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Garmin Software Version 1983.00 Cockpit Reference Guide

1. TERRAIN SVT ALERTS PFD MFD Alert Type TERRAIN SVT MFD Aural yP Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Warning Terrain Clearance Warning RTC Terrain Imminent Terrain Impact TERRAIN Warning Terrain Warning ITI Terrain Reduced Required Obstacle TERRAIN Warning Obstacle Clearance Warning ROC Obstacle Imminent Obstacle Impact TERRAIN Warning Obstacle Warning 101 Obstacle Reduced Required Terrain TERRAIN CAUTTON TERRAIN 1 Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN CAUTTON TERRAIN 1 Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRAIN CAUTTON OBSTACLE Caution Obstacle Clearance Caution ROC Obstacle 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 83 saunqea4 sanpa20Jq Buruuejd AEN 5649 S24V olpny uqax sia syu unysu paezey nubi Wil jeuonippy uoneiedo Jeuuouqy icd p x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN Alert Type PFD MFD TERRAIN SVT MFD Aural Page Pop Up Alert Message Annunciation Caution 101 Imminent Obstacle Im
2. Synthetic Vision Optional Terminal Procedure Charts een Airport Directory SiriusXM Radio Entertainment Pilot Profiles oet tte Electronic Stability amp Protection 5 71 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A E GARMIN Table of Contents ABNORMAL OPERATION L L Abnormal COM Operation s s s s s s s ss s s ss s s ss s s ssss s l Hazard Displays with Loss of GPS Position Unusual Attitudes seeennnnnnnnnnne MEC O see eee e er Ree er e eer i ANNUNCIATIONS amp G1000 System Annunciations CAS 015 2 556 System Messages sss Voice Alerts Terrain SVT Alerts Terrain SVT System Status Annunciations TAWS B Alerts a e e du dee b r TAWS B System Status Annunciations GDL 69 69A Data Link Receiver Messages MFD amp PFD Message Advisories Database Message Advisories GMA 1347 Message Advisories ssssssssseee e GIA 63W Message Advisories GEA 71 Message Advisories GTX 33 33 vv ES Message Advisories
3. sssssss GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GTS 800 Message Advisories GDC 74A Message Advisories Miscellaneous Message Advisories Flight Plan Import Export Messages Pilot Profile Import Export 55 5 PFD Softkey MED Softkey Map 12 Loading Updated Databases 15 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole l Table of Contents GARMIN Blank Page V Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure 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 S
4. MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists 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 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 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 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 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 89 saunqea4 2 Buruuejg AEN 5649 24V olpny uqax s q paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy iuc x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Al
5. The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 103 saunqea4 2 Buruuejg AEN 5649 24V oipny uadx s q syu unysu paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy c E x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ed Annunciations amp Alerts A GARMIN Flight Plan Import Export Results Too many points Flight plan truncated Description 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 Waypoints locked The flight plan on the SD card contains one or more waypoints that the system cannot find
6. 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 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 only an aid to enhance situational awareness WARNING Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole A Wamings Santions amp Notes GARMIN N WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions WARNING Do not use the indicated data
7. 2 AEN 540 nubi aoueplony paezey say uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 30 3 4 5 6 7 8 9 10 A GARMIN Press 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 lis
8. 5 6 7 8 9 10 11 12 13 14 15 16 17 18 120 After the navigation database files are copied to the bottom SD card press any key to verify as instructed After database verification is complete press any key to continue as instructed on the display Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting Press the ENT Key to acknowledge the startup screen 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 The new database is copied to the SD card in the bottom card slot of the PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle Turn system power OFF Remove the SD card from the top card slot of the MFD Turn system power ON Press the ENT Key to acknowledge the startup screen 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 Press
9. GPS integrity lost Crosscheck with other NAVS GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation d satellites ue to insufficient GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation d ue to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation d ue to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation downgraded APR DWNGRADE Approach Vertical guidance generated by SBAS is unavailable use LNAV only minimums TRUE APR True north approach Change HDG reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Retum unit for repair A failure has been detected in the GPS and j or GPS2 receiver The receiver may still be 6 52 SERVICE GP32 NEEC available The system should be serviced service Return unit for repair NAV1 SERVICE NAV1 needs AEN 540 52 oipny uadx sia Sjueumajsul aoueplony iui U105 AeN nu paezey A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced service Return unit for repair
10. in the Pilot Profile Box Press the ENT Key In the Delete Profile window turn the FMS Knob to select the profile to delete Press the ENT Key With DELETE highlighted press the ENT Key To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key Importing a profile 1 2 3 Or 4 Insert the SD card containing the Pilot Profile into the top card slot on the MED Use the FMS Knob to select the AUX System Setup Page Press the IMPORT softkey If the correct Pilot Profile file is selected with IMPORT highlighted press the ENT Key If the SD card contains more than one Pilot Profile a Turn the large FMS Knob to highlight the select file field in the Pilot Profile Importing Box b Turn the small FMS Knob to display the pilot profile list and highlight the desired profile to import and press the ENT Key c With IMPORT highlighted press the ENT Key Pilot profile import succeeded is shown in the import results box Press the ENT Key The imported profile becomes the active Pilot Profile Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Exporting a profile 1 Insert the SD card for storing the Pilot Profile into the top card slot on the MFD 2 Use the FMS Knob to select the AUX System Setup Page 3 Activate the desired Pilot Profile to export Only the active
11. 6 2 4 aoueplony puezey s s Jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 122 A GARMIN A Activate a flight plan 20 Active Channel 65 Active database 118 Active Navigation Database 118 AC U KWIK 64 ADF 11 ADS B 52 112 AHRS 79 97 98 Airport Directory 64 Airport Signs 61 62 Airways 114 Altimeter setting 1 76 AOPA 64 AOPA s Airport Directory 64 Approach channel 45 Audio panel controls NAV1 NAV2 11 Barometric Altitude Minimums 2 Barometric pressure 111 C Caution alerts 82 CDI 1 11 101 Channel Presets 66 ChartView 62 63 Clearance player 12 Clearance recorder 12 Code selection softkeys 11 COM 11 12 75 D Data Link Receiver 87 DB Mismatch 115 120 DCLTR Softkey 62 Dead Reckoning 76 Index DEC FUEL softkey 9 Declutter 76 108 115 Designated altitudes 22 23 Direct to 19 DME 11 DR mode 76 77 78 E Edit a flight plan 39 Electronic Stability 71 Enable Terrain 58 Endurance calculated ENDUR 8 9 Engine manifold pressure 6 7 ESP 71 72 F Flight Director 15 Flight ID 54 Flight path marker 61 Flight plan import export messages 103 FliteCharts amp 62 63 Frequency Transfer 12 Fuel Calculations 9 Quantity 6 H Horizon heading 61 Inhibit 58 60 Inhibit TAWS 60 Inhibit Terrain 58 Insertion Point Indicator 35 Inset Map 107
12. GARMI Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN table of Contents FLIGHT INSTRUMENTS ss s s 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Change Navigation Sources sssssssseennnnn nnns 1 Enable Disable OBS Mode While Navigating with GPS 2 Generic Turn All Vspeed Bugs On or Off Set Barometric Minimum Descent Altitude sss 2 Displaying Wind Data 3 ENGINE INDICATION 5 Engine Dp az a e e ete edm qe a e RR RET 5 Engine Pag icone nte ete ete misit niea tan 7 Landing Gear Indications 0 NAV COM TRANSPONDER AUDIO 1 Enter a Transponder Code sss 1 DME Tuning nnne ntt 1 Selecting a COM Radio seen 1 Selecting a NAV Radio 1 NAV COM Tuning nin ee rn le ie ln ben e OR rr HR Fre 2 Digital Clearance Recorder and Player 2 Intercom System ICS Isolation sse 3 AUTOMATIC FLIGHT CONTROL SYSTEM
13. NAV2 SERVICE NAV2 needs service Return unit for repair 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 cycle its operation If the problem persists the system should be serviced 6 51 FAIL G S1 is inoperative ies E A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced G S2 FAIL G S2 is inoperative 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 95 saunqea4 jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ed Annunciations amp Alerts A GARMIN Message Comments G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible TRN AUD FAIL Im Awareness audio source unavailable The audio source for terrain awareness is offline Check GIA1 or GIA 2 TERRAIN AUD CFG Trn Awareness audio config error Service req
14. A NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area A NOTE TAWS B operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 190 01462 01 Rev A 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 Black below aircraft altitude Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 59 AEN 540 S24V oipny duadx 99 s u u nnsul u02 AEN buluueld ni s mp ool
15. FT The altitude selection is shown at the bottom No Status Icon 1 TFR Depicted as an area outlined in yellow TRAFFIC SYSTEMS WARNING Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display e If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey are displayed 2 Ifa Traffic Advisory System TAS is configured a STANDBY NORMAL TEST and ALT MODE Softkey are displayed fan ADS B traffic system is configured only the ALT MODE Softkey is displayed Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation 52 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Hazard
16. MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset 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 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 Press the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 20 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 Press 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 Garmin G1000 Cockpit Reference Guide for the Pip
17. Press the ENT Key The temperature compensated altitude at the FAF is cancelled 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 4 oipny uddx s q sjuauimasu U10 AEN 3463 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Procedures Sjueuinijsu fila 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld Blank Page um aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 48 GARMIN Hazard avoidance HAZARD AVOIDANCE Customizing THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page SIRIUSXM WEATHER OPTIONAL WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accura
18. and press the ENT Key Use the FMS Knobs to edit the length and press the ENT Key Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while LOAD is highlighted to add the hold into the flight plan Creating a user defined hold at the aircraft present position 1 2 3 4 5 6 7 8 9 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD Press the MENU Key highlight Hold At Present Position and press the ENT Key The HOLD AT window appears with the course field highlighted Use the FMS Knobs to edit the entry course and press the ENT Key Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key Use the FMS Knobs to edit the length and press the ENT Key Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while ACTIVATE is highlighted to create an Offroute Direct to hold waypoint and activate the hold Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 1
19. bank angle Captures and tracks the Selected Heading Captures and tracks the selected navigation source GPS VOR LOC BC Captures and tracks the selected navigation source GPS VOR LOC Commands a constant pitch angle and wings level on the ground in preparation for takeoff Commands a constant pitch angle and wings level in the air Commands wings level with zero degree pitch angle limited to the Low Banh mode value if it is engaged 190 01462 01 Rev A Control Annunciation default HDG Key NAV Key APR Key GA Switch LVL Button ROL HDG GPS VOR LOC BC GPS VAPP LOC TO GA LVL gation VOR mode maximum roll command limit will be Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 17 sia sjuounasu olpny uqax wi0 gt AeN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy xipuaddy x pul iui nuru paezey Nav Com XPDR Audio GPS Nav AFCS Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS Appendix Alerts Operation Features Avoidance Procedures Index A AFS 0 GARMIN UNDERSPEED PROTECTION Underspeed Protection is available when the optional Electronic Stability and Protection ESP system is installed and the autopilot is on When aircraft airspeed reaches 80 knots IAS a flashing yellow MINSPD annunciation will
20. c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 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 CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM ANOTHER WAYPOINT 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 29 sjuauimasu Yid oipny uddx 93 UI0JNeN 52
21. expressly disclaim in this data express 0 merchantability and fit AC U eliability or othe maximum extent from any cause 0 information arising out of Ga do not allow the limitation o consequential damages so th uch damages User ag its re implied including but ness for a particular pu allowed by law to release an f action clai rmin s use of the exclusion of imp October 2014 s related organizations herei The infor i ated organizations herea all warranties with respect to not li KWIK Organizations do not warrant or ma wise Licensee agrees not to s ms or losses related 190 01462 01 Rev A f nafter collectively espect to the AOPA information included in this ted to the implied warranties of merchantability mation is provided as is and AOPA does not g its accuracy reliability or otherwise Under AOPA be liable for any incidental special or use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has been advised of the ees not to aw to release and hold harmless AOPA fro sue AOPA and to the maximum extent allowed m any causes of action claims or losses related formation Some jurisdictions do not allow the iability for incidental or consequential damages apply to you f ter collectively AC U KWIK Organizations the AC U KWIK information included mited to th
