Embraer Prodigy 300 - Airplane GARMIN - Free user manual and instructions

Product Type	Integrated Avionics System for Embraer Prodigy 300
Brand	Garmin
Model	Embraer Prodigy 300
Dimensions (Main Display)	12.1 inches diagonal, landscape orientation
Weight (Main Display)	Approximately 2.5 lbs (1.13 kg)
Power Input	28 VDC, 2.5 A max
Display Resolution	1280 x 720 pixels
Primary Functions	Navigation, flight planning, weather, traffic, terrain, autopilot control
Communication	VHF COM, intercom, ADS-B In/Out
Navigation Databases	Jeppesen worldwide, updated via SD card or Garmin Pilot
Maintenance	Annual software updates, periodic database subscriptions
Cleaning Instructions	Use a soft, damp cloth; avoid solvents and abrasive materials
Safety Certifications	FAA/EASA TSO-compliant for IFR operations
Spare Parts	Available through Garmin authorized dealers; includes bezels, connectors, backlight units
Warranty	2 years from date of installation
Included Accessories	Installation kit, wiring harness, quick-reference guide
Operating Temperature	-15°C to 55°C (5°F to 131°F)

Frequently Asked Questions - Embraer Prodigy 300 GARMIN

How do I update the navigation database on my Prodigy 300?

Download the latest database from Garmin's website onto an SD card. Insert the SD card into the system's slot and follow the on-screen prompts. Ensure the aircraft is powered on in the avionics bus configuration.

Does the Prodigy 300 support ADS-B In?

Yes, the Prodigy 300 includes built-in ADS-B In capability for traffic (TIS-B) and weather (FIS-B) reception, providing enhanced situational awareness.

What should I do if the display freezes during flight?

Perform a system reset by pressing and holding the power button for 10 seconds. If the issue persists, land as soon as possible and contact Garmin support. In-flight, rely on backup instruments.

Can I install the Prodigy 300 myself?

The Prodigy 300 must be installed by a certified avionics technician familiar with the aircraft's electrical system. Improper installation may void warranty and affect safety.

How often do I need to update the software?

Garmin releases software updates approximately every 6-12 months. Check the Garmin website or your dealer for the latest version. Updates can be performed via an SD card.

What is the maximum altitude the Prodigy 300 can operate?

The system is certified for operations up to 25,000 feet (7,620 meters) for normal flight modes. Higher altitudes may affect display and sensor performance.

Does the Prodigy 300 integrate with autopilots?

Yes, it can control compatible Garmin and third-party autopilots via the Garmin GFC 600 or similar systems, providing fully coupled IFR approaches.

What kind of warranty comes with the Prodigy 300?

Standard warranty is 2 years from installation for defects in materials and workmanship. Extended warranty options are available through Garmin.

How do I clean the touchscreen without damaging it?

Use a microfibre cloth slightly dampened with water or a screen-safe cleaner. Avoid paper towels and harsh chemicals. Never spray liquid directly onto the screen.

Where can I find the serial number on my unit?

The serial number is printed on a label on the back of the main display unit. It is also accessible in the system's setup menu under 'About'.

USER MANUAL Embraer Prodigy 300 GARMIN

Embraer Phenom 300

FLIGHT INSTRUMENTS

ENGINE & AIRFRAME SYSTEMS

NAV/COM/TRANSPONDER/AUDIO PANEL

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2008-2010, 2012-2014, 2016 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0734.8C or later for the Embraer Phenom 300. 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]

Aircraft On Ground (AOG) Hotline: [phone]

Aviation Dealer Technical Support: 888.606.5482

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: [phone]

Fax [phone]

Garmin (Europe) Ltd.

Liberty House, Houndown Business Park, Southampton, Hampshire SO40 9LR U.K.

Tel: [phone] Fax: [phone]

Garmin Corporation, No. 68, Zhangshu 2nd Road, Xizhi District, New Taipei City, 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.

Prodigy ^® is a registered trademark of Embraer-Empresa Brasileira de Aeronautica S.A.

Garmin ^® , WATCH ^® , FliteCharts ^® , and SafeTaxi ^® are registered trademarks of Garmin Ltd. or its subsidiaries. Connext ^™ is a trademark 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.; Honeywell ^® and Bendix/King ^® are registered trademarks of Honeywell International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.

SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.

AC-U-KWIK ^® is a registered trademark of Penton Business Media Inc.

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively "AOPA") expressly disclaim all warranties, with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided "as is" and AOPA does not warrant or make any representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you.

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to licensee.

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: Do not use outdated database information. Databases used in the system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness.

WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic.

WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age.

WARNING: The Prodigy® Integrated Flight Deck, as installed in the Embraer Phenom 300 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 300 Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the system to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: The illustrations in this guide are only examples. Never use the system to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding "by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo."

WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/environment/disposal.jsp.

WARNING: Because of variation in the earth's magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).

WARNING: Do not use GPS to navigate to any active waypoint identified as a 'NON WGS84 WPT' by a system message. 'NON WGS84 WPT' waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed.

WARNING: Do not use a QFE altimeter setting with this system. System functions will not operate properly with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure setting, as applicable.

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings.

CAUTION: The system does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot's authority to operate this device under FAA/FCC regulations.

NOTE: All visual depictions contained within this document, including screen images of the panel and displays, are subject to change and may not reflect the most current system and databases. Depictions of equipment may differ slightly from the actual equipment.

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.

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

• It is the pilot's responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can be viewed at http://fly.garmin.com by selecting 'Type 2 LOA Status.'
• Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may be presented by the system. It is the pilot's responsibility to operate in accordance with established AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

NOTE: The pilot/operator must review and be familiar with Garmin's database exclusion list as discussed in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at www.flygarmin.com by selecting 'Database Exclusions List.'

NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by selecting 'Aviation Database Alerts.'

NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to coordinate the revised DQRs.

NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select 'Report An Aviation Data Error Report.'

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 system are found in the Prodigy® Flight Deck 300 Pilot's Guide.

Part Number Change Summary

190-00761-00 Initial release

190-00761-01 Added SMS textingUpdated database update procedures in the AppendixAdded other GDU 11.12 parameters

190-0761-02 Updated CAS messagesUpdated SiriusXM Satellite Radio audio mute procedureAdded Pilot ProfilesUpdated Database Update proceduresAdded AC-U-KWIK Airport Directory capabilityUpdated GFDS registration procedureAdded Inset Map WX LGND SoftkeyAdded other GDU 12.11 parameters

190-0761-03 Added CPDLCAdded User Defined HoldsAdded Maintenance Logs PageRemoved Reports PageAdded temperature compensated altitudeAdded Steep Mode capabilityUpdated CAS and voice messagesAdded other GDU 13.02 parameters

190-0761-04 Added Profile ViewAdded input data failure annunciationsAdded Weather Radar overlay on the Navigation MapRemoved second DME optionRemoved GDC 74BUpdated CAS messagesUpdated CPDLC discussionAdded other GDU 14.02 parameters

190-0761-05 Updated Warnings, Cautions, and NotesUpdated Transponder Operational ProceduresUpdated Softkey MapsUpdated CAS MessagesUpdated System MessagesAdded Telephone ContactsAdded Position ReportingAdded other GDU 15.03 parameters

Revision Date of Revision Affected Pages Description
A February, 2016 All Production	Release

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 Minimum Descent Altitude/Decision Height 3

Displaying Wind Data 3

Engine & Airframe Systems....5

Synoptics 11

Nav/Com/Transponder/Audio Panel 21

Enter or Change Flight ID 21

ADF Tuning (Optional) 21

DME Tuning....21

Enter a Transponder Code....22

Select Transponder Mode 22

Selecting a COM Radio 22

Selecting a NAV Radio 23

NAV/COM Tuning 23

Intercom....23

Controller Pilot Data Link Communications (Optional) 24

Passenger Address (PA) System 27

Clearance Recorder and Player 27

Automatic Flight Control System 29

Flight Director Activation 30

Vertical Modes....31

Lateral Modes 32

GPS Navigation 33

Direct-to Navigation 33

Activate a Stored Flight Plan....34

Activate a Flight Plan Leg....34

Stop Navigating a Flight Plan....35

Vertical Navigation (VNAV)....35

Flight Planning....39

Weight Planning....39

Trip Planning....39

Create a User Waypoint Defined by Latitude & Longitude....41

Create a User Waypoint Defined by Radials from Other Waypoints....42

Create a User Waypoint Defined by a Radial & Distance from Another Waypoint.. 44

Delete a User Waypoint....45

Create a Flight Plan....46

Import a Flight Plan from an SD Card 47

Insert a Waypoint in the Active Flight Plan 47

Enter an Airway in a Flight Plan....48

User-Defined Holding Patterns 49

Invert An Active Flight Plan....51

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan .... 51

Store a Flight Plan....52

Edit a Stored Flight Plan .... 52

Delete a Waypoint from the Flight Plan....52

Invert and Activate a Stored Flight Plan....53

Copy a Flight Plan....53

Delete a Flight Plan....54

Graphical Flight Plan Creation....54

Export a Flight Plan to an SD Card 54

Procedures 55

Load and Activate a Departure Procedure 55

Activate A Departure Leg 55

Load An Arrival Procedure....55

Activate An Arrival Leg 56

Load and/or Activate an Approach Procedure 56

Activate An Approach in the Active Flight Plan....57

Activate A Vector to Final Approach Fix....58

Activate A Missed Approach in the Active Flight Plan 58

Temperature Compensated Altitude 58

Hazard Avoidance 61

Customizing the Hazard Displays on the Navigation Map....61

Switching Between Connext, and SiriusXM Weather Sources....61

SiriusXM Weather (Subscription Optional) 62

Connext Weather (Optional) 64

Traffic Information Service (TIS) 77

Traffic Collision Avoidance System (TCAS II) (Optional) 78

Terrain Awareness & Warning System 80

Profile View Terrain and Obstacles 83

Airborne Color Weather Radar 84

Additional Features 89

Synthetic Vision (Optional) 89

Terminal Procedure Charts 91

Airport Directory 93

Satellite Telephone and Data Link Services (Optional)....93

Wi-Fi Connections (Optional) 107

Maintenance Logs (Optional)....109

SiriusXM Satellite Radio Entertainment (Subscription Optional) 110

Electronic Checklists (Optional)....112

Position Reporting (Optional)....114

Pilot Profiles....115

Abnormal Operation 121

Engine 121

Cabin pressurization 121

Flaps 122

Trim 123

Reversionary Mode 123

Abnormal COM Operation 123

Audio Panel Fail-safe Operation....124

Hazard Displays with Loss of GPS Position....124

Unusual Attitudes 124

Dead Reckoning 125

Suspected Autopilot Malfunction 127

Overpowering Autopilot Servos 128

Annunciations & Alerts 129

CAS Messages....129

Comparator Annunciations.... 136

Reversionary Sensor Annunciations 136

TAWS-A Alerts 137

TAWS-B Alerts 140

TCAS II Alerts and Annunciations 142

GDL 69A Data Link Receiver Messages....144

CPDLC ATC Alert 145

Other Prodigy® Aural Alerts.... 145

Flight Plan Import/Export Messages 146

Pilot Profile Import/Export Messages....147

Prodigy® System Message Advisories....148

Other System Annunciations....168

Appendix....171

PFD Softkey Map 171

MFD Softkey Map 181

Updating Databases....185

Index....Index-1

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) Press the PFD Softkey to display the second-level softkeys.
2) Press the ALT UNIT Softkey.
3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).
Or :
Press the HPA Softkey to display the barometric pressure setting in hectopascals.
4) Press the BACK Softkey to return to the top-level softkeys.

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

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 FMS Knob clockwise to ON or counterclockwise to OFF.

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 small FMS Knob clockwise to ON or counterclockwise to OFF.

CHANGE NAVIGATION SOURCES

1) Press 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) Press 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 frequency.
3) Press the CDI Softkey a third time to return to GPS.

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1) Press 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.
3) Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1) Press 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 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

1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a speed has been changed from a default value, an asterisk appears next to the speed).

4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field.
5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6) To remove the window, press the CLR Key or the TMR/REF Softkey.

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 MINIMUM DESCENT ALTITUDE/DECISION HEIGHT

1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the Minimums field.
3) Turn the small FMS Knob to select BARO, RAD ALT (optional) or TEMP COMP. OFF is selected by default. Press the ENT Key or turn the large FMS Knob to highlight the next field.
4) Use the small FMS Knob to enter the desired altitude. When BARO and TEMP COMP are selected, values from zero to 16,000 feet may be entered. When RAD ALT is selected, values from zero to 2,500 feet may be entered.
5) If TEMP COMP was selected, press the ENT Key or turn the large FMS Knob to highlight the next field and then enter the destination airport temperature (-59°C to 59°C). The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value.
6) To remove the window, press the CLR Key or the TMR/REF Softkey.

DISPLAYING WIND DATA

1) Press the PFD Softkey.
2) Press the WIND Softkey to display wind data below the Selected Heading.
3) Press one of the OPTN softkeys to change how wind data is displayed.
4) To remove the Wind Data Window, press the OFF Softkey.

Blank Page

ENGINE & AIRFRAME SYSTEMS

EIS Display (Normal Mode)

EIS Display (Reversionary Mode)

① Engine Fan Rotation Speed
② Interstage Turbine Temperature (ITT)
③ Engine High Pressure Compressor Rotation Speed
④ Oil Pressure and Temperature
⑤ Fuel Display
⑥ Battery Voltmeter

⑦ Pressurization Display
⑧ Spoiler Status
⑨ Landing Gear Status
10 Flap Indicator
⑪ Trim Indicator

Engine Indications

Thrust Rating

Indication Thrust Rating
CRZ
CLB
CON	uous
TO
GA	und

Thrust Rating Indications

Selecting a thrust rating:

1) Select the SYSTEM Softkey.
2) Select the ENG SET Softkey
3) To choose the continuous thrust rating, select the CON Softkey,
To choose the maximum climb thrust rating, select the CLB Softkey.
4) Select the BACK Softkey to return to the previous softkey level.

Or:

Automatic Thrust Reserve

Indication* Description
ATR	nabled in both engines
ATR	med in both engines, but inactive
TO - RSV	R activated in at least one engine in Take Off mode
GA - RSV	R activated in at least one engine in Go-Around Mode

* When no indication is shown, ATR has not been enabled or armed in both engines.

Automatic Thrust Reserve (ATR) Status

Disabling/enabling Automatic Thrust Reserve (ATR):

1) Select the SYSTEM Softkey.
2) Select the ENG SET Softkey to display the Takeoff Data Set Window.
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.

Takeoff Data Set Window

Takeoff Data Set Window

Setting the Outside Air Temperature (OAT):

1) Select the SYSTEM Softkey.
2) Select the ENG SET Softkey to display the Takeoff Data Set Window.
3) To adjust the temperature in 1 °C increments, use the OAT↑ and OAT↓ softkeys.
4) If desired, change the ATR status 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

Fuel Display

Electrical Display

Cabin Pressurization

Cabin Pressure Display

Setting the displayed landing field elevation:

1) Select the SYSTEM Softkey.
2) Select the LFE Softkey.
3) Select the FMS LFE Softkey to set the LFE to the value for the destination airport in the current flight plan.

Or:

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

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

Spoiler and Landing Gear

Spoiler and Landing Gear Indications

Indication Description
DN	Landing Gear Down
UP	Landing Gear Up
	Landing Gear Transitioning (Normal)
DN	Landing Gear Locked Down
UP	Landing Gear Locked Up
	Landing Gear Transitioning (Abnormal)

Landing Gear Position Indications

Indication Description
X	Invalid information
SPDBRK	Spoilers out of takeoff configuration
FAIL Spoilers failed
CLOSED GND SPLR SPDBRK STEEP	Bilers retracted bound spoilers deployed edbrakes deployed b Mode enabled (optional)

Spoiler Indications

Flaps and Trim

Flap and Trim Indications

SYNOPTICS

① Flight ID
② Static Air Temperature (SAT)
③ Total Air Temperature (TAT)
4 International Standard Atmosphere (ISA)
⑤ True Airspeed (TAS)
⑥ Engine Dispatch Message Box

⑦ Oxygen
⑧ Emergency Brake Accumulator Pressure
⑨ Door Status
10 Electrical Status
⑪ Hydraulic Pressure

System Status Synoptics Page

Environmental Control System (ECS)

① Cockpit Temperature Setting
② Cabin Temperature Setting
③ Ram Air Valve (RAV)
4 Environmental Control System Valve (ECS) 1
⑤ Cockpit Duct Temperature Setting
6 Pressure Regulating Shutoff Valve (PRSOV)
⑦ Vapor Cycle System (VCS)
⑧ Outflow Valve (OFV) Status*
9 Pressure Regulating Shutoff Valve (PRSOV) 2

10 Crossbleed Valve Status (XBV)
⑪ Cabin Duct Temperature Setting
12 Heat Exchanger Cooling Pack Circuit
13 Environmental Control System Valve (ECS) 2
14 Actual Cabin Temperature
15 Cabin Evaporator Fan
16 Actual Cockpit Temperature
17 Cockpit Evaporator Fan

Environmental Control System Synoptics Page

Unit Icons and Descriptions
Fan
	On	Off
Heat Exchanger
	On	Off
Vapor Cycle System
	On	Off
ECS ValveRam Air Valve
	Open with flow	Open, no flow	Closed
Pressure Regulating Shutoff Valve (PRSOV)Crossbleed Valve (XBV)
	Open with flow	Open, no flow Closed

Environmental Control System Unit Status Indications

Electrical

Electrical Synoptics Page

Unit Icons and Descriptions
Generator	N2>52%	Bus off	N2<52%
Bus	DC BUS 1 On	DC BUS 1 Bus off
Hot Bus	HOT BUS 1 Normal	HOT BUS 1 Abnormal
Battery	Normal	Abnormal

Electrical System Unit Status Indications

Fuel

① Total Fuel
② Fuel Used
③ Left Feed Ejector
④ Left DC Pump
⑤ Left Tank Fuel Quantity
⑥ Fuel 1 SOV
⑦ LH Pressure Switch
⑧ Left Engine Feed Line
⑨ Fuel Transfer SOV
10 Right Engine Feed Line
11 RH Pressure Switch
⑫ Fuel 2 SOV
13 Right Tank Fuel Quantity
14 Right DC Pump
15 Right Feed Ejector

Fuel Synoptics Page

Unit Icons and Descriptions
Fuel Line
	Operating	Not operating
Feed Ejector
	Operating	Not operating
Fuel Pressure Switch
	Operating	Not operating
Valve
	Open with flow	Open, no flow	In transit	Closed
DC Pump
	Operating	Not operating
Fuel Transfer Valve
	Open with flow	Open, no flow	In transit	Closed

Fuel System Unit Status Indications

Ice Protection System

① Windshield Heaters
② Anti-Ice Lines
③ Anti-Ice Valve (AIV) 1
(4) Bleed Duct and Skin 1
⑤ Engine Anti Ice Valve (EAIV) 1 Valve and Bleed Line
⑥ Pressure Regulating Shut-Off Valve 1 (PRSOV 1)

⑦ Crossbleed Valve
⑧ Ice Protection Bleed Duct
9 Pressure Regulating Shut-Off Valve 2 (PRSOV 2)
⑩ Engine Anti Ice Valve (EAIV) 2 Valve and Bleed Line
⑪ Bleed Duct and Skin 2
12 Anti Ice Valve (AIV) 2

Ice Protection Synoptics Page

Unit Icons and Descriptions
Anti Ice Line
	Operating		Not operating
Crossbleed Valve (XBV)Pressure Regulating ShutoffValve (PRSOV)
	Open with flow	Open, no flow	Closed
Anti Ice Valve (AIV)Engine Anti Ice Valve (EAIV)
	Open with flow	Open, no flow	Closed

Ice Protection System Unit Status Indications

The Minimum Anti-Ice N1 Bug appears as a light blue tick mark on the N1 engine gauges. It indicates which N1 should be commanded to achieve full anti-ice capability. The bug is visible when the landing gear is extended and wing anti-ice is on, or when an engine or engine bleed air is lost. If the anti-ice capacity is not fully operational, the message “A-I LO CAPACITY” appears on the Crew Alerting System (CAS).

Engine Minimum N1 Anti-Ice Indication

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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.

ADF TUNING (OPTIONAL)

1) Press the ADF/DME Softkey.
2) Turn the small FMS Knob to enter the first digit of the desired ADF frequency.
3) Turn the large FMS Knob to select the next desired field.
4) Turn the small FMS Knob to enter the desired number.
5) Repeat steps 3 and 4 until the desired ADF frequency is entered.
6) Press the ENT Key to accept the new frequency.
7) Press the ENT Key again to transfer the frequency to the active field.
8) Turn the large FMS Knob to select the MODE field.
9) Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10) Press the ENT Key to complete the selection.

DME TUNING

1) Press the ADF/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 (XPDR/TFC if the TCAS II option is available).
2) If the aircraft is equipped with two transponders, press the XPDR1 or XPDR2 Softkey to select the active transponder. If these softkeys are not present, proceed to step 3.
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.

SELECT TRANSPONDER MODE

With TCAS II Option

1) Press the XPDR/TFC Softkey.
2) Press the MODE Softkey to display the transponder mode selection softkeys.
3) Press the desired transponder mode softkey (STBY, ON, or ALT).

Without TCAS II Option

1) Press the XPDR Softkey.
2) If the aircraft is equipped with two transponders, press the XPDR1 or XPDR2 Softkey to select the active transponder.
3) Press the desired transponder mode softkey (STBY, ON, or ALT).

SELECTING A COM RADIO

Transmit/Receive

Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (HF, if installed) on the audio panel.

Receive Only

Press the COM1, COM2, or COM3 Key (HF, if installed) on the audio panel.

SELECTING A NAV RADIO

1) To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2) Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or deselect the navigation radio audio source. All radio keys can be selected individually or together.

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 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.

INTERCOM

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 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.

When the flight crew wants to communicate with the passengers, the pilot or copilot presses the CABIN Key to signal that communication is desired. The cabin signal must be acknowledged to begin intercom conversation.

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.

• When the MAN SQ Annunciator is extinguished (Automatic Squelch is on), the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the VOL/SQ selection).
• When the MAN SQ Annunciator is illuminated (Manual Squelch), the ICS Knob controls either volume or squelch (selected by pressing the ICS Knob and indicated by the VOL or SQ annunciation).

CONTROLLER PILOT DATA LINK COMMUNICATIONS (OPTIONAL)

The CPDLC (Controller Pilot Data Link Communications) system provides data link communication between the aircraft and an Air Traffic Control facility. Communication is normally in the form of text message elements that resemble phraseology used in voice communications with ATC.

Generally, messages are closed with an acknowledgement or acceptance. When a message is acknowledged, the connection with the ATC facility is not terminated, but kept active for future communication.

Communication hand-off to the next ATC facility is usually performed automatically, but may also be accomplished manually by the pilot.

Connecting to the CPDLC System

A flight plan must be filed prior to logging on to the CPDLC system. After entering flight plan information in the required fields and successfully logging on to the system, messages may be sent and received.

The following parameters are used to log on to the system:

• Facility
• Flight ID
• Destination Airport
• Filed Departure Airport
• File Departure Time (Optional)

Performing the system log-on:

1) From the MFD, select the CPDLC Softkey.
2) Select the LOGON Softkey.
3) Turn the large FMS Knob to place the selection cursor over the Facility field.
4) Turn the small FMS Knob to select the desired ATC facility to which the CPDLC connection will be established.
5) Press the ENT Key to complete the entry.
6) Turn the large FMS Knob to place the selection cursor over the Flight ID field.
7) Turn the small FMS Knob to enter the Flight ID or aircraft registration number.
8) Press the ENT Key to complete the entry.

9) Turn the large FMS Knob to place the selection cursor over the Destination Airport field.
10) Enter the identifier of the destination airport used in the filed flight plan and press the ENT Key.
11) The Filed Departure Airport field is prefilled with the airport identifier corresponding to the current aircraft location. If the flight plan was filed using a different airport identifier, turn the large FMS Knob to place the selection cursor over the Filed Departure Airport field, enter the departure airport, and press the ENT Key.
12) (Optional) Turn the large FMS Knob to place the selection cursor over the Filed Departure Time field.
13) (Optional) Enter the departure time used in the filed flight plan and press the ENT Key.
14) Turn the large FMS Knob to place the selection cursor over SEND and press the ENT Key. The Status immediately indicates 'Connecting'. After successful log-on, the Status indicates 'Waiting For CPDLC'. Once a CPDLC session is initiated by ATC, the Status indicates 'Connected' and the Current Facility field is populated with the name of the facility. If a transfer to another facility is needed, the Next Facility field is populated. Pressing the LOGOFF Softkey terminates the log-on process.

