed sensor detects > 35 knots, and the difference in sensors is >
10 kts.

If either airspeed sensor detects > 80 knots, and the difference in sensors is
> 7 kts.

HDG MISCOMP

PIT MISCOMP
ROL MISCOMP

ALT NO COMP

IAS NO COMP

HDG NO COMP

PIT NO COMP
ROL NO COMP

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors..

REVERSIONARY SENSOR ANNUNCIATIONS

Condition

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Reversionary

Sensor Window

Text

BOTH ON ADC1
BOTH ON ADC2

BOTH ON AD STBY

BOTH ON AHRS1

BOTH ON AHRS2

BOTH ON AT STBY

BOTH ON GPS1
BOTH ON GPS2

190-00685-00 Rev. A

Condition

Both PFDs are displaying data from the number one Air Data Computer.

Both PFDs are displaying data from the number two Air Data Computer.

Both PFDs are displaying data from the standby air data input.

Both PFDs are displaying data from the number one Attitude & Heading
Reference System.

Both PFDs are displaying data from the number two Attitude & Heading
Reference System.

Both PFDs are displaying data from the standby attitude and heading reference
input.

Both PFDs are displaying data from the number one GPS receiver.

Both PFDs are displaying data from the number two GPS receiver.

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

69

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

Reversionary

Sensor Window

Flight

InstrumentsEAS

USING ADC1
USING ADC2

USING AD STBY

USING AHRS1

Nav/Com/

XPDR/AudioAFCSGPS Nav

USING AHRS2

USING AT STBY

USING GPS1
USING GPS2

TAWS ALERTS

Flight

PlanningProcedures

Alert Type

Excessive Descent
Rate Warning (EDR)

Hazard

Avoidance

Reduced Required
Terrain Clearance
Warning (RTC)

Features

Additional

Imminent Terrain
Impact Warning (ITI)

Reduced Required

Abnormal

Operation

Obstacle Clearance
Warning (ROC)

Imminent Obstacle

AlertsAppendixIndex

Annun/

Impact Warning
(IOI)

Reduced Required
Terrain Clearance
Caution (RTC)

Text

Condition

PFD2 is displaying data from the #1 Air Data Computer.

PFD1 is displaying data from the #2 Air Data Computer.

PFD1 or PFD2 is displaying data from the standby air data input.

PFD2 is displaying data from the #1 AHRS.

PFD1 is displaying data from the #2 AHRS.

PFD1 or PFD2 is displaying data from the standby attitude and heading refer­ence input.

PFD2 is displaying data from the #1 GPS.

PFD1 is displaying data from the #2 GPS.

PFD/MFD

TAWS Page

Annunciation

MFD

Pop-Up Alert

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

““Obstacle, Obstacle; Pull

Up, Pull Up”

“Caution, Terrain; Caution,

Terrain”

70

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

Alert Type

Imminent Terrain
Impact Caution (ITI)

Reduced Required
Obstacle Clearance
Caution (ROC)

Imminent Obstacle
Impact Caution (IOI)

Premature Descent
Alert Caution (PDA)

Altitude Callout
“500”

Excessive Descent
Rate Caution (EDR)

Negative Climb
Rate Caution (NCR)

PFD/MFD

TAWS Page

Annunciation

MFD

Pop-Up Alert

Aural Message

“Caution, Terrain; Caution,

“Caution, Obstacle; Cau-

tion, Obstacle”

“Caution, Obstacle; Cau-

tion, Obstacle”

“Too Low, Terrain”

None None “Five-Hundred”

Terrain”

“Sink Rate”

“Don’t Sink”

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

TAWS System Status Annunciations

PFD/MFD

Alert Type

TAWS Page

Annunciation

TAWS System Test Fail None “TAWS System Failure”

TAWS Alerting is disabled None None

No GPS position or
excessively degraded GPS
signal

System Test in progress None None

System Test pass None None “TAWS System Test OK”

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

MFD

Pop-Up Alert

Aural Message

None “TAWS Not Available”

“TAWS Available” will be
heard when sufficient GPS
signal is re-established.