22. indicates climbing down arrow indicates descending Intruder Aircraft Ground Trach extends in the direction of the aircraft movement Example ADS B Traffic Advisory GTS 800 only Symbol Description Traffic Advisory with ADS B directional information Points in the direction of the intruder aircraft track GTS 800 only Traffic Advisory without directional information Traffic Advisory out of the selected display range Displayed at outer range ring at proper bearing Non threat traffic with ADS B directional information Points in the direction of the aircraft track GTS 800 only o Non threat traffic with ADS B directional information Points in the direction of the intruder aircraft track GTS 800 only o Non threat traffic with no directional information o Traffic with ADS B directional information but positional accuracy is degraded Points in the direction of the aircraft track GTS 800 only 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 55 AeN Sd5 S24V oipny uadx si sjueumasu u105 AEN Yubilu Duruue d Wil aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts O
23. 108 IOI 83 84 85 86 J Jeppesen 63 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole ndex 1 sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy puezey qwbl4 Tuo2 NeN uoneiedo Jeuuouqy Sue v unuuy m Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Appendix Index L Level Mode 71 M Map panning 50 Message advisories 88 89 92 93 96 99 METAR 49 MKR MUTE 12 Mode 111 Mode selection softkeys 11 Multi Function Display MFD Softkeys 112 N NAV 11 12 NAV1 1 11 NAV2 1 11 Navigation database 21 23 NEXRAD 49 108 114 0 OBS 2 Obstacles 91 92 93 P Pathvvays 61 62 Pilot Profile 68 Profile View 113 R Reversionary mode 75 ROC 83 85 S SafeTaxi amp 62 71 SBAS 44 58 60 77 93 95 Index 2 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole A GARMIN Scheduler 67 SiriusXM lightning 108 114 SiriusXM Weather 50 Standby Navigation Database 119 Store Flight Plan 38 SVT 61 102 Synchronization 116 SYNC Status 120 Synthetic Vision System 61 T Tachometer 6 7 TAF 49 TAS 97 TAWS 59 60 85 TAWS B 59 Terrain 56 57 59 91 108 113 Terrain SVS 57 58 Timer 2 99 Topographical data 108 113 Traffic 49 53
24. 190 01462 01 Rev A A GARMIN GIA 63W MESSAGE ADVISORIES Annunciations amp Alerts Message GIA1 CONFIG GIA1 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 The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING G A2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature 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 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 A GIA mismatch has been detected where only one is SBAS capable MANIFEST G A1 s
25. 5 Flight Director Activation sss 5 Vertical Modes nass dato da ER och ER e 6 Lateral Modes tenentes 7 Underspeed Protection nennen 8 GPS 9 Direct to Navigation ssssssssseeee nnne 9 Activate a Stored Flight Plan 20 Activate a Flight Plan Leg 20 Stop Navigating a Flight Plan 21 Vertical Navigation VNAV l l s s s s s s s s s s s s 21 FLIGHT PLANNINI A A AA usua 25 Weight 77 5 25 Trip Planning nre eod tene tes e eri 25 Create a User Waypoint Defined by Latitude amp Longitude 2 Create a User Waypoint Defined by Radials from Other Waypoints 0 28 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 29 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole Table of Contents GARMIN Create a User Waypoint using the Map Pointer 31 Delete a User Vlaypoint s s s s s s nnn Create a Flight 5 mport a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan 34 Enter an Airway in a Flight Plan 35 User Defined Holding Patterns Invert an Active Flight Plan
26. 6 Thecursor 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 7 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 2 oipny uddx 59 sjuauimasu U105 AEN 3463 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 7 8 9 A GARMIN 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 USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 28 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the MFD to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the NEW Softkey
27. 7 Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key of the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor c Turn the large FMS Knob to highlight the desired flight plan d Press the EDIT Softkey 2 Tum the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window Flight Planning 4 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key 5 Once all changes have been made press the FMS Knob to remove the cursor 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 39 olpny uqax s q sjuauimasu U10 AEN 3463 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN INVERT AND ACTIVATE A STORED F
28. A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 25 oipny uaddx s q sjuauimasu U10 AEN 1461 4 52 2 Bujuuejd AEN Sd5 nubi aouepiony paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 26 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Press 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 Press the FPL Softkey at the bottom of the display Turn the small FMS Knob to select the desired flight plan a
29. All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes Terrain Proximity TERRAIN SVT and TAWS B are also disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 78 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails a large red X is typically displayed on windows associated with the failed data Refer to the PA 44 180 Archer Pilots Operating Handbook POH for additional information regarding pilot responses to these annunciations System Annunciation Comment Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS GPS information is either not present or is invalid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS operation may be degraded if GPS signals are not present see POH Display system is not receiving valid heading input from AHRS Display system is not receiving valid transponder information 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide
30. CLR Key or the TMR REF Softkey m a dom 32 a gt 2 59 DISPLAYING WIND DATA oipny uddx UI0JNeN 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data below the Selected Heading 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey SH lV uonesado saunqea4 2 4 AEN Sd S24V junuuy jeuuouqy paezey Wfila x pu ddy x pul 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 3 GARMIN Flight Instruments I x oipny uadx U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole A GARMIN ENGINE INDICATION ENGINE DISPLAY GPH OIL PSI g 8 01 A ALTR AMPS VOLTS BATT AMPS GAL OOJOO O 666 o LANDING GEAR n n LANDING GEAR Engine Display when Engh Pape displayed Engine Display 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole EIS sjuaumasu BU ETE EA x pu ddy su jy uoneiedo SoJnjeaJ aoueplony saunpadold buluueld AEN 540 S24JV oipny uddx unuuy jJeuuouqv Jeuonippy paezey 3461 U10 AEN x pu
31. Electrical Group ELECTRICAL 2 Engine Hours TACH TIME 3 Exhaust Gas Temperature EGT F Cylinder Head Temperature Bar Graph CHT F 5 Fuel Quantity Gauges L R FUEL QTY GAL A GARMIN Displays oil pressure in pounds per square inch psi Displays oil temperature in degrees Fahrenheit F Displays landing gear status Displays calculated fuel used GAL USED endurance ENDUR and range in nautical miles RANGE NM and fuel efficiency in nautical miles per gallon NMPG based on the displayed fuel remaining GAL REM and the fuel flow totalizer Displays the setting of the flaps in degrees Displays alternator ALTR AMPS and battery BATT AMPS currents in amperes and bus voltage VOLTS Displays the total time in hours the engine has been in service Displays the temperature for the right and left Exhaust Gas Temperature for the hottest cylinder in F Displays head temperatures for all cylinders in F Displays the total amount of fuel and the amount of fuel in gallons gal for each side of a standard fuel tank Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN 000 ES Fuel Calculations sub NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset Fuel used GAL USED endurance ENDUR range in nautical miles RANGE NM
32. FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Press the EDIT Softkey 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 Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 38 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN EDIT A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Press the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location 6 Enter the changes then press the ENT Key
33. GARMIN 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 34 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint shown by the insertion point indicator 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 5 Enter the new flight plan waypoint by one of the following a b a b o d a b d a b Enter the user waypoint identifier facility or city 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 NRST airports 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 Garmin G1000 Cockp
34. Pilot Profile can be exported 4 Press the EXPORT softkey 5 With EXPORT highlighted press the ENT Key 6 Pilot profile export succeeded is shown in the export results box Press the ENT Key to exit the Pilot Profile Exporting Box ELECTRONIC STABILITY amp PROTECTION ESP Electronic Stability and Protection ESP is an optional feature that is intended to discourage the exceedance of attitude and established airspeed parameters This feature will only function when the aircraft is above 200 feet AGL and the autopilot is not engaged ESP engages when the aircraft exceeds one or more conditions pitch roll Vmo and or Mmo beyond the normal flight parameters Enhanced stability for each condition is provided by applying a force to the appropriate control surface to return the aircraft to the normal flight envelope This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a steep attitude or high airspeed As the aircraft deviates further from the normal attitude and or airspeed the force increases up to an established maximum to encourage control movement in the direction necessary to return to the normal attitude and or airspeed range Except in the case of high airspeed when maximum force is reached force remains constant up to the maximum engagement limit Above the maximum engagement limit forces are no longer applied There is no maximum engagement
35. Position Up amp Locked In Transition Down and Locked Gear Failure EIS Engine Page LANDING GEAR LANDING GEAR 7 LANDING GEAR LANDING GEAR Landing Gear ndications 10 Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER AUDIO PANEL ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active DME TUNING 1 Press the DME Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC
36. Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Terrain Impact Warning or Ahead Pull Up T or Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Up Pull Obstacle Clearance or Up Warning ROC or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstade UMM Obstacle Ahead Pull Up Obstacle Impact Warning or Ahead Pull Up 0 a Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Terrain Clearance or or Caution RTC TERRAIN AHEAD Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AHEAD Terrain Ahead Terrain Ahead Impact Caution or or ITI CAUTION TERRAIN Caution Terrain Caution Terrain Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Caution Obstade Clearance or Obstacle Caution ROC OBSTACLE AHEAD or Obstacle Ahead Obstacle Ahead 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 85 saunqeay aoueplony SoJnpa204d Duruue d AEN 540 S24JV oipny uadx 513 sjueumasu puezey 346 U105 AEN 1461 jeuonippy uoneiedo Jeuuouqy iue E x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations
37. U KWIK Airport Directory database offers detailed information regarding services hours of operation lodging options and more for various airports This information is viewed on the WPT Airport Information Page The Airport Directory databases are revised every 56 days The Airport Directory is always available for use after the expiration date Check fly garmin com for the current database 64 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN 0 Additional Features View Airport Directory Information While viewing the WPT Airport Information Page if necessary press the INFO 1 Softkey to change the softkey label to display INFO 2 Airport information is displayed on the right half of the display SIRIUSXM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select XM Radio 3 Press 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 sel
38. Use the FMS Knob to enter the desired time HH MM and press the ENT Key Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message s m e q jeuonippy spay uoneiedo junuuy Jeuuouqy xipueddy 10 x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 67 Flight nstruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features G ARMIN Deleting a Scheduler Message 1 2 3 4 5 Select the AUX Utility Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted Press the CLR Key to clear the message text If the CLR Key is pressed again the message is restored Press the ENT Key while the message line is cleared to clear the message time When a scheduler message is waiting the MSG Softkey flashes Pressing the MSG Softkey opens the Messages Window and acknowledges the scheduler message Pressing the MSG Softkey again removes the Messages Window from the display and the scheduler message is deleted from the message queue PILOT PROFILES Creating a profile 1 2 3 4 5 6 7 68 Use the FMS Knob to select the AUX System Setup Page Pr
39. and fuel efficiency in statute miles per gallon MPG are calculated based on the displayed fuel remaining GAL REM and the fuel flow totalizer The calculated range also takes into account the aircrafts heading and the wind direction and speed 3f 2s BO 54 Adiusting the fuel totalizer quantity On the Engine Page use the DEC FUEL and INC FUEL softkeys to obtain the desired fuel remaining GAL REM Each press of the softkey increments or decrements in one gallon increments 52 AeN 549 Resetting the fuel totalizer On the Engine Page select the RST FUEL Softkey this resets displayed fuel remaining GAL REM to the maximum fuel capacity for the aircraft and fuel used to zero Duruue d Wil 2 FUEL CALC GAL REM Set Fuel Remaining GAL USED Calculated Fuel Used ENDUR k Calculated Endurance RANGE NM Calculated Range NMPG Fuel Efficiency eouepioAy paezey saunyea4 Jeuonippy Fuel Calculations Group xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 9 L Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index EIS A GARMIN LANDING GEAR INDICATIONS Landing Gear statuses are shown using the indications in the following table