Creating a Message

Creating a message consists of choosing from a pre-determined list of requests, entering the required information, and sending the request. A CPDLC session must be successfully initiated before a message can be created.

To create messages:

1) From the MFD, select the CPDLC Softkey.
2) Select the NEW Softkey. The CPDLC Thread Window appears.
3) With the Response/Request field highlighted, turn the small FMS Knob to select the desired request from the list and press the ENT Key. For discussion purposes, 'Request [level]' is selected.
4) Highlight the Level field and enter the desired altitude. To toggle between multiple units of measure (FT or FL), highlight the first numeric position and turn the small FMS Knob counterclockwise.
5) Press the ENT Key to complete the entry.

6) Highlight the Reason field and enter the desired reason from the list.
7) Press the ENT Key to complete the entry.
8) Highlight the SEND Button and press the ENT Key.

Responding to an ATC Message

Responding to an ATC message consists of choosing from a pre-determined list of responses or acknowledgements, then sending the response or acknowledgement.

To respond to a message:

1) From the MFD, select the CPDLC Softkey.
2) Turn the large FMS Knob to place the selection cursor over the desired message and press the ENT Key.
3) Turn the small FMS Knob to select the desired Response/Request from the list and press the ENT Key.
4) Highlight the SEND Button and press the ENT Key.

Viewing CPDLC Message Dialogs

The status of a string of messages, or dialog, may be checked and past message dialogs viewed. When the system power is cycled, or the end flight parameters are met, the message dialogs are deleted.

To view messages:

1) From the MFD, select the CPDLC Softkey.
2) Turn the large FMS Knob to place the selection cursor over the desired message to view and press the ENT Key.
3) Press the ENT Key to view the CPDLC Thread.

Deleting Message Dialogs

While the system deletes the list of message dialogs when power is turned off, or the end flight parameters are met, individual message dialogs may also be deleted manually. Message dialogs considered closed may also be deleted.

To delete a single message dialog:

1) From the MFD, select the CPDLC Softkey.
2) Turn the large FMS Knob to place the selection cursor over the desired message to delete.

3) Select the DELETE Softkey. A confirmation window appears.
4) Highlight OK and press the ENT Key.

To delete all closed message dialogs:

1) From the MFD, select the CPDLC Softkey.
2) Select the DEL ALL Softkey. A confirmation window appears.
3) Highlight OK and press the ENT Key.

Disconnecting from the CPDLC System

After successfully initiating a CPDLC session, the LOGOFF Softkey becomes available.

To Log-off the CPDLC System:

1) From the MFD, select the CPDLC Softkey.
2) Select the LOGOFF Softkey.

PASSENGER ADDRESS (PA) SYSTEM

A passenger address system is provided by pressing the PA Key to deliver messages to the passengers only on the available cabin headsets, not the cabin speakers. 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.

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.

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.

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.

Control Pressed	FD PFD Data Source	Modes Selected
		Lateral Vertical
FD Key (pilot-side)*	Pilot-side Roll Hold (default)	ROT Pitch Hold (default)	PIT
FD Key (copilot-side)*	Pilot-side Roll	Hold (default)	ROT 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)	ROL	Takeoff (on ground)	TO
		Roll Hold (default)	ROL	Go Around (in air)	GA
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 PathTracking**	VPTH
NAV Key	Pilot-side	Navigation***	GPSVORLOCBC	Pitch Hold (default)	PIT
APR Key	Pilot-side	Approach***	GPSVORLOC	Pitch Hold (default)	PIT
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.
** 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 NAV or APR Key press activates flight director.

VERTICAL MODES

Vertical Mode Description Control Annunciation
Pitch Hold	Holds the current aircraft pitch attitude; may be used to climb/descend to the Selected Altitude	(default) PIT
Selected Altitude Capture	Captures the Selected Altitude * ALTS
Altitude Hold	Holds the current altitude reference	ALT Key	ALT
Vertical Speed	Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude	VS Key	VS
Flight Level Change	Maintains the current aircraft airspeed (in IAS or Mach) while the aircraft is climbing/ descending to the Selected Altitude	FLC Key	FLC
Vertical Path Tracking	Captures and tracks descent legs of an active vertical profile	VNV Key	VPTH
VNV Target Altitude Capture	Captures the Vertical Navigation (VNV) Target Altitude	**	ALTV
Glidepath	Captures and tracks the SBAS or baro- VNAV glidepath on approach	APR Key	GP
Glideslope	Captures and tracks the ILS glideslope on approach		GS
Takeoff	Commands a constant pitch angle and wings level on the ground in preparation for takeoff	GA Switch	TO
Go Around	Disengages the autopilot and commands a constant pitch angle and wings level while in the air		GA

* 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

LATERAL MODES

Lateral Mode Description Control Annunciation
Roll Hold	Holds the current aircraft roll attitude or rolls the wings level, depending on the commanded bank angle	(default) ROL
Low Bank	Limits the maximum commanded roll angle	BANK Key	*
Heading Select **	Captures and tracks the Selected Heading	HDG Key	HDG
Navigation, GPS **	Captures and tracks the selected navigation source (GPS, VOR, LOC)	NAV Key	GPS
Navigation, VOR Enroute Capture/ Track **			VOR
Navigation, LOC Capture/Track (No Glideslope)			LOC
Navigation, Backcourse Arm/Capture/Track	Captures and tracks a localizer signal for backcourse approaches		BC
Approach, GPS	Captures and tracks the selected navigation source (GPS, VOR, LOC)	APR Key	GPS
Approach, VOR Capture/Track			VAPP
Approach, LOC Capture/Track (Glideslope Mode automatically armed)			LOC

* 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.
** The Heading, Navigation GPS and Navigation VOR mode maximum roll command limit will be limited to the Low Bank mode value if it is engaged.
The Garmin AFCS limits turn rate to 3 degrees per second (standard rate turn)

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation using the MFD

1) Press the Direct-to (▶) Key on the MFD or MFD Controller.
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.

Direct-to Navigation using the PFD

1) Press the Direct-to Key (▶) on the PFD.
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.

7) Turn the small FMS Knob to enter the desired altitude constraint.
8) 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.

ACTIVATE A STORED FLIGHT PLAN

1) Press the FPL Key on the MFD, or MFD Controller, 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

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

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.

NOTE: Temperature Compensated (TEMP COMP) altitudes are depicted as slanted text.

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

Altitudes that are designated for use in vertical navigation may also be made “non-designated” 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.

NOTE: Making course changes greater than 90° during a descent with vertical guidance may cause excessive and rapid movement of the vertical deviation indicator, and SVT Pathways.

The system updates vertical path guidance continuously using ground speed and the calculated distance to the Bottom of Descent (BOD). Due to turn anticipation guidance (turn-smoothing), distance to the BOD can be affected by course changes greater than approximately 5 degrees. Ground speed can be affected by factors such as shifts in wind direction, aircraft power management, pitch angle, and course changes. Abrupt and/or substantial changes to either the distance to the BOD, ground speed, or both can cause similarly abrupt/substantial changes in vertical path guidance.

Because of turn-smoothing, changes to both distance to the BOD and ground speed tend to be more extreme when the BOD is also a waypoint that marks a large course change. These speed and distance changes will be accounted for in the computed required vertical path and reflected in the vertical guidance indications.

	White Text Light	Blue Text Light Blue	Subdued Text
Large 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 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.	The system cannot use this altitude in determining vertical flight path guidance.
Small Text	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 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.

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FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Entering Weight Parameters

Turn the large FMS Knob to select the 'AUX' page group. Turn the small FMS Knob to select the Weight Planning Page.

1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty 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.

TRIP PLANNING

1) Turn the large FMS Knob to select the 'AUX' page group.
2) Turn the small FMS Knob to select the Trip Planning Page.
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.

4) For Direct-to planning:

a) Select the WPTS Softkey and verify that the starting waypoint field indicates 'P.POS' (present position).
b) If necessary, press the MENU Key and select 'Set WPT to Present Position' to display 'P.POS'.
c) Press the ENT Key and the flashing cursor moves to the ending waypoint field.
d) Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint.

Or:

For point-to-point planning:

a) Enter the identifier of the starting waypoint.
b) Once the waypoint's identifier is entered, press the ENT Key to accept the waypoint. The flashing cursor moves to the ending waypoint.
c) Again, enter the identifier of the ending waypoint.
d) Press the ENT Key to accept the waypoint.

Or:

For flight plan leg planning:

a) Select the FPL Softkey (at the bottom of the display).
b) Turn the small FMS Knob to select the desired flight plan (already stored in memory), by number.
c) Turn the large FMS Knob to highlight the 'LEG' field.
d) 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.

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.

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) The flashing cursor moves to the ground speed (GS) field. Enter the ground speed. Press the ENT Key when finished. Note that in 'automatic' page mode, ground speed is provided by the system.
8) The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press the ENT Key when finished. Note that in 'AUTOMATIC' page mode, fuel flow is provided by the system.
9) 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.
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field. Enter the calibrated airspeed. Press the ENT Key when finished. Note that in 'AUTOMATIC' page mode, calibrated airspeed is provided by the system.
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the altitude. Press the ENT Key when finished. Note that in 'AUTOMATIC' page mode, altitude is provided by the system.
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter the desired baro setting. Press the ENT Key when finished. Note that in 'AUTOMATIC' page mode, the baro setting is provided by the setting entered on the PFD.
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter the desired air temperature. Press the ENT Key when finished. Note that in 'AUTOMATIC' page mode, air temperature is provided by the system outside air temperature.

CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

1) Turn the large FMS Knob on the Control Unit 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 'WAYPOINT TYPE' field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.

a) Turn the large FMS Knob one click to the left to highlight 'TEMPORARY'.
b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the 'WAYPOINT TYPE' field.

7) With the cursor in the 'WAYPOINT TYPE' field, turn the small FMS Knob to display a list of waypoint types.
8) Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9) Press the ENT Key.

CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS

1) Turn the large FMS Knob on the Control Unit 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 'WAYPOINT TYPE' field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.

a) Turn the large FMS Knob one click to the left to highlight 'TEMPORARY'.
b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the 'WAYPOINT TYPE' field.

7) With the cursor in the 'WAYPOINT TYPE' field, turn the small FMS Knob to display a list of waypoint types.
8) Turn the small FMS Knob to select RAD/RAD (radial/radial).
9) Press the ENT Key.
10) The cursor moves to the 'REFERENCE WAYPOINTS' field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:

a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints.
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' airports 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.

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 'USER' waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.

11) Press the ENT Key. The cursor is displayed in the 'RAD' (radial) field. Enter the desired radial from the reference waypoint.
12) Press the ENT Key.
13) Repeat step 10 to enter the next waypoint name.
14) Press the ENT Key. The cursor is displayed in the 'RAD' (radial) field for the second waypoint. Enter the desired radial from the reference waypoint.
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.

CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM ANOTHER WAYPOINT

1) Turn the large FMS Knob on the MFD Control Unit 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 'WAYPOINT TYPE' field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.

a) Turn the large FMS Knob one click to the left to highlight 'TEMPORARY'.
b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the 'WAYPOINT TYPE' field.

7) With the cursor in the 'WAYPOINT TYPE' field, turn the small FMS Knob to display a list of waypoint types.
8) Turn the small FMS Knob to select RAD/DIS (radial/distance).
9) Press the ENT Key.
10) The cursor moves to the 'REFERENCE WAYPOINTS' field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:

a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints.
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' airports 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.

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 'USER' waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.

11) Press the ENT Key. The cursor is displayed in the 'RAD' (radial) field. Enter the desired radial from the reference waypoint.
12) Press the ENT Key.
13) The cursor is now displayed in the 'DIS' (distance) field. Enter the desired distance from the reference waypoint.
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.

DELETE A 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) Press the FMS Knob to activate the cursor.
4) Turn the large FMS Knob to the place the cursor in the 'USER WAYPOINT LIST' field.
5) Turn the small FMS Knob to highlight the desired waypoint.
6) Select the DELETE Softkey.
7) The message 'Would you like to delete the user waypoint?' is displayed. With 'YES' highlighted, press the ENT Key.

CREATE A FLIGHT PLAN

NOTE: When creating a flight plan in the Active Flight Plan Window, the first leg is activated automatically after it is created.

Creating an active flight plan:

1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints).
4) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6) When all waypoints have been entered, press the FMS Knob to remove the cursor.

Creating a stored flight plan:

1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Select the NEW Softkey; or press the MENU Key, highlight 'Create New Flight Plan', and press the ENT Key to display a blank flight plan for the first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints).
5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key.
6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7) 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.

IMPORT A FLIGHT PLAN FROM AN SD CARD

1) Insert the SD card containing the flight plan in the top card slot on the MFD.
2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.
5) Turn either FMS Knob to highlight an empty or existing flight plan.
6) Select the IMPORT Softkey.

If an empty flight plan is selected, a list of the available flight plans on the SD card will be displayed.

Or:

If an existing flight plan is selected, an 'Overwrite existing flight plan? OK or CANCEL' prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card. If overwriting the existing flight plan is not desired, select 'CANCEL' using the FMS Knob, press the ENT Key, select another existing or empty flight plan, and again select the IMPORT Softkey.

7) Turn the small FMS Knob to highlight the desired flight plan for importing.

8) Press the ENT Key.

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

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.

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 'USER' waypoints.
c) Turn the large FMS Knob to select the desired user waypoint.
d) Press the ENT Key.

6) Press the ENT Key again to "accept" the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

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.
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.

USER-DEFINED HOLDING PATTERNS

A holding pattern can be defined at any active flight plan waypoint, or at the aircraft present position.

Creating a user-defined hold at an active flight plan waypoint:

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the hold.
3) Press the MENU Key, highlight 'Hold At Waypoint', and press the ENT Key. The HOLD AT window appears with the course field highlighted.
4) Use the FMS Knobs to edit the entry course, and press the ENT Key.
5) Use the small FMS Knob to select 'INBOUND' or 'OUTBOUND' course direction, and press the ENT Key.
6) Use the small FMS Knob to select 'TIME' or 'DIST' length mode, and press the ENT Key.
7) Use the FMS Knobs to edit the length, and press the ENT Key.
8) Use the small FMS Knob to select 'RIGHT' or 'LEFT' turn direction, and press the ENT Key.
9) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key.
10) Press the ENT Key while 'LOAD?' is highlighted to add the hold into the flight plan.

Creating a user-defined hold at the aircraft present position:

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the MENU Key, highlight 'Hold At Present Position', and press the ENT Key. The HOLD AT window appears with the course field highlighted.
3) Use the FMS Knobs to edit the entry course, and press the ENT Key.
4) Use the small FMS Knob to select 'INBOUND' or 'OUTBOUND' course direction, and press the ENT Key.
5) Use the small FMS Knob to select 'TIME' or 'DIST' length mode, and press the ENT Key.
6) Use the FMS Knobs to edit the length, and press the ENT Key.
7) Use the small FMS Knob to select 'RIGHT' or 'LEFT' turn direction, and press the ENT Key.
8) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key.
9) Press the ENT Key while 'ACTIVATE?' is highlighted to create an Offroute Direct-to hold waypoint and activate the hold.

Creating a user-defined hold at a Direct To waypoint:

1) Press a Direct-to Key and set up the Direct To waypoint as desired, but select 'HOLD?' instead of 'ACTIVATE?' when finished (MFD or PFD).
2) Use the FMS Knobs to edit the entry course, and press the ENT Key.
3) Use the small FMS Knob to select 'INBOUND' or 'OUTBOUND' course direction, and press the ENT Key.
4) Use the small FMS Knob to select 'TIME' or 'DIST' length mode, and press the ENT Key.
5) Use the FMS Knobs to edit the length, and press the ENT Key.
6) Use the small FMS Knob to select 'RIGHT' or 'LEFT' turn direction, and press the ENT Key.
7) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key.
8) Press the ENT Key while 'ACTIVATE?' is highlighted to activate the Direct To with the user-defined hold defined at the Direct To waypoint.

Removing a user-defined hold (created at an active flight plan waypoint):

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the HOLD waypoint.
3) Press the CLR Key. A 'Remove Holding Pattern?' confirmation window is displayed.
4) Select 'OK' and press the ENT Key. The holding pattern is removed from the active flight plan. Select 'CANCEL' and press the ENT Key to cancel the removal of the holding pattern.

Removing a user-defined hold (created at the aircraft present position or at a Direct-To waypoint):

1) Press the Direct To Key to display the DIRECT TO Window (PFD or MFD).
2) Press the MENU Key to display the PAGE MENU with the cursor on the 'Cancel Direct To NAV' selection.
3) Press the ENT Key. The holding pattern is removed.

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.

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.
3) Press the CLR Key to display a confirmation window.
4) 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.
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.
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) Press the FMS Knob to return to the Flight Plan Catalog Page.

DELETE A WAYPOINT FROM THE 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 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.
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.

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.
5) Select the DELETE Softkey. A 'Delete flight plan #?' confirmation window is 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.

1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
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 ABOVE the cursor. Turn the large FMS Knob to select the desired insertion point.
4) 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.

EXPORT A FLIGHT PLAN TO AN SD CARD

1) Insert the SD card into the top card slot on the MFD.
2) Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD.
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.
5) Turn the large FMS Knob to highlight the flight plan to be exported.
6) Select the EXPORT Softkey.
7) Press the ENT Key to confirm the export.

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.

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 TO waypoint of the desired leg 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.

4) Turn the large FMS Knob to highlight the desired arrival.
5) 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) 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) Turn the large FMS Knob to highlight the TO waypoint of the desired leg 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.

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches.

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 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, optional RAD ALT, or TEMP COMP.
9) Press the ENT Key. The cursor moves to the altitude field. Turn the small FMS Knob to enter the published DA/MDA for the selected approach procedure.
10) Press the ENT Key. If BARO, RAD ALT, or OFF was selected step 8, proceed to step 11. If TEMP COMP was selected in step 8, the cursor moves to the 'TEMP AT...." field. Turn the smalFMS Knob to enter the temperature at the destination airport. The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value.
11) Press the ENT Key. 'LOAD? or ACTIVATE?' is now displayed with 'LOAD?' highlighted.
12) 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.
13) 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.

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.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

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 TO/GA switch.

TEMPERATURE COMPENSATED ALTITUDE

When temperature compensated altitude is enabled for the loaded approach, the altitudes associated with the approach waypoints are displayed in slanted text.

Altitudes Displayed Without Temperature Compensation

Altitudes Displayed With Temperature Compensation

Enabling temperature compensated altitude:

1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed.
2) Turn the FMS Knob to highlight 'Temperature Compensation'.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed.
4) Use the small FMS Knob to select the temperature at the . The compensated altitude is computed as the temperature is selected.
5) Press the ENT Key. 'ACTIVATE COMPENSATION?' is highlighted.
6) Press the ENT Key. The compensated altitudes for the approach are shown in the flight plan.

Disabling temperature compensated altitude:

1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed.
2) Turn the FMS Knob to highlight 'Temperature Compensation'.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed.
4) Press the ENT Key. 'CANCEL COMPENSATION?' is highlighted.
5) Press the ENT Key. The temperature compensated altitude at the FAF is cancelled.

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HAZARD AVOIDANCE

WARNING: Do not use data link weather information for maneuvering in, near or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age.

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.

SWITCHING BETWEEN CONNEXT, AND SIRIUSXM WEATHER SOURCES

1) Turn the large FMS Knob on the MFD to select the MAP page group.
2) Turn the small FMS Knob to select the desired Weather Data Link Page.
3) Press the MENU Key.
4) Turn the large FMS Knob to select 'Display Connext Weather', or 'Display XM Weather' (choice dependent on current weather source) and press the ENT Key.

SIRIUSXM WEATHER (SUBSCRIPTION OPTIONAL)

Displaying SiriusXM 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 XM 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 XM Weather Data Link Page.
3) Select the available softkeys to select the desired SiriusXM Weather product.
4) Select the LEGEND Softkey to view the legends for the selected products. 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 – XM 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, SIGMETs, PIREPs or AIREPs.
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

Wx Product Status Icons	Description
	NEXRAD - Available for the US and Canada. The age of the displayed data for each is shown at the right.
	ECHO TOP - The age of the displayed data is shown at the right. Not displayed when CLOUD TOP is displayed.
	CLOUD TOP - The age of the displayed data is shown at the right. Not displayed when ECHO TOP is displayed.
	XM LIGHTNING - The age of the displayed data is shown at the right.
	CELL MOVEMENT - The age of the displayed data is shown at the right.
	SIGMET & AIRMET - The age of the displayed data for each is shown at the right.
	METAR - Available for the US and Canada. The age of the displayed data for each is shown at the right.
	SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts Surface Analysis. The lower symbol depicts City Forecast. The age of the displayed data for each is shown at the right. The selected forecast period is shown at the bottom.
	FREEZING LEVEL - The age of the displayed data is shown at the right.
	WINDS ALOFT - Available for the US and Canada. The age of the displayed data for each is shown at the right. The altitude selection is shown at the bottom.
	COUNTY WARNING - The age of the displayed data is shown at the right.
	CYCLONE WARNING - The age of the displayed data is shown at the right.
	AIREP - The age of the displayed data is shown at the right.
	PIREP - The age of the displayed data is shown at the right. Urgent Pireps are displayed in yellow.
	TURBULENCE - The age of the displayed data is shown at the right. The altitude selection is shown at the bottom.
	ICING POTENTIAL - The age of the displayed data is shown at the right. The altitude selection is shown at the bottom.

CONNEXT WEATHER (OPTIONAL)

WARNING: Do not use data link weather information for maneuvering in, near or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age.

NOTE: The availability of specific Garmin Connext Weather products varies by region. For product coverage information, refer to fly.garmin.com/fly-garmin/gfds-weather.

Weather data is provided when the pilot initiates either a manual or automatic Connext data request on the Weather Data Link (CNXT) Page on the MFD. No weather data is displayed until the first Connext Weather Data Request is made.

Registering with Garmin Connex

A subscriber account must be established prior to receiving Connext Weather products. Contact Garmin Connext at https://fly.garmin.com/fly-garmin/support/applications/satelliteservices/ or by calling 1-866-739-5687 in the United States or [phone]-1135. The following information is required to register for Connext Weather services: Prodigy System ID, GSR56 (GSR1) Serial Number, Tail Number, Serail/Airframe Number, Country of Registration, Aircraft Manufacturer, and Aircraft Model.

1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select the AUX-SYSTEM STATUS. Note the System ID and GSR1 Serial Number in the AIRFRAME field.

Activating Connext Weather Registration

After a subscriber account has been established, the system must be activated for data link features such as reporting services or Connext Weather. Activation is accomplished by entering the required access code. This process is only performed when initially setting up the system for Connext services.

1) Ensure the aircraft is outside and has a clear view of the sky (if registering via an Iridium satellite telephone connection), or connected to a Wi-Fi network. Refer to the Additional Features section for more information on connecting to a Wi-Fi network.

2) Turn the large FMS Knob on the MFD to select the MAP page group.

3) Turn the small FMS Knob to select the MAP - WEATHER DATA LINK (CNXT or XM) Page. If 'XM' is displayed in the page title, it will be necessary to change the data link source to Garmin Connext (CNXT) before continuing. Refer to 'Viewing the Weather Data Link Page' procedure to change the data link source to Garmin Connext Weather prior to registration.

4) If the system displays the 'Connext Registration' window, proceed to step 7. Otherwise, press the MENU Key.

5) Turn the large FMS Knob to highlight 'Register With Connex' in the menu list.

6) Press the ENT Key. The Connext Registration window is displayed.

7) Enter the access code provided by customer service in the ACCESS CODE field.

8) Press the ENT Key. 'REGISTER' is highlighted.
9) Press the ENT Key. The system contacts the Garmin Connext service using the GDL 59 Wi-Fi connection (if available) or through the Iridium satellite network using the GSR 56. Registration is complete when the STATUS field displays 'REGISTERED'.

Accessing Connext Weather Products

1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the smallFMS Knob to select the Weather Data Link (CNXT) Page.