71

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Flight

InstrumentsEAS

DATA LOST

Message Comments

– Pilot stored data was

lost. Recheck settings.

XTALK ERROR

Nav/Com/

XPDR/AudioAFCSGPS Nav

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

service. Return unit for repair.

Flight

PlanningProcedures

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

MANIFEST

Hazard

mismatch, communication halted.

Avoidance

PFD1 CONFIG

– MFD1 software

– PFD1 config error.

Config service req’d.

Features

Additional

PFD2 CONFIG

– PFD2 config error.

Config service req’d.

MFD1 CONFIG

Abnormal

Operation

– MFD1 config

error. Config service req’d.

AlertsAppendixIndex

Annun/

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

The pilot profile data was lost. System reverts
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.

The MFD and PFDs are not communicating with
each other. The system should be serviced.

The PFD and/or MFD self-test has detected a
problem. The system should be serviced.

The PFD and/or MFD has incorrect software
installed. The system should be serviced.

The PFD configuration settings do not match
backup configuration memory. The system
should be serviced.

The MFD configuration settings do not match
backup configuration memory. The system
should be serviced.

The MFD and PFDs have different software
versions installed. The system should be
serviced.

72

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190-00685-00 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message Comments

PFD1 COOLING

cooling. Reducing power usage.

PFD2 COOLING

cooling. Reducing power usage.

MFD1 COOLING

– PFD1 has poor

– PFD2 has poor

– MFD1 has poor

The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the system should
be serviced.

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

PFD2 KEYSTK

Key is stuck.

MFD1 KEYSTK

– PFD1 [key name]

– PFD2 [key name]

– MFD [key name]

A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The system should be serviced if
the problem persists.

Key is stuck.

CNFG MODULE

configuration module is
inoperative.

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– PFD1

– PFD1 has low

– PFD2 has low

– MFD1 has low

The PFD1 configuration module backup memory
has failed. The system should be serviced.

The PFD1 voltage is low. The system should be
serviced.

The PFD2 voltage is low. The system should be
serviced.

The MFD voltage is low. The system should be
serviced.

DATABASE MESSAGE ADVISORIES

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Message Comments

MFD1 DB ERR

– MFD1 aviation

database error exists.

PFD1 DB ERR

– PFD1 aviation

database error exists.

PFD2 DB ERR

– PFD2 aviation

database error exists.

190-00685-00 Rev. A

The MFD and/or PFD detected a failure in
the aviation database. Attempt to reload the
aviation database. If problem persists, the
system should be serviced.

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

73

Alerts Appendix Index

Annun/

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

MFD1 DB ERR

InstrumentsEAS

– MFD1 basemap

database error exists.

PFD1 DB ERR

– PFD1 basemap

database error exists.

PFD2 DB ERR

database error exists.

Nav/Com/

XPDR/AudioAFCSGPS Nav

MFD1 DB ERR

– PFD2 basemap

– MFD1 terrain

database error exists.

PFD1 DB ERR

– PFD1 terrain

database error exists.

PFD2 DB ERR

– PFD2 terrain

database error exists.

MFD1 DB ERR

Flight

PlanningProcedures

database missing.

PFD1 DB ERR

– MFD1 terrain

– PFD1 terrain

database missing.

PFD2 DB ERR

– PFD2 terrain

database missing.

Hazard

MFD1 DB ERR

Avoidance

– MFD1 obstacle

database error exists.

PFD1 DB ERR

Features

Additional

database error exists.

PFD2 DB ERR

database error exists.

Abnormal

Operation

MFD1 DB ERR

database missing.

AlertsAppendixIndex

Annun/

PFD1 DB ERR

– PFD1 obstacle

– PFD2 obstacle

– MFD1 obstacle

– PFD1 obstacle

database missing.

PFD2 DB ERR

– PFD2 obstacle

database missing.