40. angles may differ from the actual magnetic heading by more than 2 SVT DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVT DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER f 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 HOLD EXPIRED Holding EFC time expired Expect Further Clearance EFC time has expired for the User Defined Hold PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the PFD or MFD contains invalid data PFD1 or MFD1 CARD 2 ERR Card
41. d Terrain audio alerts are not configured properly The system should be serviced GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d MANIFEST GEA1 software mismatch communication halted The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced The 1 GEA 71 has incorrect software installed The G1000 system should be serviced GTX 33 33 W ES MESSAGE ADVISORIES 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 MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair XPDR1 FAIL XPDR1 is inoperative The 1 transponder should be serviced when possible There is no communication with the 1 transponder XPDR1 ADS B FAIL 1 unable to transmit ADS B messages ADS B is inoperative Other transponder functions may be available Service when possible 96 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN GRS 77 MESSAGE ADVISORIES Annunciations amp Alerts Message Commen
42. fai u Left fuel quantity in warning range Right fuel quantity in warning range Left st runnin arter motor energized when engine is g runnin g Right starter motor energized when engine is detect ed A failure of a gear system component has been or Landing gear are not down and locked Landing gear is selected UP on the ground Heater unit has sensed an overheat condition Triple Chime Underspeed protection is active AIRSPEED Optional 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole s n e 4 2 Duruue d AEN Sd5 S24JV olpny uqax Sia sjuauimasu 2 ni M102 AEN qb yeuonippv uoneiedo Jeuuouqv ii Eu x pul Annunciations 8 Alers Caution Annunciations Flight Instruments Annunciation Description Audio Alert Window Text 2 Left fuel quantity in caution range Right fuel quantity in caution range HE Pitot heat failure 38 Pitot heat selected OFF A failure of a gear system component has been Double Chime detected Landing gear are not down and locked 8 Hydraulic pump is running when it should not be a running z Advisory Annunciations Annunciation Description Audio Alert 2 Window Text E dd ca EU Emergency power in use E UAM TTE Fuel imbalance left
43. failure MFD does not automatically enter reversionary mode reversionary mode must be activated manually 52 MED failure PFD automatically enters reversionary mode Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel When the DISPLAY BACKUP Button is selected both displays enter reversionay display mode AEN Sd5 buluueld Wil NOTE The PA 44 180 Seminole Pilot s Operating Handbook POH always takes precedence over the information found in this section s mp 01d 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 PFD and MFD the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios aoueplony 2 soinjeo4 Jeuonippy 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 Sue v unuuy Loss of Hazard Functions with Loss of GPS Position xipuaddy x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 75 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additi
44. for the Piper PA 44 180 Seminole 79 saunjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy 2 Wil Tuo2 NeN Yid uoneiedo Jeuuouqy iie Eu x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ed Annunciations amp Alerts A GARMIN System Annunciation Comment Display system is not receiving airspeed input from air data computer Display system is not receiving altitude input from the air data computer Display system is not receiving vertical speed input from the air data computer Other Various Red X Indications A red X through any other display field such as engine instrumentation display indicates that the field is not receiving valid data 80 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN CAS ANNUNCIATIONS The following annunciations are configured specifically for the PA 44 180 Seminole aircraft See the PA 44 180 Seminole Pilot Operating Handbook POH for information regarding pilo t responses Warning Annunciations Annunciations amp Alerts Annunciation Window Text Description Audio Alert Right engine CHT Left engine CHT in warning range in warning range Left Alternator failure Right Alternator
45. garmin com by selecting Type 2 LOA Status Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance but does not constitute authorization to fly any and all terminal procedures that may be presented by the system It is the pilot s responsibility to operate in accordance with established AFM S and regulatory guidance or limitations as applicable to the pilot the aircraft and installed equipment NOTE If the pilot operator wants or needs to adjust the database contact Garmin Product Support to coordinate the revised DQRs NOTE Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to FlyGarmin com and select Report An Aviation Data Error Report Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Record of Revisions Part Number Change Summary 190 01462 00 Initial release 190 01462 01 Added GDU 13 08 Added Garmin AFCS Updated System Messages Added ESP Revision Date of Revision Affected Pages October 2014 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole RR 1 Record of Revisions
46. heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 71 5149 011 15 UTE seunpa20Jd Puluueld AEN 540 S24V oipny uadx si lu Tuo2 AEN eouepioAy paezey s n e 4 jeuonippy xipuaddy spay yjunuuy x pul Nav Com XPDR Audio Hazard Additional Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Annun Appendix Alerts Index Abnormal Operation GARMIN As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Current Track Indicator
47. link weather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age WARNING Do not rely on information from the lightning detection system display as the sole basis for hazard weather avoidance Range limitations and interference may cause the system to display inaccurate or incomplete information Refer to the documentation from the lightning detection system manufacturer for detailed information about the system WARNING The Garmin system as installed in this 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 WARNING Do not use the system until carefully reviewing and gaining a thorough understanding of all aspects of the system s Pilot s Guide documentation and the Airplane Flight Manual Do not attempt to learn system operational procedures while the aircraft is in the air For safety reasons system operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS syste
48. related to a high airspeed condition When ESP has been engaged for more than ten seconds cumulative not necessarily consecutive seconds of a 20 second interval the autopilot is automatically engaged with the flight director in Level Mode bringing the aircraft into level flight An aural Engaging Autopilot alert is played and the flight director mode annunciation will indicate LVL for vertical and lateral modes 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 71 SaJnpa oJd AEN 540 523 olpny uqax sia u102 AEN 2 s n ze 4 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 EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features GARMIN The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering CWS or Autopilot Disconnect AP YD DISC TRIM INTRPT switch Upon releasing the CWS or AP YD DISC TRIM INTRPT switch ESP force will again be applied provided aircraft attitude and or airspeed are within their respective engagement limits ESP can also be overridden by overpowering the servos mechanical torque limit ESP is automatically enabled on system power up To Enable or Disable ESP 1 Turn t
49. the BACK Softkey to return to the top level softkeys Transponder Softkeys Level 1 Level 2 Level 3 Description XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not reply to any interrogations ON Selects Mode A transponder replies to interrogations ALT Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations GND 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 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 111 So1nje2J aoueplony s mp oold Buruue d AEN Sd5 yi oipny uddx sia sjueumasu paezey wio gt AeN jeuonippy uoneiedo Jeuuouqy Sue v unuuy gt s o m x x pul iui nu A GARMIN Appendix _ Levell1 Level2 Level3 Description 55 EE VFR Automatically enters the VFR code 1200 in the U S A only CODE Displays transponder code selection softkeys 0 7 0 7 Use numbers to enter code Se BKSP Removes numbers entered one at a time 2a x ADS B TX Activates deactivates transmission of the Y aircrafts three dimens
50. the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB Verify the correct standby navigation database cycle information is shown for each display Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN 00000 Appendix Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by the AHRS GRS If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure GRS MV DB Update Available Update from 2005 to 2010 or CANCEL GRS Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS Mag Var Database STARTING UPLOAD 0 07 Uploading Database to GRS 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 121 saunjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax sia siu uinnsu jeuonippy 2 1ubil4 JUI0 NEN ql uoneiedo Jeuuouqy sue v unuuy L GARMIN Appendix Ssjueuinijsu fila 59 oipny uadx U105 AEN S2dV AeN Sd5 Duruue d Blank Page
51. the correct frequency for the approach 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts Message Comments SLCT NAV Select NAV on CD 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 past IAF IAF waypoint for parallel offset has been passed PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed NON WGS84 WPT Do not use GPS for navigation to boxx The position of the selected waypoint poo is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint STRMSCP FAIL Stormscope has failed Stormscope has failed The G1000 system should be serviced UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Unsupported leg type in flight plan The latera
52. 113 Traffic Advisory 53 Traffic map page 53 54 55 56 Transponder 11 111 112 V vertical path guidance 22 Vertical speed guidance 23 VNV 19 76 101 Voice alerts 81 W Warning alerts 81 Waypoint Selection Submenu 32 33 Weather data link page 50 Wind data 110 190 01462 01 Rev A A GARMIN Garmin nternational Inc 1200 Fast 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT Inc _ ae 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 213 Garmin Europe Ltd Liberty House Hounsdown Busin Southampton Hampshire 5040 9LR p 44 0 23 8052 4000 f 44 0 23 8052 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2013 2014 Garmin Ltd or its subsidiaries 190 01462 01 Rev A
53. 2 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 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 11 sjuauimasu nubi 59 S24V oipny uddx JUI05 AEN SH lV uonesado saunqea4 sanpa20Jq Buruuejd AEN 5649 junuuy jeuuouqy jeuonippy paezey Wfila x pu ddy x pul Flight Instruments Nav Com AFCS XPDR Audio EIS Abnormal Additional Hazard Flight Planning Annun GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Tum the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operation Pressing the MKR MUTE Key while playing a memory block stops play Pressing the PLAY Key during play begin
54. 2 is invalid The SD card in the bottom card slot of the PFD or MFD contains invalid data 102 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts Message Comments ESP OFF ESP selected off Electronic Stability and Protection has been disabled on the AUX SYSTEM SETUP 2 page ESP FAIL ESP is inoperative The ESP function has failed and is inoperative The system should be serviced ESP DEGRADE ESP IAS mode is inoperative IAS mode of ESP is inoperative The system should be serviced ESP CONFIG ESP config error Config service req d The system has detected a problem with the ESP configuration and should be serviced FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight plan successfully imported Flight Plan Import Export Results 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 successfully The file stored on the SD card did not contain a flight plan only user waypoints No stored flight plan data was modified These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import
55. 80 Seminole 190 01462 01 Rev A GARMIN ENGINE PAGE Press the ENGINE Softkey or turn the large FMS Knob and select the EIS Engine Page 3 TACH TIME HOURS FUEL CALC GAL REM 845 GAL USED 65 ENDUR 1 39 RANGE NM 807 LANDING GEAR NPG 85 o 000 O DEC FUEL INC FUEL RST FUEL Engine Page ELECTRICAL ALTR AMPS 2 El VOLTS BATT AMP v SYSTEH FLAPS 20 O Engine Manifold Displays manifold pressure in inches of Mercury in Hg to Pressure Gauge indicate engine power MAN IN HG Tachometer RPM Displays propeller speed in revolutions per minute rpm 0 Propeller Points towards the higher speed propeller when the Indicator propellers are out of sync Exhaust Gas Displays the temperature for the right and left Exhaust Temperature Gas Temperature for the hottest cylinder in F EGT F G Fuel Flow Indicator Displays fuel flow in gallons per hour gph FFLOW GPH 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 7 Flight Instruments E Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index EIS Oil Pressure Indicator OIL PSI Oil Temperature Indicator OIL F Landing Gear Status LANDING GEAR Fuel Calculations Group FUEL CALC Flap Setting Indicator SYSTEM 10
56. 9 Sjueuinsu u105 AEN nubi Duruue d Wil e uepioAy s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 54 A GARMIN GTS 800 Optional WARNING The Traffic Advisory System TAS is intended for advisory use only to aid the pilot in visually acquiring traffic No avoidance maneuvers should be based solely upon TAS traffic information It is the responsibility of the pilot in command to see and maneuver to avoid traffic NOTE Pilots should be aware of TAS system limitations TAS systems require transponders of other aircraft to respond to system interrogations If the transponders do not respond to interrogations due to phenomena such as antenna shading or marginal transponder performance traffic may be displayed intermittently or not at all Aircraft without altitude reporting capability are shown without altitude separation data or climb descent indication Pilots should remain vigilant for traffic at all times System Self Test 1 2 3 4 Set the range to 2 6 nm Press the STANDBY Softkey Press the TEST Softkey Self test takes approximately eight seconds to complete When completed successfully traffic symbols display and a voice alert T
