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Garmin Software Version 0734.23 Cockpit Reference Guide

1. Flight Director Modes Selected Control Pressed Activated Lateral Vertical FD Key pilot side Pilot side Roll Hold default ROL Pitch Hold default PIT FD Key copilot side Copilot side Roll Hold default ROL Pitch Hold default PIT AP Key Pilot side Roll Hold default ROL Pitch Hold default PIT Roll Hold default ROL Takeoff on ground TO TGR Roll Hold 1 ROL Go 7 s 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 Path Tracking VPTH GPS NAV Key Pilot side avigation e Pitch Hold default PIT BC GPS Pitch Hold default P T APR Key Pilot side Approach VOR Glidepath GP LOC Glideslope GS HDG Key Pilot side Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 25 sv3 sjueunasu oipny uadx ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony 2 Duruue d Tunuuy Jeuuouqy Jeuonippy xipueddy x pul iui nuru JUl0 JAEN paezey Flight Instruments Nav Com XPDR Audio Flight Plan
2. Glide Slope Caution d m or ac epends on approac QHDeENH Glide Path type GLIDEPATH Altitude Voice Callout None None g ee J Four Hundred Three Hundred Two Hundred One Hundred 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 95 sjuauimasu nubi So1nje24 aoueplony s mp oold Buruue d AEN Sd5 2 444 paezey 346 3 UI05 AeN jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts TAWS A System Status Annunciations A GARMIN PFD MFD Additional Alert Type TAWS A Page TAWS A Page Aural Message Annunciation Annunciation TAWS System Fail TAWS FAIL MEZUN TANS System Failure GPWS System Fail GPHS FAIL None GPWS System Failure System Test in progress TAWS TEST TAWSTEST None System Test pass None None TAWS System Test OK Terrain or Obstacle database unavailable invalid software configuration or audio unavailable GPWS System Fail Radar Altimeter invalid Altitude or Vertical Speed unavailable None TAWS System Failure GPWS System Failure No GPS position no GPS POSITION TAWS Not Available Excessively degraded GPS signal Out of None TAWS Not Available
3. SU PAP Failure of copilot pitch trim switch RAM AIR FAIL Ram air valve failure RUD BOOST FAIL thrust asymmetry Loss of SLRB Spring Loaded Rudder Booster force assistance in case of tch position disagrees with the spoiler surfaces position ers and or speed brake functions PA ame Ventral rudder has failed XBLEED FAIL Cross bleed valve has failed closed or open o ReaD RO gem Cross bleed switch is in the OFF position 92 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN COMPARATOR ANN 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 Annunciations amp Alerts UNCIATIONS start up shut down or while taxiing Comparator Window Text Condition Difference in altitude sensors is gt 200 ft f both airspeed sensors detect 35 knots this is inhibited f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 15 kts f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 10 kts Difference in heading sensors is gt 10 degrees Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees ALT NO COMP IAS NO COMP o data from one or both altit
4. optional optional SYNVIS DFLTS WIND DME1 BRG1 HSI FMT BRG2 2 STD BARO BACK Select the BACK Softkey to return to the top level softkeys l 360 Hs ARC Back msc L TT TL L errs ck EY V3 V4 EN 75 XS 75 nnn n n on 1 1 1 0 nmpms5snnunnnnnunnstonstoun psi mens 7 SS TE TE IE E8893 pnnnmunnnnunnstontu 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 126 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN DFLTS WIND OPTN 1 OPTN 2 OPTN 3 OFF DMEI BRGI HSI FRMT 360 HSI ARC HSI BRG2 DME2 ALT UNIT METERS IN HPA Appendix Resets PFD to default settings includ ing changing units to standard Displays softkeys to select wind data parameters Wind direc
5. 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 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired select the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Moni tor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in p
6. Fuel Line Operating Feed Ejector Operating Fuel Pressure Switch Operating Valve DC Pump Operating Fuel Transfer Valve Open with flow Open no flow Open with flow Open no flow Icons and Descriptions Not operating A Not operating N Not operating In transit Closed 5 Not operating a In transit Closed Fuel System Unit Status Indications 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 17 GARMIN Ice Protection System O Windshield Heaters Crossbleed Valve Boot Lines and Valves Ice Protection Bleed Duct 0 Anti Ice Valve AIV 1 2 77 Shut Off Valve 2 O Bleed Duct and Skin 1 n Ice Valve EAIV 2 Valve and G n Ice Valve EAIV 1 Valve and 10 Bleed Duct and Skin 2 0 1 Shut Off Valve 1 2 Anti Ice Valve AIV 2 Ice Protection Synoptics Page 18 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Engine amp Airframe Systems Ice Protection System Unit Status Indications 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Closed o Closed Unit Icons and Descriptions Anti Ice Line Operating Not operating Crossbleed Valve XBV Pressure Regulating Shutoff Valve PRSOV Open with flow Open no flow Anti Ice Valve AIV D Engine Anti Ice Valve EAIV Op
7. NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative 190 00761 00 Rev A A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced Cockpit Reference Guide for the Prodigy Flight Deck 300 111 sjuaumasu sub Sonje24 e uepioAy s mp oold Buruue d AEN Sd5 2 444 paezey 3461 UI05 AeN jeuonippy uoneiedo Jeuuouqy jns PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix sd Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may
8. optional optional TERRA pairs be rcs 1L 1L 59 ev nnn Select the BACK Softkey on this level to return to the top softkey level MAP Softkeys Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map not available with TAWS A 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 Displays NEXRAD weather and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional feature Returns to top level softkeys Cockpit Reference Guide for the Prodigy Flight Deck 300 135 sjuaumasu wp saunqea4 2 Buruuejd AEN 5640 24V oipny uadx Jeuonippy paezey 16114 U105JNeN uoneiedo Jeuuouqy Sue v unuuy 5 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN DCLIR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declu
9. 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 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 4 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 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 82 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
10. A GARMIN Additional Features Enable disable Periodic Send for Periodic Test Reports 1 While viewing the Report Status Page press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to move the cursor to the PERIODIC SEND field 3 Tum the small FMS Knob to select ENABLED of DISABLED 4 Press the ENT Key Sending a Transmission Manually 1 While viewing the Report Status Page press the FMS Knob to activate the Cursor 2 Turn the large FMS Knob to move the cursor to the send button on the desired data report 3 Press the ENT Key Restore Reports Page Options to Default Settings 1 While viewing the Report Status Page press the MENU Key 2 Turn the FMS Knob to select Restore Defaults in the menu list as shown in Figure 8 106 3 Press the ENT Key 4 Aconfirmation window as shown in Figure 8 107 is now displayed 5 Tum the large FMS Knob to select YES or NO 6 With YES highlighted press the ENT Key 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 73 xipuaddy suelv uoneiedo sainyea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax sv sjuaumnasu Tunuuy Jeuuouqy jeuonippy paezey U10 AEN iui x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Avoidance Appendix Alerts Operation Index Addit
11. Annunciations amp Alerts Message Comments GEA1 CONFIG GEA1 config error Config service req d GEA2 CONFIG GEA2 config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The system should be serviced The GEA2 configuration settings do not match those of backup configuration memory The system should be serviced 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 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 GTX 33 33D MESSAGE ADVISORI ES Message Comments 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 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 se
12. Index Additional Features A GARMIN SYSTEM DATA LOGGING OPTIONAL 72 NOTE An account must be established vvith Garmin Flight Data Services to make full use of the System Data Logging feature Control and monitoring of report transmissions is accomplished through the AUX REPORT STATUS Page Viewing the Report Status Page 1 2 3 Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select AUXILIARY COMMUNICATIONS If necessary select the REPORT Softkey to display the AUX REPORT STATUS Page Changing the Transmission Method 1 2 3 4 While viewing the Report Status Page press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the 1st or 2nd transmit method for the desired data report Turn the small FMS Knob to select the desired option SAT SHORT BURST SAT RUDICS WI FI or NONE Sat Short Burst is generally used for transmission of data packets less than 300 bytes Wi Fi is used only when the aircraft on the ground Press the ENT Key Enable disable Automatic Send for Automatic Test Reports 1 2 3 4 While viewing the Report Status Page press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the AUTOMATIC SEND field Turn the small FMS Knob to select ENABLED of DISABLED Press the ENT Key Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A
13. 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 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN light Planning 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 Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to
14. 3 4 5 6 7 Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 44 1 2 3 4 5 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 Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window 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 Once all changes have been made press the FMS Knob to remove the cursor Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Flight Planning INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD or Control Unit
15. 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 E on the PFD 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob counterclockwise to place the cursor over the ALT altitude field 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 29 sjuauimasu nubi oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sa
16. Abnormal Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 50 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the TO GA switch Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page XM WEATHER SUBSCRIPTION OPTIONAL N V ARNING Use of XM vveather for hazardous vveather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather
17. 2 x x pul iui n Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix LFE STATUS ECS ELEC FUEL ICEPROT ENG MNT BACK FMS LFE 500 FT 500 FT 50 FT 50 FT ACCEPT BACK A GARMIN Accesses softkeys for manually setting the Landing Field Elevation LFE Sets current flight plan destination elevation as displayed LFE Increases currently displayed LFE value by 500 ft Decreases currently displayed LFE value by 500 ft Increases currently displayed LFE value by 50 ft Decreases currently displayed LFE value by 50 ft Confirms the LFE setting and returns to the previous softkey level Returns display to previous softkey level Displays the System Status Page Displays the System ECS Environmental Control System Page Displays the System Electrical Page Displays the System Fuel Page Displays the System Anti Ice Page Displays the Engine Maintenance Page Enabled only while aircraft is on the ground and engines are off Returns display to previous softkey level 134 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN stem 1E nn T TRaFFIC T Toro a F3 TRAFFIC TOPO TERRAIN AIRWAYS NEXRAD XM LING BACK 190 00761 00 Rev A Appendix optional optional jn m
18. 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 48 1 2 3 4 5 6 NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN 5 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 o
19. AUTOMATIC FLIGHT CONTROL SYSTEM s 25 Flight Director Activation 25 Vertical Modes t tete tri cet d Rd 26 Lateral Modes 2 GPS NAVIGATION neca dad na tatus 29 Direct to Navigation sssssssseeene nnne 29 Activate a Stored Flight Plan 30 Activate a Flight Plan Leg 30 Stop Navigating a Flight 77 55 31 Vertical Navigation VNAV ssssseeetnnnt nnne 31 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Table of Contents GARMIN FLIGHT PLANNING a a aad 33 Weight 33 Trip Planririg 5 ete acere itte tete eno ue de 33 Create a New User Waypoint Defined by Latitude amp Longitude 35 Create a New User Waypoint Defined by Radials from Other Waypoints 36 Create a New User Waypoint Defined by a Radial amp Distance from Another Waypolrt roten dre 0 0 0 0000 rn Delete a User 1 1 Create a New Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Fl
20. When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Using the PFD 1 2 3 4 5 6 1 8 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Press the FPL Key Turn the small FMS Knob to display the Waypoint Information Page Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN light Planning IMPORT A FLIGHT PLAN FROM AN SD CARD 1 2 3 4 5 6 7 8 Insert the SD card containing the flight plan in the top card slot on the MFD Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn either FMS Knob to highlight an empty or existing flight pla