When a weather product is selected for display on the Connext Weather Data Link Page, a box containing a symbol for the product and its age (in minutes) are shown in the upper right. If weather data has not been requested, 'N/A' is shown next to the product symbol instead of age. The age of the weather product is based on the time difference between when the data was assembled on the ground and the current GPS time. Weather products are updated continuously or refreshed at specific intervals (defined in the Refresh Rate column in the following table).

If for any reason, a weather product is not refreshed within the defined Expiration Time intervals, the data is considered expired and is removed from the display. The age of the expired product is replaced by dashes. If more than half of the expiration time has elapsed, the color of the product age readout changes to yellow.

The refresh rate represents the interval at which the Connext servers make available the most current known weather data. It does not necessarily represent the rate at which new content is received from weather sources.

Weather Product Symbol			Expiration Time (Minutes)	Refresh Rate (Minutes)
Radar Precipitation (PRECIP)			30	U.S./Canada: 3*Europe: 15
Infrared Satellite (IR SAT)			60 30
Data Link Lightning (DL LTNG)			30 Continuous

Weather Product Symbol		Expiration Time (Minutes)	Refresh Rate (Minutes)
SIGMETs/AIRMETs (SIG/AIR)		60 Continuous
Meteorological Aerodrome Report (METARs)		90 Continuous
Winds Aloft (WIND)		60 Continuous
Pilot Weather Report (PIREPs)		90 Continuous
Temporary Flight Restrictions (TFRs)	no product image 60 Continuous
Terminal Aerodrome Reports (TAFs)	no product image 60 Continuous

* The composite precipitation image is updated every 3 minutes, but individual radar sites may take between 3 and 10 minutes to provide new data.

Setting Up and Customizing the Connext Weather Data Link (CNXT) Page

1) Select the Weather Data Link (CNXT) Page.
2) Press the MENU Key.
3) With 'Weather Setup' highlighted, press the ENT Key.
4) Turn the small FMS Knob to select 'Product Group 1' or 'Product Group 2', and press the ENT Key.
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections.
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.).
7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Weather Data Link (CNXT) Page with the changed settings.

Restoring Default Configuration on Weather Data Link (CNXT) Page

1) Select the Weather Data Link (CNXT) Page.
2) Press the MENU Key.
3) With 'Weather Setup' highlighted, press the ENT Key.
4) Press the MENU Key.
5) Highlight the product group name (to restore default settings to the entire product group) or an individual weather product, then press the ENT Key.

Viewing Legends for Displayed Connext Weather Products

1) Select the Weather Data Link (CNXT) Page.
2) Select the LEGEND Softkey to display the legends for the displayed weather products.

Or:

a) Press the MENU Key.
b) Select 'Weather Legend' and press the ENT Key.

3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window.

4) To remove the Legend Window, select the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob.

Setting Up and Customizing Weather Data for the Navigation Map Page

1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With 'Map Setup' highlighted, press the ENT Key.
4) Turn the small FMS Knob to select the 'Weather' Group and press the ENT Key.
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections.
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

Connext Weather Data Requests

The Connext Data Request window provides the flight crew with the options to define the requested weather coverage area(s), choose automatic weather update intervals (if desired), and the ability to send or cancel weather data requests. The window also displays the status of the Connext data request process.

Requesting Connext Weather Data Manually

1) Select the Weather Data Link (CNXT) Page.
2) Press the MENU Key.
3) With 'Connext Weather Request' highlighted, press the ENT Key.
4) Turn the large FMS Knob to highlight the desired coverage option(s) and press the ENT Key to check or uncheck one of more of the following coverage selections:

• PRESENT POSITION – Requests data based on current location.
• DESTINATION – Requests data based on active flight plan destination (if the flight plan contains no destination, dashes '----' are displayed.)
• FPL – Requests data based on active flight plan. Turn the small FMS Knob to select the desired flight plan look-ahead distance option (or choose 'REMAINING FPL' to request the remainder of the flight plan).
• WAYPOINT – Requests data based on any valid waypoint.

5) Turn the large FMS Knob highlight to the 'DIAMETER / RTE WIDTH' distance field and turn the small FMS Knob to select the desired diameter and route width of the request, then press the ENT Key.

6) Turn the large FMS Knob until the 'SEND REQ' button is highlighted. Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the Connext Data Link Page without requesting data.

During a Connext Data Request, the Request Status box initially displays "Contacting Connext...". Once a connection is established, the Request Status Box displays "Receiving Wx Data... Time Remaining:" with an estimated data transfer time (either minutes or seconds). If desired, the Connext Data Request window may be closed while the data request is processing by pressing the FMS Knob; the data request will continue to process in the background. Connext Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength.

The system retrieves all available Connext Weather products within the selected coverage area during an initial Connext Data Request, regardless of which products (if any) are currently enabled for display. On subsequent requests, previously retrieved textual data (such as METARs and TAFs) is retained if it has not expired, while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request.

If the system cannot complete a Connext weather data request, one or more messages will appear in the request status window as shown in the following table.

Weather Request Status Message	Description
Auto requests inhibited Send manual request to reset.	The system has disabled automatic weather data requests due to excessive errors. Automatic weather data requests have stopped. Send a manual weather data request to resume automatic updates.
Auto update retry: ## Seconds	The system will attempt another automatic weather data request after an error occurred during the previous request. Timer counts down until the next automatic request occurs.
Connext Comm Error [2] A communications error has occurred with the GIA. The system should be serviced.
Connext Comm Error [4] This occurs if multiple automatic weather data requests have recently failed, or the GDL 59 or a GIA is off-line.
Connext Comm Error [5] The Iridium or Connext networks are not accessible. Check Iridium signal strength. If this error persists, the system should be serviced.
Connext Comm Error [6] A communications error has occurred. It this error persists, the system should be serviced.
Connext Comm Error [7] A weather data transfer has timed out. Check Iridium signal strength and re-send the data request.
Connext Comm Error [8] A server error has occurred or invalid data received.
Connext Login Invalid There is a problem with the Connext registration. Contact Garmin Connext at 1-866-739-5687 in the United States or [phone]-1135 for assistance.
Connext Server Temporarily Inop	The Connext weather data server is temporarily out of service, but is expected to return to service in less than 30 minutes.
Connext Server Inop The Conn	ext weather data server will be out of service for at least 30 minutes.
Invalid Coverage Area The weather	ther data request coverage area does not contain at least one of the following: a waypoint, a flight plan, or a flight plan destination. Verify at least one of the coverage options is enabled (checked) and contains required criteria, then re-send the data request.
No Connext Subscription The system	system is not be currently subscribed to Connext, or the access code is incorrect. Verify the access code. Contact Garmin Connext at 1-866-739-5687 in the United States or [phone]-1135 for assistance.
Reduce Request Area The Conn	next weather data request area exceeds size limits. Reduce weather coverage area and re-send data request.
Request Cancelled The user has cancelled a Connext weather data request.
Requested area too large. Reduce coverage area.	The size of the Connext weather data request has exceeded limits. Reduce the size of the coverage area and try the weather data request again.
Request Failed - Try Again	The weather data request timed-out. Re-send data request.
Transfer Preempted	The data link is busy. Retry request later.

Cancelling a Connex Data Request in Progress

1) Select the Weather Data Link (CNXT) Page.
2) Press the MENU Key.
3) With 'Connext Data Request' highlighted, press the ENT Key.
4) Turn the large FMS Knob to select 'CANCEL REQ' and press the ENT Key. The request status box indicates 'Request Cancelled'.
5) Press the FMS Knob to return to the Weather Data Link (CNXT) Page.

Enabling Automatic Connext Data Requests

1) Select the Weather Data Link (CNXT) Page.
2) Press the MENU Key.
3) With 'Connext Weather Request' highlighted, press the ENT Key.

4) Choose the desired weather coverage options.
5) Turn the large FMS Knob to select the 'UPDATE RATE' setting. Then turn the small FMS Knob to highlight the desired automatic update frequency (OFF, 5 Min, 10 Min, 15 Min, 20 Min, 25 Min, 30 Min, 45 Min, or 60 Min), then press the ENT Key.
6) The 'SEND REQ' button is highlighted and a countdown timer is displayed in the 'REQUEST STATUS' based on the currently selected update rate. Press the ENT Key to immediately send an immediate Connext Data Request.

Or:

Press the FMS Knob to return to the Weather Data Link (CNXT) Page.

Connext Weather Products

Precipitation

Precipitation data is not real-time. The lapsed time between collection, processing, and dissemination of radar images can be significant and may not reflect the current radar synopsis. Due to the inherent delays and the relative age of the data, it should be used for long-range planning purposes only.

NOTE: Precipitation data cannot be displayed on the Navigation Map Page at the same time as terrain.

Displaying Precipitation Weather Information

1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link (CNXT) Page.
2) Select the PRECIP Softkey.

Radar data shown represents lowest level, base reflectivity, of radar returns. The display of the information is color-coded to indicate the weather severity level. All weather product legends can be viewed on the Weather Data Link (CNXT) Page. For the Precipitation legend, select the LEGEND Softkey when Precipitation is selected for display.

Precipitation Limitations

Radar images may have certain limitations:

• Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics (wet hail vs. rain). For example, it is not possible to distinguish between wet snow, wet hail, and rain.
• Radar base reflectivity is sampled at the minimum antenna elevation angle. An individual radar site cannot depict high altitude storms at close ranges. It has no information about storms directly over the site.
• When zoomed in to a range of 30 nm, each square block on the display represents an area of four square kilometers.

The following may cause abnormalities in displayed radar images:

• Ground clutter
  • Strobes and spurious radar data
• Sun strobes (when the radar antenna points directly at the sun)
  • Interference from buildings or mountains, which may cause shadows
• Metallic dust from military aircraft, which can cause alterations in radar scans

Infrared Satellite

Infrared Satellite (IR SAT) data depicts cloud top temperatures from satellite imagery. Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes.

Displaying Cloud Tops information

1) Select the Weather Data Link (CNXT) Page.
2) Select the IR SAT Softkey.

To display the Infrared Satellite legend, select the LEGEND Softkey when Infrared Satellite data is selected for display.

Data Link Lightning

Lightning data shows the approximate location of cloud-to-ground lightning strikes. A strike icon represents a strike that has occurred within a two-kilometer region. Neither cloud-to-cloud nor the exact location of the lightning strike is displayed.

Displaying Data Link Lightning information

1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link (CNXT) Page.
2) Select the DL LTNG Softkey.

To display the Data Link Lightning legend on the Weather Data Link (CNXT) Page, select the LEGEND Softkey when Data Link Lightning is selected for display.

SIGMETs and AIRMETs

The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring within the coverage area of the Connext data request.

Displaying SIGMETs and AIRMETs

1) Select the Weather Data Link (CNXT) Page.
2) Select the SIG/AIR Softkey.
3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon.
4) Press the ENT key.

To display the SIGMET and AIRMET legend on the Weather Data Link (CNXT) Page, select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display.

METARs and TAFs

NOTE: METAR information is only displayed within the installed navigation database service area.

METAR and TAF text are displayed on the WPT-Weather Information Page. TAF information is displayed in its raw form when it is available.

Displaying METAR and TAF text

1) On the Weather Data Link (CNXT) Page, select the METAR Softkey.
2) Press the RANGE Knob and pan to the desired airport.
3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text.
4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely scrolled through before scrolling through the TAF text.
5) Press the FMS Knob or the CLR Key to return to the Weather Data Link (CNXT) Page.

Or:

1) Select the Weather Information Page.

a) Turn the large FMS Knob to select Airport Information from the Waypoint Page Group.
b) Select the WX Softkey to select the Weather Information Page.

2) Press the FMS Knob to display the cursor.
3) Use the FMS Knob to enter the desired airport and press the ENT Key.
4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. Note that the METAR text must be completely scrolled through before scrolling through the TAF text.

To display the METAR legend on the Weather Data Link (CNXT) Page, select the LEGEND Softkey when METARs are selected for display.

Winds Aloft

Winds Aloft data shows the forecasted wind speed and direction at the surface and at selected altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000 feet MSL.

Displaying Winds Aloft data on the Navigation Map

1) Select the Weather Data Link (CNXT) Page.
2) Select the MORE WX Softkey.
3) Select the WIND Softkey.
4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected.

To display the Winds Aloft legend on the Weather Data Link (CNXT) Page, select the LEGEND Softkey when Winds Aloft is selected for display.

Enabling/disabling winds aloft display in Profile View

1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With Map Setup highlighted, press the ENT Key.
4) Turn the small FMS Knob to select the Profile Group and press the ENT Key.
5) Turn the large FMS Knob to select 'Profile Winds'.
6) Turn the small FMS Knob to select 'On' or 'Off'.
7) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

PIREPs

Pilot Weather Reports (PIREPs) describe in-flight weather encountered by pilots. A PIREP may contain unforecast adverse weather conditions, such as low in-flight visibility, icing conditions, wind shear, turbulence, and type of aircraft flown. PIREPs are issued as either Routine (UA) or Urgent (UUA).

Displaying PIREP text

1) Select the Weather Data Link (CNXT) Page.
2) Select the MORE WX Softkey.
3) Select the PIREPS Softkey.
4) Press the RANGE Knob and pan to the desired weather report. A gray circle will appear around the weather report when it is selected.
5) Press the ENT Key. The PIREP text is first displayed in a decoded fashion, then as raw text.
6) Use the FMS Knob or the ENT Key to scroll through the PIREP text.
7) Press the FMS Knob or the CLR Key to close the PIREP text window and return to the Weather Data Link (CNXT) Page.

To display the PIREP or AIREP legend, select the LEGEND Softkey when PIREPs or AIREPs are selected for display.

The PIREP color is determined by the type (routine or urgent).

TRAFFIC INFORMATION SERVICE (TIS)

NOTE: If the system is configured to use the optional TCAS II, TIS is not available for use.

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.
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' will be displayed in the Traffic Mode field.
5) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6) Select the TNA MUTE Softkey to mute the "TIS Not Available" aural alert.

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 will now be displayed on the map.

TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS II) (OPTIONAL)

NOTE: If the system is configured to use TIS, the optional TCAS II is not available for use.

WARNING: The TCAS II system is intended for advisory use only. TCAS II is intended to help the pilot locate transponder-equipped traffic visually and to provide advisory vertical maneuver guidance to avoid traffic. It is the responsibility of the pilot to see and maneuver to avoid traffic, terrain, and obstacles.

Traffic Symbol	Description
	Non-Threat Traffic(intruder is beyond 5 nm and greater than 1200' vertical separation)
	Proximity Advisory (PA)(intruder is within 5 nm and less than 1200' vertical separation)
	Traffic Advisory (TA)(Potential collision area is within 20 to 48 seconds)
	Traffic Advisory Off Scale
	Resolution Advisory (RA)(Potential collision area is within 15 to 35 seconds)
	Resolution Advisory Off Scale

Traffic Symbol Description

System Test

1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.

3) Select the TEST Softkey. The aural annunciation "TCAS Test" will be heard. A test pattern of traffic symbols is displayed on the Traffic Page and inset map on the PFD. The VSI will display a red no descent indication and a green climb indication of 2000 feet per min. and red from 2000 to 4000+. The pitch display will also display the appropriate indications appropriate with the VSI. The self test takes approximately eight seconds to complete, after which a voice alert "TCAS Test Passed" is heard. In the event the system test fails, a voice alert "TCAS Test Failed" is heard and a visual annunciation 'TCAS FAIL' appears on the PFD. In addition, a visual annunciation 'FAIL' appears in the Operating Mode box on the Traffic Map Page.

Displaying Traffic on the Traffic Map Page

1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.
3) Select the TA ONLY or TA/RA Softkey to begin displaying traffic. 'TA/RA' or 'TA ONLY' respectively, is displayed in the TCAS Mode field.
4) Select the STANDBY Softkey to place the system in the Standby Mode. 'TFC STBY' will be displayed in the TCAS Mode field.
5) Select the ABS (absolute) or REL (relative) Softkey to display intruder altitude as an absolute altitude or an altitude relative to own aircraft altitude.
6) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Changing the Altitude Range

1) On the Traffic Page, select the ALT RNG Softkey.
2) Select one of the following Softkeys:

AB OVE: Displays non-threat and proximity traffic from 9900 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight.

NO RMAL: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight.

BE LOW: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight.

UN REST (unrestricted): All traffic is displayed.

3) To return to the Traffic Page, select the BACK Softkey.

Displaying Traffic on the Navigation Map

1) Ensure TCAS II system is operating. With the Navigation Map displayed, select the MAP Softkey.
2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map.

TERRAIN AWARENESS & WARNING SYSTEM

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.

NOTE: TAWS operation is only available when the system is configured for a TAWS-A or TAW-B installation.

Manual System Test

1) While the TAWS-A or TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select 'Test TAWS System'.
3) Press the ENT Key. During the test 'TAWS TEST' is displayed in the center of the TAWS-A Page.
When all is in working order, "TAWS System Test, OK" is heard.

Displaying the TAWS-A or TAW-B Page

1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the TAWS-A or TAWS-B 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
Red	Terrain/Obstacle above or within 100' below current aircraft altitude.
Yellow	Terrain/Obstacle between 100' and 1000' below current aircraft altitude.
Black	Terrain/Obstacle is more than 1000' below aircraft altitude.

Enable/Disable Aviation Data

1) While the TAWS-A or TAWS-B 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.

Inhibiting/Enabling FLTA and PDA Alerting (TAWS-A Only)

1) Select the TAWS-A Page.
2) Press the TAWS INH Softkey to inhibit or enable TAWS-A (choice dependent on current state).

Overriding Flaps-based FIT Alerting (TAWS-A Only)

1) Select the TAWS-A Page.
2) Press the FLAP OVR Softkey.

Inhibiting/Enabling GPWS Alerting (TAWS-A Only)

1) Select the TAWS-A Page.
2) Press the GPWS INH Softkey to inhibit or enable GPWS alerts (choice dependent on current state).

Inhibiting/Enabling GSD Alerting (TAWS-A Only)

NOTE: Only available during a GSD alert.

On the PFD, press the GS INH or GP INH Softkey (only displayed during a GSD alert) to inhibit or enable GSD alerts (softkey choice dependent on present GSD alert type).

TAWS Inhibit (TAWS-B Only)

NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS 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.

Disable TAWS

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

Or:

1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select 'Enable TAWS'.
3) Press the ENT Key.

Displaying Terrain and Obstacles on the Navigation Map

1) With the Navigation Map displayed, press the MAP Softkey.
2) Select the TERRAIN Softkey. Terrain and obstacles will now be displayed on the map.

PROFILE VIEW TERRAIN AND OBSTACLES

The system offers a Profile View of terrain and obstacles relative to the aircraft's current flight path and altitude on the Navigation Map Page of the MFD. Profile View does not provide terrain or obstacle caution or warning annunciations or voice alerts, nor does it display potential impact points inside the Profile View.

Enabling/Disabling Profile View

While viewing the Navigation Map Page, select the PROFILE Softkey.

Enabling/Disabling Terrain on the Profile View

1) Select the Navigation Map Page.
2) Select the MAP Softkey.
3) Select the TERRAIN Softkey.

Customizing the Profile Path display on the Navigation Map Page

1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With 'Map Setup' highlighted, press the ENT Key.
4) Turn the small FMS Knob to select the 'Profile' Group and press the ENT Key.
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections.

- PROFILE PATH – Turns the display of the Profile Path on or off and sets maximum map range at which the Profile Path is shown

6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings).

7) Press the ENT Key to select an option.

8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

AIRBORNE COLOR WEATHER RADAR

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 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) Select the MODE Softkey.
4) If the aircraft is on the ground, select the STANDBY Softkey to initiate the one minute warm-up period (GWX 68 only). 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 (GWX 68 only). 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.

Enabling/Disabling Weather Radar Overlay on the Navigation Map Page

Only tilt and bearing can be changed from the Navigation Map radar overlay. Other functions are only accessible from the Weather Radar Page.

1) Select the Navigation Map Page.
2) Select the MAP Softkey.
3) Select the WX RADAR Softkey.

Or:

1) On the Navigation Map Page, press the MENU Key.
2) With 'Map Setup' highlighted, press the ENT Key.
3) Turn the small FMS Knob to select the 'Weather' group, then press the ENT Key.
4) Turn the large FMS Knob to scroll through the product selections and highlight the WX RADAR overlay selection ('On' or 'Off'). Turn the small FMS knob to highlight the desired selection.
5) To remove the menu, press the FMS Knob or CLR Key.

Adjusting Antenna Tilt

Move the Joystick up or down to adjust the tilt of the antenna up or down. Monitor the displayed tilt value in the TILT field.

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:

Display the Tilt Line

1) Press the MENU Key
2) Turn the large FMS Knob to select 'Show Tilt Line'.
3) Press the ENT Key.

Adjusting Antenna Tilt on the Horizontal Scan Display

1) Press the FMS Knob to activate the cursor in the TILT field.
2) Turn the small FMS Knob to select the desired antenna tilt angle.
3) Press the FMS Knob to remove the cursor.

The Joystick can also be used to adjust tilt up and down.

Adjusting Antenna Tilt on the Vertical Scan Display

1) Press the TILT Softkey to activate the cursor in the TILT field and display the Tilt Line.

If the Tilt Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Tilt Line. Press the ENT Key.

2) Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt angle is implemented when Horizontal Scan is again selected.

The Joystick can also be used to adjust tilt.

Vertical Scanning

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.

Display the Bearing Line

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, press the BRG Softkey. This places the cursor in the BEARING field and displays the Bearing Line.
2) Press the ENT Key.
3) Turn the small FMS Knob to place the Bearing Line on the desired storm cell or other area to be vertically scanned.
4) Press the VERTICAL Softkey. A vertical slice of the selected area is displayed.
5) The small FMS Knob may be used to move the scanned slice a few degrees right or left.
6) Turn the Joystick to adjust the range.
7) Press the FMS Knob to remove the cursor.
8) To select a new area to be vertically scanned, press the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps.

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.

Ground Mapping

1) Press the MODE Softkey.
2) Press the GROUND Softkey to place the radar in Ground Map mode.
3) Press the BACK Softkey.
4) Press the FMS Knob to activate the cursor.
5) Turn the large FMS Knob to place the cursor in the TILT field.
6) Adjust the antenna tilt angle by turning the small FMS Knob to display ground returns at the desired distance.
7) Press the FMS Knob to remove the cursor.

Ground Map Mode Color	Intensity
Black	0 dB
Light blue	>0 dB to < 9 dB
Yellow	9 dB to < 18 dB
Magenta	18 dB to < 27 dB
Blue	27 dB and greater
Ground Target Return Intensity Levels

Sector Scan

1) While in horizontal scan mode, press the BRG Softkey to display the Bearing Line and place the cursor in the BEARING field. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line.
2) Press the ENT Key.
3) Turn the small FMS Knob to place the Bearing Line in the desired position. The location of the Bearing Line becomes the center point of the Sector Scan.
4) Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
5) Turn the small FMS Knob to select FULL, 60°, 40°, or 20° scan.
6) If desired, readjust the Bearing Line as discussed previously to change the center of the Sector Scan.
7) Press the BRG Softkey again to remove the Bearing Line and cursor. The bearing reference resets to 0° .

Antenna Stabilization

1) To activate or deactivate the antenna stabilization, select the MODE Softkey.
2) 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®)

To activate or deactivate the WATCH ^® feature, select the WATCH Softkey. This feature is only available in the Horizontal Scan Mode.

Weather Alert

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

ADDITIONAL FEATURES

SYNTHETIC VISION (OPTIONAL)

WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.

Synthetic Vision Technology (SVT) functionality is offered as an optional enhancement to the Prodigy® Flight Deck 300.

SVT is primarily comprised of a computer-generated forward-looking, attitude aligned view of the topography immediately in front of the aircraft from the pilot's perspective. SVT information is shown on the primary flight display (PFD).

SVT offers a three-dimensional view of terrain and obstacles. Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red.

In addition to SVT enhancement to the PFD, the following feature enhancements have been added to the PFD:

• Pathways
• Flight Path Marker
  • Horizon Heading Marks
  • Terrain and Obstacle Alerting
  • Three-dimensional Traffic
• Airport Signs
• Runway Display

Displaying Synthetic Terrain

1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the SYN TERR Softkey.
4) Press the BACK Softkey to return to the previous page.

Displaying Pathways

NOTE: When the optional TCAS II system issues a Resolution Advisory (RA) Pathways are automatically removed from the display. Pathways may again be displayed by the pilot manually selecting Pathways.

NOTE: Pathways are not available when the cross-pointer (X-Pointer) flight director format is selected.