57. 90 01462 01 Rev A A GARMIN Creating a user defined hold at a Direct To waypoint 1 Press a Direct to Key and set up the Direct To waypoint as desired but select HOLD instead of ACTIVATE when finished MFD or PFD 2 Use the FMS Knobs to edit the entry course and press the ENT Key 3 Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key 4 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 5 Use the FMS Knobs to edit the length and press the ENT Key 6 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 7 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key 8 Press the ENT Key while ACTIVATE is highlighted to activate the Direct To with the user defined hold defined at the Direct To waypoint Removing a user defined hold created at an active flight plan waypoint Flight Planning 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the HOLD waypoint 3 Press the CLR Key A Remove Holding Pattern confirmation window is displayed 4 Select OK and press the ENT Key The holding pattern is removed from the active flight p
58. A amp GARMIN Appendix APPENDIX sjuauimasu nubi PFD SOFTKEY MAP 53 OBS CDI DME XPDR IDENT TMRRREF NRST MSG Eg amp im o 7 HE 74 x ve SE nu 5 Dn 54 CDI GPS Top Level PFD 50 5 9 z r 7 um u Duruue d u u optional optional optional NEXRAD XM LTNG METAR BACK MSG F3 F3 P3 mrs m SoJnpa20Jd Select the BACK or OFF Softkey to return to the top level softkeys eouepioAy paezey Inset Map Softkeys saunqea4 jeuonippy Level 1 Level 2 Description uoneiedo Jeuuouqy CAS Displayed only when a sufficient number of items are displayed in the Annunciation Window to warrant scrolling Sue v unuuy CAS 1 When available scrolls up through the alerts when pressed CAS 4 When available scrolls down through the alerts when pressed gt s o s m x INSET Displays Inset Map in PFD lower left corner x pul OFF Removes Inset Map 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 107 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Description DCLIR 3 Selects desired amount of map detail cycles through declutter levels DC
59. 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 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 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN light Planning 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
60. Avoidance Traffic Symbol Description Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS 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 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 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 6 Press the TNA MUTE Softkey to mute the Traffic Not Available aural alert if desired Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 53 ACN Sd5 S24V oipny uadx 9
61. D Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed When power is cycled all messages are retained until deleted and message timer countdown is resumed sjuauimasu Yid oipny uddx UI0JNeN Entering a Scheduler Message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Tur the large FMS Knob to highlight the first empty scheduler message naming field 4 Usethe FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key 52 AEN 540 5 Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type Duruue d ni 6 Turn the small FMS Knob to select the message type Event Message issued at the specified date time s snp old One time Message issued when the message timer reaches zero default setting eouepioAy paezey e Periodic Message issued each time the message timer reaches zero 7 Press the ENT Key again or use the large FMS Knob to move the cursor to the next field 8 For periodic and one time message use the FMS Knob to enter the timer value HH MM SS from which to countdown and press the ENT Key 9 For event based messages a Use the FMS Knob to enter the desired date DD MM YY and press the ENT Key b Press the ENT Key again or use the large FMS Knob to move the cursor to the next field
62. G1000 Integrated Flight Deck Cockpit Reference Guide for the Piper PA 44 180 Seminole A GARMIN Copyright 2013 2014 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 1983 00 or later for the Piper PA 44 180 Seminole Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton Hampshire 040 OLR U K Tel 44 0 23 8052 4000 Fax 44 0 23 8052 4004 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 For after hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and o
63. Group and press the ENT Key Turn the large FMS Knob to select Profile Winds Turn the small FMS Knob to select On or Off Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings NOTE NEXRAD data cannot be displayed at the same time as terrain echo tops turbulence or icing data is displayed Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Hazard Avoidance SiriusXM Weather Products and Symbols Wx Product Status Icons Description US 3m CN Em x NEXRAD Available for the US and Canada The age of the displayed data for each is shown at the right b om ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed p 12m CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed QJ z XM LIGHTNING The age of the displayed data is shown at the right SIGMET 2m AIRMET 5m F us 8m CN 8m JL CELL MOVEMENT The age of the displayed data is shown at the right SIGMET amp AIRMET The age of the displayed data for each is shown at the right METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The a
64. Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN X U Abnormal operation A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the ovm aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored t is important to note that estimated navigation data supplied by the G1000 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 G1000 through DR while there is no
65. LIGHT PLAN 1 Press the FPL Key for the MFD 2 Tum 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 Press 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 for the MFD 2 Tum 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 Press the COPY Softkey A Copy to flight plan 22 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 for the MFD 2 Tum 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 Press the DELETE Softkey A Delete flight plan 4 confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and
66. LTR 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 WX LGND Displays icon and age on the Inset Map for the selected weather products optional TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window optional feature TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays SiriusXM lightning information on Inset Map optional feature METAR Displays METAR flags on airport symbols shown on the Inset Map optional 108 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN mumu r Ge Ezs 1 E991 Cae nn mn x Rs s 2 m z a a sjuauimasu nubi LAL wn 2201 NAVI Select the BACK Softkey to return to the top level softkeys BRG1 GPS x v JA optional optional H Emu BRG1 OFF 2 EY EY EY EN EY EY EN 73 74 IY EY NN l 1 1 METERS FA l T Msc L ome orm L
67. Piper PA 44 180 Seminole sjuaumasu nubi 59 olpny uqax uo2 AEN suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Appendix Index GPS Navigation GARMIN Altitudes associated with approach procedures are auto designated This means the system will automatically use the altitudes loaded with the approach for giving vertical flight path guidance outside the FAFE Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system will not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical flight path guidance Other displayed altitudes may change due
68. R 1 2 3 4 5 6 Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint Press the ENT Key The User Waypoint Information Page is displayed with the captured position NOTE If the pointer has highlighted a map database feature one of three things happens upon pressing the ENT Key 1 information about the selected feature is displayed instead of initiating a new waypoint 2 a menu pops up allowing a choice between Review Airspaces or Create User Waypoint or 3 anew waypoint is initiated with the default name being the selected map item Enter a user waypoint name up to six characters Press the ENT Key to accept the selected name If desired define the type and location i e LAT LON RAD RAD or RAD DIS of the waypoint Press the ENT Key to accept the new waypoint 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 31 s tin su nubi oipny uadx si U105 AeN 52 2 4 AEN 540 nubi eouepioAy paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 7 8 9 A GARMIN If desired change the storage method of th
69. Remove a Departure Arrival Approach or Airway from a Flight Plan 38 Store a Flight Plan teer cett e 38 Edit a Stored Flight Plan 39 Delete a Waypoint from the Flight Plan ss 39 Invert and Activate a Stored Flight Plan 40 Copy a Flight Plan Delete a Flight Plan etico Graphical Flight Plan Creation Export a Flight Plan to an SD Card PROCEDURES LD dde URS ER Load and Activate a Departure Procedure Activate a Departure Leg Load an Arrival Procedure Activate an Arrival Leg Load and or Activate an Approach Procedure 44 Activate an Approach in the Active Flight Plan 46 Activate a Vector to Final Approach Fix sss 46 Activate a Missed Approach in the Active Flight Plan 46 Temperature Compensated Altitude sssssseee 46 HAZARD AVOIDANCE inti 49 Customizing the Hazard Displays on the Navigation Map 49 SiriusXM Weather Optional 2 49 Traffic Systems ood eode od obe ed edu ed dale itas 52 Terrain and Obstacle Proximity 56 Terrain S VS 0007000 0200007 007000 e Da do 57 Terrain Awareness amp Warning System TAWS B Display Optional 59 ADDITIONAL 5
70. T PLANNING WEIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters Flight Planning The Weight Planning Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the Weight Planning Pge 1 Press 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 Enter the 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 Press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Turn the small FMS Knob to enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Turn the small FMS Knob to enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor 7 Press the ENT Key TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the Trip Planning Page 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL Softkey 190 01462 01 Rev
71. Taxi Airport Terrain Obstacle and Airport Directory Databases These databases may be copied to one Supplemental Data Card then automatically synchronized to other card in the system 1 2 3 4 5 6 7 8 9 10 11 12 116 VVith system povver OFF remove the MFD database card from the bottom card slot of the MFD Update the basemap SafeTaxi airport terrain obstacle and or airport directory 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 If a Verifying message is seen wait for 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 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system 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 Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each disp
72. V VPTH an active vertical profile Key VNV Target Altitude Captures the Vertical Navigation AV Capture VNV Target Altitude Glidepath Captures and tracks the WAAS GP glidepath on approach ma Captures and tracks the LS Glideslope i GS glideslope on approach Commands a constant pitch angle Takeoff and wings level on the ground in TO preparation for takeoff GA Disengages the autopilot and Switch Go Around commands a constant pitch angle GA and wings level in the air Commands a zero degree pitch LVL IL angle and wings level Button ALTS armed automatically when PIT VS FLC TO or GA active and under VPTH when Selected Altitude is to be captured instead of VNV Target Altitude ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude 16 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN LATERAL MODES AFCS Lateral Mode Roll Hold Heading Select Navigation GPS Navigation VOR Enroute Capture Track Navigation LOC Capture Track No Glideslope Navigation Backcourse Capture Track Approach GPS Approach VOR Capture Track Approach LOC Capture Track Glideslope Mode automatically armed Takeoff Go Around Level The Heading Navigation GPS and Navi Description Holds the current aircraft roll attitude or rolls the wings level depending on the commanded
73. al Hazard Alerts Operation Features Avoidance Procedures Appendix Index 14 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis AFCS 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 Control Pressed FD Key AP Key CWS Button GA Switch ALT Key VS Key VNV Key NAV Key APR Key HDG Key Modes Selected Lateral Vertical Roll Hold default ROL Pitch Hold default PIT Roll Hold default ROL Pitch Hold default PIT Roll Hold default ROL Pitch Hold default PIT Takeoff on ground TO Takeoff on ground TO Go Around in air GA Go Around in air GA Roll Hold default ROL Altitude Hold ALT Roll Hold default ROL Vertical Speed VS Roll Hold default ROL Vertical Path Tracking VPTH GPS Navigation i Pitch Hold default PIT BC GPS Approach VOR Pitch Hold default PIT LOC Heading Select HDG Pitch Hol
74. amp Alerts A GARMIN PFD MFD MED Alert Type TAWS B Page Aural Message ee Pop Up Alert Annunciation mminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Ahead mpact Caution or or 10l CAUTION OBSTACLE Caution Obstacle Caution Obstacle Premature Descent TERRAIN 100 Low TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Fve Hundred 500 Excessive Descent TERRAIN RATE Sink Rate Rate Caution EDR Negative Cimb TERRAIN pors Don t Sink Rate Caution or or NCR T00 LOW TERRAIN Too Low Terrain TAWS B SYSTEM STATUS ANNUNCIATIONS Alert Type H M i TAWS B Page Annunciation Aural Message Annunciation TANS System System Test Pass None None Test OK TAWS Alerting is disabled TAWS INH None None MFD Terrain or Obstacle database unavailable or invalid TAWS operating None None with PFD Terrain or Obstacle databases TAWS B System Test Fail 5 Failure Terrain or Obstacle database unavailable or TAWS System invalid invalid software E dM Failure configuration system audio fault 86 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations amp Alerts GPS signal Out of database coverage area PFD MFD Alert 7 Annunciation No GPS position Ex
75. an navigation database update Verify use of airways in stored flight plans and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach 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 penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm APR INACTV Approach is not active Special use airspace is within 2 nm of the aircraft position The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach 100 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select
76. and between 12 and 50 nose down Maximum opposing force is applied between 25 and 50 nose up and between 22 and 50 nose down The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel This force is intended to encourage movement in the pitch axis in the direction of the normal pitch attitude range for the aircraft There are no indications marking the pitch ESP engage and disengage limits in these nose up nose down conditions 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 13 uonesado aoueplony s mp oold Buruue d AEN Sd5 yi oipny uadx 913 siu umnnsu unuuy jeuuouqy paezey xipuaddy x pul ui wo gt AeN n gt a 2 z GARMIN itional Features Add Sjueuinijsu fila 59 olpny uddX u102 AEN S2dV AeN Sd5 Duruue d r Blank Page 6 2 4 aoueplony puezey s l Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 74 GARMIN 0 Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE In reversionary mode critical flight instrumentation is combined with engine m instrumentation on the remaining displays When a system detected failure occurs the display reversionary modes are as follows s tin sul nubi olpny uqax 0105 AEN PFD