21. amp Warning System sssssssssseen 56 Airborne Color Weather Radar 60 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN table of Contents ADDITIONAL 5 63 Synthetic Vision Optional 63 Terminal Procedure Charts ssssssseeeeenn 65 AOPA Airport Directory Satellite Telephone Communication 67 Wi Fi Connections Optional sseenennnn System Data Logging Optional XM Radio Entertainment Subscription 74 Electronic Checklists 76 Reversionary Mode Abnormal COM Operation 5 s s s s s s s ss s s ss s s ss s siss s s l Audio Panel Fail safe Operation Hazard Displays with Loss of GPS Position Unusual Attitudes Dead Reckonllg nmn terme e ae n RR ANNUNCIATIONS amp ALERTS CAS Messages eot temet Comparator Annunciations Reversionary Sensor Annunciations TAWS A Alerts TAWS B Alerts TCAS II Annunciations ssssssseetn nnne Other
22. but is missing on the specified LRU 106 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists Comments The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If pr
23. database coverage area Out of database None TAWS Not Available coverage area TAWS Available when aircraft enters database Coverage area 96 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN TAWS A Alert Availability Annunciations amp Alerts TAWS A Alert Type Available TAWS A Status Annunciation RTC Il ROC IOI PDA EDR ECR NCR FIT GSD VCO Displayed No No No No No No No No No No TAMS N A No No No No No Yes Yes Yes Yes Yes Yes 5 FAIL 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 Alert available unless GPS signal is invalid or unavailable 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 97 s m p q aoueplony S
24. junuuy Jeuuouqy x pul GARMIN itional Features Add Sjueuinijsu fila 573 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey s s uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 78 GARMIN Abnormal Operation ABNORMAL OPERATION Sjueuinijsu Yid NOTE The Embraer Phenom 300 Airplane Flight Manual AFM always takes precedence over the information found in this section ENGINE oipny udax UI0JNeN When an engine failure occurs besides the CAS message corresponding to the failed engine El 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 AeN Sd5 S24V Duruue d SeJnpa20Jd Engine Failure Indication Engine Fire Indication HE CABIN PRESSURIZATION Bi 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 R
25. mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 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 COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible COM1 PTT 1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the system should be serviced COM1 RMT XFR COM remote transfer key is stuck COM2 RMT COM2 remote transfer key is stuck The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its
26. operation If the problem persists the system should be serviced 110 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message with other NAVS LOI GPS integrity lost Crosscheck Comments GPS integrity is insufficient for the current phase of flight 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 GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 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 NAV1 SERVICE NAV1 needs service Return unit for repair
27. press the OFF Softkey mal zi a g 2 o a xipuaddy Suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax sv unuuy Jeuuouqy Jeuonippy paezey Wfl U10 AEN x pul A GARMIN Flight Instruments i U105 AEN S2dV AeN Sd5 Duruue d qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 GARMIN ENGINE amp AIRFRAME SYSTEMS ENGINE INDICATION SYSTEM OIL PRES PSI OIL TEMP C FPM J PSI DELTA P PSI J LFE FT oxy750 1450 pst EIS Display Normal Mode EIS Display Reversionary Mode G ELEC 6 HU as 8 0 11 Dr ngine Fan Rotation Speed 0 Pressurization Display Interstage Turbine Temperature ITT Spoiler Status 0 Engine High Pressure Compressor Landing Gear Status Rotation Speed O Oil Pressure and Temperature Flap Indicator G Fuel Display 1 Trim Indicator Battery Voltmeter 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Leas Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Automatic Thrust Reserve Status Commanded NI Rating Mini
28. still be available The system should be serviced when possible GSD 41 MESSAGE ADVISORIES Message Comments GSD1 CONFIG GSD1 config error Config service req d GSD1 and the CDU have different copies of the GSD1 configuration GSD2 CONFIG GSD2 config error Config service req d GSD2 and the CDU have different copies of the GSD2 configuration GSD1 COOLING GSD temperature too low GSD1 is reporting a low temperature condition GSD2 COOLING GSD2 temperature too low GSD2 is reporting a low temperature condition GSD1 COOLING 501 over temperature GSD2 COOLING GSD2 over temperature GSD1 is reporting an over temperature condition GSD2 is reporting an over 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 SERVICE GSD2 needs service Return unit for repair GSD2 is reporting an internal error condition The GSD may still be usable 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 112 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN GEA 71 MESSAGE ADVISORIES
29. 131 Telephone 67 Temperature oil 5 Terrain 56 58 94 95 108 124 135 Thrust rating 6 Tilt line 60 Timer 2 119 Topographical data 124 135 Traffic 51 53 55 135 Traffic Advisory 53 54 Traffic map page 53 55 56 Transponder 21 22 128 129 130 131 132 Trim Indicator 5 11 81 V Vertical speed guidance 32 VNV 29 83 121 Voltmeter battery 5 Vspeed 2 W WAAS 110 WATCH 62 Weather Attenuated Color Highlight 62 Weather data link page 51 Weather radar 60 Wi Fi 69 70 71 72 Wind data 127 X XM lightning 124 135 XM weather 51 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Index Index 3 sjuauimasu sub saunqea4 uepjoay 2 Buruuejg AEN Sd 24V oipny uadx Jeuonippy paezey L L ulo2 AEN uoneiedo Jeuuouqy Sue v unuuy GARMIN Index Sjueuinijsu 3 5973 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy mu 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Index 4 A GARMIN im Garmin International Inc j 1200 Fast 151st Street a _ Olathe KS 66062 U S A p 913 397 8200 f 91 WEE Tt aa o 2345 Turner Road SE tendens OR 97302 USA 1 2009 Garmin Ltd or its subsidiaries 1
30. 52 2 AEN 540 nubi uonesado saunyea4 aoueplony Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 34 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint For flight plan leg planning a b o d Select the FPL Softkey at the bottom of the display Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to
31. 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 54 Traffic Symbol Description System Test 1 2 3 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00
32. Fire Shutoff valve was commanded to dose but failed to close BPTI DP 2 Fire Shutoff valve was commanded to close but failed to close BEIC Aircraft is flying in icing conditions BESTE Landing gear weight on wheels system failure BP T FD configuration error Het with the MFD MD over temperature Oxygen system pressure low E Parking brake not released BEZ OSA TES Cabin altitude high and passenger oxygen system pressure low PERC a CHE F 1 configuration error BPE a CHEN F 2 configuration error PRN F it with PFD 1 PPA PFD 2 OVHT Do 1 over temperature PFD2OVHT Do 2 over temperature BEES P ressurization controller failure BET EZ Loss of backup pitch trim actuator PTRIMNML FAIL o of normally operating pitch trim actuator Stall Warning amp Protection System pusher has failed MEH NN Stall Warning Pusher is off B Spring Loaded Rudder Booster uncommanded actuation ailure of standby heate Warning amp Protection System inoperative Warning amp Protection System activation angles anticipated to servative settings Warning amp Protection System has not been tested Traffic amp Collision Avoidance System failure TCASII installations only Windshield 1 heater failure Windshield 2 heater failure Loss of yaw damper function in yaw axis when YD is engaged ca r Z2 F C
33. ME Pitch slip clutch maintenance test passed ene d CO Pitch slip clutch maintenance test in progress ene b Roll slip clutch maintenance test passed ene iC Roll slip clutch maintenance test in progress eure BS Yaw slip clutch maintenance test passed AVTA OCE Yaw slip clutch maintenance test in progress DC BUS 1 OFF JjDCbus 1 offline BUS 2 OFF DC bus 2 offline DOORR OP Refueling door is open Chip detected by engine 1 oil chip detector SA aa Chip detected by engine 2 oil chip detector ADEC fault in engine 1 3A 2e ADEC fault in engine 2 NUM M Engine 1 oil filter impending bypass set AM M 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 91 Sonjeoj Seinpexojd Puluueld ARN SdD S24V oipny uadx sva Sjueumajsul 2 nubi uio AeN qb jeuonippy uoneiedo Jeuuouqy b PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix m Annunciations amp Alerts A GARMIN Message Description A Electrical system fault EMER BUS
34. Prodigy Aural Alerts Flight Plan Import Export Messages MFD amp PFD Message Advisories ssssssse Database Message Advisories GMA 1347D Message Advisories GIA 63W Message Advisories sss GSD 41 Message Advisories sss 2 GEA 71 Message Advisories GTX 33 33D Message 5 5 sss 3 GRS 77 Message Advisories 4 GMU 44 Message Advisories GSR 56 Message Advisories sssssssseeeen enn 6 GDL 59 Message Advisories 6 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 l Table of Contents GARMIN GDL 69A Message Advisories sssssseene 117 GWX 68 Alert Messages nnne 117 GCU 477 Message Advisories sssssssssee ne 118 GMC 715 Message Advisories sssssssseene 118 Miscellaneous Message 501165 sss 119 APPENDIX 1 PFD Softkey Map 1 MED Softkey Map nennen 133 Dual Navigation Databases 136 Automatic Database Synchronization 137 INDEX Index 1 iv Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING ST
35. Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 5 AEN 540 S24V orpnyyuqax svi siu umnnsul Tuo2 AEN fid Duruue d nubi aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 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 Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to
36. 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 Tum 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 4 sjuauimasu nubi olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uonesado saunyea4 aoueplony Junuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 6 7 8 9 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway 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 2 3
37. The percentage of change i the day night crossover point based on backlighting intensity 7 Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY S AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check flygarmin 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 AOPA airport information is displayed on the right half of the display SATELLITE TELEPHONE COMMUNICATION OPTIONAL NOTE Separate accounts must be established to access the Iridium satellite network for voice and low speed data transmission and high speed data transmission for the maintenance reports 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 AUXILIARY COMMUNICATIONS 3 If necessary select the TEL Softkey to display the AUX TELEPHONE Page Answering a 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Fligh
38. a desired point on the map and select the SHW CHRT Softkey 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 Select the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart will be displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN _ Additional Features 6 In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob
39. and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The system should be serviced The MFD and PFDs have different software versions installed The system should be serviced Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The system should be serv
40. and press the ENT Key 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 45 sjuauimnasu UATE olpny uqax wi0 gt AeN 52 2 4 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index A Flight Planning GARMIN GRAPHICAL FLIGHT PLAN CREATION 1 2 3 4 5 Press the FPL Key to display the Active Flight Plan Page on the MFD 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 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 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 To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 1 2 3 4 5 6 7 46 Insert
41. available with active leg CDI Cycles through GPS VORI 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 optional sunnuunnummmmn Press the BACK Softkey to return to the top level softkeys Mux Selecting BACK returns to the previous softkey level A TeerTser TseeT ss 75 IN EESHHEHUHU Uu mmm nmn 74 Transponder Softkeys XPDR Displays transponder mode selection softkeys XPDRI Selects the 1 transponder as active optional XPDR2 Selects the 2 transponder as active optional STBY Selects Standby Mode transponder does not reply to any interrogations ON Selects Mode A transponder replies to identification interrogations 128 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN ALT GND VFR CODE 0 7 BKSP IDENT TMR REF NRST MSG Appendix Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Not available with TCAS II option Automatically enters the VFR code 1200 in the U S A only Not available when TCAS II option is installed Displays transponder code s
42. below the aircraft Typically used during climb phase of flight NORMAL 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 BELOW 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 UNREST unrestricted All traffic is displayed 3 To return to the Traffic Page select the BACK Softkey 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 55 AEN Sd5 52 44 0105 AEN Duruue d ni aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Displaying Traffic on the Navigation Map 1 2 Ensure TCAS system is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS A Optional 56 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 g
43. or the card may have been removed prematurely 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 sjuauimasu nubi sainqea4 s mp oold Buruue d AEN Sd5 2 444 paezey 3461 UI05 AeN jeuonippy uoneiedo Jeuuouqy 75 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD
44. reverted to pitch or roll default Vertical track mode High Speed Maximum operating speed exceeded Landing Gear Warning Gear up in landing condition Minimums The aircraft has descended below the preset minimums barometric minimum descent altitude No Takeoff Brake No Takeoff Configuration due to brake status No Takeoff Flaps No Takeoff Configuration due to flap status No Takeoff Spoilers No Takeoff Configuration due to spoiler status No Takeoff Trim No Takeoff Configuration due to trim status Rudder Overboost Rudder Booster system uncommanded actuation Stall Stall Airplane in stall condition Timer Expired Countdown timer on the PFD has reached zero Thrust Thrust CSC disengaged abno s Aircraft has deviated 200 feet of the selected Altitude altitude uni The Traffic Information Service TIS has issued a Traffic Traffic Advisory Advisory alert Trim Trim Trim Trim switch malfunction The aircraft is one minute from Top of Descent Issued igation is enabled ab only when vertical n V Aural Warning OK Aural Warning One Channel Incoming Call SelCal Takeoff OK TIS not available Status Aural warning system test passes channel Aural warning system test detects failure in one Satellite telephone is receiving a call Incoming communicati on thr
45. 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 76 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A Additional Features 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 selecting the EXIT Softkey the system will return to the last selected checklist item Immediately Accessing Emergency Procedures 1 From any
46. speed constraints The system automatically transitions to the next vertical waypoint 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 VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid 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 NO WGS84 WPT Non WGS 84 waypoint for navigation xxxx The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources TRAFFIC FAIL Traffic device has failed The system is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU GSD 41 GDL 69 or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may diff
47. 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 Ifa 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 24 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN 465 AUTOMATIC FLIGHT CONTROL SYSTEM A 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 A 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
48. the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Antenna Stabilization 1 2 To activate or deactivate the antenna stabilization select the MODE Softkey 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 Soltkey 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 62 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoi
49. the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the Prodigy system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the Prodigy Flight Deck 300 Pilot s Guide 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 amp Warnings tauuens SMotes GARMIN Blank Page Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Change Summary Revision pate of Revision atfected Pages 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 RR 1 Record of Revisions Ss GARMIN Blank Page RR 2 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN table of Contents FLIGHT INSTRUMENTS atrii ttl tte atit 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure sssssssse 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure Settings 5 1 Synchronize CD isis sich uei orina a e HER Change Navigation Sources Enab
50. the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints 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 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name 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 11 12 13 14 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 37 sjuauimasu sub oipny uddx UI0JNeN 52 s mp oold Duiuue d AEN Sd5 fila uoneiado SoJnjeaJ aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A N
51. turns red inverse video white text on red background A and B 2 Flaps have failed or become jammed Flap pointer turns yellow and readout turns yellow inverse video black text on yellow background C e 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 FLAPS A Flaps Retracted B Flaps at FULL C Flaps Failed D Flaps Unavailable at Takeoff Landing Position at Takeoff 80 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Abnormal operation 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 Aileron Mistrim T Rudder YAH Mistrim B Pitch Trim A Mistrim 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 Manua
52. 0105 AEN 52 2 4 AEN 540 nubi sual uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 7 8 9 A GARMIN 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 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER 36 1 2 3 4 5 6 7 8 9 10 WAYPOINTS Turn the large FMS Knob on the Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key
53. 17LcPs LPY 259 18 8NH 3 3NH 3 2NM 3 9NM RW17L map 76 5 3NM 930FT 8NM POLKE SIUE Cross AT or ABOVE 5 000 fi Facing Cross AT 2 300 ft ICI Cross AT or BELOW 3 000 ft 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Large Whi Text e Large Light Blue Tex cea zd mall Lig Blue Tex S 7 t Blue Subdued Text Small VVhite Text with Altitude Restriction Bar Sjueuingjsu Yid sva oipny uadx 010 AEN suey uoneiedo sainjea4 aoueploay 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey Wfl x pu ddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EAS Procedures Appendix Alerts Operation Features Index GPS Navigation GARMIN 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
54. 90 00761 00 Rev A
55. A GARMIN Embraer Prodigy Flight Deck 300 Cockpit Reference Guide Embraer Phenom 300 Copyright 2009 Garmin Ltd or its subsidiaries All rights reserved This Phen in thi manual reflects the operation of System Software version 0734 23 or later for the Embraer om 300 Some differences in operation may be observed when comparing the information s manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 5 Garmi Sout i Garm Tel 8 Web 03 391 3411 Fax 503 364 2138 n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park ampton 5040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 in Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan 86 02 2642 9199 Fax 886 02 2642 9099 For after hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 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 down othe or p
56. ANDARD 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 Tum 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 1 Sue v uoneiado SoJnjeaJ aoueplony 2 Fuluueld AEN Sd5 2 oipny uadx svi yunuuy jeuuouqy jeuonippy paezey xipuaddy x pul uo2 AEN n Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Flight Instruments A GARMIN CHANG
57. AP optional optional n rv EY FX FX rv ExcseT ue T GO ecs T see rum oro Excunf sex EY FN EY F3 EN ES ES 7 TO Sa Sa T soT TsoFT T 1L I Ree esq 31 EY EY ES EY EY EN XY ES EN S NS cow es Toar L oari TerRon krnorrl TeccePT ex F3 VFV V3 F3 V3 V3 V3 V3 ES VS D SYSTEM Softkeys SYSTEM Accesses EIS 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 f 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 ATRON 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 ACCEPT Confirms the selected takeoff settings BACK Returns display to previous softkey level 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 133 SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN SdD 2 oipny uadx svi Sjueunasu paezey U105 AEN jeuonippy uoneiedo Jeuuouqy SHO unuuy gt 5 o 3
58. ATE 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 saunqea4 jeuonippy sue v unuuy RATE 127006 xipuaddy DELTA P PSI x pul Cabin Leak Indication 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 79 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operations GARMIN Excessive cabin differential pressure DELTA P causes the pressure readout to dis play 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
59. BSR aia Du 1 temperature over specified safe value BSA sila uc 2 temperature over specified safe value BESSER Engine 1 responds slowly or not at all to thrust commands 88 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A 5 GARMIN Amunciations amp Alerts Message Description Engine 2 responds slowly or not at all to thrust commands Uncommanded shutdown detected for engine 1 Uncommanded shutdown detected for engine 2 Fire detection system failure in engine 1 E2 FIREDET FAIL detection system failure in engine 2 Fire extinguisher failure in engine 1 z n ee ire extinguisher failure in engine 2 MHMHUNU F filter impending bypass condition for engine 1 BESEUSI TET cue filter impending bypass condition for engine 2 MH hust Lever Angle failure for engine 1 H TR Thrust Lever Angle failure for engine 2 BEST eater failure in engine 1 BEST eater failure in engine 2 BEES TUE c k inside E Bay ectrical bay over temperature ow control valve monitor for ECS 1 detected improper valve operation ow control valve monitor for ECS 2 detected improper valve operation Baa Red ai Few emergency brake functions available BESSER Emergency lights switch not in ARMED position BST e Limit exceeded in engine s during f
60. DIATE CLOSED O Cockpit Temperature Setting Crossbleed Valve Status XBV Cabin Temperature Setting 10 Cabin Duct Temperature Setting 0 Ram Air Valve RAV 2 Heat Exchanger Cooling Pach Circuit 77 Control System Valve 3 7 onmental Control System Valve G bdo Duct Temperature Setting u m Cabin Temperature 5 77 Regulating Shutoff Valve PRSOV 5 Cabin Evaporator Fan O Vapor Cycle System VCS Actual Cockpit Temperature Outflow Valve OFV Status 2 Cockpit Evaporator Fan 2 Pressure Regulating Shutoff Valve PRSOV 2 Environmental Control System Synoptics Page Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Engine amp Airframe Systems Unit Icons and Descriptions Fan Heat Exchanger Vapor Cycle System ECS Valve Ram Air Valve Open with flow Open no flow Pressure Regulating Shutoff Valve PRSOV Crossbleed Valve XBV Open with flow Open no flow Environmental Control System Unit Status Indications 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 o Closed Closed sjueumansu sual uonesado s n e 4 eouepioAy SoJnpa20Jd Buruue d AEN Sd5 yi oipny uddx junuuy jeuuouqy feuonippv xipuaddy x pul 3 JU105 AEN nu paezey Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav A
61. E NAVIGATION SOURCES 1 2 3 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 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 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 Tum 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 2 3 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob
62. EW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 38 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key 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 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key 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 smal
63. Engine amp Airframe Systems Indication Description Landing Gear Down Landing Gear Up Landing Gear Transitioning Normal Landing Gear Locked Down Landing Gear Locked Up Landing Gear Transitioning Abnormal Landing Gear Position Indications Indication Description Invalid information Spoilers not in takeoff SPDBRK 25 configuration Spoiler failed to deploy Spoiler retracted Ground spoiler deployed Speedbrakes deployed Spoiler Indications 10 Cockpit Reference Guide for the Prodigy Flight Deck 300 A GARMIN 190 00761 00 Rev A A Al ram Systems Flaps and Trim SYNOPTICS mm ENG 2 SHORT DISPATCH 1270 pst Flight ID 5 Oxygen Static Air Temperature SAT G Emergency Brake Accumulator Pressure 0 Total Air Temperature TAT Door Status True Airspeed TAS 2 Electrical Status G Engine Dispatch Message Box Hydraulic Pressure System Status Synoptics Page 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 11 Sjueunasu x v 2 Suelv uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui z t s a TL GARMIN Environmental Control System ECS SET ACTUAL 25 1 TTF TEMPERATURE EVAP 25 C 2570 OPEN INTERME
64. FCS XPDR Audio EAS Instruments Appendix Index Engine amp Airframe Systems Electrical Battery GEN 1 GPU CONNECTED Ground Power Uni Electrical Synoptics Page 14 Cockpit Reference Guide for the Prodigy Flight Deck 300 A GARMIN 190 00761 00 Rev A GARMIN Systems Unit Icons and Descriptions 2 5g om Generator N2 gt 52 Bus off N2 lt 52 Bus 82 Bus off ES Hot Bus Normal Abnormal d Battery m 3 Normal Abnormal s Electrical System Unit Status Indications suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 15 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Engine amp Airframe Systems A GARMIN t Engine Feed Line t Tank Fuel Quantity t Feed Ejector Fuel Total Fuel 2 Fuel Transfer SOV Fuel Used Rig 0 Left Feed Ejector 10 RH Pressure Switch 2 Left DC Pump 12 Fuel 250v 5 Left Tanh Fuel Quantity 3 Rig 6 Fuel 1 SOV Right DC Pump LH Pressure Switch 5 Rig Left Engine Feed Line Fuel Synoptics Page Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Unit
65. Flight plan waypoint is locked FPL WPT MOVE Flight plan waypoint moved 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 Or update the waypoint name identifier to reflect the new information 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 TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired 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 FPL TRUNC F
66. GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 have an error in the aud configuration The system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature io GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 saunqea4 uepjoay seinpa2o0Jd Buruuejg AEN 5640 S24V oipny uadx sv3 syu unysu paezey ETSI Juo ney Wil jeuonippy uoneiedo Jeuuouqy PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix eu Annunciations 8 Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message Comments GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted AGIA mismatch has been detected where only one is WAAS capable MANIFEST GIA1 software
67. Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Displaying Pathways 1 2 3 4 5 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 Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the PATHWAY Softkey Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 2 3 4 5 Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the HRZN HDG Softkey Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 2 3 4 5 64 Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the APTSIGNS Softkey Press the BACK Softkey to return to the previous page Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Md itinal Features TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or Fl
68. O GPS POSITION annunciation on the map and the system stops navigating in GPS Mode xipuaddy 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 x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 83 Nav Com XPDR Audio Hazard Avoidance Additional Flight Instruments Flight Planning EAS AFCS Procedures GPS Nav Features Annun Appendix Alerts Index Abnormal Operation GARMI N prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the system in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function 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 th
69. OFF Emergency bus OFF SG Engine fire extinguisher discharge aM TEAM Haps not available FUELEQUAL 5 quantity asymmetry corrected XFEED SOV is open FUEL 1 FEED FAULT l FUEL 2 FEED FAULT fi FUELTPSWFAIL l C pump on due to low fuel pressure C pump on due to low fuel pressure el pressure switch stuck in high position aU PA ANE Fuel pressure switch stuck in high position FUEL PUMP 1 FAIL K om pump 1 failure A F el pump 2 failure GEA 1 FAIL Failure of GEA 1 GEA 2 FAIL Failure of GEA 2 GEA 3 FAIL Failure of GEA 3 PU CO JM Ground power unit connected to the aircraft GSD 1 FAIL GSD 1 non communicative RALT FAIL Radar altitude failure SHED BUS OFF Shed bus off S US BET Speed brake swi SPOILER FAULT Loss of roll spoi UL d2 NEM Stall Warning System activation angles anticipated due to icing conditions GSD 2 FAIL GSD 2 non communicative B FA A LRU has stopped communicating over an HSDB BA ON HSDB switch in reversionary position PA Degradation of hydraulic system available power ICE DET FAIL Ice Detector failure MFD FAN FAIL Failure of MFD fan AX A EA EOM Oxygen system switch in manual mode ua A Y Failure of PFD 1 fan ua PRA Y NN Failure of PFD 2 fan MEER M Pitch trim is being actuated in low rate BST P Failure of pilot pitch trim switch
70. 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 30 1 2 3 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 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 With Activate highlighted press the ENT Key Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN 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 GPS Navigation 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 ACTIVE FLIGHT PLAN 2217 11 7NM COVIE 221 9 QNM LEMYN 220 8 0NH Approach KDFW RNAY
71. RAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN ME Rate Caution NCR 98 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts TAWS B System Status Annunciations PFD MFD MFD Alert Type TAWS B Page TAWS B Page Aural Message Annunciation Annunciation System Test in Progress TAWS TEST 222 System Test Pass None None TAWS System Test OK TAWS B System Test Fail TAWS System Failure Terrain or Obstacle database unavailable or nvalid invalid software configuration system audio fault TAWS System Failure 0 GPS position TAWS Not Available Excessively degraded GPS gnal Out of database None TAWS Not Available 5 coverage area 5 ufficient GPS signal received after loss None TAWS Available 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 99 SaJnjeoJ 2 Duruue d AEN Sd5 S24JV olpny uqax sv sjuauimasu 2 nubi u102 AEN Yid jeuonippy uoneiedo Jeuuouqy Ins PE x pul Annunciations amp Alerts A GARMIN 2 TCAS Il ANNUNCIATION
72. Rev A GARMIN Hazard avoidance 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 FA L appears on the PFD In addition a visual annunciation FAIL appears in the Operating Mode box on the Traffic Map Sjueuingjsu 3 SV3 Page Displaying Traffic on the Traffic Map Page 1 Tum 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 counter clockwise 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 ABOVE Displays non threat and proximity traffic from 9900 feet above the aircraft to 2700 feet
73. S 5 as 2 PFD Mode MFD Traffic Traffic Display Mode Annunciation Map Page Mode Status Icon 9 Annunciation Other Maps 2 TCASII Self test Initiated TEST MODE also 8 TEST None shown in white on top 24 2 center of page Traffic Advisory and 9 Resolution Advisory TA None RA Traffic Advisory Only TA only TA ONLY or E TCAS II Standby Be 28 TFC STBY TCAS STBY also shown in white in x center of page TCAS I Failed TCAS FAIL xt E Annunciation appears yellow while in flight 25 TCASIIFailure Annunciations 32 Traffic Map Page Annunciation Abnormal Operation Index Appendix Ea Description Data is not being received from the TCAS II unit Data is being received from the TCAS II unit but the unit is self reporting a failure Incorrect data format received from the TCAS II unit Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Amnunciations amp Alerts TCAS II Status Annunciations siu uinnsu UATE Traffic Status Banner Annunciation Description A Resolution Advisory is outside the selected display range Annunciation is removed when traffic comes within the selected display range A Traffic Advisory is outside the selected display range Annunciation is removed when traffic comes within the selected display range olpny uadX JUI05 AEN 52 System
74. VISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database error exists Comments The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU
75. 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 7 sjuauimnasu UATE uonesado s n e 4 s mp oold Buruue d AEN Sd5 S24JV oipny uddx junuuy jeuuouqy Jeuonippy paezey ETSI xipuaddy x pul Flight Instruments k s l Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Engine amp Airframe Systems A GARMIN Takeoff Data Set Window TAKEOFF DATA SET OAT 19 C ATR ON Takeoff Data Set Window Setting the Outside Air Temperature OAT 1 2 3 4 5 Select the SYSTEM Softkey Select the ENG SET Softkey to display the Takeoff Data Set Window To adjust the temperature in 1 C increments use the OAT4 and OAT softkeys If desired change the ATR status while the Takeoff Data Set Window is displayed 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 I
76. akers 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 sides 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 COMI and NAVI 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 correspondin
77. ata 3 Press the ENT Key Inhibiting Enabling FLTA and PDA Alerting 1 Select the TAWS A Page 2 Select the TAWS INH Softkey to inhibit or enable TAWS A choice dependent on current state Black Overriding Flaps based FIT Alerting 1 Select the TAWS A Page 2 Select the FLAP OVR Softkey Inhibiting Enabling GPWS Alerting 1 Select the TAWS A Page 2 Select the GPWS INH Softkey to inhibit or enable GPWS alerts choice dependent on current state Inhibiting Enabling GSD Alerting A 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 57 ACN 540 S24V oipny duadx Sv3 s u u nnsul u102 AEN Duruue d ni s mp oold paezey spay uoneiedo s m junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index A Hazard Avoidance 0 GARMIN TAWS B 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 s
78. ate the cursor 4 Tur 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 39 sjuauimasu sub olpny uqax 0105 AEN 52 2 4 AEN 540 nubi sual uonesado saunyea4 e uepioAy unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A NEW FLIGHT PLAN 40 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Using the MFD 1 Press the FPL Key 2 Turn the small FMS Knob to display the Flight Plan Catalog Page 3 Selectthe NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of the departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint 8
79. aypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 2 Duruue d AEN Sd5 Juil aoueplony paezey s D wu jeuonippy xipueddy suelv junuuy x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 85 GARMIN Abnormal Operation Sjueuinijsu fila Sv3 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy suay yunuuy xipuaddy x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 86 GARMI N n n ANNUNCIATIONS amp 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 Bets oke detected in baggage compartment BESTES Cabin altitude pressure altitude high BESSER Emergency door open Bee IS Passenger door open 22 in engine 1 M H in engine 2 Low oil pressure in engine 1 Low oil pressure in engine 2 1491117 1919 Ml Generators offline Generators offline and electrical emergency transfer has failed Low fuel level in tank 1 Low fuel level in tank 2 Landing gear position and control lever disagreement o takeoff configuration Caution Messages See the A
80. cannot determine bearing of Resolution Advisory Annunciation indicates distance in nm altitude separation in hundreds of feet and altitude trend arrow climbing descending AEN Sd5 System cannot determine bearing of Traffic Advisory Annunciation indicates distance in nm altitude separation in hundreds of feet and altitude trend arrow climbing descending Duruue d TCAS II unit has failed unit is self reporting a failure or sending incorrectly formatted data Data is not being received from the TCAS II unit saunpa20Jd Shown as symbol on Traffic Map Page Shown in center of Traffic Map Page eouepioAy paezey saunyea4 jeuonippy uoneiedo Jeuuouqy gt o 2 x x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 101 Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix bees Annunciations amp Alerts OTHER PRODIGY AURAL ALERTS A GARMIN Flight Director Message Priority Description Warning Autopilot is disengaged Autopilot Sing e alert for manual AP aisengagement Continuous alert for automatic AP disengagement cancelled with AP DISC Switch Cabin High cabin altitude Fire Fire Engine fire Flight director has
81. cussed 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 make the call 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 Tum the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select AUXILIARY COMMUNICATIONS 3 If necessary select the WI FI Softkey to display the AUX VVI H SETUP Page 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 69 sjuaumasu UATE xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 52 olpny uqax unuuy Jeuuouqy Jeuonippy paezey U10 AEN x pul Nav Com XPDR Audio Hazard Avoidance Additional Features Abnormal Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 70 A GARMIN Setting Up a New Wi Fi Connection 1 2 3 4 5 6 7 8 9 10 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 requirements and whether the network has been saved in the system s memory If necessary select the RESCAN Softkey to have the system scan again for available n
82. dance SVS 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 System SVS functionality is offered as an optional enhancement to the Prodigy Flight Deck 300 SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS 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 SVS enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 63 2 Buruuejd AeN Sd5 S24V olpny uqax sva siu u nnsul Wfl Tu102 AEN fil eouepioAy paezey s m e q jeuonippy xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments
83. due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating entered by the pilot use this altitude in the altitude of the Altitude is designated determining vertical aircraft as it passes for use in giving flight path guidance over the navigation vertical flight path point This altitude guidance Altitude is provided as a does not match the reference and is not published altitude in designated to be used navigation database or in determining vertical no published altitude flight path guidance exists Small Text Altitude is not Altitude is designated 1 The system cannot designated to be used for use in giving vertical use this altitude in in determining vertical flight path guidance determining vertical flight path guidance Altitude has been flight path guidance Altitude has been etrieved from the retrieved from the navigation database navigation database or has been entered by and is provided as a the pilot and matches eference a published altitude in the navigation database 32 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN WEIGHT PLANNING Flight Planning FLIGHT PLANNING All procedures apply to the MFD unless other
84. election soft keys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Messages Window 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 129 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax sv sjuaumasu jeuonippy nubi JUI0 NEN uoneiedo Jeuuouqy Sue v unuuy k Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Index Appendi X A GARMIN PIN Le 2 3s s s L J sss T back Er Tes yarasa Ter TT Te nnnnnnn os cow ARES nnnnnnnnnnnun JI 99 JE Tar osa TT I8 E88 nnnnnnnnnnnun Press the BACK Softkey to return to the top level nnm Selecting BACK returns to the previous softkey level Selecting BACK returns to the previous softkey level Selecting BACK returns to the previous softkey level Selecting BACK returns to the previous softkey level FI VV V nnnm n nn on un Transponder Traffic Softkeys with TCAS II Option XPDR TFC XPDRI XPDR2 MODE Cockpit Reference Guide for the Prodigy Flight Deck 300 STBY Dis
85. en with flow no flow syu wnysu Suelv uoneiedo soinjeo4 9e2uepioAy s mp old buluueld ACN 540 S24V olpny uqax junuuy jeuuouqy jeuonippy xipuaddy x pul iui JUI05 AEN TL paezey GARMIN Engine amp Airframe Systems Sjueuinijsu fila oipny uadx U105 AEN S2dV AeN Sd5 buruue d qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 20 A GARMIN NAV COM TRANSPONDER AUDIO PANEL Nav Com XPDR 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 Tum 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 a