1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
4) Press the PATHWAY Softkey.
5) Press the BACK Softkey to return to the previous page.

Displaying Heading on the Horizon

1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
4) Press the HRZN HDG Softkey.
5) Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
4) Press the APTSIGNS Softkey.
5) Press the BACK Softkey to return to the previous page.

TERMINAL PROCEDURE CHARTS

NOTE: With the availability of SafeTax ^® , ChartView, or FliteCharts ^® , it may be necessary to carry another source of charts on-board the aircraft.

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.

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

The SafeTaxi database contains detailed airport diagrams for selected airports. These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways, ramps, runways, terminals, and services. This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground. This database is updated on a 56-day cycle.

ChartView (Optional)

ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams.

TheChartView database is updated on a 14-day cycle. If theChartView database is not updated within 70 days of the expiration date,ChartView will no longer function.

FliteCharts® (Optional)

FliteCharts ^® resemble the paper version of AeroNav Services terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams.

The FliteCharts database contains procedure charts for the United States only. This database is updated on a 28-day cycle. If not updated within 180 days of the expiration date, FliteCharts will no longer function.

View Charts from the Navigation Map Page

1) Select the SHW CHRT Softkey when displayed.

Or:

Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey.

2) Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for departures, arrivals, approaches, weather and NOTAMs. Note that NOTAMS are only available with ChartView.
3) Select the GO BACK Softkey to return to the previous page.

View Charts from the Active Flight Plan Page

1) While viewing the Active Flight Plan Page, press the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to select the departure airport, destination airport, departure, arrival, or approach.
3) Select the SHW CHRT Softkey. The appropriate chart will be displayed, if available for the item selected.
4) Select the GO BACK Softkey to return to the previous page.

Change Day/Night View

1) While viewing a chart press the MENU Key to display the Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the 'Chart Setup' Menu Option and press the ENT Key.
3) Turn the large FMS Knob to move between the 'FULL SCREEN' and 'COLOR SCHEME' Options.
4) Turn the small FMS Knob to choose between the 'On' and 'Off' Full Screen Options.
5) Turn the small FMS Knob to choose between 'Day', 'Auto', and 'Night' Options.

6) In Auto Mode, turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob. The percentage of change is the day/night crossover point based on backlighting intensity.
7) Press the FMS Knob when finished to remove the Chart Setup Menu.

AIRPORT DIRECTORY

The AOPA or AC-U-KWIK Airport Directory adds enhanced airport information when viewing airports on the WPT-Airport Information Page.

The Airport Directory databases are revised every 56 days. Check fly.garmin.com for the current database.

View Airport Directory Information

While viewing the WPT-Airport Information Page, if necessary, select the INFO-1 Softkey to change the softkey label to display INFO-2. Airport Directory information is displayed on the right half of the display.

SATELLITE TELEPHONE AND DATA LINK SERVICES (OPTIONAL)

Operation of these features in the cockpit is accomplished through the AUX-TELEPHONE, AUX-TEXT MESSAGING, AUX-MAINTENANCE LOGS, and AUX-WI-FI SETUP Pages. For operation using the cabin handset, consult the instructions provided with the handset.

Registering With Garmin Connext Satellite Services

A subscriber account must be established prior to using the Iridium Satellite System. Before setting up an Iridium account, obtain the serial number of the Iridium Transceiver and the System ID by viewing the AUX- SYSTEM STATUS Page. Contact Garmin Connext at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135.

Telephone Communication

The pilot or copilot can place and answer calls on the Iridium satellite network as well as to or from the telephone handset in the cabin. Calls can also be answered or made from the cabin phone, however, only actions initiated from the cockpit phone will be discussed here. See the cabin handset user guide for more information. Control and monitoring of telephone functions are accomplished through the AUX-TELEPHONE Page.

Viewing the Telephone Page

1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select SATELLITE PHONE.
3) If necessary, select the TEL Softkey to display the AUX-TELEPHONE Page.

Internal Phone	External Phone	Description
		Phone is Idle
		Phone is ringing
		Phone has a dial tone (off hook) or connected to another phone
		Phone dialed is busy
		Phone is dialing another phone
		Phone has failed
		Phone status not known
		Phone is disabled
		Phone is reserved for data transmission
		Calling other phone or incoming call from other phone
		Other phone is on hold
		Phones are connected

Enable the Iridium Tranceiver System

1) With the AUX-TELEPHONE Page displayed, select the MENU Key on the MFD to display the Page Menu.
2) Turn either FMS Knob to place the cursor on 'Enable Iridium Transmission'.
3) Press the ENT Key.

Disable the Iridium Transceiver System

1) With the AUX-TELEPHONE Page displayed, select the MENU Key on the MFD to display the Page Menu.
2) Turn either FMS Knob to place the cursor on 'Disable Iridium Transmission'.
3) Press the ENT Key.

Contacts

The names, telephone number, and email addresses can be saved in a list of contacts for easy use when making telephone calls.

Entering a new contact:

1) With the AUX-TELEPHONE Page displayed, press the FMS Knob to display the cursor.
2) If necessary, turn either FMS Knob to place the cursor on 'NEW ENTRY'.
3) Press the ENT Key. The cursor moves the 'NAME' field of the 'CONTACT DETAILS' window.
4) Enter the desired name of the new contact. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD.
5) Press the ENT Key. The cursor moves to the 'PHONE NUMBER' field.

6) Enter the desired telephone number. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD.
7) Press the ENT Key. The cursor moves to the 'EMAIL' field.
8) Enter the desired email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD.
9) Press the ENT Key. The SAVE button is highlighted.
9) Press the ENT Key. The new contact entry is added to the list of saved contacts.

Delete a contact:

1) With the AUX-TELEPHONE Page displayed, press the FMS Knob to display the cursor.
2) Turn either FMS Knob to place the cursor on the desired contact name.
3) Select the DELETE Softkey. A confirmation window is displayed.
4) With 'OK' highlighted, press the ENT Key to delete the selected contact.

Edit a contact:

1) With the AUX-TELEPHONE Page displayed, press the FMS Knob to display the cursor.
2) Turn either FMS Knob to place the cursor on the desired contact name.
3) Select the EDIT Softkey. The cursor is placed in the 'NAME' field. Enter the desired changes. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or the FMS Knobs on the controller or the MFD.
4) Press the ENT Key when each field is complete. The SAVE Button is now highlighted.
5) Press the ENT Key to save the changes.

Incoming Calls

When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up alert will be displayed. If the call is from the cabin, CABIN will be displayed. If the incoming call is an Iridium network call, IRIDIUM will be displayed. The pop-up alert may be inhibited at times, such as during takeoff. In addition to the pop-up alert, a ringing phone symbol will be displayed to the right of the MFD page title. Also, the voice alert “Incoming Call” will be heard on the selected cockpit audio.

Answer an Incoming Call in the Cockpit

1) Press the TEL Key on the appropriate audio panel.
2) Select the ANSWER Softkey on the MFD.

Or:

While viewing the AUX-TELEPHONE Page:

1) Press the TEL Key on the appropriate audio panel.
2) Press the MENU Key to display the Page Menu.
3) Turn either FMS Knob to place the cursor on 'Answer Incoming Call'.
4) Press the ENT Key.

Selecting the IGNORE Softkey will extinguish the pop-up window and leave the current call unanswered. Selecting the IGNRE ALL Softkey will extinguish the pop-up window for the current and all future incoming calls and leave the current call unanswered. Selecting the TEL Softkey will display the AUX-TELEPHONE Page allowing additional call information to be viewed before answering.

Disabling Incoming Call Alerts

1) With the AUX-TELEPHONE Page displayed, press the MENU Key on the MFD to display the Page Menu.
2) Turn either FMS Knob to place the cursor on 'Disable Incoming Call Alerts'.
3) Press the ENT Key. The voice and pop-up alert will not be displayed now when an incoming call is received.

Outgoing Calls

Voice calls can be made from the cockpit to the handset in the cabin, or to an external phone through the Iridium Satellite Network.

Make a Call to the Cabin:

1) Press the TEL Key on the appropriate audio panel.
2) Select the DIAL Softkey on the MFD.
3) Press the ENT Key. The cursor will move from 'CABIN' to 'OK'.
4) Press the ENT Key again. The cabin phone will now ring.

To exit the call, select the HANGUP Softkey.

To make an external call from the cockpit by dialing the number:

1) Press the TEL Key on the appropriate audio panel.
2) Select the DIAL Softkey on the MFD.
3) Turn the small FMS Knob to select 'IRIDIUM'.
4) Press the ENT Key. The cursor has now moved to the phone number entry field.
5) Enter the desired telephone number by selecting the number softkeys on the MFD or by pressing the numeric keys on the MFD Control Unit. The International dialing sequence is necessary to place a call from the cockpit to an external phone: Country Code + City/Area Code (if any) + Telephone Number. The following country codes may be used when calling other satellite telephone systems.

Satellite System Country Code
Inmarsat	870
ICO	8810 or 8811
Ellipso	8812 or 8813
Iridium	8816 or 8817
Globalstar	8818 or 8819

6) Press the ENT Key. 'OK' is highlighted.

7) Press the ENT Key. The system will begin calling the number.

When numeric entries are required while a call is connected, such as selecting menu items like “dial zero to get an operator”, select the KEYPAD Softkey to access the numeric softkeys. To exit the call, select the HANGUP Softkey.

To make an external call from the cockpit by using the Contact List:

1) Press the TEL Key on the appropriate audio panel.
2) Press the FMS Knob to activate the cursor.
3) Turn the small FMS Knob to select the desired contact name in the list of contacts.
4) Select the CALL Softkey. The external call is initiated and the number associated with the contact name is dialed.

To exit the call, select the HANGUP Softkey.

Placing The Cockpit Phone on Hold

Select the HOLD Softkey on the MFD.

Or:

1) Press the MENU Key to display the Page Menu.
2) Turn either FMS Knob to place the cursor on 'Put Current Call On Hold'.
3) Press the ENT Key.

Select the HOLD Softkey again to resume the call.

Transferring a Call from the Cockpit

From the cockpit phone, an external call can be transferred to the cabin phone, or a call with the cabin phone can be transferred to an external phone.

To transfer a call:

1) Select the TRANS Softkey on the MFD.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Transfer Current Call'.
c) Press the ENT Key.

2) Press the ENT Key. The cursor now highlights the phone number entry field.

3) Enter the phone number as discussed earlier for making an external call on the Iridium satellite network.

4) Press the ENT Key. 'OK' is now highlighted.

5) Press the ENT Key again to place the call.

Making a Conference Call from the Cockpit

1) Select the CONF Softkey on the MFD.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Conference Current Call'.
c) Press the ENT Key.

2) Press the ENT Key. The cursor now highlights the phone number entry field.
3) Enter the phone number as discussed earlier for making an external call on the Iridium satellite network.
4) Press the ENT Key. 'OK' is now highlighted.
5) Press the ENT Key again to place the call.

Text Messaging (SMS)

Messages may be sent to an email address or text message capable cellular telephone. Message length is limited to 160 characters, including the email address.

The text messaging user interface is mainly through the AUX-TEXT MESSAGING Page.

Viewing the Text Messaging Page

1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select SATELLITE PHONE.
3) If necessary, select the SMS Softkey to display the AUX-TEXT MESSAGING Page.

Message Symbol Description
	Received text message that has not been opened
	Received text message that has been opened
	Saved text message, draft not sent
	System is sending text message
	Text message has been sent
	System failed to send text message
	Predefined text message

Viewing a Text Message When Received

When viewing MFD pages other than the AUX-TEXT MESSAGING Page, a pop-up alert will be displayed when a new text message is received.

Select the VIEW Softkey to view the message. Selecting the IGNORE Softkey will extinguish the pop-up window and leave the text message unopened. Selecting the IGNR ALL Softkey will extinguish the pop-window and ignore all future incoming text messages. Selecting the SMS Softkey will display the AUX-TEXT MESSAGING Page.

The pop-up alerts may be enabled or disabled through the Page Menu.

Enable/Disable Incoming Text Message Pop-Up Alerts

1) With the AUX-TEXT MESSAGING Page displayed, press the MENU Key on the MFD to display the Page Menu.
2) Turn either FMS Knob to place the cursor on 'Disable New Message Popups' or 'Enable New Message Popups'.
3) Press the ENT Key. The pop-up alert will not be displayed when an incoming text message is received.

Reply to a Text Message

While viewing the text message, select the REPLY Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Reply To Message'.
c) Press the ENT Key.

Sending a Text Message

1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey. Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Draft New Message'.
c) Press the ENT Key.

2) The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the 'TO' field. Enter the desired telephone number or email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey.

3) Press the ENT Key. The cursor is now displayed in the 'MESSAGE' field.
4) Enter the desired message using any combination of entry methods as described in step 2.
5) Press the ENT Key.
6) Select the SEND Softkey to send the message immediately, or select the SAVE Softkey to save the message in Outbox for sending at a later time. Select the CANCEL Softkey to delete the message.

Predefined Text Messages

Time and effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message.

Create a Predefined Text Message

1) While viewing the AUX-TEXT MESSAGING Page, press the MENU Key to display the Page Menu.
2) Turn either FMS Knob to select 'Edit Predefined Messages'.
3) Press the ENT Key. The PREDEFINED MESSAGES view is now displayed.

4) Select the NEW Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Draft New Predefined Message'.
c) Press the ENT Key. The PREDEFINED SMS TEXT MESSAGE Window is now displayed.

5) The cursor is displayed in the 'TITLE' field. Enter the desired message title. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey.

6) Press the ENT Key. The cursor is now displayed in the 'MESSAGE' field.
7) Enter the desired message using any combination of entry methods as described in step 5.
8) Press the ENT Key.
9) Select the SAVE Softkey. The new predefined message is now shown in the displayed list. Selecting the CANCEL Softkey will delete the message without saving.
10) Press the MENU Key to display the Page Menu.
11) Turn either FMS Knob to place the cursor on 'Stop Editing Predefined Message'.
12) Press the ENT Key.

Send a Predefined Text Message

1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey.
2) The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the 'TO' field. Enter the desired telephone number or email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey.

3) Press the ENT Key. The cursor is now displayed in the 'MESSAGE' field.
4) Select the PREDEFD Softkey. The PREDEFINED MESSAGE MENU Window is displayed.
6) Press the ENT Key. The predefined message text is inserted into the message field. If desired, the message can be edited by using the FMS Knobs.
7) Press the ENT Key.
8) Select the SEND Softkey to transmit the message.

Text Message Boxes

Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The Outbox contains ‘Sent’ and ‘Unsent’ text messages. Saved messages that are meant to be sent later are stored as Drafts. Each text message box may be viewed separately, or together in any combination.

Show Inbox Messages

While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the INBOX Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Show Inbox Messages'.
c) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window.

Show Outbox Messages

While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the OUTBOX Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Show Outbox Messages'.
c) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window.

Show Draft Messages

While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the DRAFTS Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Show Draft Messages'.
c) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window.

Arranging Text Messages

The viewed messages may be listed according to the date/time the message was sent or received, the type of message (read, unread, sent, unsent, etc.), or by message address.

View Messages Sorted by Message Date/Time:

While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the TIME Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Sort By Date/Time'.
c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window.

View Messages Sorted by Message Type

While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the TYPE Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Sort By Type'.
c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window.

View Messages Sorted by Address:

While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the ADDRESS Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Sort By Address'.
c) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window.

Viewing The Content of a Text Message

1) While viewing the AUX-TEXT MESSAGING Page, select the desired message box.
2) Press the FMS Knob to activate the cursor.
3) Turn either FMS Knob to select the desired message.
4) Select the VIEW Softkey.

Or:

Press the ENT Key.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'View Selected Message'.
c) Press the ENT Key.

5) To close the text message, select the CLOSE Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Close Message'.
c) Press the ENT Key.

Mark Selected Message As Read

1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the FMS Knob to activate the cursor.
2) Turn either FMS Knob to select the desired message.

3) Select the MRK READ Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Mark Selected Message As Read'.
c) Press the ENT Key.

The message symbol now indicates the message has been opened.

Mark All Messages As Read

1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the MENU Key to display the Page Menu.
2) Turn either FMS Knob to place the cursor on 'Mark All New Messages As Read'.
3) Press the ENT Key. A confirmation window is displayed.
4) With cursor highlighting 'YES', press the ENT Key. The message symbols now indicate all the message have been opened.

Delete a Message

1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the FMS Knob to activate the cursor.
2) Turn either FMS Knob to select the desired message.
3) Select the DELETE Softkey.

Or:

a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on 'Delete Selected Message'.
c) Press the ENT Key.

WI-FI CONNECTIONS (OPTIONAL)

Control and monitoring of Wi-Fi functions are accomplished through the AUX-WI-FI SETUP Page.

Viewing the Wi-Fi Setup Page

1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select DATA LINK.

Setting Up a New Wi-Fi Connection

1) Select the AVAIL Softkey on the MFD. A list of available networks will be displayed in the AVAILABLE NETWORKS window. Signal strength is shown for each network, as well as security methods and whether the network has been saved in the system's memory.
2) If necessary, select the RESCAN Softkey to have the system scan again for available networks.
3) Press the FMS Knob to place the cursor in the list of networks.
4) Turn either FMS Knob to select the desired network.
5) Select the CONNECT Softkey.
6) If the network is secured, enter the necessary passcode. Use the FMS Knobs to enter the desired alpha numeric characters. Select the CAP LOCK Softkey to enter upper case letters. If there is no security associated with the network, proceed to step 9.
7) Press the ENT Key. 'OK' will be highlighted.
8) Press the ENT Key again.
9) The SAVE SETTINGS window is now displayed with the cursor highlighting 'SAVE CONNECTION'.
10) The selected network can be saved to system memory to make reconnection easier at a later time.

To connect the selected network without saving:

a) Turn the large FMS Knob to move the cursor to highlight 'CONNECT'.
b) Press the ENT Key.

To save and connect the selected network:

a) Press the ENT Key. A checkmark is placed in the checkbox and the cursor moves to the airport field.
b) Using the FMS Knobs, enter an airport identifier to be associated with the saved network. This aids in identifying the network later in the event of duplicate network names.
c) Press the ENT Key. The cursor moves to 'CONNECT'.
d) Press the ENT Key again to connect to the selected network.

Editing a Saved Network

1) While viewing list of saved networks, press the FMS Knob to activate the cursor.
2) Turn either FMS Knob to highlight the network to be edited.
3) Pressing the ENT Key at this point will check or uncheck the AUTO CONNECT checkbox. When a checkmark is present, the system will automatically connect to the network when within range.
4) Select the EDIT Softkey. The cursor now appears in the CONNECTION SETTINGS window.
5) Turn the large FMS Knob to select the network attribute to be edited.
6) Turn the small FMS Knob to begin editing the field.
7) When the entry is complete, press the ENT Key.
8) Turn the large FMS Knob or press the ENT Key until 'SAVE' is highlighted.
9) Press the ENT Key.

Disconnecting a Wi-Fi Network

Select the DISCNCT Softkey.

Deleting a Saved Wi-Fi Network

1) While viewing the list of saved networks, press the FMS Knob to activate the cursor.
2) Turn either FMS Knob to highlight the network to be deleted.
3) Select the DELETE Softkey. The selected network is removed from the list.

MAINTENANCE LOGS (OPTIONAL)

NOTE: An account must be established with Garmin Flight Data Services to make full use of the System Data Logging feature.

The system provides recording of CAS, CMC, exceedances, and other critical aircraft data that occur while the aircraft is on the ground or in flight. This information may be used by aircraft maintenance personnel in determining specific maintenance requirements.

The Maintenance Logs feature is accessible by entering a password. No pilot action is required.

Viewing the Maintenance Logs Page:

1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select 'MAINTENANCE LOG'. The AUX-MAINTENANCE LOGS Page is now displayed.
3) Select the PSWD Key to enter the password.
4) Enter the password.
5) Press the ENT Key to access the page.

SIRIUSXM SATELLITE RADIO ENTERTAINMENT (SUBSCRIPTION OPTIONAL)

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

Selecting the XM Radio Page

1) Turn the large FMS Knob to select the AUX Page Group.
2) Turn the small FMS Knob to select XM RADIO.
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.

Selecting a Category

The Category Box of the XM Radio Page displays the currently selected category 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:
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 down through the list in the Channel Box, or move up the list with the CH - Softkey.

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

1) While on the XM Radio Page, select the CHNL Softkey.
2) 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

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). Selecting the MORE Softkey repeatedly cycles through the preset channels.
3) Select the SET Softkey.
4) Select any one of the (PS1 - PS15) softkeys to assign a number to the active channel.

Adjusting Volume

1) With the XM Radio Page displayed, press the VOL Softkey.
2) Press the VOL – Softkey to reduce volume or press the VOL + Softkey to increase volume. (Once the VOL Softkey is pressed, the volume can also be adjusted using the small FMS Knob.)

Mute SiriusXM Audio

1) Select the XM Radio Page or XM Information Page.
2) Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to unmute the audio.

ELECTRONIC CHECKLISTS (OPTIONAL)

The system accesses the checklists from an SD card inserted into the card slot. If the SD card contains an invalid checklist file or no checklist, the Power-up Page messages display 'Checklist File: Invalid' or 'Checklist File: N/A' (not available) and the CHKLIST Softkey is not available.

The following colors are used for checklist items:

- Light Blue - Items not selected or checked

• Gray - General notes
• Yellow - Caution notes
• Red - Warning notes

- White - Item is selected

- Green - Item has been checked

Accessing and Navigating Checklists

1) From any page on the MFD, select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page.
2) Turn the large FMS Knob to select the 'GROUP' field.
3) Turn the small FMS Knob to select the desired procedure and press the ENT Key.
4) Turn the large FMS Knob to select the 'CHECKLIST' field.
5) Turn the small FMS Knob to select the desired checklist and press the ENT Key. The selected checklist item is indicated with white text surrounded by a white box.
6) Press the ENT Key or select the CHECK Softkey to check the selected checklist item. The line item turns green and a checkmark is placed in the associated box. The next line item is automatically selected for checking.
Either FMS Knob can be used to scroll through the checklist and select the desired checklist item.
Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item.

7) When all checklist items have been checked, '*Checklist Finished*' is displayed in green text at the bottom left of the checklist window and 'GO TO NEXT CHECKLIST?' is highlighted. If 'GO TO NEXT CHECKLIST?' is selected prior to checking all the checklist items, '*CHECKLIST NOT FINISHED*' will be displayed in yellow text.
8) Press the ENT Key. If 'GO TO NEXT CHECKLIST?' is displayed when pressing the ENT Key, the next checklist in the group will be displayed. If 'EXIT CHECKLISTS?' is displayed when pressing the ENT Key, the system will exit the Checklist Page.
9) Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed. When returning to the Checklist Page after pressing the EXIT Softkey, the system will return to the last selected checklist item.

Immediately Accessing Emergency Procedures

1) From any page on the MFD, select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page.
2) Select the EMERGCY Softkey.
3) Turn the FMS Knob to select the desired emergency checklist and press the ENT Key.
4) Press the ENT Key or select the CHECK Softkey to check the selected emergency checklist item. The line item turns green and a checkmark is placed in the box next to it. The next line item is automatically highlighted for checking.

Either FMS Knob can be used to scroll through the checklist and select the desired checklist item.

Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item.

5) When all checklist items have been checked, '*Checklist Finished*' is displayed in green text at the bottom left of the checklist window and 'GO TO NEXT CHECKLIST?' is highlighted. If 'GO TO NEXT CHECKLIST?' is selected prior to checking all the checklist items, '*CHECKLIST NOT FINISHED*' will be displayed in yellow text.
6) Press the ENT Key to advance to the next checklist.
7) Select the RETURN Softkey to return to the previous checklist.
8) Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed.

POSITION REPORTING (OPTIONAL)

NOTE: An account must be established with Garmin Connext ^™ to make full use of the Position Reporting feature.

The position reports are received by Garmin Connext and forwarded to select flight tracking provider(s), such as FlightAware.com.

While active, the position reports are transmitted over the Iridium Short Burst Datalink periodically at a pilot specified interval or by selecting the SEND RPT Softkey. The minimum automatic transmission period between reports is two minutes with more frequent transmissions possible via manually sending reports with the SEND RPT Softkey. During voice communications and data transfers the Iridium datalink is occupied and position reports will not be sent. During this period the reports will buffer and be sent as a package as soon as the link is available.