77. appear above the airspeed indicator If the aircraft continues to decelerate Underspeed Protection becomes active Vertical flight director modes can be divided into two categories Those in which it is important to maintain altitude for as long as possible altitude critical modes and those in which maintaining altitude is less crucial non altitude critical modes Altitude Critical Modes ALT GS GP TO GA FLC If the aircraft decelerates to stall warning the lateral and vertical flight director modes will change from active to armed and the autopilot will provide input causing the aircraft to pitch down and the wings to level An aural AIRSPEED alert will sound every five seconds and a red USP ACTIVE annunciation will appear to the right of the vertical speed indicator see Annunciations and Alerts The pitch down force will continue until the aircraft reaches a pitch attitude at which IAS equals the IAS at which stall warning turns off plus two knots When airspeed increases as a result of adding power thrust to above the IAS at which stall warning turns off plus two knots the autopilot will cause the aircraft to pitch up until recapturing the vertical reference and the vertical and lateral flight director modes will change from armed to active Non Altitude Critical Modes VS VNAV IAS When the airspeed trend vector reaches a predetermined airspeed specific to each flap setting a single aural AIRSPEED wi
78. ard prior to its effective date The Jeppesen Navigation Database is available from Jeppesen seven days prior to its effective date NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of the PFD and the MFD 3 Turn the system ON A prompt is displayed DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON R AFTER 00 00 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO REGION WORLDWIDE WORLDWIDE 204 1285 CYCLE EFFECTIVE 9 APR 2012 07 MAY 2812 EXPIRES 7 MAY 2812 04 1UN 2812 NO WILL BE ASSUMED IN 21 SECONDS 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 119 sainjea4 aueplony s mp o d Duruue d AEN Sd5 241V oipny uddx sia siu uinnsu jeuonippy 2 Wil Tuo2 NeN nubi uoneiedo Jeuuouqy Sue v unuuy k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix 6 GARMIN
79. ata card is properly inserted Replace data card If problem persists 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 90 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts Message Comments DB MISMATCH Navigation database version mismatch Xtalk is off The PFD and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Standby Navigation database mismatch The PFD and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or types installed Install correct terrain databas
80. ation Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A amp GARMIN ____ Waring Cautions k Notes NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 Ifyou have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication if the air or on the ground Go to FlyGarmin com and select Aviation Data Error Report NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not int
81. ce facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 115 sainjea4 aoueplony 2 buluueld AEN Sd5 S24JV oipny uddx sia siu un sul jeuonippy 2 nubi Tuo2 NeN qb uoneiedo Jeuuouqy Sue v unuuy Feed Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix CCUG ARMIN Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Updating Basemap Safe
82. cessively degraded TAWS NA None TAWS B Page Annunciation Aural Message TAWS Not Available TAWS Not Available Sufficient GPS signal received after loss None TANS Available GDL 69 69A DATA LINK RECEIVER MESSAGES Message 190 01462 01 Rev A Message Location XM Information Page Descr Data Link Rece iption iver antenna MFD error service required XM Information Page 1 Data Link Receiver updating MFD encryption code XM Information Page Weather Datalink Page 7 MFD XM Radio Page MFD Acquir ng channel audio or nformation XM Radio Page MFD Channel not in service XM Radio Page MFD issing channel information Weather Datalink Page lo communication from Data Link Receiver within last 5 MFD nutes XM Information Page SiriusXM subscription is not MFD activated Weather Datalink Page SiriusXM subscription is MFD activating SiriusXM subscription 25 confirmed downloading MFD vveather data Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 87 soinjeo4 9e2uepioAy s mp old Duruue d ACN 540 S24V olpny uqax s q Sjueuinijsu 2 nubi uio AeN BATE jeuonippy uoneiedo jeuuouqy ic R x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additi
83. d PFD1 COOLING PFD1 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage 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 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 serviced if the problem persists 88 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts Message Comments 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 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 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
84. d 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 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 15 sia siu u nnsu oipny uadx 0105 AEN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d Tunuuy Jeuuouqy Jeuonippy xipueddy x pul iui nu paezey Flight Instruments Nav Com XPDR Audio GPS Nav AFCS Flight Planning Abnormal Additional Hazard Avoidance Annun Procedures Appendix Alerts Operation Features Index A ARS 08 70 08 GARMIN VERTICAL MODES Vertical Mode Description con Annunciation Holds the current aircraft pitch Pitch Hold attitude may be used to climb default PIT descend to the Selected Altitude 77174 Captures the Selected Altitude ALTS Capture Altitude Hold Holds the current Altitude Reference ALT Key nnnnn rr Maintains the current aircraft Vertical Speed vertical speed may be used to dimb VS Key VS nnnn Fem descend to the Selected Altitude Maintains the current aircraft Flight Level Change airspeed while the aircraft is FLC Key FIC nma IAS Hold dimbing descending to the Selected Altitude Vertical Path Tracking Captures and tracks descent legs of VN
85. d paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Enable Disable Aviation Data 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Show or Hide Aviation Data Press the ENT Key TAWS Inhibit NOTE If TAWS B alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed press 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 press 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 60 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL WARNING Use appropriate primary systems for navigation and for ter
86. e 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 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 desired waypoint within the arrival Press 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 44 1 2 3 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Select the airport and approach a Use the FMS Knob to select an airport and press the ENT Key b Select an approach from the list and press the ENT Key Or Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Procedures a If necessary push the FMS Knob to exit the approach list and use the large FMS Knob to move the cursor to the APPROACH CHANNEL field b Use the FMS Knob to enter the approach channel number and press the ENT Key to accept the approach channel number The airport and approach are selected 4 A li
87. e implied warranties of formation is provided as is and esentations regarding its accuracy WIK Organizations and to the d hold harmless AC U KWIK Organizations to any actual or alleged inaccuracies in the information in the datasets Some jurisdictions lied warranties or liability for incidental or S pose The in e any rep ue AC U K e above limitations or exclusions may not apply to licensee Printed in the U S A amp GARMIN Notes e e WARNING Do not use the terrain avoidance feature as the sole means of navigation and terrain separation The terrain avoidance feature is only to be used as and aid to terrain avoidance Garmin obtains terrain database content from third party sources and is not able to independently verify the accuracy of the terrain data WARNING Do not rely on the displayed minimum safe altitude MSAs as the sole source of obstacle and terrain avoidance information The displayed minimum safe altitudes MSAs are only advisory in nature Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING Do not use GPS derived geometric altitude for compliance with air traffic control altitude requirements in the National Airspace System NAS or internationally The primary barometric altimeter must be used for compliance With all air traffic control altitude regulations requirements instructions and clearance
88. e version or type in all displays Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database installed Install correct obstacle database in all displays Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 91 s m aoueplony SoJnpa204d Duruue d AEN 540 S24JV oipny uadx 513 sjueumasu puezey ubi Wo gt AeN BUTTER jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN Message Comments DB MISMATCH Airport Terrain database mismatch The PFD and MFD have different airport terrain databases installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchron
89. e waypoint to TEMPORARY or NORMAL by moving the cursor to TEMPORARY and pressing the ENT Key to check or uncheck the box Press the FMS Knob to remove the flashing cursor Press the GO BACK Softkey to return to the map page DELETE A USER WAYPOINT 1 2 3 4 5 6 1 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Press the DELETE Softkey The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A FLIGHT PLAN 32 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or sel
90. e when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key for the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure 4 Press 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 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 43 oipny uddx s q sjuauimasu U105 AEN 16114 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 0000000 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 larg
91. ebsite at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole A Warnings Gatans S Motes GARMIN 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 le
92. ect a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN ight Planning Creating a stored flight plan 1 Press the FPL Key 2 Tum the small FMS Knob clockwise to display the Flight Plan Catalog Page 3 Press the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window siu uinnsu iui 59 oipny uddx UI0JNeN with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway vvaypoints 5 Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key 6 Repeat step numbers 4 and 5 to enter each additional flight plan waypoint 7 When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in
93. ected category of audio 1 Press the CATGRY Softkey on the XM Radio Page 2 Press the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page press the CHNL Softkey 2 Press the CH Softkey to go down through the list in the Channel Box or move up the list with the CH Softkey 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 65 uonesado s n e 4 s mp oold Buruue d AEN Sd5 2 444 sia sjueumasu unuuy jeuuouqy jeuonippy paezey il 0105 AEN ubi xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features _ GARMIN 66 Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page press the CHNL Softkey 2 Press the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Press the numbered softkeys located on the bo
94. ended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft NOTE The pilot operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation The database alerts can be viewed at www flygarmin com by selecting Aviation Database Alerts NOTE The pilot operator must review and be familiar with Garmin s database exclusion list as discussed in SAIB CE 14 04 to determine what data may be incomplete The database exclusion list can be viewed at www flygarmin com by selecting Database Exclusions List 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole A Wamings Cautions amp Notes GARMIN NOTE The FAA has asked Garmin to remind pilots who fly with Garmin database dependent avionics of the following It is the pilot s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements DQRs by virtue of a Type 2 Letter of Authorization LOA from the FAA A copy of the Type 2 LOA is available for each database and can be viewed at http fly
95. er PA 44 180 Seminole 190 01462 01 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 GPS Navigation 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually NOTE Temperature Compensated TEMP COMP altitudes are depicted as slanted text ACTIVE FLIGHT PLAN KIXD KDFW 2277 11 7NM 13000FT nsertion C 221 3 2 12400FT m 220 8 0NM 9900FT Approach KDFH RNAV 17Lsps LPY RIVET iaf 9 18 8NM 4000 DRAAK 3 3NM 2000FT INWOD 76 3 2NM MENOL faf i 3 9NM RW17L map 176 5 3NM 930FT 174 8NM POLKE RISUS Cross AT or ABOVE 5 000 fi PAGO Cross AT 2 300 fi Cinn Cross AT or BELOW 3 000 ft Large White Large Light Blue Text Sma Blue Tex Sma Blue Subdued Text Sma wi ext l Light Light White Text th Altitude Res riction Bar 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the
96. erts A GARMIN Message Comments MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists 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 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 MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFD detected a failure in the SafeTaxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced The MFD detected a failure in the ChartView database optional feature Ensure the data card is properly inserted Replace data card If problem persists system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure the d
97. ess the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight CREATE in the Pilot Profile Box Press the ENT Key A Create Profile window is displayed Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key Pilot profile names cannot begin with a blank as the first letter In the next field use the small FMS Knob to select the desired settings upon which to base the new profile Profiles can be created based on Garmin factory defaults default profile settings initially based on Garmin factory defaults unless edited by the pilot or current system settings Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN 8 With CREATE highlighted press the ENT Key to create the profile Or Use the large FMS Knob to select CREATE and ACTIVATE and press the ENT Key to activate the new profile 9 To cancel the process select CANCEL with the large FMS Knob and press the ENT Key Selecting an active profile 1 Use the FMS Knob to select the AUX System Setup Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Tum the large FMS Knob to highlight the active profile field in the Pilot Profile Box 4 Turn the small FMS Knob to display the pilot profile list and highlight the desired profile 5 Press the ENT Key The system loads and displa