The MFD and/or PFD detected a failure in the
basemap database.

The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card
is properly inserted in display. Replace terrain
card. If problem persists, the system should be
serviced.

The terrain database is present on another LRU,
but is missing on the specified LRU.

The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.

The obstacle database is present on another LRU,
but is missing on the specified LRU.

74

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

terrain database error exists.

PFD2 DB ERR

– MFD1 airport

– PFD1 airport

– PFD2 airport

The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.

terrain database error exists.

MFD1 DB ERR

– MFD1 airport

terrain database missing.

PFD1 DB ERR

– PFD1 airport

terrain database missing.

PFD2 DB ERR

– PFD2 airport

The airport terrain database is present on
another LRU, but is missing on the specified LRU.

terrain database missing.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– PFD2 Safe Taxi

The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.

database error exists.

MFD1 DB ERR

database error exists.

– MFD1 Chartview

The MFD and/or PFDs detected a failure in the
ChartView database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, the system should
be serviced.

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

The MFD and/or PFDs detected a failure in the
FliteCharts database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, the system should
be serviced.

DB MISMATCH

database version mismatch. Xtalk
is off.

– Aviation

The PFDs and MFD have different aviation
database versions installed. Crossfill is off. Install
correct aviation database version in all displays.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

75

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEAS

DB MISMATCH

Message Comments

– Aviation
database type mismatch. Xtalk is
off.

DB MISMATCH

Nav/Com/

XPDR/AudioAFCSGPS Nav

– Terrain database
version mismatch.

DB MISMATCH

– Terrain database
type mismatch.

DB MISMATCH

– Obstacle
database version mismatch.

Flight

PlanningProcedures

DB MISMATCH

– Airport Terrain
database mismatch.

GMA 1347D MESSAGE ADVISORIES

Hazard

Avoidance

Message Comments

GMA1 FAIL

Features

Additional

GMA2 FAIL

GMA XTALK

Abnormal

Operation

has occurred.

AlertsAppendixIndex

Annun/

GMA1 CONFIG

– GMA1 is inoperative. The audio panel self-test has detected a failure.
– GMA2 is inoperative.

– GMA crosstalk error

– GMA1 config
error. Config service req’d.

GMA2 CONFIG

– GMA2 config
error. Config service req’d.

The PFDs and MFD have different aviation
database types installed (Americas, European,
etc.). Crossfill is off. Install correct aviation
database type in all displays.

The PFDs and MFD have different terrain
database versions installed. Install correct terrain
database version in all displays.

The PFDs and MFD have different terrain
database types installed. Install correct terrain
database type in all displays.

The PFDs and MFD have different obstacle
database versions installed. Install correct
obstacle database version in all displays.

The PFDs and MFD have different airport terrrain
databases installed. Install correct airport terrain
database in all displays.

The audio panel is unavailable. The system
should be serviced.

An error has occurred in transferring data
between the two GMAs. The system should be
serviced.

The audio panel configuration settings do not
match backup configuration memory. The system
should be serviced.

76

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

GMA 1347D MESSAGE ADVISORIES (CONT.)

Message Comments

MANIFEST – GMA1 software

mismatch, communication halted.

MANIFEST – GMA2 software

The audio panel has incorrect software installed. The
system should be serviced.

mismatch, communication halted.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

GMA2 SERVICE – GMA2 needs

service. Return unit for repair.

The audio panel self-test has detected a problem
in the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.

GIA 63W MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG

Config service req’d.

– GIA1 config error.

The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The

GIA2 CONFIG

– GIA2 config error.

system should be serviced.

Config service req’d.

GIA1 CONFIG

error. Config service req’d.

GIA2 CONFIG

– GIA1 audio config

– GIA2 audio config

The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.

error. Config service req’d.

GIA1 COOLING

temperature too low.

– GIA1

The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to

GIA2 COOLING

– GIA2

operating temperature.

temperature too low.

GIA1 COOLING

temperature.