The following are position reports contents:

• Tail Number
• Time
• Latitude/Longitude
• Ground Speed
• Ground Track
• True Heading
• Barometric Altitude
• True Airspeed
• Outside Air Temperature
• Destination Airport
  • Estimated Time Enroute to Destination (ETE)
• Airborne Status

The Airborne Status field is the indication that the aircraft is on the ground or in the air at the time the position report was generated. The avionics generate a position report when the Airborne Status field changes state.

- Passenger Onboard

Passenger Onboard indicates passengers are on the aircraft at the time the position report was generated. A position report is generated when the Passenger Onboard field changes state.

Viewing the Connext Page:

1) Turn the large FMS Knob on the MFD to select the AUX page group.

2) Turn the small FMS Knob to select AUX-CONNEXT Page.

Setting up Position Reporting:

1) With the AUX-CONNEXT Page displayed, press the FMS Knob to display the cursor in the TRANSMISSION PERIOD field.
2) Turn the small FMS Knob to select 'AUTO' for automatic transmission of position reports or 'OFF' to disable transmission of position reports.
3) Press the ENT Key. The selection is entered and the cursor is placed in the TRANSMISSION RATE field.
4) Turn the small FMS Knob to highlight the first digit.
5) Again, turn the small FMS Knob to enter the desired number (between 2 and 60 minutes).
6) Turn the large FMS Knob to highlight the second digit.
7) Turn the small FMS Knob to enter the desired number.
8) Press the ENT Key. The selection is entered and the cursor is placed in the PASSENGERS ON BOARD field.
9) Turn the small FMS Knob left or right to select 'YES' or 'NO'.
10) Press the FMS Knob to remove the cursor.

To send a position report manually:

1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select AUX-CONNEXT Page.
3) If necessary, set the TRANSMISSION PERIOD to 'AUTO'.
4) Select the SEND RPT Softkey.

PILOT PROFILES

When the system is powered on, the last selected pilot profile is shown on the MFD power-up screen. The system can store up to 25 profiles; the currently active profile, the amount of memory used, and the amount of memory available are shown at the top of the AUX - System Setup Page in the box labeled 'Pilot Profile'.

Creating a Profile

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

3) Turn the large FMS Knob to highlight 'CREATE' in the Pilot Profile Box.
4) Press the ENT Key. A 'Create Profile' window is displayed.
5) Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key. Pilot profile names cannot begin with a blank as the first letter.
6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile. Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin factory defaults unless edited by the pilot), or current system settings.
7) Press the ENT Key.
8) With 'CREATE' highlighted, press the ENT Key to create the profile. Or:

Use the large FMS Knob to select 'CREATE and ACTIVATE' and press the ENT Key to activate the new profile.

9) To cancel the process, select 'CANCEL' with the large FMS Knob and press the ENT Key.
10) Press the FMS Knob to deactivate the cursor.

Selecting an Active Profile

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box.
4) Turn the small FMS Knob to display the pilot profile list and highlight the desired profile.
5) Press the ENT Key. The system loads and displays the system settings for the selected profile.
6) Press the FMS Knob to deactivate the cursor.

Renaming a Profile

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

3) Turn the large FMS Knob to highlight 'RENAME' in the Pilot Profile Box.
4) Press the ENT Key.
5) In the 'Rename Profile' window, turn the FMS Knob to select the profile to rename.
6) Press the ENT Key.
7) Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key.
8) With 'RENAME' highlighted, press the ENT Key.
9) To cancel the process, use the large FMS Knob to select 'CANCEL' and press the ENT Key.
10) Press the FMS Knob to deactivate the cursor.

Deleting a Profile

NOTE: The profile that is currently active cannot be deleted. If this is the desired profile to delete, select another profile, then delete the desired profile.

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight 'DELETE' in the Pilot Profile Box.
4) Press the ENT Key.
5) In the 'Delete Profile' window, turn the FMS Knob to select the profile to delete.
6) Press the ENT Key.
7) With 'DELETE' highlighted, press the ENT Key.
8) To cancel the process, use the large FMS Knob to select 'CANCEL' and press the ENT Key.
9) Press the FMS Knob to deactivate the cursor.

Importing a Profile from an SD Card

1) Insert an SD card containing the pilot profile(s) into the top card slot on the MFD.
2) Turn the FMS Knob to select the AUX - System Setup Page.
3) Select the IMPORT Softkey.
4) The system displays the Pilot Profile Importing Window with 'IMPORT' highlighted. To change the selected profile to be imported from the SD card (shown as 'SELECT FILE'), turn the large FMS Knob to highlight the profile file name, then turn the small FMS Knob to highlight a profile from the list, and press the ENT Key.
5) If desired, the profile name to be used after profile has been imported can be changed by turning the FMS Knob to highlight the 'PROFILE NAME' field, then use the large and small FMS Knobs to enter the name, and press the ENT Key. Imported profile names cannot begin with a blank space or be named 'DEFAULT', 'GARMIN DEFAULTS' or 'DEFAULT SETTINGS'.
6) With 'IMPORT' highlighted, press the ENT Key.
7) If the imported profile name is the same as an existing profile on the system, the system displays an 'Overwrite existing file? OK or CANCEL' prompt. Press the ENT Key to replace profile on the system with the profile imported from the SD card, or turn the FMS Knob to highlight 'CANCEL' and press the ENT Key to return to the Pilot Profile Importing Window.
8) If successful, the system displays 'Pilot profile import succeeded.' in the IMPORT RESULTS window below. With 'OK' highlighted, press the ENT or CLR Keys or press the FMS Knob to return to the AUX - System Setup Page. The imported profile becomes the active profile.

Exporting a Profile to an SD Card

1) Insert the SD card for storing the Pilot Profile into the top card slot on the MFD.
2) Turn the FMS Knob to select the AUX - System Setup Page.
3) If necessary, activate the desired pilot profile to export. Only the currently active Pilot Profile can be exported.
4) Select the EXPORT Softkey. The system displays the Pilot Profile Exporting Window.

5) To export the pilot profile using the current supplied name, press the ENT Key with 'EXPORT' highlighted. To change the profile file name turn the large FMS Knob to highlight the 'SELECT FILE' field, then enter the new name with the large and small FMS Knobs, then press the ENT Key. Then press the ENT Key with 'EXPORT' highlighted.
6) If the profile name to be exported is the same as an existing profile file name on the SD card, the system displays an 'Overwrite existing file? OK or CANCEL' prompt. Press the ENT Key to replace the profile on the SD card with the profile to be exported, or turn the FMS Knob to highlight 'CANCEL' and press the ENT Key to return to the Pilot Profile Exporting Window without exporting the profile.
7) If successful, the EXPORT RESULTS window displays 'Pilot profile export succeeded.' With 'OK' highlighted, press the ENT or CLR Keys, or press the FMS Knob to return to the AUX - System Setup Page.

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ABNORMAL OPERATION

NOTE: The Embraer Phenom 300 Airplane Flight Manual (AFM) always takes precedence over the information found in this section.

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 inverse video (black text on yellow background). Detection of an engine fire causes the red inverse video (white text on red background) annunciation “FIRE” to be displayed over the ITT gauge.

Engine Failure Indication Engine Fire Indication

CABIN PRESSURIZATION

If the cabin altitude (ALT) reaches a caution level, the readout displays black text on a yellow background. When a high cabin altitude warning occurs, the readout is displayed with white text on a red background, and the corresponding CAS message "CAB ALTITUDE HI" is issued.

A cabin pressure change rate (RATE) caution readout is indicated with black text on a yellow background. If low flow or a cabin leak is detected, the cabin pressure change rate readout displays white text on a red background and the trend arrow turns red.

Cabin Leak Indication

Excessive cabin differential pressure (DELTA-P) causes the pressure readout to display a yellow background and black text; warnings are indicated with red background with white readout text. The CAS message “CAB DELTA-P FAIL” accompanies this condition.

Low oxygen system pressure (OXY) is indicated by a yellow background and black text. The CAS message “OXY LO PRES” is also issued.

If the pilot selected landing field elevation (LFE) differs by more than five feet from the FMS LFE value, the LFE readout is shown as black text with a yellow background for 30 seconds.

A red “X” is displayed in place of any readout on the Cabin Display that is invalid or out of range.

FLAPS

The following denote abnormal flap conditions:

• Flaps not in position for takeoff – Flap pointer turns red and readout turns red inverse video (white text on red background) (A and B).
• Flaps have failed or become jammed – Flap pointer turns yellow and readout turns yellow inverse video (black text on yellow background) (C)
• Flaps unavailable – Flap pointer is removed and readout turns light blue inverse video (black text on light blue background) (D)
• Flaps position data invalid – Flap pointer and readout displayed with a red “X”

A - Flaps Retracted at Takeoff

B - Flaps at FULL (Landing) Position at Takeoff

C - Flaps Failed D - Flaps Unavailable

TRIM

Aileron or rudder mistrim are denoted with yellow arrows pointing in the direction 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 pointer turns red and readout turns red inverse video (white text on red background) (B).

A - Mistrim

B - Pitch Trim Outside Takeoff Configuration

REVERSIONARY MODE

If the system detects a failure in PFD1 or MFD, reversionary mode is entered automatically. Reversionary mode must be entered manually in the case of PFD2 failure. In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display.

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.

AUDIO PANEL FAIL-SAFE OPERATION

If there is a failure of both Audio Panels, a fail-safe circuit connects the pilot's headset and microphone directly to the COM1 transceiver and the copilot's headset directly to the COM2 transceiver. Audio is not available on the speakers. If there is a failure of one Audio Panel, that side only has access to their respective on-side fail-safe COM.

NOTE: Audio is not available on the speakers in case of an Audio Panel and its cross-side GIA unit simultaneous failure.

If there is a failure of one Audio Panel, the remaining Audio Panel does not have access to the other side's COM or NAV. For example, if the pilot side Audio Panel fails, the copilot side Audio Panel has access to all the radios except for COM1 and NAV1. In this case, the copilot can receive the audio from NAV2 and operate COM2 for transmission/reception.

In addition, if there is a failure of one Audio Panel, the following functions are no longer available on the failed side; NAV/ILS audio, speaker, cockpit/cockpit-passengers intercom, aural warning alerts on headset, entertainment inputs, and digital recording radio. Also, if a stereo headset is in use, and an Audio Panel fails, only the left channel will be heard in the headphones.

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.

Loss of Hazard Functions with Loss of GPS Position

UNUSUAL ATTITUDES

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

• Traffic Annunciations
• AFCS Annunciations
  • Flight Director Command Bars
• Inset Map
  • Temperatures
  • DME Information Window
• Wind Data
• Selected Heading Box

• Selected Course Box
  • Transponder Status Box

• 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, Glide-path, and Vertical Deviation Indicators

• Altimeter Barometric Setting
• Selected Altitude
  • VNV Target Altitude

Extreme Pitch Indication

DEAD RECKONING

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.

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/SBAS 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 may 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/SBAS 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.

Dead Reckoning Indications

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 navigation source information. This data includes the following:

• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
  • Wind data and pointers in the Wind Data Box on the PFD
• Current Track Indicator
• All Bearing Pointer Distances
  • Active Flight Plan distances, bearings, and ETE values

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

SUSPECTED AUTOPILOT MALFUNCTION

NOTE: Consult the aircraft documentation for the location of circuit breakers as well as specifics that may supplement or amplify this procedure.

If an autopilot failure or trim failure is suspected to have occurred, perform the following steps:

1) Firmly grasp the control wheel.
2) Press and hold the AP DISC Switch. The autopilot will disconnect and power is removed from the trim motor. Power is also removed from all primary servo motors and engaged solenoids. Note the visual and aural alerting indicating autopilot disconnect.
3) Retrim the aircraft as needed. Substantial trim adjustment may be needed.
4) Pull the appropriate circuit breaker(s) to electrically isolate the servo and solenoid components.
5) Release the AP DISC Switch.

OVERPOWERING AUTOPILOT SERVOS

In the context of this discussion, “overpowering” refers to any pressure or force applied to the pitch controls when the autopilot is engaged. A small amount of pressure or force on the pitch controls can cause the autopilot automatic trim to run to an out-of-trim condition. Therefore, any application of pressure or force to the controls should be avoided when the autopilot is engaged.

Overpowering the autopilot during flight will cause the autopilot's automatic trim to run, resulting in an out-of-trim condition or cause the trim to hit the stop if the action is prolonged. In this case, larger than anticipated control forces are required after the autopilot is disengaged.

The following steps should be added to the preflight check:

1) Check for proper autopilot operation and ensure the autopilot can be overpowered.
2) Note the forces required to overpower the autopilot servo clutches.

ANNUNCIATIONS & ALERTS

CAS MESSAGES

Warning Messages

See the Airplane Flight Manual (AFM) for recommended pilot actions. Accompanied by a triple chime tone which repeats until acknowledged.

Message Description
BAG SMK	detected in baggage compartment
CAB ALTITUDE HI	pin altitude pressure altitude high
DOOR EMER OPEN	emergency door open
DOOR PAX OPEN	ssenger door open
E1 FIRE	engine 1
E2 FIRE	engine 2
E1 OIL LO PRES	Low oil pressure in engine 1
E2 OIL LO PRES	Low oil pressure in engine 2
ELEC EMERGENCY	Generators offline
ELEC XFR FAIL	Generators offline and electrical emergency transfer has failed
LG LEVER DISAG	ding gear position and control lever disagreement
NO TO CONFIG	No takeoff configuration

Caution Messages

See the Airplane Flight Manual (AFM) for recommended pilot actions. Accompanied by a single chime tone which repeats until acknowledged.

Message Description
ADS 1 FAIL	ADS 1 offline or failed
ADS 2 FAIL	ADS 2 offline or failed
ADS 1 HTR FAIL	t heater 1 offline or heater element failed
ADS 2 HTR FAIL	t heater 2 offline or heater element failed
AHRS 1 FAIL	AHRS 1 failure
AHRS 2 FAIL	AHRS 2 failure
A-I E1 FAIL	Anti-ice system failure in engine 1
A-I E2 FAIL	Anti-ice system failure in engine 2
A-I LO CAPACITY	Not enough thermal energy available for WHSAIS (Wing and Horizontal Stabilizer Anti-ice System) operation
A-I WINGSTB FAIL	Component failure (AIV, pressure transducers, AMS Controller, other)
A-I WINGSTB INHB	WHSAIS switched ON outside the icing envelope. Or, aircraft is in single bleed configuration and above the 15,000 ft. icing envelope when WHSAIS is switched on.
A-I WINGSTB LEAK	eed hot air leakage at WHSAIS pneumatic ducting
AMS CTRL FAIL	umatic sources and icing protection are not available
ANTI-SKID FAIL	-skid function lost; main brake still available
AP FAIL	AP function
AP PITCH MISTRIM	rplane mistrimmed in pitch axis when AP is engaged
AP ROLL MISTRIM	rplane mistrimmed in roll axis when AP is engaged
AUDIO PNL 1 FAIL	Audio panel 1 is offline
AUDIO PNL 2 FAIL	Audio panel 2 is offline
AURAL WRN FAIL	Aural warning system failure due to non-communicating LRUs
AUTO PTRIM FAIL	Auto pitch trim failure; other pitch trim functions still available
BAG SMK FAIL	Baggage compartment smoke detector has failed
BATT DISCHARGE	Battery discharging under normal operation
BATT 1 OFF BUS	Battery 1 offline
BATT 2 OFF BUS	Battery 2 offline
BATT EXCEEDANCE	Battery 1 voltage or Battery 2 voltage greater than expected
BLEED 1 FAIL	Bleed 1 system not under control.
BLEED 2 FAIL	Bleed 2 system not under control.
BLEED 1 LEAK	Bleed 1 hot air leakage at some region of the ducting
BLEED 2 LEAK	Bleed 2 hot air leakage at some region of the ducting
BLEED 1 OVERPRES	Pressure in bleed ducting is higher than an acceptable value chosen to not compromise ECS and Anti-ice components integrity
BLEED 2 OVERPRES	Pressure in bleed ducting is higher than an acceptable value chosen to not compromise ECS and Anti-ice components integrity
BRK FAIL	Main brake system lost
CAB DELTA-P FAIL	Excessive cabin pressure differential
CLUTCH PIT FAIL	Pitch slip clutch maintenance test failed
CLUTCH ROL FAIL	Roll slip clutch maintenance test failed
CLUTCH VNTL FAIL	Ventral slip clutch maintenance test failed
CLUTCH YAW FAIL	w slip clutch maintenance test failed
CONFIG MDL FAIL	Master Configuration Module failed or non-communicative
DOORBAG AFT OPEN	Crew baggage door open
DOORBAG LH OPEN	Forward left-hand baggage door open
DOORBAG RH OPEN	Forward right-hand baggage door open
DUCT 1 OVERTEMP	Duct 1 temperature over specified safe value
DUCT 2 OVERTEMP	Duct 2 temperature over specified safe value
E1 CTRL FAULT	Engine 1 responds slowly or not at all to thrust commands
E2 CTRL FAULT	Engine 2 responds slowly or not at all to thrust commands
E1 FAIL Uncommanded shutdown detected for engine 1
E2 FAIL Uncommanded shutdown detected for engine 2
E1 FIRE DET FAIL	detection system failure in engine 1
E2 FIRE DET FAIL	detection system failure in engine 2
E1 FIREX FAIL	extinguisher failure in engine 1
E2 FIREX FAIL	extinguisher failure in engine 2
E1 FUEL IMP BYP	el filter impending bypass condition for engine 1
E2 FUEL IMP BYP	el filter impending bypass condition for engine 2
E1 TLA FAIL	Lever Angle failure for engine 1
E2 TLA FAIL	Lever Angle failure for engine 2
E1 TTO HTR FAIL	Heater failure in engine 1
E2 TTO HTR FAIL	Heater failure in engine 2
E1 TTO PROBE ICE	Engine 1 probe frozen
E2 TTO PROBE ICE	Engine 2 probe frozen
EBAY LEAK	Leak inside E-Bay
EBAY OVHT	cal bay over temperature
ECS 1 VALVE FAIL	Flow control valve monitor for ECS 1 detected improper valve operation
ECS 2 VALVE FAIL	Flow control valve monitor for ECS 2 detected improper valve operation
EMER BRK LO PRES	Few emergency brake functions available
EMER LT NOT ARM	Emergency lights switch not in ARMED position
ENG NO TO DATA	No takeoff data entered
FLAP FAIL	Loss of flaps deployment or retraction
FUEL 1 LO LEVEL	v fuel level in tank 1
FUEL 2 LO LEVEL	v fuel level in tank 2
FUEL 1 LO PRES	pressure low in engine 1 feed line
FUEL 2 LO PRES	pressure low in engine 2 feed line
FUEL 1 SOV FAIL	l feed SOV 1 closed or unavailable
FUEL 2 SOV FAIL	l feed SOV 2 closed or unavailable
FUEL IMBALANCE	el is imbalanced between the tanks
FUEL PUMP 1 FAIL	Fuel pump 1 failure
FUEL PUMP 2 FAIL	Fuel pump 2 failure
FUEL XFEED FAIL	agreement between valve command and its feedback
GEN 1 OFF BUS	erator 1 offline
GEN 2 OFF BUS	erator 2 offline
GEN OVLD	Motor(s) overload
GEN START FAULT	Generator start fault
GIA 1 FAIL Failure of GIA 1
GIA 2 FAIL Failure of GIA 2
GIA 1 OVHT	over temperature
GIA 2 OVHT	over temperature
GND SPLR FAIL	of ground spoilers
HYD HI TEMP	aulic temperature high
HYD LO PRES	aulic pressure low
HYD SOV 1 FAIL	EDP 1 Fire Shutoff valve was commanded to close, but failed to close
HYD SOV 2 FAIL	EDP 2 Fire Shutoff valve was commanded to close, but failed to close
ICE CONDITION*	Aircraft is flying in icing conditions
LG WOW SYS FAIL	Landing gear weight-on-wheels system failure
MFD CONFIG	configuration error
MFD FAULT	with the MFD
MFD OVHT	MFD over temperature
OXY LO PRES	en system pressure low
PARK BRK NOT REL	Parking brake not released
PAX OXY NO PRES	Cabin altitude high and passenger oxygen system pressure low
PFD 1 CONFIG	PFD 1 configuration error
PFD 2 CONFIG	PFD 2 configuration error
PFD 1 FAULT	Fault with PFD 1
PFD 2 FAULT	Fault with PFD 2
PFD 1 OVHT	PFD 1 over temperature
PFD 2 OVHT	PFD 2 over temperature
PRESN AUTO FAIL	Pressurization controller failure
PTRIM BKP FAIL	Loss of backup pitch trim actuator
PTRIM NML FAIL	Loss of normally-operating pitch trim actuator
PUSHER FAIL	Stall Warning & Protection System pusher has failed
PUSHER OFF	Stall Warning Pusher is off
RUD GUST LOCKED*	The rudder is gust locked
RUD OVERBOOST	SLRB (Spring Loaded Rudder Booster) uncommanded actuation
STBY HTR FAIL	Failure of standby heater
STEEP FAIL*	Steep approach mode has failed
SWPS FAIL	Stall Warning & Protection System inoperative
SWPS FAULT	Stall Warning & Protection System activation angles anticipated to conservative settings
SWPS UNTESTED	Stall Warning & Protection System has not been tested
TCAS FAIL*	Traffic & Collision Avoidance System failure. TCASII installations only.
WSHLD 1 HTR FAIL	Windshield 1 heater failure
WSHLD 2 HTR FAIL	Windshield 2 heater failure
XPDR FAIL	The active transponder has failed
XPDR IN STBY	active transponder is in standby mode
YD FAIL	yaw damper function
YD MISTRIM	ane mistrimmed in yaw axis when YD is engaged

* Optional

Advisory Messages

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

Message Description
ADS-B NOT AVAIL	The ADS-B out functionality is not available, because the active transponder is not receiving the GPS position or the active XPDR is failed
A-I E1 FAULT	the 1 Anti-ice system valve failed when commanded to close
A-I E2 FAULT	the 2 Anti-ice system valve failed when commanded to close
A-I E1 ON	Anti-ice system on in engine 1
A-I E2 ON	Anti-ice system on in engine 2
A-I WINGSTB ARM	WINGSTAB toggle switch has been armed prior to takeoff or WHSAIS switched ON above 30,000 ft.
A-I WINGSTB ON	WHSAIS is operating
ADS 1 SLIP FAIL	1 side-slip compensation is off
ADS 2 SLIP FAIL	2 side-slip compensation is off
ADS HTR SW ON	ADS Probe switch is on
AHRS 1 FAULT	Fault with AHRS 1
AHRS 2 FAULT	Fault with AHRS 2
AMS CTRL FAULT	One pneumatic and Anti-ice controller channel is inoperative
ATC DLK FAIL*	The CPDLC system is inoperative
AUDIO PNL 1 FAULT	Fault with audio panel 1
AUDIO PNL 2 FAULT	Fault with audio panel 2
AURAL WRN FAULT	Partial loss of aural warning function
AVNX FAN FAIL	onics fan failure
BAG SMK FAULT	to baggage compartment smoke detectors have failed
BLEED 1 OFF	pressure regulator 1 and shut-off valve closed
BLEED 2 OFF	pressure regulator 2 and shut-off valve closed
CLUTCH PIT PASS	ch slip clutch maintenance test passed
CLUTCH PIT PROG	ch slip clutch maintenance test in progress
CLUTCH ROL PASS	bll slip clutch maintenance test passed
CLUTCH ROL PROG	bll slip clutch maintenance test in progress
CLUTCH VNTL PASS	entral slip clutch maintenance test passed
CLUTCH VNTL PROG	Ventral slip clutch maintenance test in progress
CLUTCH YAW PASS	Yaw slip clutch maintenance test passed
CLUTCH YAW PROG	Yaw slip clutch maintenance test in progress
DC BUS 1 OFF	DC bus 1 offline
DC BUS 2 OFF	DC bus 2 offline
DOOR REFUEL OPEN	Refueling door is open
E1 CHIP DETECTED	Chip detected by engine 1 oil chip detector
E2 CHIP DETECTED	Chip detected by engine 2 oil chip detector
E1 FADEC FAULT	DEC fault in engine 1
E2 FADEC FAULT	DEC fault in engine 2
E1 OIL IMP BYP	Engine 1 oil filter impending bypass set
E2 OIL IMP BYP	Engine 2 oil filter impending bypass set
ECS 1 OFF	Flow control valve monitor detected improper valve operation
ECS 2 OFF	Flow control valve monitor detected improper valve operation
ELEC SYS FAULT	Electrical system fault
EMER BUS OFF	Emergency bus OFF
ENG EXCEEDANCE	Limit exceeded in engine(s) during flight
ENG FIREX DISCH	Engine fire extinguisher discharge
ENG NO DISPATCH	FADEC detected no dispatch fault condition in engine(s)
FLAP NOT AVAIL	bs not available
FUEL EQUAL	Fuel quantity asymmetry corrected; XFEED SOV is open
FUEL 1 FEED FAULT	DC pump on due to low fuel pressure
FUEL 2 FEED FAULT	DC pump on due to low fuel pressure
FUEL 1 PSW FAIL	Fuel pressure switch stuck in “high” position
FUEL 2 PSW FAIL	Fuel pressure switch stuck in “high” position
GEA 1 FAIL	Failure of GEA 1
GEA 2 FAIL	Failure of GEA 2
GEA 3 FAIL	Failure of GEA 3
GPU CONNECTED	Ground power unit connected to the aircraft
GSD 1 FAIL	GSD 1 non-communicative
GSD 2 FAIL GSD 2 non-communicative
HSDB FAULT	RU has stopped communicating over an HSDB
HSDB SW REV POS	DB switch in reversionary position
HYD SYS FAULT	radation of hydraulic system available power
ICE DET FAIL*	detector failure
MFD FAN FAIL	ure of MFD fan
OXY SW NOT AUTO	oxygen system switch in manual mode
PFD 1 FAN FAIL	ure of PFD 1 fan
PFD 2 FAN FAIL	ure of PFD 2 fan
PTRIM LO RATE	h trim is being actuated in low rate
PTRIM SW1 FAIL	ure of pilot pitch trim switch
PTRIM SW2 FAIL	ure of copilot pitch trim switch
RALT FAIL*	Radar altitude failure
RAM AIR FAIL	air valve failure
RUD BOOST FAIL	Loss of SLRB (Spring Loaded Rudder Booster) force assistance in case of thrust asymmetry
SHED BUS OFF	Shed bus off
SPDBRK SW DISAG	Speed brake switch position disagrees with the spoiler surfaces position
SPOILER FAULT	Ground Spoiler arm logic failedGround Spoiler command disagreeSpoiler position disagreeGround Spoiler Control Valve failedSpeed brake command failedSpeed brake command inhibit failed
STEEP NOT AVAIL*	Steep approach mode is not available
SWPS ICE SPEED	Stall Warning System activation angles anticipated due to icing conditions
VENTRAL RUD FAIL	Ventral rudder has failed
XBLEED FAIL	Cross bleed valve has failed closed or open
XBLEED SW OFF	Cross bleed switch is in the OFF position
XPDR FAULT*	The backup/standby transponder has failed

* Optional

COMPARATOR ANNUNCIATIONS

Note that operating the system in the vicinity of metal buildings or other metal structures can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut down, or while taxiing.