98. euonippy 2 Wil Tuo2 NeN uoneiedo Jeuuouqy sue v unuuy L A Appendix 6 GARMIN Loading the leppesen Navigation Database as the Active Navigation Database Flight Instruments The Jeppesen Navigation Database that is loaded to internal memory as the active database will be used by the system EIS NOTE Loading the Jeppesen Navigation Database as the active database prior to its effective date vvill result in the expiration date on the povver up screen and the effective date on the AUX System Status Page being displayed in yellow Nav Com XPDR Audio AFCS A NOTE After the navigation database is loaded or copied the top SD card may be removed GPS Nav 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD or MFD to be updated label of SD card facing left 2 Turn the system ON A prompt is displayed in the upper left corner of the display Flight Planning Procedures DO YOU WANT T UPDATE THE STANDBY NAVIGATION DATABASE N THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 00 00 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO REGION WORLDWIDE WORLDWIDE Hazard Avoidance CYCLE 1204 1285 09 RPR 2012 7 MAY 2012 7 MAY 2812 04 1UN 2012 N WILL BE ASSUMED IN 21 SECONDS Additional Features 3 Press the NO Softkey
99. ex Hazard Avoidance A GARMIN Displaying Weather on the SiriusXM Weather Data Link Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the SiriusXM Weather Data Link Page Press the available softkeys to select the desired SiriusXM Weather product Press 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 SiriusXM Weather Data Link Page 1 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs 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 Enabling disabling winds aloft data display in Profile View 1 2 3 4 5 6 7 50 Select the Navigation Map Page Press the MENU Key With Map Setup highlighted press the ENT Key Turn the small FMS Knob to select the Profile
100. ey The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation using the PFD 1 Press the Direct to Key Z on the PFD 2 Tum the large FMS Knob to place the cursor in the desired selection field GPS Navigation 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 to place the cursor over the ALT altitude field 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 19 sjuaumasu nubi 59 oipny uddx JUI0JNeN ACN 540 52 Suelv uoneiedo sainjea4 aoueplony sainpadold Duruue d unuuy Jeuuouqy Jeuonippy 2 Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS 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 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
101. f any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and 610006 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin f NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications Honeywell and Bendix King are registered trademarks of Honeywell International Inc SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio Inc AOPA Membership Publications Inc and it AOPA expressly disclaim all warranties with data express or implied including but not lim and fitness for a particular purpose warrant or make any representations regard no circumstances including negligence sha consequential damages that result from the possibility of s by to any actual or alleged inaccuracies in the in limitation or exclusion of implied warranties 0 so the above limitations or exclusions may not AC U KWIK and
102. ge of the displayed data for each is shown at the right The selected forecast period is Shown at the bottom FREEZING LEVEL The age of the displayed data is shown at the right WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right CYCLONE WARNING The age of the displayed data is shown at the right AIREP The age of the displayed data is shown at the right 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 51 AEN Sd5 S24V oipny uadx s z syuauinyysuy Tuo2 AEN 364 Duruue d u u s mp oold paezey xipuaddy suelv uoneiedo SoJnjeaJ unuuy qeuuouqy Jeuonippy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Wx Product Status Icons Description a 8m PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow iss TURBULENCE The age of the displayed data is shown at the right The VATES MEM altitude selection is shown at the bottom Ell ICING POTENTIAL The age of the displayed data is shown at the right B R
103. he large FMS Knob to select the AUX Page Group 2 Tum the small FMS Knob to select the System Setup Page 3 If necessary select the SETUP 2 Softkey to display the AUX SYSTEM SETUP 2 Page 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to place the cursor in the STABILITY amp PROTECTION field 6 Turn the small FMS Knob to select ENABLE or DISABLE 7 Press the FMS Knob to remove the cursor Roll Engagement Roll Limit Indicators are displayed on the roll scale at 45 right and left indicating where ESP will engage As roll attitude exceeds 45 ESP will engage and the on side Roll Limit Indicator will move to 30 The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases Once engaged ESP force will be applied between 30 and 75 The force increases as roll attitude increases and decreases as roll attitude decreases The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude As roll attitude decreases ESP will disengage at 30 ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75 72 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Additional Features Pitch Engagement ESP engages at 18 nose up and 17 nose down Once ESP is engaged it will apply opposing force between 15 and 50 nose up
104. highlighted 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted USER DEFINED HOLDING PATTERNS A holding pattern can be defined at any active flight plan waypoint or at the aircraft present position Creating a user defined hold at an active flight plan waypoint 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the waypoint for the hold 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 35 oipny uddx UI0JNeN 52 2 suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 36 3 4 5 6 7 8 9 10 A GARMIN Press the MENU Key highlight Hold At Waypoint and press the ENT Key The HOLD AT window appears with the course field highlighted Use the FMS Knobs to edit the entry course and press the ENT Key Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key Use the small FMS Knob to select TIME or DIST length mode
105. 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 104 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts PILOT PROFILE IMPORT EXPORT MESSAGES Pilot Profile Import Export Results Description No pilot profile plan files found to import Displayed if the SD card does not have one or more valid pilot profile filenames Ove
106. io Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 5 GARMIN View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Press the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 4 Press the GO BACK Softkey to return to the previous page Change Day Night View 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options 4 Turn the small FMS Knob to choose between the On and Off Full Screen Options 5 Tum the small FMS Knob to choose between Day Auto and Night Options 6 In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity 7 Press the FMS Knob when finished to remove the Chart Setup Menu AIRPORT DIRECTORY The Aircraft Owners and Pilots Association AOPA or AC
107. ional position and aircraft heading for reception by ADS B systems IDENT Activates the Special Position Identification 5 SPI pulse for 18 seconds identifying the transponder return on the ATC screen 22 TMR REF Displays Timer References Window NRST Displays Nearest Airports Window 5 MSG Displays Message Window SOFTKEY MAP 55 ps zg A T A optional E Press the ENGINE Softkey to return E 2 f L to the previous softkey level EY v3 v V3 794 pares Default softkey ES is dependant on Press the BACK Softkey on this es the selection made level to return to the top softkey level So in the map setup a 8 optional options optional optional eric 1 PROFILE TOPO TERRAIN AIRWAYS NEXRAD XMLING METAR tEGEND BACK nn F3 A VF se E 2 AIRWY ON AIRWY LO x AIRWAY HI MFD Softkeys 112 Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Level 4 Description ENGINE Displays the default engine softkey level Press again to return to the previous softkey level DEC FUEL Press to decrease fuel quantity in 1 gallon increments INC FUEL Press to increase fuel quantity in 1 gallon increments RST FUEL Resets remaining fuel to Zero Enables second level Navigation Map softkeys TRAFFIC PROFILE Displays traffic information o
108. ists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations 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 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 99 saunqea4 2 Buruuejg AEN 5640 24V oipny uddx sia syu unysu paezey Wil jeuonippy uoneiedo Jeuuouqy es p x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ee Annunciations amp Alerts A GARMIN Message Comments 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
109. it Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN c Turn the large FMS Knob to select the desired user waypoint d Press the ENT Key 6 Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN Flight Planning sjuauimasu sub 59 1 Press the FPL Key 2 Press the FMS Knob to activate the cursor not required on the PFD 3 Turn the large FMS Knob to highlight the waypoint after the desired airway entry point The airway is inserted before the highlighted waypoint as shown by the insertion point indicator If this waypoint is not a valid airway entry point a valid entry point should be entered at this time 4 Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey or press the MENU Key and press 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 as indicated by the insertion point indicator 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 2 AEN 540 nubi 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is
110. ization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DISABLED Terrain Awareness DB resolution too low Terrain database of sufficient resolution 9 arc second or better is not currently installed TERRAIN DSP PFD1 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347 MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailable The system should be serviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The System should be serviced GMA1 SERVICE GMAT needs Service Return unit for repair The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible 92 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole
111. l Flight nstruments E Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index EIS Engine Manifold Pressure Gauge MAN IN HG Tachometer RPM 0 Indicator Exhaust Gas Temperature EGT F G Fuel Flow Indicator FFLOW GPH 5 Oil Pressure Indicator OIL PSD Oil Temperature Indicator OIL F Alternator Current ALTR AMPS Voltage VOLTS Battery Current BATT AMPS 11 Fuel Quantity Indicator FUEL QTY GAL A GARMIN Displays manifold pressure in inches of Mercury in Hg to indicate engine power Displays propeller speed in revolutions per minute rpm Points towards the higher speed propeller when the propellers are out of sync Displays the temperature for the right and left Exhaust Gas Temperature for the hottest cylinder in F Displays fuel flow in gallons per hour gph Displays oil pressure in pounds per square inch psi Displays oil temperature in degrees Fahrenheit F Displays each alternator current in amperes Displays the bus voltage Displays the battery current in amperes Displays the amount of fuel in gallons gal for each side of a standard fuel tank 2 Landing Gear Status Displays landing gear status LANDING GEAR 6 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 1
112. l 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 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 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 101 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu piezeH ubi UI05 AeN 3461 uoneiedo Jeuuouqy em E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Eod Annunciations amp Alerts A GARMIN Message Comments 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 or the GIA 63W 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
113. lan Select CANCEL and press the ENT Key to cancel the removal of the holding pattern Removing a user defined hold created at the aircraft present position or at a Direct To waypoint 1 Press the Direct To Key to display the DIRECT TO Window PFD or MFD 2 Press the MENU Key to display the PAGE MENU with the cursor on the Cancel Direct To NAV selection 3 Press the ENT Key The holding pattern is removed 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 37 oipny uddx s q sjuauimasu U105 AEN 16114 52 2 4 AEN 540 nubi eouepioAy paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Flight Procedures Planning GPS Nav Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Appendix Alerts Operation Features Index Flight Planning A GARMIN INVERT AN ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT 1 2 3 4 PLAN Press the
114. lay Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Appendix Updating Terrain FliteCharts and ChartView Databases These databases must be copied to both Supplemental Data Cards 1 2 3 4 5 6 7 8 9 With system power OFF remove the Supplemental Data Card from the bottom card slot of the MFD and PFD Update the terrain and or FliteCharts or ChartView databases on each of the Supplemental Data Cards Insert the updated Supplemental Data Cards into the bottom card slot of the MFD and PFD Apply power to the system check that the databases are initialized and displayed on the power up screen A Verifying message may be seen If this message is present wait for 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 Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display Remove power from the system 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 117 sainjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuauimasu j
115. ld be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The system should be serviced GTS 800 MESSAGE ADVISORIES Message Comments GTS CONFIG GTS config error Config service req d The GTS and GDU have incompatible configurations This alert is also set when the GTS has an invalid mode address configured or the mode S address does not match both XPDR mode S addresses MANIFEST GTS software mismatch communication halted The GTS has incorrect software installed The system should be serviced 98 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN GDC 74A MESSAGE ADVISORIES Annunciations amp Alerts Message Comments MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The system should be serviced MISCELLANEOUS MESSAGE ADVI SORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer ex