86. enetrate 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 APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required 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 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 PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF 120 Cockpit Reference Guide for the Prodigy Flight Deck 300 IAF waypoint for parallel offset has been passed 190 00761 00 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message UNABLE V WPT Can t reach current vertical waypoint Comments The current vertical waypoint can not be reached within the maximum flight path angle and vertical
87. 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 Il Option 1 Press the XPDR Softkey 2 Ifthe 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 ALT or GND 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 COM 1 COM2 or COM3 Key HF if installed on the audio panel 22 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Nav Com XPDR Audio Panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VORT 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 Turn the respective tuning
88. er from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 121 sjuaumnasu sub s m s mp oold Buruue d AEN Sd5 yi oipny uadx paezey 3461 u102 AEN jeuonippy uoneiedo Jeuuouqy IBN PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Annunciations 8 Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message SVS SVS DISABLED Terrain DB resolution too low Comments Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOCI 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 PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from t
89. erence Guide for the Prodigy Flight Deck 300 15 sjuaumasu Yid xipueddy suelv uoneiedo sainyea4 aoueplony SoJnpa204d Duruue d AEN Sd5 52 olpny uqax unuuy Jeuuouqy jeuonippy paezey nu U10 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 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 e Light Blue Items not selected or Gray General notes checked White Item is selected Yellow Caution notes Red Warning notes 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
90. ersions 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 DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database installed Install correct obstacle database in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstade databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347D MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative GMA XTALK GMA crosstalk error has occurred The audio panel self test has detected a failure The audio panel is unavailable The system should be serviced An error has occurred in transferring data between the two GMAs The system should be serviced Cockpit Reference Guide f
91. etworks Press the FMS Knob to place the cursor in the list of networks Turn either FMS Knob to select the desired network Select the CONNECT Softkey If the network is secured a window will be displayed in order to enter the necessary passcode Enter alpha numberic characters using the keypad Select the CAP LOCK Softkey to enter upper case letters If there is no security associated with the network proceed to step 9 Press the ENT Key OK will be highlighted Press the ENT Key again The SAVE SETTINGS window is now displayed with the cursor highlighting SAVE CONNECTION 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Additional Features Editing a Saved Network 1 While viewing list of saved n
92. etworks 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 sjuauimasu sub xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 52 olpny uqax unuuy Jeuuouqy jeuonippy paezey TL U10 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation
93. g GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Lees Appendix Index Inhibit 59 Inhibit TAWS 59 Inset Map 124 nterstage Turbine Temperature ITT 5 79 101 94 95 98 Iridium 67 68 69 J Jeppesen 65 L Landing gear status 5 9 M Maintenance reports 67 Map panning 52 Message advisories 104 112 114 115 116 118 122 METAR 51 Minimum Anti Ice N1Bug 6 MISCOMP 93 Mode 5 129 Multi Function Display MFD Softkeys 133 N N1 gauge 79 N1 Transient Limit 6 NACO 65 NAV 23 NAV1 2 23 NAV2 2 23 Navigation database 31 32 103 105 108 119 136 Netvvork 67 69 70 71 NEXRAD 51 52 124 135 ndex 2 Cockpit Reference Guide for the Prodigy Flight Deck 300 A GARMIN 0 085 2 Obstacles 108 110 Oil engine 5 Outside Air Temperature 0AT 8 Overspeed Protection 26 P Pathways 63 64 PIT 93 Power up page 76 Pressure oil 5 Pressurization 9 R Resolution Advisory 54 64 Reversionary mode 81 ROC 94 95 98 S SafeTaxi amp 63 65 Sector scan 62 Secure Digital SD card 76 Sensor 93 Spoiler status 5 9 STAB 62 Standby 60 Store Flight Plan 44 SVS 63 121 122 Synchronization 137 138 Synoptics 11 18 Synthetic Vision System 63 T TAF 51 TAS 114 TAWS 56 59 94 96 98 99 190 00761 00 Rev A A GARMIN TAWS A 56 57 94 96 97 99 124 135 TAWS B 56 58 TCAS Il 22 53 54 56 64 124 129 130
94. g softkeys are disabled when the aircraft experiences unusual attitudes 82 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Traffic Annunciations System Time Abnormal Operation Glideslope Glide AFCS Annunciations PFD Setup Menu path and Vertical 52 Flight Director Windows displayed in Deviation Indicators 5 Command Bars the lower right corner Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude g Window Flight Plan 3 5 VVind Data Messages Selected Heading Box Procedures Selected Course Box ADF DME Tuning 8 Transponder Status Barometric Minimum Box Descent Altitude Box AEN Sd5 Duruue d nubi SeJnpa20Jd Extreme Pitch Indication aoueplony paezey DEAD RECKONING gt of EXES go os vD 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 aircrafts current estimated position Sue v unuuy 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 N
95. gain 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 Tum the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 5 If two DMEs are installed press the AUX Key on the desired audio panel to monitor DME2 audio 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 sjueumansu S24V oipny 4ddX sva JUI05 AEN Sue v uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN Sd5 yunuuy jeuuouqy jeuonippy paezey xipuaddy x pul T L TE Wfl Flight Instruments Nav Com AFCS XPDR Audio EAS Abnormal Additional Hazard Flight Planning Annun GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey XPDR TFC if the TCAS II option is available 2 Ifthe 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
96. h PFDs are displaying data from the number one GPS receiver Both PFDs are displaying data from the number two GPS receiver iz FD2 is displaying data from the 1 Air Data Computer iz FD1 is displaying data from the 2 Air Data Computer W FD1 or PFD2 is displaying data from the standby air data input FD2 is displaying data from the 1 AHRS FD1 is displaying data from the 2 AHRS W FD1 or PFD2 is displaying data from the standby attitude and heading eference input FD2 is displaying data from the 1 GPS W FD1 is displaying data from the 2 GPS gt gt gt m 2 un Alert Type PFD MFD TAWS A Page Annunciation MFD Map Page Pop Up Alert Aural Message Clearance Caution RTC Reduced Required Terrain PULL UP Terrain Terrain Pull Clearance Warning RTC Up Pull Up Imminent Terrain Impact PULL UP Terrain Terrain Pull Warning ITI Up Pull Up Reduced Required Obstacle UMM Obstacle Obstacle Clearance Warning ROC Pull Up Pull Up Imminent Obstacle Impact PULL UP Obstacle Obstacle Warning 101 Pull Up Pull Up Excessive Descent Rate PULL UP lt whoop gt lt whoop gt Warning EDR Pull Up Excessive Closure Rate PULL UP lt whoop gt lt whoop gt Warning ECR Pull Up Reduced Required Terrain TERRAIN CAUTION TERRAN Caution Terrai
97. he terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by the GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually ac
98. he 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 122 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A amp GARMIN o Appendix APPENDIX sjuauimasu wp PFD SOFTKEY MAP 5 3 optional r r m A r m or olpny uqax UI05 AeN CDI NAV1 52 Top Level PFD Softkeys AEN Sd5 optional n py v v m pm vi n n nom Duruue d Wil Select the BACK Softkey on this level to return to the top softkey level Least easi O 1 TT Mea EY IS NS HEMEN N 7 74 s snp old CAS Softkeys CAS Displays the scroll up and scroll down softkeys s CAS 1 Scroll up Displayed only when a sufficient number 5 of items are displayed in the Crew Alerting System d Display to warrant scrolling CAS 4 Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolli
99. ical data e g coastlines ter rain rivers lakes and elevation scale on Inset Map Displays terrain information on Inset Map not available with TAWS A Displays NEXRAD weather and coverage information on Inset Map optional feature Displays XM lightning information on Inset Map optional feature Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN optional CAS INSET SENSOR Prp oss ADFDME XPDR IDENT Fu V EF V3 V3 V3 V3 V3 V 93 S Press the BACK Softkey to return to the top level softkeys C CNO eS nez amen 1L ee J EY EY EY EY 7 NN KEN EN NS SENSOR Softkeys SENSOR Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer ADC2 Selects the 2 Air Data Computer ADCSTBY Selects standby air data input AHRSI Selects the 1 AHRS AHRS2 Selects the 42 AHRS ATTSTBY Selects standby AHRS input 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 125 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax sv sjuauimasu Jeuonippy nf Tuo2 NeN sub uoneiedo Jeuuouqy Suey unuuy k Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Index A Appendix 00887 GARMIN n nnmnnnannnnnu
100. iced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed 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 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 soJnjeoJ 2 Buruuejd AEN Sd 2 oipny uadx svi sjuawinasu paezey nubi u102 AEN nubi jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN DATABASE MESSAGE AD
101. ight Plan 41 Enter an Airway in a Flight Plan 42 Invert An Active Flight Plan 43 Remove a Departure Arrival Approach or Airway from a Flight Plan 43 Store a Flight Plan cerae ciet e 44 Edit a Stored Flight Plan 44 Delete a Waypoint from the Flight Plan ss 44 Invert and Activate a Stored Flight Plan 45 Copy a Flight Plan Delete a Flight Plan etc Graphical Flight Plan Creation Export a Flight Plan to an SD Card ssssssss 46 PROCEDURES LARLA a AA Rl E Load and Activate a Departure Procedure Activate A Departure Leg ssssssseeenennnnnnnnnn Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure sssssss 48 Activate An Approach in the Active Flight Plan 49 Activate a Vector to Final Approach Fix sss 49 Activate A Missed Approach in the Active Flight Plan 50 HAZARD AVOIDANCE o 51 Customizing the Hazard Displays on the Navigation 51 XM Weather Subscription 51 Traffic Information Service TIS s s s s s sensen 53 Traffic Collision Avoidance System TCAS II 54 Terrain Awareness
102. ing 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 AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match 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 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 GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid 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 GMU 44 MESSAGE ADVISORIES Message HDG FAULT AHRS1 magnetometer fault has occurred Commen
103. injea4 aoueplony sainpadold Duruue d unuuy Jeuuouqy Jeuonippy 2 xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude constraint 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 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired offset distance from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD or MFD Controller and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With
104. ional Features A GARMIN XM RADIO ENTERTAINMENT SUBSCRIPTION OPTIONAL 74 The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select XM Radio 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 2 3 Select the CATGRY Softkey on the XM Radio Page 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 Press the ENT Key Select an Available Channel within the Selected Category 1 2 3 While on the XM Radio Page select the CHNL Softkey 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 With the desired channel highligh
105. irplane Flight Manual AFM for recommended pilot actions Accompanied by a single chime tone which repeats until acknowledged Message Description ADS 1 offline or failed BEEN VIZ 5 2 offline or failed HEM Pitot heater 1 offline or heater element failed BE VEU Pitot heater 2 offline or heater element failed 5 1 620 AHRS 1 failure 5 2 221 ns 2 failure Sin d system failure in engine 1 MU i i system failure in engine 2 Not enough thermal energy available for WHSAIS Wing and Horizontal Stabilizer Anti ice System operation 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 87 sainjea4 SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax sv3 sjuauimasu 2 nubi uio AeN Yid jeuonippyv uoneiedo Jeuuouqy 5 x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional E 3 S 2 lt EAS AFCS GPS Nav Features Avoidance Procedures Operation Appendix Index Annunciations GARMIN Message Description Component failure AIV pressure transducers AMS Controller other 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 BE ENSE Beed hot air leakage at WHSAIS pneumatic ducting BSG TEFEN Pneu
106. iteCharts in electronic form it is still advisable 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 aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle 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 show
107. knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 2 Press the appropriate Frequency Transfer Key to place the frequency into the active frequency field Or 1 Press the COM or NAV Key on the Control Unit to select the desired COM or NAV frequency box 2 Turn the FMS Knob to tune the desired frequency large knob for MHz small knob for kHz 3 Press the Frequency Transfer Key to transfer the frequency to the active 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 23 sjuauimasu UATE 5 3 S24V oipny uddx JUI05 AEN sualy uonesado saunqea4 2 Buruuejg AEN Sd junuuy jeuuouqy jeuonippy paezey nubi xi
108. l 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Flight Planning 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 Tum 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 activ
109. l activation of reversionary display mode is accomplished by pressing the DISPLAY BACKUP Button on the appropriate audio panel PFDI By pressing the DISPLAY BACKUP Button on the left audio panel e MED 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 81 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sv3 sjueumasu puezey 34 Wo gt AeN 1461 saunyea4 Jeuonippy xipuaddy Sue v junuuy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN AUDIO PANEL FAIL SAFE OPERATION If there is a failure of both Audio Panels a fail safe circuit connects the pilots headset and microphone directly to the COMI transceiver and the copilot s headset directly to the COM2 transceiver Audio is not available on the spe
110. layed To exit the call select the HANGUP Softkey Making an External Call from the Cockpit Using the Iridium Satellite Network 1 Press the TEL Key on the appropriate audio panel 2 With the AUX Telephone Page displayed 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 Control Unit Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN _ Additional Features 6 Press the ENT Key OK is highlighted 7 Press the ENT Key The system will begin calling the number To exit the call select the HANGUP Softkey Placing a Call on Hold Select the HOLD Softkey on the MFD Select the HOLD Softkey again to resume the call Transferring a Call 1 Select the TRANS Softkey on the MFD 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 make the call Adding Another Phone to an Active Call 1 Select the CONF Softkey on the MFD 2 Press the ENT Key The cursor now highlights the phone number entry field 3 Enter the phone number as dis
111. le Disable OBS Mode While Navigating with 6 5 2 aeo non De HU Rm dad des GaGa 2 Configure Vspeed Bugs Individually sss Turn Vspeed Bugs On or Off by Category Set Barometric Radar Altimeter Optional Minimum Descent Altitude 3 Displaying Wind Data 3 ENGINE amp AIRFRAME SYSTEMS 5 Engine Indication System s s s s s s s s s iss s issss i 5 SYMOPUCS mme PE 11 NAV COM TRANSPONDER AUDIO PANEL 21 Enter or Change Flight ID 55 21 ADF Tuning 21 DIME T nlfij ien a nm m Gem OR IRE RR saz 21 Enter a Transponder Code L sss 22 Select Transponder Mode ss s s s sss s s sss s s sss ssss s ssis 22 Selecting a COM Radio seen 22 Selecting a NAV Radio 23 NAV COM Tuning 5 23 Iitercom oett rte te p e a bt er o eis 23 Passenger Address PA System 24 Clearance Recorder and Player 24
112. light ENG NO DISPATCH c detected no dispatch fault condition in engine s V No takeoff data entered of flaps deployment or retraction uel pressure low in engine 1 feed lin uel pressure low in engine 2 feed lin uel feed SOV 1 closed or unavailable uel feed SOV 2 closed or unavailable uel is imbalanced between the tanks BESTE SIE Disagreement between valve command and its feedback erator 1 offline erator 2 offline erator s overload erator start fault Failure of GIA Failure of GIA 2 GIA 1 over temperature GIA2OVHT s 2 over temperature BET o of ground spoilers s uawinajsu nubi orpnyyuqax JUI05 AEN 52 AEN 540 Duruue d nubi saunpa20Jd eouepioAy paezey D om saunyea4 Jeuonippy uoneiedo Jeuuouqy gt o 2 x x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 89 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard 9 5 lt E 3 S S lt EAS AFCS GPS Nav Procedures Avoidance o El u Operation Appendix Index Amundatons amp Alerts GARMIN Message Description Hydraulic temperature high BEES Hydraulic pressure low ED 1
113. light 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 119 sjuauimasu UTE sainqea4 SoJnpa20Jd Buruue d AEN Sd5 yi oipny sadx paezey 3461 UI05 AeN jeuonippy uoneiedo Jeuuouqy 5 D x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix end Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message LOCKED FPL Cannot navigate locked flight plan Comments 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 WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will p
114. m should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair MANIFEST GWX software mismatch communication halted A failure has been detected in the GWX 68 The GWX 68 may still be usable The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm soJnjeoJ 2 Buruuejg AEN 5640 24V oipny uadx svi sjuawinasu paezey nubi u102 NEN nubi jeuonippy uoneiedo Jeuuouqy Ins EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix poc Annunciations amp Alerts GCU 477 MESSAGE ADVISORIES A GARMIN Message GCU CNFG GCU Config error Config service req d Comments GCU 477 configu
115. matic sources and icing protection are not available MEHMET A BB An ti skid function lost main brake still available of AP function BE EGET Airplane mistrimmed in pitch axis when AP is engaged B ERIS B Airplane mistrimmed in roll axis when AP is engaged BENE Audio panel 1 is offline BE WEZ T Audio panel 2 is offline BENE EZ Aural warning system failure due to non communicating LRUs BAG Au pitch trim failure other pitch trim functions still available HE Baggage compartment smoke detector has failed BE WDR discharging under normal operation BETTE Battery 1 offline BE WERE 2 offline Gas di Battery voltage has exceeded 29 VDC BLEEDT FAIL eed 1 system not under control eed 2 system not under control eed 1 hot air leakage at some region of the ducting eed 2 hot air leakage at some region of the ducting ressure in bleed ducting is higher than an acceptable value chosen to ot compromise ECS and Anti ice components integrity essure in bleed ducting is higher than an acceptable value chosen to ot compromise ECS and Anti ice components integrity ain brake system lost BG PASAT NM cessive cabin pressure differential M min Slip clutch maintenance test failed BATT ONE Slip clutch maintenance test failed BEI IZ Slip clutch maintenance test failed BERE Master Configuration Module failed or non communicative IBN i Crew baggage door open Bb T Forward left hand baggage door open IO ES Forward right hand baggage door open
116. mum Anti Ice N1 Bug nterstage Turbine Temperature Engine High Pressure Compressor Speed Thrust Rating A Engine amp Airframe Systems GARMIN Thrust Rating Thrust Rating Max Speed NI for Thrust Rating Max Speed Current Speed control Arc NI Transient Limit ITT Steady State Limit ITTE NITT Transient Limit Ignition Status N2z OIL PRES PSI OIL TEMP C Engine Indications Indication 1 Thrust Rating Takeoff 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A amp GARMIN Engine amp Airframe Systems Or To choose the maximum climb thrust rating select the CLB Softkey 4 Select the BACK Softkey to return to the previous softkey level Automatic Thrust Reserve Indication Description ATR enabled in both engines ATR armed in both engines but inactive ATR activated in at least one engine in Take Off mode ATR 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
117. n Caution Terrain Ko 4 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts ie MFD Map Page Alert Type TAWS A Page Pop U Aural Message Annunciation x Imminent Terrain Impact TERRAIN TERRAIN Caution Terrain Caution ITI Caution Terrain Reduced Required Obstacle TERRAIN CAUTION OBSTACLE Caution Obstacle Clearance Caution ROC TERRAIN Caution Obstacle Imminent Obstacle Impact TERRAIN CAUTION OBSTACLE Caution Obstacle Caution 101 TERRAIN Caution Obstacle Premature Descent Alert TERRAIN 100 08 TERRAIN Too Low Terrain Caution PDA Excessive Descent Rate TERRAIN SKRE Sink Rate Caution EDR Excessive Closure Rate TERRAIN TERAN Terrain Terrain Caution ECR Negative Climb Rate TERRAIN DNTS Don t Sink Caution NCR Flight Into Terrain High TERRAIN 100 04 TERRAIN Too Low Terrain Speed Caution FIT TERRAIN Flight Into Terrain Gear TERRAIN Too Low Gear Caution FIT Flight Into Terrain Flaps TERRAIN FLAP Too Low Flaps Caution FIT Flight Into Terrain Takeoff TERRAIN 1 100 L TERRAIN Too Low Terrain Caution FIT Glide Slope Glide Path GLIDESLOPE eLroesLoe
118. n 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 Turn the small FMS Knob to highlight the desired flight plan for importing Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint Th new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 e oipny udax sva U105 AeN 52 2 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy
119. n the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO or optional RAD ALT 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 LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 49 sjuauimasu nubi svi olpny uqax 0105 AEN 52 AEN 540 buluueld ni s mp old uonesado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance
120. navigation database in each PFD and the MFD on the AUX System Status Page Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN 1 Appendix AUTOMATIC DATABASE SYNCHRONIZATION The automatic database synchronization feature automatically transfers the database from a single SD database card to the SD cards on each PFD and the MFD to ensure that all databases are synchronized throughout the system After power up the Prodigy system compares all copies of each applicable database If similar databases do not match the most recent valid database is automatically copied to each card in the system that does not already contain that database NOTE The 9 arc second terrain database may take as long as 100 minutes to synchronize using this method Therefore the user may want to transfer the data using a PC or connect the Prodigy system to a ground power source while performing the database synchronization Synchronizing Databases 1 2 3 4 5 6 7 8 9 10 11 12 Remove the MFD database card from the bottom card slot of the MFD Update the Garmin databases on the MFD card Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases an in progress message may be seen If this message is present wait fo
121. ndications Tank Fuel Quantity Fuel Temperature Engine Fuel Flow Total Fuel Quantity Electrical Display Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Bigine k al ram Systems Cabin Pressurization High Landing Field Elevation Pressure Altitude FT Pressure Change Rate Pressure Differential P PSI m Landing Field Elevation Oxygen System Pressure Wai psit 145U Ps1 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 3500 and 50 FT softkeys to set the desired elevation 4 Toconfirm the new LFE value select the ACCEPT Softkey Spoiler and Landing Gear Spoiler Status Main Landing Gear Left side Landing Gear Right side Landing Gear Spoiler and Landing Gear Indications 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 9 Sjueunasu E uoneiedo sainjea4 e uepioAy 2 4 Duruue d AEN Sd5 S24V oipny uddx junuuy Jeuuouqy Jeuonippy Tu102 AEN xipuaddy x pul iui Wfil4 paezey Flight Instruments k s l Annun Abnormal Additional Hazard Flight Nav Com Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Appendix Index
122. ng uoneiedo Jeuuouqy Sue v unuuy gt s o 5 m E x pul 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 123 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix optional TCAS II TRFC MAP A GARMIN optional TCAS II optional XPDR TFC Leas L NSET SENSOR ero oss CDI ADFIDME XPDR DENT INSET or TRFC MAP OFF DCLTR 3 TRAFFIC TOPO TERRAIN NEXRAD XM LING optional optional T r esc mag Toro Fema reas parang 1 n 9w v v v mm mnn VS Select the BACK Softkey to return to the top level softkeys INSET Map Softkeys 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 Removes Inset Map 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 Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window Displays topograph
123. ning Abnormal Additional Hazard Avoidance Annun EAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude AFCS armed to capture the altitude displayed in the Selected Altitude ALTS Capture window Altitude Hold Holds the current Altitude Reference ALT Key ALT Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS to the Selected Altitude Maintains the current aircraft airspeed FLC in IAS or Mach while the aircraft is hangs climbing descending to the Selected FLC key Altitude Vertical Path Captures and tracks descent legs ofan 1 VNV VPTH Tracking active vertical profile Key VNAV Target Captures the Vertical Navigation VNV ATV Altitude Capture Target Altitude Glidepath Captures and tracks the WAAS GP glidepath on approach Captures and tracks the ILS glideslope Ie Glideslope aptures and tracks the ILS glideslope GS on approach Commands a constant pitch angle Takeoff and wings level on the ground in TO preparation for takeoff TO GA Disengages the autopilot Switch Go Around commands a constant pitch attitude GA and wings level ALTS armed aut
124. ning 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 NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tum 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 35 sjuauimnasu nubi olpny uqax
125. nob 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 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 43 sjueumasu UTE oipny uadx 0105 AEN 52 2 AEN 540 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN STORE A FLIGHT PLAN 1 2 3 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 2
126. nsible 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 amp Wamings Cauvons Motes GARMIN WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local