– GIA1 over

The GIA1 and/or GIA2 temperature is too
high. If problem persists, the system should be

GIA2 COOLING

– GIA2 over

serviced.

temperature.

GIA1 SERVICE

service. Return the unit for repair.

– GIA1 needs

The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be

GIA2 SERVICE

– GIA2 needs

serviced.

service. Return the unit for repair.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

77

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

HW MISMATCH

InstrumentsEAS

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

– GIA hardware
mismatch. GIA2 communication
halted.

Nav/Com/

XPDR/AudioAFCSGPS Nav

MANIFEST

– GIA1 software

mismatch, communication halted.

MANIFEST

– GIA2 software

mismatch, communication halted.

MANIFEST

– GFC software

mismatch, communication halted.

COM1 TEMP

Flight

Reducing transmitter power.

PlanningProcedures

COM2 TEMP

– COM1 over temp.

– COM2 over temp.

Reducing transmitter power.

COM1 SERVICE

– COM1 needs

service. Return unit for repair.

COM2 SERVICE

Hazard

Avoidance

– COM2 needs

service. Return unit for repair.

COM1 PTT

Features

Additional

key is stuck.

COM2 PTT

key is stuck.

Abnormal

Operation

COM1 RMT XFR

transfer key is stuck.

AlertsAppendixIndex

Annun/

COM2 RMT XFR

– COM1 push-to-talk

– COM2 push-to-talk

– COM1 remote

– COM2 remote

transfer key is stuck.

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

A GIA mismatch has been detected, where only
one is WAAS capable.

The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.

Incorrect servo software is installed, or gain
settings are incorrect.

The system has detected an over temperature
condition in COM1 and/or COM2. The
transmitter is operating at reduced power. If the
problem persists, the system should be serviced.

The system has detected a failure in COM1 and/or
COM2. COM1 and/or COM2 may still be usable.
The system should be serviced when possible.

The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”) position.
Press the PTT switch again to cycle its operation.
If the problem persists, the system should be
serviced.

The COM1 and/or COM2 transfer switch is stuck
in the enabled (or “pressed”) position. Press
the transfer switch again to cycle its operation.
If the problem persists, the system should be
serviced.

GPS integrity is insufficient for the current phase
of flight.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

GPS NAV LOST

navigation. Insufficient satellites.

GPS NAV LOST

navigation. Position error.

GPS NAV LOST

navigation. GPS fail.

ABORT APR

navigation. Abort approach.

APR DWNGRADE

downgraded.

TRUE APR

Change HDG reference to TRUE.

– Loss of GPS

– Loss of GPS

– Loss of GPS

– Loss of GPS

– Approach

– True north approach.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS navigation.

Vertical guidance generated by WAAS is
unavailable, use LNAV only minimums.

Displayed after passing the first waypoint of a
true north approach when the nav angle is set
to ‘AUTO’.

GPS1 SERVICE

service. Return unit for repair.

– GPS1 needs

A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be

GPS2 SERVICE

– GPS2 needs

available. The system should be serviced.

service. Return unit for repair.

NAV1 SERVICE

service. Return unit for repair.

– NAV1 needs

A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be

NAV2 SERVICE

– NAV2 needs

available. The system should be serviced.

service. Return unit for repair.

NAV1 RMT XFR

transfer key is stuck.

NAV2 RMT XFR

transfer key is stuck.

– NAV1 remote

– NAV2 remote

The remote NAV1 and/or NAV2 transfer switch
is stuck in the enabled (or “pressed”) state.
Press the transfer switch again to cycle its
operation. If the problem persists, the system
should be serviced.

G/S1 FAIL

– G/S1 is inoperative.

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The system should

G/S2 FAIL

– G/S2 is inoperative.

be serviced.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

79

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

G/S1 SERVICE

InstrumentsEAS

– G/S1 needs

service. Return unit for repair.

G/S2 SERVICE

– G/S2 needs

service. Return unit for repair.