116. ll sound alerting the pilot to the impending underspeed condition If the aircraft decelerates to an IAS below the minimum commandable autopilot airspeed a red USP ACTIVE annunciation will appear to the right of the vertical speed indicator The vertical flight director mode will change from active to armed and the autopilot will cause the aircraft to pitch down until reaching a pitch attitude at which IAS equals the minimum commandable autopilot airspeed 18 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 Press the Direct to I Key on the MFD 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob 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 Tum the small FMS Knob to select MSL or AGE 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 K
117. lready stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key vvhen 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 The flashing cursor moves to the fuel onboa
118. m 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A amp GARMIN Cautions Notes WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the Pilot s Guide documentation and the 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 Do not use the system to attempt to penetrate a thunderstorm The illustrations in this guide are only examples Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding any thunderstorm identified as severe of giving intense radar echo by at least 20 miles WARNING Lamp s inside this product contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our w
119. mits 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 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 97 s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V olpny uqax 913 Sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy uic Eu x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts GMU 44 MESSAGE ADVISORIES A GARMIN Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The system shou
120. n Navigation Map optional Displays removes Profile View on Navigation Map Page TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 113 sainjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy piezeg nubi Tuo2 NeN nubi uoneiedo Jeuuouqy Sue v yunuuy ES eed Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Level 4 Description AIRWAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed INEXRAD Displays NEXRAD weather and coverage information on the Navigation Map optional XM LING Displays XM lightning information on Navigation Map optional feature XM lightning and Stormscope lightning are mutually exclusive when displaying on the Navigation Map METAR Displays METAR flags on airport symbols shown on the Navigation Map opti
121. ns 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 When using Stormscope there are several atmospheric phenomena in addition to nearby thunderstorm that can cause isolated discharge points in the strike display mode However clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleaned NOTE Do not rely upon data link services to provide Temporary Flight Restriction TFR information Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control NOTE All visual depictions contained within this document including screen images of the panel and displays are subject to change and may not reflect the most current system and databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired oper
122. oftkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys CHANGE NAVIGATION SOURCES 1 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency 3 Press the CDI Softkey a third time to return to GPS 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 1 uonesado s n e 4 aoueplony s mp oold Buruue d AEN Sd5 2 444 sia junuuy jeuuouqy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Press the OBS Softkey to select OBS Mode 2 Turn a CRS Knob to select the desired course to from the waypoint Press the CRS Knob to synchronize the Selected Course with the bearing to the next 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 p
123. oftware mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The system should be serviced 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 93 saunqea4 aDueplony seinpa2o0Jd Buruuejg AEN Sd 24V oipny uadx sia syu unysu paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy es Du x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN Message Comments mismatch comm MANIFEST GFC software unication halted Incorrect servo software is installed or gain settings are incorrect MANIFEST CO mismatch comm M1 software unication halted MANIFEST CO mismatch comm M2 software unication halted The COM1 and or COM2 has incorrect software installed The system should be serviced mismatch comm MANIFEST NAV1 software unication halted MANIFEST NAV2 software mismatch communication halted The NAV1 and or NAV2 has incorrect software installed The system should be serviced COM1 CONFIG COM config error Config service req d COM2 CONFIG COM config error Config service req d The COM1 and or COM2 configuration set
124. onal LEGEND Displays the legend for the selected weather products Available only when NEXRAD XM LTNG PROFILE and or METAR softkeys are selected 114 BACK Returns to top level soft keys Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Level 4 Description DCLIR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHW CHRT When available displays optional airport and terminal procedure charts LOADING UPDATED DATABASES CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in main tenance being required to reboot the system SYSTEM STATUS Page NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized servi
125. onal Abnormal Operation Index Appendix Ed Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFD are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair service Return unit for repair MFD1 SERVICE MFD1 needs The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 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 The MFD configuration settings do not match backup configuration memory The system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFD have different software versions installed The system should be service
126. onal Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations Transponder Status Barometric Minimum AFCS Annunciations Box Descent Altitude Box Flight Director System Time Glideslope Glidepath Command Bars PFDSetup Menu and Vertical Deviation nset Map Windows displayed in Indicators Temperatures the lower right corner Altimeter Barometric DME Information of the PFD Setting Window Timer References Selected Altitude Wind Data Nearest Airports e VNV Target Altitude Selected Heading Box Flight Plan Selected Course Box Messages Procedures Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 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 G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position 16 Garmin G1000 Cockpit Reference
127. or L L L L vse E V3 IY F3 EM EN non n n n onm pss Farma S 1L 1L ae vo vvmxumummmummm PFD Configuration Softkeys 52 NEN 540 Wil SeJnpa20Jd Level 1 Level 2 Level 3 Description 2 PFD Displays second level softkeys for amp additional PFD configurations gt SYN VIS Displays the softkeys for enabling or H 5 disabling Synthetic Vision features PATHVVAY 1 Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan uoneiedo Jeuuouqy Sue v unuuy SYN TERR Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero Pitch line gt 5 o z m x x pul 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 109 Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm DFLTS Resets PFD to default settings including changing units to standard WIND Displays softkeys to select wind data parame
128. ort The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing 62 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Additional Features the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView Optional ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on
129. pact ERRAIN Foma asra Caution Obstacle Obstacle TERRAIN SVT SYSTEM STATUS ANNUNCIATIONS disabled PFD MFD Alert TERRAIN SVT Page Alert Type Annunciation Annunciation Aural Message System Test in Terrain System System Test Pass None None Test OK Terrain Alerting is TER M finis None MFD Terrain or Obstacle database unavailable or invalid received after loss Terrain SVS operating Nong with PFD Terrain or Obstacle databases Terrain System Test TER FAIL Terrain System Terrain or Obstacle database unavailable or invalid TER FAIL Terrain System invalid software Failure configuration system audio fault No GPS position TER WA Sisto ot Available Excessively degraded GPS signal Out of TER WA Nin errain Sys em database coverage ot Available area Sufficient GPS signal None None Terrain System Available 84 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts TAWS B ALERTS PFD MFD MFD Alert Type TAWS B Page Aural Message bs Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Pull Up Terrain Clearance or or Warning RTC Terrain Ahead Pull Up
130. peration Features Index A Hazard Avoidance GARMIN TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Terrain Proximity Page 3 If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 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 Black below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map 3 Terrain and obstacles may be displayed in the Profile View by selecting the PROFILE Softkey Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A 1 sean Avaidanes TERRAIN SVS A NOTE Terrain SVS is only available when
131. press the ENT Key 40 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Flight Planning 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 as indicated by the insertion point indicator Turn the large FMS Knob to select the desired insertion point Press 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 Insert the SD card into 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 the large FMS Knob to highlight the flight plan to be exported Press the EXPORT Softkey Press the ENT Key
132. procedure into the active flight plan and activates the first leg of the approach S 24V oipny uddx 59 sjuauimasu Tu102 AEN sub AEN Sd5 Duruue d Jubii uonesado saunqee4 jeuonippy paezey jeuuouqy Sue v unuuy 12 Press the ENT Key 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 45 xipueddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window is displayed 4 With ACTIVATE highlighted press the ENT Key Or Press the Go around Switch TEMPERATURE COMPENSATED ALTITUDE When temperature compensated altitude is enabled for the loaded approach the altitudes associated with the approach waypoints are displayed in slan
133. raffic Advisory System Test Passed is heard If the self test fails the system reverts to Standby Mode and a voice alert Traffic Advisory System Test Failed is heard Enabling Disabling Flight ID Display On the Traffic Map Page press the FLT ID Softkey Displaying Traffic on the Traffic Map Page 1 2 3 4 5 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic mode field Press the ALT MODE Softkey to change the altitude volume Press the STANDBY Softkey to place the system in the Standby mode STANDBY is displayed in the Traffic mode field Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN 6 Tum the RANGE Knob clockwise to display a larger area or counter clockvvise to display a smaller area Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed press the MAP Softkey 3 Press the TRAFFIC Softkey Traffic is now displayed on the map Hazard Avoidance ADS B symbology for aircraft providing ADS B data NOTE A 1090 MHz extended squitter transponder is required to display Aircraft Identification l tail number or Flight ID number Relative Altitude in this case 1200 feet above own aircraft Fal Altitude Trend up arrow
134. rain obstacle and traffic avoidance SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic A WARNING Do not use SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Synthetic Vision Technology SVT functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVT 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 SVT information is shown on the primary flight display PFD SVT offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVT enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying SVT 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 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for
135. rd field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is provided by the fuel totalizer 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 AIRTEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key
136. ress the ENT Key The UP DOWN field is now highlighted 2 Tum 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 TURN ALL VSPEED BUGS ON OR OFF 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 MINIMUM DESCENT ALTITUDE 1 2 3 4 Press the TMR REF Softkey Turn the large FMS Knob to highlight the Minimums field Turn the small FMS Knob to select BARO or TEMP COMP OFF is selected by default Press the ENT Key or turn the large FMS Knob to highlight the next field Use the small FMS Knob to enter the desired altitude from zero to 16 000 feet Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Flight instruments 5 If TEMP COMP was selected press the ENT Key or tum the large FMS Knob to highlight the next field and then enter the destination airport temperature 59 C to 59 C The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value 6 To remove the window press the
137. rwrite existing profile Profile name invalid Enter a different profile name Displayed if the profile name matches the name of existing profile Displayed if the profile name is invalid All available pilot profiles in use Delete a profile before importing another Displayed if the maximum number for pilot profiles has been reached Pilot profile import failed Displayed if the importing operation fails for any other reason Pilot profile import succeeded Displayed if the importing operation succeeds Overwrite existing file Displayed if the filename matches the name of an existing file on the SD card Pilot profile export failed Displayed if the export operation fails Pilot profile export succeeded Displayed if the export operation succeeds 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 105 sainjeay aoueplony SoJnpa204d buluueld AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy ic Eu x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional Hazard Avoidance Abnormal EIS AFCS Procedures GPS Nav Features Operation Appendix Index Annunciations amp Alerts 106 Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole A GARMIN 190 01462 01 Rev