127. o o 5 ia wala ped co m a 2 3 4 3 3 I 0 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Amnunciations amp Alerts Advisory Messages See the Airplane Flight Manual AFM for recommended pilot actions ME Description A Engine 1 Anti ice system valve failed when commanded to close A E2 FAULT Engine 2 Anti ice system valve failed when commanded to close A E1 ON Anti ice system on in engine 1 A I E2 ON Anti ice system on in engine 2 SR TINGS DAVEE V NGSTAB toggle switch has been armed prior to takeoff TAUN A MM WHSAIS is operating RES RAT ADS 1 side slip compensation is off PS MEM ADS 2 side slip compensation is off PASSES EO M ADS Probe switch is on AHRS 1 FAULT Fault with AHRS 1 AHRS 2 FAULT Fault with AHRS 2 NG Mis One pneumatic and Anti ice controller channel is inoperative NUON aN RE Fault with audio pane TUNA HB Fault with audio panel 2 NR EZ NIRE Partial loss of aural warning function AVNX FAN FAIL Avionics fan failure AO IST UM Two baggage compartment smoke detectors have failed BLEED 1 OFF Bleed pressure regulator 1 and shut off valve closed BLEED 2 OFF Bleed pressure regulator 2 and shut off valve closed eue dU
128. o4 e2uepioAy SoJnpa20Jd Duruue d ACN 540 S24V oipny uadx Jeuonippy puezey 164 wio3 neN uoneiedo Jeuuouqy Sue v unuuy m 5 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix IDENT TMR REF NRST CODE Cockpit Reference Guide for the Prodigy Flight Deck 300 TEST BACK 0 7 IDENT BKSP A GARMIN NORMAL Displays non threat traffic from BELOW UNREST 2700 feet above the aircraft to 2700 feet below the aircraft Typically used during enroute phase of flight Displays non threat traffic from 2700 feet above the aircraft to 9900 feet below the aircraft Typically used during descent phase of flight All traffic is displayed Activates Test Mode and displays test intruder symbols Returns to the previous softkey level Displays transponder code selection softkeys 0 7 Use numbers to enter code Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Messages Window 190 00761 00 Rev A A GARMIN Appendix MFD SOFTKEY M
129. oJnpa204d Duruue d AEN 540 S24V olpny uqax sv sjueumasu puezey ubi UI05 AeN ufi jeuonippy uoneiedo Jeuuouqy Ins x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN TAWS B ALERTS PFD MFD MFD Alert Type 1 TAWS B Page Aural Message Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance Pull Up Warning RTC Imminent Terrain PULL UP Terrain Terrain Pull Up Impact Warning ITI Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance Up Pull Up Warning ROC Imminent Obstacle PULL UP Obstacle Obstacle Pull Impact Warning Up Pull Up 101 Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance Terrain Caution RTC Imminent Terrain TERRAIN CAUTION TERRAIN Caution Terrain Caution Impact Caution ITI Terrain Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Obstacle Clearance Caution Obstacle Caution ROC Imminent Obstacle TERRAIN CAUTION OBSTACLE Caution Obstacle Impact Caution 101 Caution Obstacle Premature Descent TERRAIN TOOLOW TER
130. oad a single copy of this manual and of any revision to this manual onto a hard drive or electronic storage medium to be viewed for personal use provided that such electronic nted 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 revisi Prodi on hereto is strict y prohibited gy is a trademark of Embraer Empresa Brasileira de Aeronautica S A Garmin is a registered trademark of Garmin Ltd or its subsidiaries WATCH FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmi NavData is a registered trademark o n f Jeppesen Inc and XM is a registered trademark of XM Satellite Radio Inc Honeywell and Bendix King are registered trademarks of Honeywell International Inc CO Guardian is a trademark of CO Guardian Inc October 2009 190 00761 00 Rev A Printed in the U S A amp Warnings Cantans amp Notes GARMIN 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 T
131. oblem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 sjuaumnasu sub saunqea4 aoueplony s mp oold Buruue d AEN Sd5 yi oipny uddx paezey 346 3 UI05 AeN jeuonippy uoneiedo Jeuuouqy n EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments 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 Standby Navigation database mismatch The PFDs and MFD have different standby navigation database v
132. ode value if it is engaged Cockpit Reference Guide for the Prodigy Flight Deck 300 roll command limit will be 2 sv3 sjueuinasu oipny dadx UI0JNeN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d junuuy Jeuuouqy Jeuonippy paezey xipueddy x pul iui wy Flight EAS Instruments Nav Com XPDR Audio GPS Nav AFCS Annun Abnormal Additional Hazard Flight Alerts Operation Features Avoidance Procedures Planning Appendix Index A AFS GARMIN Current Speed Control CSC NOTE For CSC engagement and disengagement detailed conditions see the approved Pilot s Operating Handbook POH Current Speed Control CSC is available while the AFCS Altitude Hold Mode is active and the autopilot is engaged When active green arcs appear on the N1 gauges at values corresponding to the current speed selected Selecting Current Speed Control CSC 1 Enter Altitude Hold Mode and engage the autopilot see the AFCS Section for details 2 Press the CSC Key on the AFCS Control Unit 28 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 Press the Direct to Z 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
133. omatically 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 Selected Altitude 26 Cockpit Reference Guide for the Prodigy Flight Deck 300 hen VNAV Target Altitude is to be captured instead of 190 00761 00 Rev A A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds the current aircraft roll attitude Roll Hold or rolls the wings level depending on default ROL the commanded bank angle Limits the maximum commanded roll BANK Low Bank angle Key Heading Select Captures and tracks the Selected HDG HDG Heading Key Navigation GPS GPS Navigation VOR 75 ae Captures and tracks the selected YOR navigation source GPS VOR LOC Navigation LOC NAV Capture Track Key LOC No Glideslope Navigation casei as an fas ln Sr x Capture Track PP Approach GPS GPS Approach VOR VAPP Arm Capture Track Captures and tracks the selected APR Ke Approach LOC navigation source GPS VOR LOC y Capture Track LOC Glideslope Mode automatically armed No annunciation appears in the AFCS Status Box The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator The Heading Navigation GPS and Navigation VOR mode maximun limited to the Low Ban 190 00761 00 Rev A
134. omputer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS2 TAS AHRS2 not receiving valid 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 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 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 AHRS1 GPS AHRS1 not receiving any GPS information AHRS2 GPS AHRS2 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 The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS1 GPS AHRST not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The system should be serviced Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES CONT Message AHRS2 GPS AHRS2 not receiving backup GPS information Comments The 2 AHRS is not receiv
135. only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun cated 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 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
136. or the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts GMA 1347D MESSAGE ADVISORIES CONT Message GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d Comments The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMAT software mismatch communication halted o The audio panel has incorrect software installed Th e Service Return unit for repair u GMA2 SERVICE GMA2 needs service Return unit for repair MANIFEST GMA software system should be serviced mismatch communication halted GMA1 SERVICE GMAT needs The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d Comments The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d GIA1 COOLING GIA1 temperature too low
137. ositioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 1 2 3 60 Press the MENU Key Turn the large FMS Knob to select Show Tilt Line Press the ENT Key Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Hazara avoidance Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain o WARNING Changing the gain in Weather Mode will cause precipitation intensity to be dis
138. ough the HF radio Takeoff configuration test passed The aircraft is outside the Traffic Information Service TIS coverage area 102 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description 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 o flight plan files found to import Flight plan import failed The SD card contains no flight plan data us 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
139. outh NOTE TAWS operation is only available when the system is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS System Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain and Obstacles on the TAWS B Page 1 2 3 4 58 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS B Page 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 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Hazard avoidance EnablelDisable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Pre
140. paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 a b d a b o d a b o d A GARMIN Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired user waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 42 1 2 3 4 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD 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 entr
141. 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 Sjueuingjsu ii AEN 540 52 oipny uadx sv3 Wfil4 JUI05 AEN eouepioAy paezey s m e q FNISHED 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 7 xipueddy Suelv uoneiedo
142. place the panning arrow on AIRMETs TFRs METARs or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cyclone Warnings AIREPs City Forecast Icing Potential PEE Cell Movement Freezing Levels Turbulence P IREP m XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMETSAIRMET Winds Aloft 52 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Hazard Avoidance TRAFFIC INFORMATION SERVICE TIS A 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
143. played 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 61 sjuauimasu nub ARN Sd5 52 44 0105 AEN Duruue d nf aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Ground Mapping 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become
144. plays the transponder and TCAS II selection softkeys Selects the 1 transponder as active optional Selects the 2 transponder as active optional Displays transponder mode selection softkeys 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 190 00761 00 Rev A A GARMIN ON ALT TA ONLY BACK TCAS REL ABS ALT RNG ABOVE Appendix Activates transponder transponder replies to identification interrogations When the transponder is set to ON the TCAS II system is set to standby 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 Activates the TCAS II system in TA Only Mode and sets the transponder to ALT Activates the TCAS II system in TA RA Mode and sets the transponder to ALT Returns to the previous softkey level Displays the TCAS control softkeys Displays intruder altitude as altitude relative to own aircraft altitude Displays intruder MSL altitude Displays the altitude display range softkeys Displays non threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft Typically used during climb phase of flight 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 131 sjuauimasu sub soinje
145. puaddy x pul Flight Instruments Nav Com AFCS XPDR Audio EAS Flight Planning Abnormal Additional Hazard Avoidance Annun Procedures GPS Nav Appendix Alerts Operation Features Index A Nav Com XPDR Audio Panel GARMIN 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 PASSENGER ADDRESS PA SYSTEM passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels PA messages are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the
146. quiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A amp GARMIN Warnings Cautions 5 Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD vveather data should not be used for short range weather avoidance 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 respo
147. r the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page If necessary select the SYNC DBS Softkey so it is enabled A YES NO prompt is displayed With YES highlighted press the ENT Key Monitor the Sync Status in the Database Window wait for all databases to complete synching Remove and reapply power to the system select the AUX System Status Page and verify that all databases have been synchronized 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 137 sjuauimasu Yid so1njeoJ 2 Bujuuejd AEN SdD S24V oipny uadx Jeuonippy paezey 16114 uo2 AEN uoneiedo Jeuuouqy Sue v unuuy nn Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN If an error occurs during the synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If a synchronization completes on one display but an error occurs on another the error message will be displayed with the affected display listed after it When an error mes
148. ration settings do not match those of backup configuration memory The system should be serviced GCU FAIL GCU is inoperative MANIFEST GCU software mismatch communication halted A failure has been detected in the GCU 477 The GCU 477 is unavailable The GCU 477 has incorrect software installed The system should be serviced 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 GMC 715 MESSAGE ADVISORIES Message Comments GMC CONFIG GMC Config error Config service req d GMC 715 configuration settings do not match those of backup configuration memory The system should be serviced GMC FAIL GMC is inoperative MANIFEST GMC software mismatch Communication halted A failure has been detected in the GMC 715 The GMC 715 is unavailable The GMC 715 has incorrect software installed The system should be serviced 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK
149. reater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the system is configured for a TAWS A installation Manual System Test 1 2 3 While the TAWS A Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS System 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 Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS A Page 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 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN avoidance Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude EnablelDisable Aviation Data 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation D
150. rough DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored eS Ces tpt CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 84 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Abnormal operation As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following sjueuinasu yp Navigation Status Box fields except Active Leg TAS and DIK 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 sv4 oipny uddx UI0JNeN 52 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 w
151. rviced 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 XPDR1 SRVC XPDR1 needs The 1 transponder should be serviced when service Return unit for repair possible 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 soJnjeoJ s np 01d Buruuejg AEN 5640 S24V oipny uadx svi paezey nubi u102 AEN nubi jeuonippy uoneiedo Jeuuouqy IBN 1 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN GTX 33 33D MESSAGE ADVISORIES CONT Message XPDR2 SRVC XPDR2 needs service Return unit for repair Comments The 2 transponder should be serviced when possible XPDR1 FAIL XPDR1 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data c
152. s the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts Optional FliteCharts resemble the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 65 AEN 540 52 oipny uadx sjueunasu Wo gt AeN aoueplony 2 s m e q jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipuaddy x pul iui nu Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 66 A GARMIN 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 2 3 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to
153. s Airport Directory 67 ATR 7 133 Attitude amp Heading Reference System 93 Audio Panel 82 Audio panel controls NAV1 NAV2 23 Aural alerts 102 Automatic Thrust Reserve 7 133 Barometric Altitude Minimums 3 Barometric pressure 128 Battery indications 5 Bearing line 61 62 C Cautions CAS 87 89 CDI 1 2 23 120 Channel Presets 75 ChartView 65 Checklists 76 77 Code selection softkeys 22 COM 22 23 81 Current Speed Control CSC 28 Index D Database synchronization 137 138 Data reports 72 DCLTR Softkey 65 Dead Reckoning 83 Declutter 82 124 136 Designated altitudes 32 Direct to 29 DME 21 23 DR mode 83 84 85 E Edit a flight plan 44 Electrical indications 8 14 Electronic checklists 76 77 Emergency checklist 77 Engine failure 79 Engine fire 79 Engine rotation speeds 5 Environmental Control System ECS 12 13 F Flap Indicator 5 11 80 Flight Director 25 Flight ID 21 Flight path marker 63 FliteCharts 65 Frequency Transfer 23 Fuel indications 5 8 16 G Gain 61 H HF 22 Horizon heading 63 Horizontal scan 61 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 ndex 1 sjuaumasu nubi saunqea4 2 AEN Sd 24V oipny uadx Jeuonippy paezey L L ulo2 AEN uoneiedo Jeuuouqy Sue v unuuy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Plannin
154. sage is displayed the problem must be corrected before the synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled An active synchronization has been canceled using the SYNC DBS Softkey 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 The SYNC DBS Softkey on the AUX System Status Page allows enabling and disabling the automatic database synchronization feature If the SYNC DBS Softkey is selected while a database synchronization is in progress the current synchronization process will be canceled Canceling Database Synchronization 1 Tum the large FMS Knob to select the AUX Page group on the MFD 2 Turn the small FMS Knob to select the System Status Page 3 Select the SYNC DBS Softkey if needed to disable automatic database synchronization 4 Acknowledge the cancellation by pressing the ENT Key 138 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN A Activate a flight plan 30 Active Channel 74 ADF 21 23 Advisories CAS 91 92 AHRS 114 115 118 Airport Signs 63 64 Airways 135 Air Data Computer 93 Alert messages 117 Altimeter setting 1 Antenna stabilization 62 Antenna tilt 60 AOPA
155. se 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 SERVICE GDL 59 needs service Return unit for repair A failure has been detected in the GDL 59 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 REGISTER GFDS Data services are inoperative register w GFDS The GDL 59 is not registered with Garmin Flight Data Services or it s current registration data has failed authentication MANIFEST GDL software mismatch communication halted The GDL 59 has incorrect software installed The system should be serviced 116 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN GDL 69A MESSAGE ADVISORIES Annunciations amp Alerts Message GDL69 CONFIG GDL 69 config error Config service req d Comments 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 MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The syste
156. 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings 7 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 Theflashing 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 Plan
157. ss the ENT Key TAWS Inhibit A NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS 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 select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacles will now be displayed on the map 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 59 sjuauimnasu wp AEN Sd5 52 oipny uddx 010 AEN buluueld ni aoueploay s mp oold paezey Suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN AIRBORNE COLOR WEATHER RADAR
158. state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The system does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained
159. t Deck 300 67 sjuaumasu Yid xipueddy Suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax Tunuuy Jeuuouqy jeuonippy paezey U10 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 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 call unanswered Selecting the TEL Softkey will display the AUX TELEPHONE allowing additional call information to be viewed before answering 68 Muting 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 Mute Incoming Call Alerts 3 Press the ENT Key The voice alert is muted and the pop up alert will not be displayed when an incoming call is received Making 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 ringing symbol will now be disp
160. ted press the ENT Key Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN _ Additional Features 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 select the VOL Softkey 2 Select the VOL Softkey to reduce volume or select the VOL Softkey to increase volume Once the VOL Softkey is selected the volume can also be adjusted using the small FMS Knob 3 Select the MUTE Softkey to mute the audio Select the MUTE Softkey again to unmute the audio 190 00761 00 Rev A Cockpit Ref
161. the SD card into the top card slot on the MFD Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN 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 Tum 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 Procedures 1 Press the FPL Key on the MFD or 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
162. tion arrows with headwind and crosswind components Wind direction arrow and speed Total direction with head and crosswind speed components Information not displayed Select to display the DMEI information window Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree for mat Displays the HSI in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Select to display the DME2 information window Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter and selected altitude in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 127 sjuaumasu Yid saunqea4 uepjoay seinpa2o0Jd Buruuejd AEN Sd 24V oipny uadx Jeuonippy paezey L L uo2 AEN uoneiedo Jeuuouqy Sue v unuuy m Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa OBS Selects OBS mode on the CDI when navigating by GPS only
163. 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A GARMIN Flight instruments 4 5 6 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey TURN VSPEED BUGS ON OR OFF BY CATEGORY 1 2 3 4 Press the TMR REF Softkey Press the MENU Key Turn the FMS Knob to highlight the desired option Press the ENT Key Press the TMR REF Softkey to remove the window SET BAROMETRIC RADAR ALTIMETER OPTIONAL MINIMUM DESCENT 1 2 3 4 5 6 7 ALTITUDE Press the TMR REF Softkey Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS Turn the small FMS Knob clockwise to select BARO or RAD ALT Press the ENT Key Use the small FMS Knob to enter the desired altitude Press the ENT Key To remove the window press the CLR Key or the TMR REF Softkey DISPLAYING WIND DATA 1 2 3 4 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 3 Press the PFD Softkey Press the WIND Softkey to display wind data below the Selected Heading Press one of the OPTN softkeys to change how wind data is displayed To remove the Wind Data Window
164. ts 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 saunqea4 2 AEN Sd 2 oipny uadx svi sjuawinasu paezey nubi u102 NEN nubi jeuonippy uoneiedo Jeuuouqy Ea x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix pes Annunciations amp Alerts A GARMIN GMU 44 MESSAGE ADVISORIES CONT Message MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted Comments The GMU 44 has incorrect software installed The system should be serviced GSR 56 MESSAGE ADVISORIES Message Comments GSR1 FAIL GSR1 has failed A failure has been detected in the 1 GSR 56 The system should be serviced GDL 59 MESSAGE ADVISORIES Message GDL59 CONFIG GDL 59 config error Config service req d Comments GDL 59 configuration settings do not match tho
165. tter 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 Displays optional checklists DUAL NAVIGATION DATABASES The dual navigation database feature allows each display to store an upcoming navigation database on the bottom SD card so that the system can automatically load it to replace the active database when the new database becomes effective the next cycle becomes available seven days prior to its effective date Uploading the standby database to the active location takes approximately 45 55 seconds Loading a Navigation Database 1 2 3 4 5 6 1 8 With the system OFF insert the SD card containing the navigation database update into the top card slot of the desired PFD or the MFD Verify that an SD card is inserted in the bottom slot Turn the system ON At the prompt if it is desired to update the standby navigation database on the bottom SD card press the YES Softkey and proceed to step 6 If it is desired to update the active navigation database press the NO Softkey and proceed to step 5 At the next prompt press the YES Softkey to update the active navigation database After the update the display starts in normal mode Repeat steps 1 6 for the remaining displays Verify the effectivity of the active
166. ude sensors o data from one or both airspeed sensors HDG NO COMP o data from one or both heading sensors PIT NO COMP o data from one or both pitch sensors ROL NO COMP o data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Sensor Window Text Condition X Both PFDs are displaying data from the n mber one Air Data Computer Both PFDs are displaying data from the number two Air Data Computer Both PFDs are displaying data from the standby air data input Both PFDs are displaying data from the n Reference System mber one Attitude amp Heading 190 00761 00 Rev A f Both PFDs are displaying data from the n Reference System E mber two Attitude amp Heading Cockpit Reference Guide for the Prodigy Flight Deck 300 sainjea4 2 Duruue d AEN Sd5 S24JV olpny uqax sv sjuauimasu 2 wold uio AeN Yid euonippv uoneiedo Jeuuouqv id E x pul Flight EAS Instruments Nav Com XPDR Audio Hazard Flight Features Avoidance Procedures Planning GPS Nav AFCS Additional Abnormal Operation Index Appendix nd Amundatons amp Alerts GARMIN Reversionary Sensor Window Text Condition Both PFDs are displaying data from the standby attitude and heading reference input Bot
167. vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Displaying Traffic on the Traffic Map Page 1 Tum 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 counter clockwise to display a smaller area 6 Select the TNA MUTE Softkey to mute the Traffic 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 53 sjuaumasu BUT AEN Sd5 52 oipny uddx 010 AEN Duruue d 1ubil4 s mp oold paezey suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Alerts Operation Features Avoidance Procedures Appendix Index Hazard Avoidance A GARMIN TRAFFIC COLLISION
168. wise 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 amp STORES field 4 Enterthe desired weight of Pilot amp 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 Tum 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 190 00761 00 Rev A Cockpit Reference Guide for the Prodigy Flight Deck 300 33 sjuauimnasu UATE olpny uqax 0105 AEN
169. 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A amp GARMIN Nanings Caulons amp Notes 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
170. y point should be entered at this time 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 Cockpit Reference Guide for the Prodigy Flight Deck 300 190 00761 00 Rev A A GARMIN Flight Planning 5 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan 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 K

Garmin Software Version 0734.23 Cockpit Reference Guide

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