Comparator Window Text	Condition
ALT MISCOMP	Difference in altitude sensors is ≥ 200 ft.
IAS MISCOMP	If both airspeed sensors detect < 35 knots, this is inhibited.
	If either airspeed sensor detects ≥ 35 knots, and the difference in sensors is > 15 kts.
	If either airspeed sensor detects ≥ 80 knots, and the difference in sensors is > 10 kts.
HDG MISCOMP	Difference in heading sensors is > 10 degrees.
PIT MISCOMP	Difference in pitch sensors is > 5 degrees.
ROL MISCOMP	Difference in roll sensors is > 6 degrees.
VDI MISCOMP	Difference in temperature compensated altitudes is > 50 feet.
ALT NO COMP	No data from one or both altitude sensors.
IAS NO COMP	No data from one or both airspeed sensors.
HDG NO COMP	No data from one or both heading sensors.
PIT NO COMP	No data from one or both pitch sensors.
ROL NO COMP	No data from one or both roll sensors.
VDI NO COMP	No temperature compensated altitude data available.

REVERSIONARY SENSOR ANNUNCIATIONS

Reversionary Sensor Window Text	Condition
BOTH ON ADC1	Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON ADC2	Both PFDs are displaying data from the number two Air Data Computer.
BOTH ON ADCSTBY	Both PFDs are displaying data from the standby air data input.
BOTH ON AHRS1	Both PFDs are displaying data from the number one Attitude & Heading Reference System.
BOTH ON AHRS2	Both PFDs are displaying data from the number two Attitude & Heading Reference System.
BOTH ON ATTSTBY	Both PFDs are displaying data from the standby attitude and heading reference input.
BOTH ON GPS1	Both PFDs are displaying data from the number one GPS receiver.
BOTH ON GPS2	Both PFDs are displaying data from the number two GPS receiver.
USING ADC1	PFD2 is displaying data from the #1 Air Data Computer.
USING ADC2	PFD1 is displaying data from the #2 Air Data Computer.
USING ADCSTBY	PFD1 or PFD2 is displaying data from the standby air data input.
USING AHRS1	PFD2 is displaying data from the #1 AHRS.
USING AHRS2	PFD1 is displaying data from the #2 AHRS.
USING ATTSTBY	PFD1 or PFD2 is displaying data from the standby attitude and heading reference input.
USING GPS1	PFD2 is displaying data from the #1 GPS.
USING GPS2	PFD1 is displaying data from the #2 GPS.

TAWS-A ALERTS

Alert Type	PFD/MFDTAWS-A PageAnnunciation	MFD Map PagePop-Up Alert	Aural Message
Reduced Required Terrain Clearance Warning (RTC)	PULL UP	TERRAIN - PULL-UP	“Terrain, Terrain; Pull Up, Pull Up”
Imminent Terrain Impact Warning (ITI)	PULL UP	TERRAIN - PULL-UP	“Terrain, Terrain; Pull Up, Pull Up”
Reduced Required Obstacle Clearance Warning (ROC)	PULL UP	OBSTACLE - PULL-UP	“Obstacle, Obstacle; Pull Up, Pull Up”
Imminent Obstacle Impact Warning (IOI)	PULL UP	OBSTACLE - PULL-UP	“Obstacle, Obstacle; Pull Up, Pull Up”
Excessive Descent Rate Warning (EDR)	PULL UP	PULL-UP	“<whoop><whoop>Pull Up”
Excessive Closure Rate Warning (ECR)	PULL UP	PULL-UP	“<whoop><whoop>Pull Up”
Reduced Required Terrain Clearance Caution (RTC)	TERRAIN	CAUTION - TERRAIN	“Caution, Terrain; Caution, Terrain”
Imminent Terrain Impact Caution (ITI)	TERRAIN	CAUTION - TERRAIN	"Caution, Terrain; Caution, Terrain"
Reduced Required Obstacle Clearance Caution (ROC)	TERRAIN	CAUTION - OBSTACLE	"Caution, Obstacle; Caution, Obstacle"
Imminent Obstacle Impact Caution (IOI)	TERRAIN	CAUTION - OBSTACLE	"Caution, Obstacle; Caution, Obstacle"
Premature Descent Alert Caution (PDA)	TERRAIN	TOO LOW - TERRAIN	"Too Low, Terrain"
Excessive Descent Rate Caution (EDR)	TERRAIN	SINK RATE	"Sink Rate"
Excessive Closure Rate Caution (ECR)	TERRAIN	TERRAIN	"Terrain, Terrain"
Negative Climb Rate Caution (NCR)	TERRAIN	DON'T SINK	"Don't Sink"
Flight Into Terrain High Speed Caution (FIT)	TERRAIN	TOO LOW - TERRAIN	"Too Low, Terrain"
Flight Into Terrain Gear Caution (FIT)	TERRAIN	TOO LOW - GEAR	"Too Low, Gear"
Flight Into Terrain Flaps Caution (FIT)	TERRAIN	TOO LOW - FLAPS	"Too Low, Flaps"
Flight Into Terrain Takeoff Caution (FIT)	TERRAIN	TOO LOW - TERRAIN	"Too Low, Terrain"
Glide Slope/Glide Path Deviation Caution (GSD) (depends on approach type)	GLIDESLOPE or GLIDEPATH	GLIDESLOPE or GLIDEPATH	"Glide Slope" or "Glide Path"
Altitude Voice Callout (VCO)	None None	Five-Hundred"	"Four-Hundred" "Three-Hundred" "Two-Hundred" "One-Hundred"

TAWS-A System Status Annunciations

Alert Type	PFD/MFD TAWS-A Page Annunciation	Additional TAWS-A Page Annunciation	Aural Message
TAWS System Fail, Terrain or Obstacle database unavailable or invalid, invalid software configuration, system audio fault	TAWS FAIL	TAWS FAIL	“TAWS System Failure”
GPWS System Fail None	GPWS SYSTEM		Failure”
System Test in progress	TAWS TEST	TAWS TEST	None
System Test pass None None	“TAWS System		Test OK”
MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases	None	TERRAIN DATABASE FAILURE	None
GPWS System Fail, Radar Altimeter invalid, Altitude or Vertical Speed unavailable	GPWS FAIL	None “GPWS System	Failure”
No GPS position	TAWS N/A	NO GPS POSITION	“TAWS Not Available”
Excessively degraded GPS signal, Out of database coverage area	TAWS N/A	None	“TAWS Not Available”
Out of database coverage area	TAWS N/A	None	“TAWS Not Available”“TAWS Available” when aircraft enters database coverage area.

TAWS-A Alert Availability

	TAWS-A Alert Type Available
TAWS-A Status Annunciation Displayed	RTC	ITI	ROC	OI PD	AEDR	ECR NCR FIT	GSD VCO
TAWS TEST	No	No	No	No	No	No	No	No	No	No	No
TAWS N/A	No	No	No	No	No	Yes	Yes	Yes	Yes	*No	**Yes
TAWS FAIL	No	No	No	No	No	Yes	Yes	Yes	Yes	Yes	**Yes
TAWS INH	No	No	No	No	No	Yes	Yes	Yes	Yes	Yes	Yes
GPWS FAIL	Yes	Yes	Yes	Yes	Yes	No	No	No	No	No	**Yes
GS INH	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	No	Yes
GP INH	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	No	Yes
FLAP OVR	Yes	Yes	Yes	Yes	Yes	Yes	Yes	Yes	#Yes	Yes	Yes

* GSD alert will be available if a valid ILS is being used for navigation, even if no valid GPS signal is being received.

** VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available.

# Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is displayed.

TAWS-B ALERTS

Alert Type	PFD/MFDTAWS-B PageAnnunciation	MFDPop-Up Alert	Aural Message
Excessive Descent Rate Warning (EDR)	PULL UP	PULL-UP	“Pull Up”
Reduced Required Terrain Clearance Warning (RTC)	PULL UP	TERRAIN - PULL-UP	“Terrain, Terrain; Pull Up, Pull Up”
Imminent Terrain Impact Warning (ITI)	PULL UP	TERRAIN - PULL-UP	“Terrain, Terrain; Pull Up, Pull Up”
Reduced Required Obstacle Clearance Warning (ROC)	PULL UP	OBSTACLE - PULL-UP	“Obstacle, Obstacle; Pull Up, Pull Up”
Imminent ObstacleImpact Warning (IOI)	PULL UP	OBSTACLE - PULL-UP	“”Obstacle, Obstacle; Pull Up, Pull Up”
Reduced Required Terrain Clearance Caution (RTC)	TERRAIN	CAUTION - TERRAIN	“Caution, Terrain; Caution, Terrain”
Imminent Terrain Impact Caution (ITI)	TERRAIN	CAUTION - TERRAIN	“Caution, Terrain; Caution, Terrain”
Reduced Required Obstacle Clearance Caution (ROC)	TERRAIN	CAUTION - OBSTACLE	“Caution, Obstacle; Caution, Obstacle”
Imminent Obstacle Impact Caution (IOI)	TERRAIN	CAUTION - OBSTACLE	“Caution, Obstacle; Caution, Obstacle”
Premature Descent Alert Caution (PDA)	TERRAIN	TOO LOW - TERRAIN	“Too Low, Terrain”
Altitude Callout “500”	None None “Five-Hundred”
Excessive Descent Rate Caution (EDR)	TERRAIN	SINK RATE	“Sink Rate”
Negative Climb Rate Caution (NCR)	TERRAIN	DON'T SINK	“Don't Sink”

TAWS-B System Status Annunciations

Alert Type	PFD/MFDTAWS-A PageAnnunciation	AdditionalTAWS-A PageAnnunciation	Aural Message
System Test in Progress	TAWSTEST
System Test Pass None None	“TAWS	System Test OK”
TAWS-B System TestFail, Terrain or Obstacledatabase unavailable orinvalid, invalid softwareconfiguration, systemaudio fault	TAWS FAIL	TAWS FAIL	“TAWS System Failure”
MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases	None	TERRAIN DATABASE FAILURE	None
No GPS positionNO GPS POS	TAWS" TAXAS No
Excessively degraded GPS signal, Out of database coverage area	TAWS N/A	None "TAWS Not Available"
Sufficient GPS signal received after loss	None None	"TAWS Available"

TCAS II ALERTS AND ANNUNCIATIONS

Mode	PFD Mode Annunciation	MFD Traffic Map Page Mode Annunciation	Traffic Display Status Icon (Other Maps)
TCAS II Self-test Initiated (TEST)	None	TEST('TEST MODE' also shown in white on top center of page)
Traffic Advisory and Resolution Advisory (TA/RA)	None TA/RA
Traffic Advisory Only (TA ONLY)	TA ONLY	TA ONLYSTANDBY(also shown in white in center of page when aircraft on ground, yellow in air)
TCAS II Standby (TFC STBY)	TCAS STBY*
TCAS II Failed	TCAS FAIL	FAIL

* Annunciation appears white when aircraft is on the ground and yellow while in the air.

TCAS II Modes

Traffic Map Page Annunciation	Description
NO DATA	not being received from the TCAS II unit
DATA FAILED	Data is being received from the TCAS II unit, but the unit is self-reporting a failure
FAILED	data format received from the TCAS II unit

TCAS II Failure Annunciations

Traffic Status BannerAnnunciation	Description
RA OFF SCALE	A Resolution Advisory is outside the selected display range*.Annunciation is removed when traffic comes within the selected display range
TA OFF SCALE	A Traffic Advisory is outside the selected display range*.Annunciation is removed when traffic comes within the selected display range.
RA X.X ± XX ↑	System cannot determine bearing of Resolution Advisory**.Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/descending).
TA X.X ± XX ↑	System cannot determine bearing of Traffic Advisory**.Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/descending).
TRFC FAIL	TCAS II unit has failed (unit is self-reporting a failure or sending incorrectly formatted data)
NO TCAS DATA	is not being received from the TCAS II unit

*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page

TCAS II Traffic Status Annunciations

GDL 69A DATA LINK RECEIVER MESSAGES

Message Message	Location Description
CHECK ANTENNA	SiriusXM Info Screen (Touchscreen Controller)	Data Link Receiver antenna error; service required
UPDATING	Music Screen (Touchscreen Controller)	Data Link Receiver updating encryption code
NO SIGNAL	SiriusXM Info Screen, Music Screen (Touchscreen Controller)SiriusXM Weather Pane	Loss of signal; signal strength too low for receiver
Loading Music Channels...	Music Screen (Touchscreen Controller)	Acquiring channel audio or information
OFF AIR	Music Screen (Touchscreen Controller)	Channel not in service
---	Music Screen (Touchscreen Controller)	Missing channel information
No Channels Available Please Check Connection	Music Screen (Touchscreen Controller)	System has not acquired any channels. Verify antenna is outside with a clear view of the sky.
WEATHER DATA LINK FAILED	Weather Data Link (XM) Pane	No communication from Data Link Receiver within last 5 minutes
DETECTING ACTIVATION	Weather Data Link (XM) Pane	SiriusXM subscription is activating
WAITING FOR DATA...	Weather Data Link (XM) Pane	SiriusXM subscription confirmed. Downloading weather data.
GDL 69A Data Link Receiver Messages

CPDLC ATC ALERT

The following PFD alert informs the flight crew of a received CPDLC message from ATC. When the message is received, the alert flashes five times, then stays illuminated until the required action is accomplished.

CPDLC Alert on the PFD

OTHER PRODIGY® AURAL ALERTS

Message Priority Description
"Autopilot"	Warning – Autopilot is disengagedSingle alert for manual AP disengagementContinuous alert for automatic AP disengagement; cancelled withAP DISCSwitch
"Cabin" High cabin altitude
"Fire, Fire" Engine fire
"High Speed" Maximum Wamping speed exceeded
"Landing Gear"
"No Takeoff Brake"
"No Takeoff Flaps"
"No Takeoff Spoilers"
"No Takeoff Trim"
"Stall, Stall"
"Traffic"	Caution	The Traffic Information Service (TIS) has issued a Traffic Advisory alert.
Message Priority Description
"Altitude"	Data Link mAdvisory	Aircraft has deviated ±200 feet of the selected altitude
"Message ATC" New		message received from ATC
"Minimums, minimums"		The aircraft has descended below the preset barometric minimum descent altitude.
"Rudder Overboost"		SLRB (Spring Loaded Rudder Booster) uncommanded actuation
"TIS not available"		The aircraft is outside the Traffic Information Service (TIS) coverage area.
"Trim Trim Trim" Trim switch malfunction
"Vertical track"		The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled.
"Aural Warning OK"	director has status telephone communication	Aural warning system test passes
"Aural Warning One Channel"		Aural warning system test detects failure in one channel
"Flight Director" Flight		reverted to pitch or roll default mode
"Incoming Call" Satellite		is receiving a call
"SelCal" Incoming		ation through the HF radio
"Takeoff OK"		Takeoff configuration test passed
"Timer Expired" Countdown timer		on the PFD has reached zero

FLIGHT PLAN IMPORT/EXPORT MESSAGES

In some circumstances, some messages may appear in conjunction with others.

Flight Plan Import/Export Results	Description
'Flight plan successfully imported.'	A flight plan file stored on the SD card was successfully imported as a stored flight plan.
'File contained user waypoints only.User waypoints imported success-fully. No stored flight plan data was modified.'	The file stored on the SD card did not contain a flight plan,only user waypoints. These waypoints have been saved to the system user waypoints. No flight plans stored in the system have been modified.
'No flight plan files found to import.'	The SD card contains no flight plan data.
'Flight plan import failed.'	Flight plan data was not successfully imported from the SD card.
'Flight plan partially imported.'	Some flight plan waypoints were successfully imported from the SD card, however others had errors and were not imported.A partial stored flight plan now exists in the system.
‘File contained user waypoints only.’ The	file stored on the SD card did not contain a flight plan, only user waypoints. One or more of these waypoints did not import successfully.
‘Too many points. Flight plan truncated.’	The flight plan on the SD card contains more waypoints than the system can support. The flight plan was imported with as many waypoints as possible.
‘Some waypoints not loaded. Way-points locked.’	The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database. The flight plan has been imported, but must be edited within the system before it can be activated for use.
‘User waypoint database full. Not all loaded.’	The flight plan file on the SD card contains user waypoints. The quantity of stored user waypoints has exceeded system capacity, therefore not all the user waypoints on the SD card have been imported. Any flight plan user waypoints that were not imported are locked in the flight plan. The flight plan must be edited within the system before it can be activated for use.
‘One or more user waypoints renamed.’	One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system.
‘Flight plan successfully exported.’ The st	stored flight plan was successfully exported to the SD card.
‘Flight plan export failed.’ The stored flight	plan was not successfully exported to the SD card. The SD card may not have sufficient available memory or the card may have been removed prematurely.

PILOT PROFILE IMPORT/EXPORT MESSAGES

Pilot Profile Import/Export Results Description
‘No pilot profile plan files found to import.’ Displayed if the SD card does not have one or more valid pilot profile filenames.
‘Overwrite existing profile?’	Displayed if the profile name matches the name of existing profile.
‘Profile name invalid. Enter a different profile name.’	Displayed if the profile name is invalid.
‘All available pilot profiles in use. Delete a profile before importing another.’	Displayed if the maximum number for pilot profiles has been reached.
‘Pilot profile import failed.’ Displayed if the importing operation fails for any other reason.
‘Pilot profile import succeeded.’ Displayed if the importing operation succeeds.
‘Overwrite existing file?’ Displayed if the filename matches the name of an existing file on the SD card.
‘Pilot profile export failed.’ Displayed if the export operation fails.
‘Pilot profile export succeeded.’ Displayed if the export operation succeeds.

PRODIGY® SYSTEM MESSAGE ADVISORIES

Message Comments
ABORT APR – Loss of GPS navigation. Abort approach.	Abort approach due to loss of GPS navigation.
AHRS MAG DB – AHRS magnetic model database version mismatch.	The #1 AHRS and #2 AHRS magnetic model database versions do not match.
AHRS1 GPS – AHRS1 not receiving any GPS information.	The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced.
AHRS1 GPS – AHRS1 not receiving backup GPS information.	The #1 AHRS is not receiving backup GPS information. The system should be serviced.
AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode.	The #1 AHRS is operating exclusively in no-GPS mode. The system should be serviced.
AHRS1 GPS – AHRS1 using backup GPS source.	The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible.
AHRS1 SRVC – AHRS1 Magnetic-field model needs update.	The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical.
AHRS1 TAS – AHRS1 not receiving airspeed.	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 GPS – AHRS2 not receiving any GPS information.	The #2 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced.
AHRS2 GPS – AHRS2 not receiving backup GPS information.	The #2 AHRS is not receiving backup GPS information. The system should be serviced.
AHRS2 GPS – AHRS2 operating exclusively in no-GPS mode.	The #2 AHRS is operating exclusively in no-GPS mode. The system should be serviced.
AHRS2 GPS – AHRS2 using backup GPS source.	The #2 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible.
AHRS2 SRVC – AHRS2 Magnetic-field model needs update.	The #2 AHRS earth magnetic field model is out of date. Update magnetic field model when practical.
AHRS2 TAS – AHRS2 not receiving airspeed.	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.
APR ADVISORY - SBAS VNAV not available. Using Baro VNAV.	SBAS not available. The system is calculating the VNAV profile using BARO VNAV.
APR DWNGRADE – Approach downgraded. Use LNAV minima.	Vertical guidance generated by SBAS is unavailable. Use LNAV only minimums.
APR DWNGRADE – Baro VNAV. Use LNAV/VNAV minima.	Vertical guidance generated by SBAS is unavailable. Use Baro LNAV/VNAV minimums
APR INACTV – Approach is not active.	The system notifies the pilot that the loaded approach is not active. Activate approach when required.
ARSPC AHEAD – Airspace ahead less than 10 minutes.	Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within 10 minutes.
ARSPC NEAR – Airspace near and ahead.	Special use airspace is near and ahead of the aircraft position.
ARSPC NEAR – Airspace near – less than 2 nm.	Special use airspace is within 2 nm of the aircraft position.

Message Comments

CHECK CRS – Database course for LOC1 / [LOC ID] is [CRS] ° .	Selected course for LOC1 differs from published localizer course by more than 10 degrees.
CHECK CRS – Database course for LOC2 / [LOC ID] is [CRS] ° .	Selected course for LOC2 differs from published localizer course by more than 10 degrees.
CNFG MODULE – PFD1 configuration module is inoperative.	The PFD1 configuration module backup memory has failed. The system should be serviced.
COM1 PTT – COM1 push-to-talk key is stuck.	The COM1 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.
COM1 RMT XFR – COM1 remote transfer key is stuck.	The COM1 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.
COM1 SERVICE – COM1 needs service. Return unit for repair.	The system has detected a failure in COM1.COM1 may still be usable. The system should be serviced when possible
COM1 TEMP – COM1 over temp.Reducing transmitter power.	The system has detected an over temperature condition in COM1. The transmitter is operating at reduced power. If the problem persists, the system should be serviced.
COM2 PTT – COM2 push-to-talk key is stuck.	The 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.
COM2 RMT XFR – COM2 remote transfer key is stuck.	The 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.
Message Comments
COM2 SERVICE – COM2 needs service. Return unit for repair.	The system has detected a failure in COM2.COM2 may still be usable. The system should be serviced when possible.
COM2 TEMP – COM2 over temp.Reducing transmitter power.	The system has detected an over temperature condition in COM2. The transmitter is operating at reduced power. If the problem persists, the system should be serviced.
CPDLC – CPDLC facility logon failed.	Logon failed. Check pertinent entries for accuracy.
CPDLC – CPDLC session terminated.	The currently active CPDLC session has been terminated.
DATA LOST – Pilot stored data was lost. Recheck settings.	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.
DB CHANGE – Database changed.Verify user modified procedures.	This occurs when a stored flight plan contains procedures that have been manually edited.This alert is issued only after an navigation database update. Verify that the user-modified procedures in stored flight plans are correct and up to date.
DB CHANGE – Database changed.Verify stored airways.	This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database. This alert is issued only after an navigation database update. Verify use of airways in stored flight plans and reload airways as needed.
DB MISMATCH – Navigation database mismatch. Xtalk is off.	The PFDs and MFD have different navigation database versions or types (Americas, European, etc.) installed. Crossfill is off. Install correct navigation database version or type in all displays.
DB MISMATCH – Obstacle database mismatch.	The PFDs and MFD have different obstacle database installed. Install correct obstacle database in all displays.
DB MISMATCH – Standby Navigation database mismatch.	The PFDs and MFD have different standby navigation database versions or types (Americas, European, etc.) installed. Install correct standby navigation database version or type in all displays.
DB MISMATCH – Terrain database mismatch.	The PFDs and MFD have different terrain database versions or types installed. Install correct terrain database version or type in all displays.