138. s Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key A NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the 58 active waypoint in a GPS SBAS approach a LOWALT 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Hazard Avoidance TERRAIN AWARENESS amp WARNING SYSTEM TAWS B DISPLAY OPTIONAL WARNING Do not use the terrain avoidance feature as the sole means of navigation and terrain separation The terrain avoidance feature is only to be used as and aid to terrain avoidance Garmin obtains terrain database content from third party sources and is not able to independently verify the accuracy of the terrain data
139. s playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block 12 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select those isolated from hearing the Nav Nav Com XPDR Audio Panel Com radios PILOT KEY COPLT KEY Copilot Passenger Mode aNNUNCIATOR ANNUNCIATOR PilotHears Hears Selected Selected Selected radios pilot radios pilot radios pilot ALL OFF OFF copilot copilot copilot passengers passengers passengers music music music Copilot Copilot PILOT ON OFF 7 passengers passengers radios pilot music music Selected Selected COPILOT OFF ON radios pilot copilot b Mu passengers passengers music music Selected Selected aaz CREW ON ON radios pilot radios pilot Engers music copilot copilot 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 13 sjuauimasu sub 53 S24V oipny uddx JUI05 AEN sual uonesado s n e 4 aoueplony s mp oold Buruue d AEN Sd5 junuuy jeuuouqy Jeuonippy paezey nubi xipuaddy x pul A Nav Com XPDR Audio Panel GARMIN Flight Instruments EIS Nav Com 05 x 22 o x GPS Nav AFCS Flight Planning Blank Page Annun Abnormal Addition
140. st of available transitions for the selected approach procedure is now displayed 5 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 6 Press the ENT Key The cursor moves to the MINIMUMS field 7 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO or TEMP COMP 8 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 9 Press the ENT Key If BARO or OFF was selected in step 8 proceed to step 11 If TEMP COMP was selected in step 8 the cursor moves to the TEMP AT field Turn the small FMS Knob to enter the temperature at the destination airport The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value s mp old 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
141. t 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 Tum the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A GARMIN Flight Planning 11 12 13 14 15 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 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 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint Press the ENT Key Press the FMS Knob to remove the flashing cursor CREATE A USER WAYPOINT USING THE MAP POINTE
142. ted text HABUK iaf 021 5 7NM HABUK iaf 021 5 7NM 22788rFT FALUR 261 4 7NH FALUR 91 4 7NM 8418Fr CEGIX faf 51 5 9NH CEGIX fuf SSH 5 SNM 27529FT RW35R map 5 1NH RW35R map d r 5 11NM 6368FT r 5NM B3BBEFT 6368FT 348 5NM 5355FT MOGAL mahp MOGAL mahp 97121 HOLD 8 2211 HOLD 38 6 0NH L Altitudes Displayed Without Altitudes Dis Ded With Temperature Compensation eae ompensation 46 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Enabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Procedures 4 Use the small FMS Knob to select the temperature at the lt airport gt The compensated altitude is computed as the temperature is selected 5 Press the ENT Key ACTIVATE COMPENSATION is highlighted 6 Press the ENT Key The compensated altitudes for the approach are shown in the flight plan Disabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed 4 Press the ENT Key CANCEL COMPENSATION is highlighted 5
143. tely depict current weather conditions V ARNING Do not use the indicated data link vveather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing vveather data for data link transmission the vveather information shovvn by the data link vveather product may be significantly older than the indicated vveather product age Displaying SiriusXM VVeather on the Navigation Map Page 1 Press the MAP Softkey 2 Press the NEXRAD or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Tum the small FMS Knob to select the Airport Information Page 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 49 sjuauimasu nubi APN 540 523 olpny uqax U105 AeN Duruue d Wil s mp oold paezey Suelv uoneiedo s m Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Ind
144. tered 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 The system cannot for use in giving vertical flight path guidance Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database use this altitude in determining vertical flight path guidance 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 23 sjuauimasu UATE 59 olpny uqax uo2 AEN suelv uoneiedo sainjea4 saunpadold Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul GARMIN GPS Navigation Ssjueuinijsu fila 59 Tu102 AEN s24v 549 Buruuejd 1i Blank Page 6 2 4 aoueplony puezey saunjyea4 jeuonippy uoneiedo jewuouqy suay unuuy x pu ddy x pul 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 24 A GARMIN FLIGH
145. ters OPIN 1 Wind direction arrows with headwind and crosswind components OPTN 2 Wind direction arrow and speed OPTN 3 Wind direction arrow with headwind tailwind and crosswind components OFF Information not displayed DME BRGI Press to display the DME information vvindovv Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information HSI FRMT Displays the HSI formatting softkeys 360 HSI Displays the HSI in a 360 degree format ARC HSI Displays the HSI in an arc format BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units 10 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Description METERS VVhen enabled displays altimeter in meters IN Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa Select the BACK Softkey to return to the top level softkeys L T T 124 125 L s TL 7 lev ekse T eack L veo 1 EY 75 ES EN ES EN VX VS ES ES on on Select
146. the Piper PA 44 180 Seminole 61 saunpar0dd Buruuejd AeN Sd5 S24V oipny uadx sia siu u nnsul Wfl Tu102 AEN 346 aoueplony paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airp
147. the Synthetic Vision Technology SVT option is installed and the TAWS B option has not been installed A NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Display Terrain on the TERRAIN SVS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 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 Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 57 AEN Sd5 S24V oipny duadx 99 s u u nnsul u102 AEN nubi Duruue d wold aoueploay s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedure
148. the list IMPORT A FLIGHT PLAN FROM AN SD CARD 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the MFD to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Press 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 press the IMPORT Softkey 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 33 52 2 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A
149. 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 FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts The MFD depiction shows the aircraft position on the plan view of most approach charts 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 Press the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey 2 Press the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Press the GO BACK Softkey to return to the previous page 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 63 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd buluueld AEN Sd5 S24V olpny uqax sia sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi u105 AeN ubiu x pul Flight Instruments Nav Com XPDR Aud
150. tings do not match backup configuration memory The system should be serviced COM1 TEMP COM over temp Reducing transmitter power Reducing transmitter power COM2 TEMP COM 2 over temp 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 COM1 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 COM and or COM2 may still be usable The system should be serviced when possible COMI PTT COM1 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 1 remote transfer key is stuck COM2 RMT XFR 2 remote transfer key is stuck The COM1 and or COM transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the system should be serviced 94 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations 8 Alerts Message Comments LOI
151. to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude The system updates vertical path guidance continuously using ground speed and the calculated distance to the Bottom of Descent BOD Due to turn anticipation guidance turn smoothing distance to the BOD can be affected by course changes greater than approximately 5 degrees Ground speed can be affected by factors such as shifts in wind direction aircraft power management pitch angle and course changes Abrupt and or substantial changes to either the distance to the BOD ground speed or both can cause similarly abrupt substantial changes in vertical path guidance Because of turn smoothing changes to both distance to the BOD and ground speed tend to be more extreme when the BOD is also a waypoint that marks a large course change These speed and distance changes will be accounted for in the computed required vertical path and reflected in the vertical guidance indications 22 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN GPS Navigation designated to be used in determining vertical flight path guidance Altitude has been retrieved from the navigation database and is provided as a reference White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating en
152. to confirm the export 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 41 oipny uddx s q sjuauimasu U105 AEN 3463 52 2 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul GARMIN Flight Planning Ssjueuinijsu fila 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld 346 Blank Page 5 2 4 puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01462 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 42 GARMIN 5 PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Tum 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 activ
153. to proceed to loading the active database 4 A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database Abnormal Operation DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL OUERHRITE THE ACTIVE NAVIGATION DATABASE FROM TO WORLDWIDE WORLDWIDE 1204 1285 Annun Alerts 09 RPR 2012 07 NAY 2012 7 MAY 2812 04 1UN 2012 3 o 2 2 lt NO WILL BE ASSUMED IN 8 SECONDS Index 118 Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN 5 After the update completes the display starts in normal mode 6 Tum the system OFF and remove the SD card from the top card slot 7 Repeat steps 1 through 6 for the other display PFD or MFD 8 Apply power to the system and press the ENT Key to acknowledge the startup screen 9 Tum the large FMS Knob to select the AUX Page group on the MFD 10 Turn the small FMS Knob to select the System Status Page 11 Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB Verify the Appendix correct active navigation database cycle information is shown for each display Loading the Jeppesen Navigation Database as the Standby Navigation Database The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Jeppesen Navigation Database to the bottom SD c
154. ts AHRS1 TAS AHRS1 not receiving airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced The 1 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS1 SERVICE AHRS1 needs service Return unit for repair A failure has been detected in the 1 AHRS The system should be serviced AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS1 CONFIG AHRS1 config error Config service req d AHRS configuration settings do not match those of backup configuration memory The system should be serviced GEO LIMITS AHRS1 too far North South no magnetic compass The aircraft is outside geographical li
155. ttom 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 press the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels 3 Press the SET Softkey 4 Press any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 1 With the XM Radio Page displayed press the VOL Softkey 2 Press the VOL Softkey to reduce volume or press the VOL Softkey to increase volume Once the VOL Softkey is pressed the volume can also be adjusted using the small FMS Knob Mute SiriusXM Audio 1 Select the XM Radio Page or XM Information Page 2 Press the MUTE Softkey to mute the audio Press the MUTE Softkey again to unmute the audio Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 190 01462 01 Rev A A GARMIN SCHEDULER The Scheduler feature can be used to enter and display reminder messages e g Change oil Altimeter Transponder or Hot Section Inspection or Phase 1 Maintenance Check in the Messages Window on the PF
156. vs right tank quantity is PN Maintenance Mode ON 2 Single Chime ADA VENIE PED display fan is inoperative L DEZ EZ MEE MED display fan is inoperative Additional Features NAZAR BB Avionics fan fail SYSTEM MESSAGES Abnormal Operation Alerts Window Text Description WOW MISCOMPARE Left and right squat switches do not agree Index Appendix 82 Garmin G1000 Cockpit Reference Guide for the Piper 44 180 Seminole 190 01462 01 Rev A A GARMIN Annunciations amp Alerts VOICE ALERTS Message Priority Description Stall Imminent stall is sensed by stall vane Airspeed Airspeed exceeds VNE Warning Aircraft has descended below the preset barometric Minimums minimums minimum descent altitude TAS System Test Failed Vertical track TIS Not Available Timer Expired Check Gear Landing gear are not down and locked Traffic TIS Traffic Alert Traffic distance bearing altitude Caution TAS Traffic Alert Check Gear Landing gear are not down and locked TAS System Test Passed TAS system initiated test passed Advisory TAS system initiated test failed Aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Aircraft is outside TIS coverage area Countdown timer on the PFD has reached zero
157. ys the system settings for the selected profile Renaming a profile 1 Use the FMS Knob to select the AUX System Setup Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight RENAME in the Pilot Profile Box 4 Press the E NT Key Additional Features 5 In the Rename Profile window turn the FMS Knob to select the profile to rename 6 Press the E 7 Use the FMS Knob to enter a new profile name up to 16 characters long NT Key and press the ENT Key 8 With RENAME highlighted press the ENT Key 9 To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key 190 01462 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 44 180 Seminole 69 2 Buruuejd AeN Sd5 S24V olpnyyuqax sia s u u nnsul Tu102 AEN UTE eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 70 A GARMIN Deleting a profile 1 2 3 4 5 6 7 8 Use the FMS Knob to select the AUX System Setup Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight DELETE

Garmin Software Version 1983.00 Cockpit Reference Guide

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