GSD 41 MESSAGE ADVISORIES

Nav/Com/

XPDR/AudioAFCSGPS Nav

Message Comments

GSD1 CONFIG

– GSD1 config error.

Config service req’d.

GSD1 COOLING

– GSD1

temperature too low.

GSD1 COOLING

temperature.

Flight

PlanningProcedures

GSD1 SERVICE

– GSD1 over

– GSD1 needs

service. Return unit for repair.

GSD1 COOLING

– GSD1 over

temperature.

GSD1 SERVICE

Hazard

Avoidance

service. Return unit for repair.

– GSD1 needs

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.

GSD1 and the CDU have different copies of
the GSD1 configuration.

GSD1 is reporting a low temperature
condition.

GSD1 is reporting an over-temperature
condition.

GSD1 is reporting an internal error condition.
The GSD may still be usable.

GSD1 is reporting an over-temperature
condition.

GSD1 is reporting an internal error condition.
The GSD may still be usable.

GEA 71 MESSAGE ADVISORIES

Features

Additional

Message Comments

GEA1 CONFIG

Abnormal

Operation

Config service req’d.

AlertsAppendixIndex

Annun/

GEA2 CONFIG

– GEA1 config error.

– GEA2 config error.

Config service req’d.

MANIFEST

– GEA1 software

mismatch, communication halted.

MANIFEST

– GEA2 software

mismatch, communication halted.

80

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

The GEA1 configuration settings do not match
those of backup configuration memory. The
system should be serviced.

The GEA2 configuration settings do not match
those of backup configuration memory. The
system should be serviced.

The #1 GEA 71 has incorrect software installed.
The system should be serviced.

The #2 GEA 71 has incorrect software installed.
The system should be serviced.

190-00685-00 Rev. A

Annunciations & Alerts

GTX 33/33D MESSAGE ADVISORIES

Message Comments

XPDR1 CONFIG

error. Config service req’d.

– XPDR1 config

The transponder configuration settings do not
match those of backup configuration memory.
The system should be serviced.

XPDR2 CONFIG

error. Config service req’d.

– XPDR2 config

The transponder configuration settings do not
match those of backup configuration memory.
The system should be serviced.

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

XPDR1 SRVC

service. Return unit for repair.

XPDR2 SRVC

service. Return unit for repair.

XPDR1 FAIL

inoperative.

XPDR2 FAIL

inoperative.

– GTX1 software

– GTX2 software

– XPDR1 needs

– XPDR2 needs

– XPDR1 is

– XPDR2 is

The transponder has incorrect software installed.
The system should be serviced.

The transponder has incorrect software installed.
The system should be serviced.

The #1 transponder should be serviced when
possible.

The #2 transponder should be serviced when
possible.

There is no communication with the #1
transponder.

There is no communication with the #2
transponder.

GRS 77 MESSAGE ADVISORIES

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

AHRS1 TAS

valid airspeed.

AHRS2 TAS

valid airspeed.

AHRS1 GPS

GPS source.

190-00685-00 Rev. A

Message Comments

– AHRS1 not receiving

The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.

– AHRS2 not receiving

The #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.

– AHRS1 using backup

The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

81

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEAS

AHRS2 GPS

Message Comments

– AHRS2 using backup

GPS source.

AHRS1 GPS

any GPS information.

Nav/Com/

XPDR/AudioAFCSGPS Nav

AHRS2 GPS

– AHRS1 not receiving

– AHRS2 not receiving

any GPS information.

AHRS1 GPS

– AHRS1 not receiving

backup GPS information.

AHRS2 GPS

Flight

backup GPS information.

PlanningProcedures

AHRS1 GPS

– AHRS2 not receiving

– AHRS1 operating

exclusively in no-GPS mode.

AHRS2 GPS

– AHRS2 operating

exclusively in no-GPS mode.

Hazard

AHRS MAG DB

Avoidance

– AHRS magnetic

model database version mismatch.

AHRS1 SRVC

Features

Additional

field model needs update.