FAILED PATH— A data path has failed.	A data path connected to the GDU, GSD 41, or the GIA 63/W has failed.
FPL TRUNC — Flight plan has been truncated.	This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan. The obsolete procedure is removed from the flight plan. Update flight plan with current arrival or approach.
FPL WPT LOCK — Flight plan waypoint is locked.	Upon power-up, the system detects that a stored flight plan waypoint is locked. This occurs when an navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.Remove the waypoint from the flight plan if it no longer exists in any database,Orupdate the waypoint name/identifier to reflect the new information.
Message Comments
FPL WPT MOVE – Flight plan waypoint moved.	The system has detected that a waypoint coordinate has changed due to a new navigation database update. Verify that stored flight plans contain correct waypoint locations.

G/S1 FAIL – G/S1 is inoperative. A failure has been detected in glideslope receiver 1. The system should be serviced.
G/S1 SERVICE – G/S1 needs service. Return unit for repair.	A failure has been detected in glideslope receiver 1. The receiver may still be available. The system should be serviced when possible.
G/S2 FAIL – G/S2 is inoperative. A failure has been detected in glideslope receiver 2. The system should be serviced.
G/S2 SERVICE – G/S2 needs service. Return unit for repair.	A failure has been detected in glideslope receiver 2. The receiver may still be available. The system should be serviced when possible.
GCU CNFG – GCU Config error. Config service req’d.	GCU 477 configuration settings do not match those of backup configuration memory. The system should be serviced.
GCU FAIL – GCU is inoperative. A failure has been detected in the GCU 477. The GCU 477 is unavailable.
GCU KEYSTK – GCU [key name] Key is stuck.	A key is stuck on the GCU 477 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists.
GEA1 CONFIG – GEA1 config error. Config service req’d.	The GEA1 configuration settings do not match those of backup configuration memory. The system should be serviced.
GEA2 CONFIG – GEA2 config error. Config service req’d.	The GEA2 configuration settings do not match those of backup configuration memory. The system should be serviced.
GEA3 CONFIG – GEA3 config error. Config service req’d.	The GEA3 configuration settings do not match those of backup configuration memory. The system should be serviced.
Message Comments
GEO LIMITS – AHRS1 too far North/South, no magnetic compass.	The aircraft is outside geographical limits for approved AHRS operation. Heading is flagged as invalid.
GEO LIMITS – AHRS2 too far North/South, no magnetic compass.
GDL59 CONFIG – GDL 59 config error. Config service req'd.	GDL 59 configuration settings do not match those of backup configuration memory. The system should be serviced.
GDL59 FAIL – GDL 59 has failed. A failure has been detected in the GDL 59. The receiver is unavailable. The system should be serviced.
GDL59 RTR FAIL – The GDL 59 router has failed.	A failure has been detected in the GDL 59 router. The system should be serviced.
GDL59 SERVICE – GDL 59 needs service. Return unit for repair.	A failure has been detected in the GDL 59. The system should be serviced.
GDL69 CONFIG – GDL 69 config error. Config service req'd.	GDL 69 configuration settings do not match those of backup configuration memory. The system should be serviced.
GDL69 FAIL – GDL 69 has failed. A failure has been detected in the GDL 69. The receiver is unavailable. The system should be serviced
GDR AUX MANIFEST – GDR AUX software mismatch, communication halted.	The GDR secondary processor has incorrect software installed. The system should be serviced.
GDR CONFIG – GDR config error. Config service req'd.	GDR configuration settings do not match those of backup configuration memory. The system should be serviced.
GDR FAIL – GDR is inoperative. A failure has been detected in the GDR. The system should be serviced.
GDR MANIFEST – GDR software mismatch, communication halted.	The GDR has incorrect software installed. The system should be serviced.
GDR PTT – GDR push-to-talk key is stuck.	The GDR 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.
GDR RMT XFR – GDR remote transfer key is stuck.	The GDR 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.
GDR SERVICE – GDR needs service. Return unit for repair.	The GDR should be serviced when possible.
GDR TEMP – GDR over temp. Reducing transmitter power.	The system has detected an over temperature condition in the GDR. The transmitter operates at reduced power. If the problem persists, the system should be serviced.
GDR TX FAIL – GDR transmitter is inoperative.	The system should be serviced.
GIA1 CONFIG – GIA1 audio config error. Config service req’d.	The GIA1 have an error in the audio configuration. The system should be serviced.
GIA1 CONFIG – GIA1 config error. Config service req’d.	The GIA1 configuration settings do not match backup configuration memory. The system should be serviced.
GIA1 COOLING – GIA1 over temperature.	The GIA1 temperature is too high. If problem persists, the system should be serviced.
GIA1 COOLING – GIA1 temperature too low.	The GIA1 temperature is too low to operate correctly. Allow units to warm up to operating temperature.
GIA1 SERVICE – GIA1 needs service. Return the unit for repair.	The GIA1 self-test has detected a problem in the unit. The system should be serviced.
GIA2 CONFIG – GIA2 audio config error. Config service req’d.	The GIA2 have an error in the audio configuration. The system should be serviced.
GIA2 CONFIG – GIA2 config error. Config service req’d.	The GIA2 configuration settings do not match backup configuration memory. The system should be serviced.
GIA2 COOLING – GIA2 over temperature.	The GIA2 temperature is too high. If problem persists, the system should be serviced.
GIA2 COOLING – GIA2 temperature too low.	The GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature.
GIA2 SERVICE – GIA2 needs service. Return the unit for repair.	The GIA2 self-test has detected a problem in the unit. The system should be serviced.
GMA1 CONFIG – GMA1 config error. Config service req'd.	The audio panel configuration settings do not match backup configuration memory. The system should be serviced.
GMA1 FAIL – GMA1 is inoperative.	The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced.
GMA1 SERVICE – GMA1 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.
GMA2 CONFIG – GMA2 config error. Config service req'd.	The audio panel configuration settings do not match backup configuration memory. The system should be serviced.
GMA2 FAIL – GMA2 is inoperative.	The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced.
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.
GMA XTALK – GMA crosstalk error has occurred.	An error has occurred in transferring data between the two GMAs. The system should be serviced.
GMC CONFIG – GMC Config error. Config service req'd.	Error in the configuration of the GMC 715.
GMC FAIL – GMC is inoperative. A failure has been detected in the GMC 715. The GMC 715 is unavailable.
GMC KEYSTK – GMC [key name] Key is stuck.	A key is stuck on the GMC 715 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists.
GPS NAV LOST – Loss of GPS navigation. GPS fail.	Loss of GPS navigation due to GPS failure.
GPS NAV LOST – Loss of GPS navigation. Insufficient satellites.	Loss of GPS navigation due to insufficient satellites.
GPS NAV LOST – Loss of GPS navigation. Position error.	Loss of GPS navigation due to position error.
GPS1 SERVICE – GPS1 needs service. Return unit for repair.	A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still be available. The system should be serviced.
GPS2 SERVICE – GPS2 needs service. Return unit for repair.
GSD1 CONFIG – GSD1 config error. Config service req'd.	GSD1 and the CDU have different copies of the GSD1 configuration.
GSD1 COOLING – GSD1 over temperature.	GSD1 is reporting an over-temperature condition.
GSD1 COOLING – GSD1 temperature too low.	GSD1 is reporting a low temperature condition.
GSD1 SERVICE – GSD1 needs service. Return unit for repair.	GSD1 is reporting an internal error condition. The GSD may still be usable.
GSD2 CONFIG – GSD2 config error. Config service req'd.	GSD2 and the CDU have different copies of the GSD2 configuration.
GSD2 COOLING – GSD2 over temperature.	GSD2 is reporting an over-temperature condition.
GSD2 COOLING – GSD2 temperature too low.	GSD2 is reporting a low temperature condition.
GSD2 SERVICE – GSD2 needs service. Return unit for repair.	GSD2 is reporting an internal error condition. The GSD may still be usable.
GSR1 FAIL – GSR1 has failed. A failure has been detected in the #1 GSR 56. The system should be serviced.
GSR2 FAIL – GSR2 has failed. A failure has been detected in the #2 GSR 56.The system should be serviced.
GWX CONFIG – GWX config error.Config service req'd.	GWX 68/GWX 70 configuration settings do not match those of the GDU configuration. The system should be serviced.
GWX FAIL – GWX is inoperative. The GDU is not receiving status packet from the GWX 68/GWX 70 or the GWX 68/GWX 70 is reporting a fault. The GWX 68/GWX 70 radar system should be serviced.
GWX SERVICE – GWX needs service. Return unit for repair.	A failure has been detected in the GWX 68/GWX 70. The GWX 68/GWX 70 may still be usable.

HDG FAULT-AHRS1 magnetometer fault has occurred.	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.
HDG FAULT-AHRS2 magnetometer fault has occurred.	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.
HW MISMATCH-GIA hardware mismatch. GIA1 communication halted.	A GIA mismatch has been detected, where only one is SBAS capable.
HW MISMATCH-GIA hardware mismatch. GIA2 communication halted.
INSIDE ARSPC-Inside airspace. The aircraft is inside the airspace.
INVALID ADM-Invalid ADM: ATN communication halted.	Data link avionics were not configured correctly and therefore will not be able to communicate with the ground network.
Message Comments
LOCKED FPL – Cannot navigate locked flight plan.	This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint.
LOI – GPS integrity lost. Crosscheck with other NAVS.	GPS integrity is insufficient for the current phase of flight.

MANIFEST – GCU software mismatch, communication halted.	The GCU 477 has incorrect software installed. The system should be serviced.
MANIFEST – GDL software mismatch, communication halted.	The GDL 59 has incorrect software installed. The system should be serviced.
MANIFEST – GDL software mismatch, communication halted.	The GDL 69 has incorrect software installed. The system should be serviced.
MANIFEST – GEA1 software mismatch, communication halted.	The #1 GEA 71 has incorrect software installed. The system should be serviced.
MANIFEST – GEA2 software mismatch, communication halted.	The #2 GEA 71 has incorrect software installed. The system should be serviced.
MANIFEST – GEA3 software mismatch, communication halted.	The #3 GEA 71 has incorrect software installed. The system should be serviced.
MANIFEST – GFC software mismatch, communication halted.	Incorrect servo software is installed, or gain settings are incorrect.
MANIFEST – GIA1 software mismatch, communication halted.	The GIA1 and/or GIA 2 has incorrect software installed. The system should be serviced.
MANIFEST – GIA2 software mismatch, communication halted.
MANIFEST – GMA1 software mismatch, communication halted.	The audio panel has incorrect software installed. The system should be serviced.
MANIFEST – GMA2 software mismatch, communication halted.
MANIFEST – GMC software mismatch. Communication halted.	The GMC 715 has incorrect software installed. The system should be serviced.
Message Comments
MANIFEST – GMU1 software mismatch, communication halted.	The GMU 44 has incorrect software installed. The system should be serviced.
MANIFEST – GMU2 software mismatch, communication halted.
MANIFEST – GRS1 software mismatch, communication halted.	The #1 AHRS has incorrect software installed. The system should be serviced.
MANIFEST – GRS2 software mismatch, communication halted.	The #2 AHRS has incorrect software installed. The system should be serviced.
MANIFEST – GSD1 software mismatch. Communication halted.	GSD1 has incorrect software installed. The system should be serviced.
MANIFEST – GSD2 software mismatch. Communication halted.	GSD2 has incorrect software installed. The system should be serviced.
MANIFEST – GTX1 software mismatch, communication halted.	The transponder has incorrect software installed. The system should be serviced.
MANIFEST – GTX2 software mismatch, communication halted.	The transponder has incorrect software installed. The system should be serviced.
MANIFEST – GWX software mismatch, communication halted.	The GWX 68/GWX 70 has incorrect software installed. The system should be serviced.
MANIFEST – MFD1 software mismatch, communication halted.	The MFD has incorrect software installed. The system should be serviced.
MANIFEST – PFD1 software mismatch, communication halted.	The PFD has incorrect software installed. The system should be serviced.
MANIFEST – PFD2 software mismatch, communication halted.
MFD1 COOLING – MFD1 has poor cooling. Reducing power usage.	The MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced.
MFD1 CONFIG – MFD1 config error. Config service req'd.	The MFD configuration settings do not match backup configuration memory. The system should be serviced.
MFD1 DB ERR – MFD1 Airport Directory database error exists.	The MFD detected a failure in the Airport Directory database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 basemap database error exists.	The MFD detected a failure in the basemap database.
MFD1 DB ERR – MFD1 basemap database is incompatible.	The MFD detected a that the basemap database is incompatible.
MFD1 DB ERR – MFD1 Chartview database error exists.	The MFD detected a failure in the ChartView database (optional feature). Ensure the data card is properly inserted. Replace data card. If problem persists, system should be serviced.
MFD1 DB ERR – MFD1 FliteCharts database error exists.	The MFD detected a failure in the FliteCharts database (optional feature). Ensure the data card is properly inserted. Replace data card. If problem persists, system should be serviced.
MFD1 DB ERR – MFD1 navigation database error exists.	The MFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 obstacle database error exists.	The MFD 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.
MFD1 DB ERR – MFD1 obstacle database missing.	The obstacle database is present on another LRU, but is missing on the specified LRU.
MFD1 DB ERR – MFD1 Safe Taxi database error exists.	The MFD detected a failure in the SafeTaxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 terrain database error exists.	The MFD 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.
MFD1 DB ERR – MFD1 terrain database missing.	The terrain database is present on another LRU, but is missing on the specified LRU.
MFD1 KEYSTK – MFD [key name] Key is stuck	A key is stuck on the MFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists
MFD1 SERVICE – MFD1 needs service. Return unit for repair.	The MFD self-test has detected a problem. The system should be serviced.
MFD1 VOLTAGE– MFD1 has low voltage. Reducing power usage	The MFD voltage is low. The system should be serviced.

NAV DB UPDATED-Active navigation database updated.	System has updated the active navigation database from the standby navigation database.
NAV1 RMT XFR - NAV1 remote transfer key is stuck.	A failure has been detected in the NAV1 receiver. The receiver may still be available. The system should be serviced.
NAV1 SERVICE - NAV1 needs service. Return unit for repair.	A failure has been detected in the NAV1 receiver. The receiver may still be available. The system should be serviced.
NAV2 RMT XFR - NAV2 remote transfer key is stuck.	The remote 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.
NAV2 SERVICE - NAV2 needs service. Return unit for repair.	A failure has been detected in the NAV2 receiver. The receiver may still be available. The system should be serviced.
NON-MAG UNITS - Non-magnetic NAV ANGLE display units are active.	Navigation angle is not set to MAGNETIC at power-up.
NON WGS84 WPT - Do not use GPS navigation to [xxxx].	The position of the selected waypoint [xxxx] is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed. Do not use GPS to navigate to the selected non-WGS84 waypoint.

Message Comments

PFD1 CONFIG – PFD1 config error. Config service req'd.	The PFD configuration settings do not match backup configuration memory. The system should be serviced.
PFD1 COOLING – PFD1 has poor cooling. Reducing power usage.	The PFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced.
PFD1 DB ERR – PFD1 basemap database error exists.	The PFD detected a failure in the basemap database.
PFD1 DB ERR – PFD1 basemap database is incompatible.	The PFD detected a that the basemap database is incompatible.
PFD1 DB ERR – PFD1 navigation database error exists.	The PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced.
PFD1 DB ERR – PFD1 obstacle database error exists.	The 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.
PFD1 DB ERR – PFD1 obstacle database missing.	The obstacle database is present on another LRU, but is missing on the specified LRU.
PFD1 DB ERR – PFD1 Safe Taxi database error exists.	The PFD detected a failure in the SafeTaxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced.
PFD1 DB ERR – PFD1 terrain database error exists.	The 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.
PFD1 DB ERR – PFD1 terrain database missing.	The terrain database is present on another LRU, but is missing on the specified LRU.
Message Comments
PFD1 KEYSTK – PFD1 [key name] Key is stuck.	A key is stuck on the PFD . Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists.
[PFD1, PFD2, or MFD1] CARD 1 REM – Card 1 was removed. Reinsert card.	The SD card was removed from the top card slot of the specified PFD or MFD. The SD card needs to be reinserted.
[PFD1, PFD2, or MFD1] CARD 2 REM – Card 2 was removed. Reinsert card.	The SD card was removed from the bottom card slot of the specified PFD or MFD. The SD card needs to be reinserted.
[PFD1, PFD2, or MFD1] CARD 1 ERR – Card 1 is invalid.	The SD card in the top card slot of the specified PFD or MFD contains invalid data.
[PFD1, PFD2, or MFD1] CARD 2 ERR – Card 2 is invalid.	The SD card in the bottom card slot of the specified PFD or MFD contains invalid data.
PFD1 SERVICE – PFD1 needs service. Return unit for repair.	The PFD self-test has detected a problem. The system should be serviced.
PFD1 VOLTAGE– PFD1 has low voltage. Reducing power usage	The PFD1 voltage is low. The system should be serviced.
PFD2 CONFIG – PFD2 config error. Config service req'd.	The PFD configuration settings do not match backup configuration memory. The system should be serviced.
PFD2 COOLING – PFD2 has poor cooling. Reducing power usage.	The PFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced.
PFD2 DB ERR – PFD2 basemap database error exists.	The PFD detected a failure in the basemap database.
PFD2 DB ERR – PFD2 basemap database is incompatible.	The PFD detected a that the basemap database is incompatible.
PFD2 DB ERR – PFD2 navigation database error exists.	The PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced.
PFD2 DB ERR – PFD2 obstacle database error exists.	The 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.
PFD2 DB ERR – PFD2 obstacle database missing.	The obstacle database is present on another LRU, but is missing on the specified LRU.
PFD2 DB ERR – PFD2 Safe Taxi database error exists.	The PFD detected a failure in the SafeTaxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced.
PFD2 DB ERR – PFD2 terrain database error exists.	The 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.
PFD2 DB ERR – PFD2 terrain database missing.	The terrain database is present on another LRU, but is missing on the specified LRU.
PFD2 KEYSTK – PFD2 [key name] Key is stuck.	A key is stuck on the PFD . Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists.
PFD2 SERVICE – PFD2 needs service. Return unit for repair.	The PFD self-test has detected a problem. The system should be serviced.
PFD2 VOLTAGE – PFD2 has low voltage. Reducing power usage	The PFD2 voltage is low. The system should be serviced.

REGISTER CONNEXT – Data services are inoperative, register w/ Connext.

The GDL 59 is not registered with Garmin Connext, or its current registration data has failed authentication.

SCHEDULER [#] –. Message criteria entered by the user.
SLCT FREQ – Select appropriate frequency for approach.	The system notifies the pilot to load the approach frequency for the appropriate NAV receiver. Select the correct frequency for the approach.
Message Comments
SLCT NAV – Select NAV on CDI for approach.	The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to the correct NAV receiver.
STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn.
SVT – SVT DISABLED: Out of available terrain region.	Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database.
SVT – SVT DISABLED: Terrain DB resolution too low.	Synthetic Vision is disabled because a terrain database of sufficient resolution (9 arc-second or better) is not currently installed.
SW MISMATCH – GDU software version mismatch. Xtalk is off.	The MFD and PFDs have different software versions installed. The system should be serviced.

TCAS FAIL - TCAS system is inoperative.	The TCAS or TAS system is not operational.
TERRAIN DSP – [PFD1, PFD2 or MFD1] Terrain awareness display unavailable.	One of the terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid.
TIMER EXPIRD – Timer has expired.	The system notifies the pilot that the timer has expired.
TRAFFIC FAIL – Traffic device has failed.	The system is no longer receiving data from the traffic system. The traffic device should be serviced.
UNABLE V WPT – Can’t reach current vertical waypoint.	The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint.

VNV – Unavailable. Excessive track angle error.	The current track angle error exceeds the limit, causing the vertical deviation to go invalid.
Message Comments
VNV – Unavailable. Excessive crosstrack error.	The current crosstrack exceeds the limit, causing vertical deviation to go invalid.
VNV – Unavailable. Parallel course selected.	A parallel course has been selected, causing the vertical deviation to go invalid.
VNV – Unavailable. Unsupported leg type in flight plan.	The lateral flight plan contains a procedure turn, vector, or other unsupported leg type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint.

WPT ARRIVAL – Arriving at waypoint -[xxxx]	Arriving at waypoint [xxxx], where [xxxx] is the waypoint name.
WX ALERT – Possible severe weather ahead.	Possible severe weather detected within +/- 10 degrees of the aircraft heading at a range of 80 to 320 nm.

XPDR1 CONFIG – XPDR1 config error. Config service req'd.	The transponder configuration settings do not match those of backup configuration memory. The system should be serviced.
XPDR1 FAIL – XPDR1 is inoperative.	There is no communication with the #1 transponder.
XPDR1 SRVC – XPDR1 needs service. Return unit for repair.	The #1 transponder should be serviced when possible.
XPDR2 CONFIG – XPDR2 config error. Config service req'd.	The transponder configuration settings do not match those of backup configuration memory. The system should be serviced.
XPDR2 FAIL – XPDR2 is inoperative.	There is no communication with the #2 transponder.
XPDR2 SRVC – XPDR2 needs service. Return unit for repair.	The #2 transponder should be serviced when possible.
XTALK ERROR – A flight display crosstalk error has occurred.	The MFD and PFDs are not communicating with each other. The system should be serviced.

OTHER SYSTEM ANNUNCIATIONS

System Annunciation Comment
	Attitude and Heading Reference System is aligning.
	Display system is not receiving attitude information from the AHRS.
	Indicates a configuration module failure.
	Display system is not receiving airspeed input from air data computer.
	Display system is not receiving valid heading input from AHRS.
	System is not receiving valid heading input from GMU, but is receiving GPS-derived track information.
	Display system is not receiving altitude input from the air data computer.
	Display system is not receiving vertical speed input from the air data computer.
	Display system is not receiving valid transponder information.
	CDI is not receiving valid data from the corresponding GIA. Does not apply when the CDI is set to GPS.
	GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFM).
Other Various Red X Indications	A red “X” through any other display field (such as engine instrumentation display) indicates that the field is not receiving valid data.

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APPENDIX

PFD SOFTKEY MAP

Top Level PFD Softkeys

CAS Softkeys

CAS		Displays the scroll up and scroll down softkeys.
	CAS ↑	Scroll up (Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling)
	CAS ↓	Scroll down (Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling)

INSET Map Softkeys

INSET or TRFC/MAP		Pressing the INSET Softkey Displays Inset Map in the PFD lower left corner. The TRFC/MAP Softkey is displayed when the TCAS II option is installed. Pressing the TRFC/MAP Softkey displays the Inset Map showing Traffic Map Page.
	OFF	Removes Inset Map
	DCLTR (3)	Selects desired amount of map detail; cycles through declutter levels:DCLTR (No Declutter): All map features visibleDCLTR-1: Declutters land dataDCLTR-2: Declutters land and SUA dataDCLTR-3: Removes everything except the active flight plan
	WX LGND	Displays icon and age on the Inset Map for the selected weather products (optional)
	TRAFFIC	Cycles through traffic display options:TRFC-1: Traffic displayed on inset mapTRFC-2: Traffic Map Page is displayed in the inset map window
	TOPO	Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map
	TERRAIN	Displays terrain information on Inset Map (not available with TAWS-A)
	NEXRAD-CorPRECIP	Displays NEXRAD-C weather and coverage information on Inset Map (optional feature)Displays Connext Weather precipitation on Navigation Map (optional)
	XM LTNGorDL LTNG	Displays SiriusXM lightning information on Inset Map (optional)Displays Connext Worldwide Weather lightning information on Inset Map (optional)
	METAR	Displays METAR flags on airport symbols shown on the Inset Map

SENSOR		Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers
	ADC1	Selects the #1 Air Data Computer
	ADC2	Selects the #2 Air Data Computer
	ADCSTBY	Selects standby air data input
	AHRS1	Selects the #1 AHRS
	AHRS2	Selects the #2 AHRS
	ATTSTBY	Selects standby AHRS input

PFD Configuration Softkeys

PFD			Displays second-level softkeys for additional PFD configurations
	SYN VIS		Displays the softkeys for enabling or disabling Synthetic Vision features
		PATHWAY	Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan
		SYN TERR	Enables synthetic terrain depiction
		HRZN HDG	Displays compass heading along the Zero-Pitch line
		APTSIGNS	Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9 nm.
	DFLTS		Resets PFD to default settings, including changing units to standard
	WIND		Displays softkeys to select wind data parameters
		OPTN 1	Headwind/tailwind and crosswind arrows with numeric speed components
		OPTN 2	Wind direction arrow with numeric speed
		OPTN 3	Wind direction arrow with headwind/tailwind and crosswind speed components
		OFF	Information not displayed
	DME		Select to display the DME information window
	BRG1		Cycles the Bearing 1 Information Window through NAV1 or GPS/waypoint identifier and GPS-derived distance information, and ADF/frequency.
	HSI FRMT		Displays the HSI formatting softkeys
		360 HSI	Displays the HSI in a 360 degree format
		ARC HSI	Displays the HSI in an arc format
	BRG2		Cycles the Bearing 2 Information Window through NAV2 or GPS/waypoint identifier and GPS-derived distance information, and ADF/frequency.
	ALT UNIT		Displays softkeys for setting the altimeter and BARO settings to metric units
		METERS	When enabled, displays altimeter and selected altitude in meters
		IN	Press to display the BARO setting as inches of mercury
		HPA	Press to display the BARO setting as hectopacals
	STD BARO		Sets barometric pressure to 29.92 in Hg (1013 hPa)
OBS			Selects OBS mode on the CDI when navigating by GPS (only available with active leg)
CDI			Cycles through GPS, VOR1 (LOC1), and VOR2 (LOC2) navigation sources on the CDI
ADF/DME			Displays the ADF/DME Tuning Window, providing ADF tuning capability and allowing selection of the NAV source for tuning each DME

Transponder Softkeys without Optional TCAS II installed

XPDR			Displays transponder mode selection softkeys
	XPDR1		Selects the #1 transponder as active. Not available with TCAS II option.
	XPDR2		Selects the #2 transponder as active. Not available with TCAS II option.
	STBY		Selects Standby Mode (transponder does not reply to any interrogations)
	ON		Selects Mode A (transponder replies to identification interrogations)
	ALT		On Ground - (White mode indication)Generates Mode S replies to discrete interrogations as well as transmission of acquisition and extended squitters, including ADS-B out. Mode A, Mode C, and Mode S all-call replies are inhibitedAirborne - (Green mode indication)Generates Mode A, Mode C, and Mode S replies as well as transmissions of acquisition and extended squitters, including ADS-B out.
	VFR		Automatically enters the VFR code (1200 in the U.S.A. only). Not available when TCAS II option is installed.
	CODE		Displays transponder code selection soft-keys 0-7
		0 — 7	Use numbers to enter code
		BKSP	Removes numbers entered, one at a time
IDENT			Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen
TMR/REF			Displays Timer/References Window
NRST			Displays Nearest Airports Window
MSG			Displays Messages Window

Transponder/Traffic Softkeys with TCAS II Option

XPDR/TFC				Displays the transponder and TCAS II selection softkeys
	MODE			Displays transponder mode selection softkeys
		STBY		Selects transponder Standby Mode (transponder does not reply to any interrogations).When the transponder is set to standby, the TCAS II system is also set to standby.
		ON		Activates transponder (transponder replies to identification interrogations).When the transponder is set to ON, the TCAS II system is set to standby.
		ALT		Altitude Reporting Mode(transponder replies to identification and altitude interrogations). When the transponder is set to ALT,the TCAS II system is set to standby.
		TA ONLY		Activates the TCAS II system in TA Only Mode and set the transponder to ALT
		TA/RA		Activates the TCAS II system in TA/RA Mode and sets the transponder to ALT
		BACK		Returns to the previous softkey level
	TCAS			Displays the TCAS control softkeys
		REL		Displays intruder altitude as altitude relative to own aircraft altitude
		ABS		Displays intruder MSL altitude
		ALT RNG		Displays the altitude display range softkeys
			ABOVE	Displays non-threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft.Typically used during climb phase of flight.
			NORMAL	Displays non-threat traffic from 2700 feet above the aircraft to 2700 feet below the aircraft.Typically used during enroute phase of flight.
			BELOW	Displays non-threat traffic from 2700 feet above the aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight.
			UNREST	All traffic is displayed
		TEST		Activates Test Mode and displays test intruder symbols
		BACK		Returns to the previous softkey level
	CODE			Displays transponder code selection softkeys 0-7
		0 — 7		Use numbers to enter code
		IDENT		Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen
		BKSP		Removes numbers entered, one at a time
IDENT				Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen
TMR/REF				Displays Timer/References Window
NRST				Displays Nearest Airports Window
MSG				Displays Messages Window

MFD SOFTKEY MAP

when the checklist item is already checked.

SYSTEM Softkeys

SYSTEM			Accesses engine and airframe softkeys
	ENG SET		Accesses the FADEC settings softkeys; displays the Takeoff Data Set Window when aircraft is parked or taxiing
		CON	Selects the continuous thrust rating. Disabled when aircraft is on the ground.
		CLB	Selects the maximum climb thrust rating. Disabled when aircraft is on the ground.
		OAT ↑	Increases the takeoff outside air temperature setting in one-degree Celsius increments. Disabled when aircraft is in the air.
		OAT ↓	Decreases the takeoff outside air temperature setting in one-degree Celsius increments. Disabled when aircraft is in the air.
		ATR ON	Enables Automatic Thrust Reserve (ATR). Disabled when aircraft is in the air.
		ATR OFF	Disables Automatic Thrust Reserve (ATR). Disabled when aircraft is in the air.
		BACK	Returns display to previous softkey level
		ACCEPT	Confirms the selected takeoff settings
	LFE		Accesses softkeys for manually setting the Landing Field Elevation (LFE)
		FMS LFE	Sets current flight plan destination elevation as displayed LFE
		+500 FT	Increases currently displayed LFE value by 500 ft
		-500 FT	Decreases currently displayed LFE value by 500 ft
		+50 FT	Increases currently displayed LFE value by 50 ft
		-50 FT	Decreases currently displayed LFE value by 50 ft
		ACCEPT	Confirms the LFE setting and returns to the previous softkey level
		BACK	Returns display to previous softkey level
	STATUS		Displays the System-Status Page
	ECS		Displays the System-ECS (Environmental Control System) Page
	ELEC		Displays the System-Electrical Page
	FUEL		Displays the System-Fuel Page
	ICEPROT		Displays the System-Deice Page
	ENG MNT		Displays the Engine Maintenance Page. Enabled only while aircraft is on the ground and engines are off.
	BACK		Returns display to previous softkey level

CPDLC Softkeys

CPDLC		When available, accesses CPDLC softkeys.
	LOGON	Displays Logon screen for the CPDLC system
	LOGOFF	Displays Logoff screen for the CPDLC system
	NEW	Accesses New CPDLC message screen
	DELETE	Delete selected CPDLC message.
	DEL ALL	Delete all CPDLC messages.
	BACK	Returns display to previous softkey level

MAP		Enables second-level Navigation Map softkeys
	TRAFFIC	Displays traffic information on Navigation Map
	PROFILE	Displays/removes Vertical Situation Display on Navigation Map Page
	TOPO	Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Navigation Map
	TERRAIN	Displays terrain information on Navigation Map (not available with TAWS-A)
	AIRWAYS	Displays airways on the map; cycles through the following: AIRWAYS: No airways are displayed AIRWY ON: All airways are displayed AIRWY LO: Only low altitude airways are displayed AIRWY HI: Only high altitude airways are displayed
	NEXRAD-C or PRECIP	Displays NEXRAD weather and coverage information on the Navigation Map (optional) Displays Connext Weather precipitation on Navigation Map (optional)
	XM LTNG or DL LTNG	Displays SiriusXM Weather lightning information on the Navigation Map (optional) Displays Connext Weather lightning information on the Navigation Map (optional)
	METAR	Displays METAR flags on airport symbols
	WX RADAR	Displays the weather radar scan on the Navigation Map
	BACK	Returns to top-level softkeys
DCLTR (3)		Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except the active flight plan
SHW CHRT		When available, displays optional airport and terminal procedure charts
CHKLIST		When available, displays optional checklists

UPDATING DATABASES

CAUTION: Never disconnect power to the system when loading a database. Power interruption during the database loading process could result in maintenance being required to reboot the system.

CAUTION: When downloading updates to the Jeppesen Navigation Database, copy the data to an SD card other than a Garmin Supplemental Data Card. Otherwise, data corruption can occur.

NOTE: When loading database updates, the 'DB Mismatch' message will be displayed until database synchronization is complete, followed by turning system power off, then on. Synchronization can be monitored on the AUX-SYSTEM STATUS Page.

NOTE: DO NOT use the database SD cards for any purpose other than database storage.

In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional. It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features.

If an error occurs during synchronization, an error message will be displayed, followed by the affected display in the Sync Status section of the Database Window. If synchronization completes on one display, but an error occurs on another, the error message will be displayed with the affected displays listed after it. When an error message is displayed, the problem must be corrected before synchronization can be completed. A power cycle is required to restart synchronization when 'Card Full' or 'Err' is shown.

Error Message Description
Canceled Database	synchronization has been canceled by removing the bottom SD card in display being updated
Card Full	SD card does not contain sufficient memory
Err	Displayed for all other errors that may cause the synchronization process to be halted
Timeout	System timed-out prior to the database transfer completing

Garmin Databases

Updating Basemap, SafeTaxi, Obstacle, Airport Directory, and FlightCharts Databases

These databases may be copied to one Supplemental Data Card, then automatically synchronized to other card in the system:

1) With the system OFF, remove the Garmin SD Cards from the bottom SD card slot of each flight display unit.
2) Go to www.flygarmin.com. Download the applicable software and install the databases on the Garmin SD card for each display. (The FliteChart database must only be installed on the MFD SD Card).
3) Put the Garmin SD Cards back in the bottom SD card slots of each flight display unit.
4) Turn the system ON.
5) During MFD power-up, check the MFD Power-Up screen and make sure that the database is initialized and shown on the database information.
6) Press the ENT Key on MFD display to acknowledge the startup screen.
7) Turn the large FMS Knob to select the AUX Page group on the MFD.
8) Turn the small FMS Knob to select the System Status Page.
9) Press the Display Database Selection Softkey to show database information for each display. Verify the correct database cycle information is shown for each display.
10) Remove Power from the system.

Jeppesen Databases

Updating the active Jeppesen navigation database (not using the Dual Navigation Database or Automatic Database Synchronization Features):

The Jeppesen Navigation Database that is loaded to internal memory as the active database will be used by the system.

NOTE: Loading the Jeppesen Navigation Database as the active database prior to its effective date will result in the expiration date on the power-up screen and the effective date on the AUX-System Status Page being displayed in yellow.

NOTE: After the navigation database is loaded or copied, the top SD card may be removed.

1) Go to www.flygarmin.com or www.jeppesen.com. Download the applicable software and install the navigation database on a blank SD card.
2) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the display (label of SD card facing left).
3) Turn the system ON. A prompt similar to the following is displayed in the upper left corner of the display:

DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD?
THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON-GROUND POWER CYCLE ON OR AFTER 00:00 SYSTEM TIME ON THE EFFECTIVE DATE.
FROM TO
REGION: WORLDWIDE WORLDWIDE
CYCLE: 1511 1512
EFFECTIVE: 26-AUG-2015 23-SEP-2015
EXPIRES: 23-SEP-2015 21-OCT-2015
NO WILL BE ASSUMED IN 21 SECONDS. 

4) Press the NO Softkey to proceed to loading only the active database.

5) A prompt similar to the following is displayed, press the YES Softkey to update the active navigation database.

DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE?
SELECTING YES WILL OVERWRITE THE ACTIVE NAVIGATION DATABASE.
FROM TO
REGION: WORLDWIDE WORLDWIDE
CYCLE: 1511 1512
EFFECTIVE: 26-AUG-2015 23-SEP-2015
EXPIRES: 23-SEP-2015 21-OCT-2015
NO WILL BE ASSUMED IN 8 SECONDS.
UPDATING THE ACTIVE NAVIGATION DATABASE, PLEASE WAIT.
UPDATED 1 FILES SUCCESSFULLY!
PRESS ANY KEY TO CONTINUE.
CONTINUING IN 8 SECONDS. 

6) After the update completes, the display starts in normal mode. Do not remove power while the display is starting.

7) Turn the system OFF and remove the SD card from the top card slot.
8) Repeat steps 2 through 7 for the other displays. Remove the SD card when finished.
9) Apply power to the system and press the ENT Key or the right-most softkey on the MFD to acknowledge the startup screen.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
12) Press the Display Database Selection Softkey to show active navigation database information for each display. Verify the correct active navigation database cycle information is shown for each display.
13) Remove power from the system.

Loading the Jeppesen Navigation Database as the Standby Navigation Database

The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Jeppesen Navigation Database to the bottom SD card, prior to its effective date. (The Jeppesen Navigation Database is available from Jeppesen seven days prior to its effective date.)

NOTE: After the navigation database is loaded or copied, the top SD card may be removed.

NOTE: To do this procedure, use a blank SD card to copy the navigation database. Garmin SD Cards (bottom SD card slots) must NOT be used. The use of SanDisk SD Card is recommended to update the navigation database file. Before utilization, it is recommended to format the SD Card with the FAT32 file system so that displays will read it.

1) Go to www.flygarmin.com or www.jeppesen.com. Download the applicable software and install the navigation database on a blank SD card.
2) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the display.
3) Verify that an SD card is inserted in the bottom slot of each display.
4) Turn the system ON. A prompt similar to the following is displayed.

DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD?
THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON-GROUND POWER CYCLE ON OR
AFTER 00:00 SYSTEM TIME ON THE EFFECTIVE DATE.
FROM    TO
REGION: WORLDWIDE   WORLDWIDE
CYCLE: 1511    1512
EFFECTIVE: 26-AUG-2015  23-SEP-2015
EXPIRES: 23-SEP-2015  21-OCT-2015
NO WILL BE ASSUMED IN 21 SECONDS. 

5) Press the YES Softkey. The navigation database is copied to the SD card in the bottom card slot of the display.
6) After the navigation database files are copied to the bottom SD card, the display will appear.

INITIALIZING SYSTEM
DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD?
THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON-GROUND POWER CYCLE ON OR AFTER 00:00 SYSTEM TIME ON THE EFFECTIVE DATE.
FROM    TO
REGION: WORLDWIDE   WORLDWIDE
CYCLE: 1511    1512
EFFECTIVE: 26-AUG-2015  23-SEP-2015
EXPIRES: 23-SEP-2015  21-OCT-2015

NO WILL BE ASSUMED IN 18 SECONDS.
UPDATING STANDBY NAVIGATION DATABASE, PLEASE WAIT.

UPDATED STANDBY NAVIGATION DATABASE SUCCESSFULLY.
PRESS ANY KEY TO CONTINUE.
CONTINUING IN 9 SECONDS. 

7) As instructed on the display, press any key to continue. The display will now appear.

DATABASE NAVIGATION WILL BE VERIFIED BEFORE USE.
DATABASE STANDBY NAV WILL BE VERIFIED BEFORE USE.
PRESS ANY KEY TO CONTINUE.
CONTINUING IN 6 SECONDS. 

8) Press any key to continue.

DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE?
SELECTING YES WILL OVERWRITE THE ACTIVE NAVIGATION DATABASE.
FROM TO
REGION: WORLDWIDE WORLDWIDE
CYCLE: 1511 1512
EFFECTIVE: 26-AUG-2015 23-SEP-2015
EXPIRES: 23-SEP-2015 21-OCT-2015
NO WILL BE ASSUMED IN 8 SECONDS.
UPROUTING THE ACTIVE NAVIGATION DATABASE PLEASE WAIT 

9) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid, it should not be loaded as the active database. The display now starts in normal mode. Do not remove power while the display is starting.
10) Turn the system OFF and remove the SD card from the top card slot.
11) Repeat steps 2 through 10 for the remaining displays.
12) Apply power to the system and press the ENT Key on the MFD display to acknowledge the startup screen.
13) Turn the large FMS Knob to select the AUX Page group on the MFD.
14) Turn the small FMS Knob to select the System Status Page.
15) Press the Display Database Selection Softkey to show standby navigation database information for each display. Verify the correct standby navigation database cycle information is shown for each display.
16) Remove power from the system.

Updating Jeppesen Chartview Database

The ChartView database should be downloaded to the Garmin supplied Supplemental Data Card which will reside in the bottom card slot on the MFD. Contact Jeppesen (www.jeppesen.com) for subscription and update information.

1) With the system OFF, remove the Garmin SD Card from the bottom SD card slot of the MFD.
2) Go to www.flygarmin.com or www.jeppesen.com. Download the applicable software and install the Chartview database on a blank SD card.
3) Put the Garmin SD Card back in the bottom SD card slots of the MFD.
4) Apply power to the system and press the ENT Key on the MFD display to acknowledge the startup screen.
5) Turn the large FMS Knob to select the AUX Page group on the MFD.
6) Turn the small FMS Knob to select the System Status Page.
7) Press the Display Database Selection Softkey to show database information for MFD (MFD DB). Use the FMS knob to select the ChartView Database field and verify the correct database cycle information is shown.
8) Remove power from the system.

Loading the Magnetic Field Variation Database Update:

A copy of the current magnetic field variation database (MV DB) is included with the navigation database. At startup, the system compares this version of the MV DB with that presently being used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs to be updated, a prompt is displayed on the Navigation Map Page, as shown in the following figure. Note, in the following example, GRS1 is the first AHRS to indicate an update is available. In actuality, this is dependent on which AHRS is the first to report status to the system. GRS2 may be displayed before GRS1. The order is not important, only that both AHRS be updated.

GRS1 Magnetic Field Variation Database Update Prompt

1) With 'OK' highlighted, press the ENT Key on the MFD. A progress monitor is displayed.

Uploading Database to GRS1

2) When the upload is complete, the prompt for the next GRS upload is displayed.

GRS2 Magnetic Field Variation Database Update Prompt

3) With 'OK' highlighted, press the ENT Key on the MFD. A progress monitor is displayed. When the upload is complete, the system is ready for use.

Uploading Database to GRS2

A

Access code 65

Activate a flight plan 34

Active Channel 110

Active database 187

AC-U-KWIK Airport Directory 93

ADF 21, 23, 175

Advisories, CAS 133–134

AHRS 148, 149, 153, 154, 156, 158

Airport Directory 93

Airport Signs 89, 90

Airways 184

Air Data Computer 136

Alerts, Aircraft 129

Altimeter setting 1

Antenna stabilization 88

Antenna tilt 85

AOPA Airport Directory 93

ATC RR-7, 24, 25, 26, 133, 146, 177, 180

ATR 7,181,182

Attitude & Heading Reference System 136

Audio Panel 124

Audio panel controls NAV1, NAV2 23

Aural alerts 145

Automatic Thrust Reserve 7, 181, 182

B

Barometric pressure 175

Battery indications 5

Bearing line 86, 88

C

Cautions, CAS 129–131

CDI 1, 2, 23, 166

Channel Presets 111

ChartView 91

Checklists 112–113

CLD TOP Softkey 73

Code selection softkeys 22

COM 22, 23, 123

CPDLC RR-1, 24, 25, 26, 27, 183

D

Database Synchronization 186

Data link communication 24

Data Link Receiver 144

DB Mismatch 185

DCLTR Softkey 91

Dead Reckoning 125

Declutter 124, 172, 184

Designated altitudes 36, 37

Direct-to 33

DME 21, 23

DR mode 125, 126, 127

E

Edit a flight plan 52

Electrical indications 8, 14

Electronic checklists 113

Emergency checklist 113

Engine failure 121

Engine fire 121

Engine rotation speeds 5

Environmental Control System (ECS) 12–13

F

Flap Indicator 5, 11, 122

Flight Director 29

Flight ID 21

Flight path marker 89

FliteCharts® 91

Frequency Transfer 23

Fuel indications 5, 8, 16

G

Gain 87

Garmin Flight Data Services 114

Ground mapping 87

H

HF 22

Horizon heading 89

Horizontal scan 85, 86

|

Inhibit TAWS 82

Inset Map 172, 173, 184

Interstage Turbine Temperature (ITT) 5, 121

101 137, 138, 141

Iridium 93, 98

Iridium satellite network 93, 99, 100

J

Jeppesen 91

L

Landing gear status 5, 9

M

Map panning 62

Message dialogs 26, 27

METAR 62

Minimum Anti-Ice N1 Bug 6, 19

MISCOMP 136

Multi Function Display (MFD)

Softkeys 181

N

N1 gauge 121

N1 Transient Limit 6

NAV 23

NAV1 2,23

NAV2 2,23

Navigation database 35, 37, 147, 151, 152

Network 108, 109

NEXRAD 62,184

NEXRAD Softkey 72

0

OBS 2

Obstacles 152, 158

Oil, engine 5

Outside Air Temperature (OAT) 8

Overspeed Protection 31

P

Pathways 89, 90

PIREP 76

PIT 136

Power-up page 112

Predefined message 102, 103

Pressure, oil 5

Pressurization 9

R

Register 66

Resolution Advisory 78, 90

Response/Request 25, 26

Reversionary mode 123

ROC 137, 138, 140, 141

S

SafeTaxi® 89, 91

SBAS 56, 82, 126, 149, 158

Sector scan 88

Secure Digital (SD) card 112

Sensor 136

SiriusXM 110

SiriusXM Weather 62

Spoiler status 5, 9

STAB 88

Standby 84

Standby Navigation Database 188, 190

Store Flight Plan 52

SVT 89, 166

Synchronization 185

Synoptics 11–18

Synthetic Vision System 89

T

TAF 62,74

TAS 148, 149

TAWS 80, 81, 82, 137, 139, 140, 141

TAWS-A 80, 81, 137, 139, 140, 141, 172, 184

TAWS-B 80

TCAS II 22, 77, 78, 80, 90, 142, 143, 172, 176, 177, 178, 179

Telephone 93, 94

TEMP COMP 35

Temperature, oil 5

Terrain 80, 137, 138, 152, 172, 184

Text message 101, 102, 104

Text messaging 100

Thrust rating 6

Tilt 85

Tilt line 85

Timer 2, 166

Topographical data 172, 184

Traffic 61, 77, 79, 183

Traffic Advisory 77, 78, 145

Traffic map page 77, 79, 80

Transponder 21, 22, 176, 177, 178, 179, 180

Trim Indicator 5, 11, 123

V

Vertical path guidance 36

Vertical speed guidance 37

VNV 33, 125, 166, 167

Voltmeter, battery 5

Vspeed 2

W

WATCH® 88

Waypoint Selection Submenu 46

Weather Attenuated Color Highlight 88

Weather radar 84

Wi-Fi 107, 108, 109

Wind data 175

Winds Aloft 75

WIND Softkey 75

X

XM Weather Data Link Page 62

Blank Page

GARMIN®

Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

p:913.397.8200 f:913.397.8282

Aircraft On Ground (AOG) Hotline: [phone]

Aviation Dealer Technical Support: 888.606.5482

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

p: 503.581.8101 f: 503.364.2138

Garmin (Europe) Ltd

Liberty House, Houndown Business Park

Southampton, Hampshire SO40 9LR, U.K.

p: 44 (0) 23 8052 4000 f: 44 (0) 23 8052 4004

Aviation Support: 44 (0) 87 0850 1243

Garmin Corporation

No. 68, Jangshu 2nd Road

Shijr, Taipei County, Taiwan

p: 886/2.2642.9199 f: 886/2.2642.9099

www.garmin.com