AHRS2 SRVC

field model needs update.

Abnormal

Operation

GEO LIMITS

– AHRS1 Magnetic-

– AHRS2 Magnetic-

– AHRS1 too far

North/South, no magnetic compass.

AlertsAppendixIndex

Annun/

GEO LIMITS

– AHRS2 too far

North/South, no magnetic compass.

MANIFEST

– GRS1 software

mismatch, communication halted.

MANIFEST

– GRS2 software

mismatch, communication halted.

The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.

The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.

The #2 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.

The #1 AHRS is not receiving backup GPS
information. The system should be serviced.

The #2 AHRS is not receiving backup GPS
information. The system should be serviced.

The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.

The #2 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.

The #1 AHRS and #2 AHRS magnetic model
database versions do not match.

The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.

The #2 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.

The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged
as invalid.

The #1 AHRS has incorrect software installed.
The system should be serviced.

The #2 AHRS has incorrect software installed.
The system should be serviced.

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Cockpit Reference Guide for the Prodigy™ Flight Deck 100

190-00685-00 Rev. A

Annunciations & Alerts

GMU 44 MESSAGE ADVISORIES

Message Comments

HDG FAULT

– AHRS1

magnetometer fault has occurred.

HDG FAULT

– AHRS2

magnetometer fault has occurred.

MANIFEST

– GMU1 software

mismatch, communication halted.

MANIFEST

– GMU2 software

mismatch, communication halted.

GDL 69A MESSAGE ADVISORIES

Message Comments

GDL69 CONFIG

– GDL 69 config

error. Config service req’d.

GDL69 FAIL

MANIFEST

– GDL 69 has failed. A failure has been detected in the GDL 69. The

– GDL software

mismatch, communication halted.

A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The system
should be serviced.

A fault has occurred in the #2 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The system
should be serviced.

The GMU 44 has incorrect software installed.
The system should be serviced.

GDL 69 configuration settings do not match
those of backup configuration memory. The
system should be serviced.

receiver is unavailable. The system should be
serviced

The GDL 69 has incorrect software installed.
The system should be serviced.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00685-00 Rev. A

Cockpit Reference Guide for the Prodigy™ Flight Deck 100

83

Alerts Appendix Index

Annun/

Annunciations & Alerts

GWX 68 ALERT MESSAGES

Flight

InstrumentsEAS

GWX CONFIG

Message Comments

– GWX config error.

Config service req’d.

GWX FAIL

Nav/Com/

XPDR/AudioAFCSGPS Nav

GWX SERVICE

– GWX is inoperative. The GDU is not recieving status packet from the

– GWX needs

service. Return unit for repair.

MANIFEST

– GWX software

mismatch, communication halted.

WX ALERT

– Possible severe

weather ahead.

Flight

PlanningProcedures

GDC 74B MESSAGE ADVISORIES

Message Comments

ADC1 ALT EC

Hazard

correction is unavailable.

Avoidance

ADC2 ALT EC

correction is unavailable.

Features

Additional

ADC1 AS EC

– ADC1 altitude error

– ADC2 altitude error

– ADC1 airspeed error

correction is unavailable.

ADC2 AS EC

Abnormal

Operation

– ADC2 airspeed error

correction is unavailable.

MANIFEST

AlertsAppendixIndex

Annun/

mismatch, communication halted.

MANIFEST

– GDC1 software

– GDC2 software

mismatch, communication halted.

GWX 68 configuration settings do not match
those of the GDU configuration. The system
should be serviced.

GWX 68 or the GWX 68 is reporting a fault.
The GWX 68 radar system should be serviced.

A failure has been detected in the GWX 68. The
GWX 68 may still be usable.

The GWX 68 has incorrect software installed.
The system should be serviced.

Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80
to 320 nm.

GDC1 or GDC2 is reporting that the altitude
error correction is unavailable.

GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable.

The GDC 74B has incorrect software installed.
The system should be serviced.

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190-00685-00 Rev. A