Garmin PA-44-180 Reference Guide

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G1000

Cockpit Reference Guide for the Piper PA-44-180 Seminole

Integrated Flight Deck

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

NAV/COM/TRANSPONDER/AUDIO PANEL

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

This manual reﬂects the operation of System Software version 1648.01 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, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251

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 of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin® and G1000® 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.

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

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

June, 2013 190-01462-00 Rev. A Printed in the U.S.A.

Warnings, Cautions & Notes

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.

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.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Warnings, Cautions & Notes

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

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

WARNING: 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 system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Warnings, 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 website at www.garmin.com/aboutGarmin/ environment/disposal.jsp.

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

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

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Warnings, Cautions & Notes

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

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

NOTE: 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 operation.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Warnings, Cautions & Notes

NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition

65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.

NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition.

NOTE: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

NOTE: 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 intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Warnings, Cautions & Notes

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Record of Revisions

Part Number Change Summary

190-01462-00 Initial release

Revision Date of Revision Affected Pages Description

A June, 2013 All Initial release

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Record of Revisions

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RR-2

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Table of Contents

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

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

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

Turn ALL Vspeed Bugs On or Off ............................................................................................ 2

Set Barometric Minimum Descent Altitude ........................................................................ 2

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

ENGINE INDICATION .................................................................................................................... 5

Engine Display ........................................................................................................................... 5

Engine Page................................................................................................................................ 7

Landing Gear Indications ...................................................................................................... 10

NAV/COM/TRANSPONDER/AUDIO PANEL ....................................................................... 11

Enter a Transponder Code..................................................................................................... 11

DME Tuning...............................................................................................................................11

Selecting a COM Radio .......................................................................................................... 11

Selecting a NAV Radio ........................................................................................................... 11

NAV/COM Tuning ..................................................................................................................... 12

Digital Clearance Recorder and Player .............................................................................. 12

Intercom System (ICS) Isolation .......................................................................................... 13

GPS NAVIGATION ........................................................................................................................ 15

Direct-to Navigation .............................................................................................................. 15

Activate a Stored Flight Plan ............................................................................................... 16

Activate a Flight Plan Leg ..................................................................................................... 16

Stop Navigating a Flight Plan .............................................................................................. 17

Vertical Navigation (VNAV)................................................................................................... 17

FLIGHT PLANNING ...................................................................................................................... 21

Weight Planning ...................................................................................................................... 21

Trip Planning ............................................................................................................................ 21

Create a User Waypoint Deﬁned by Latitude & Longitude ........................................... 23

Create a User Waypoint Deﬁned by Radials from Other Waypoints ........................... 24

Create a User Waypoint Deﬁned by a Radial & Distance from Another Waypoint .. 25

Create a User Waypoint using the Map Pointer............................................................... 27

Delete a User Waypoint ......................................................................................................... 28

Create a Flight Plan ................................................................................................................ 28

Import a Flight Plan from an SD Card ................................................................................ 29

Insert a Waypoint in the Active Flight Plan ...................................................................... 30

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Table of Contents

Enter an Airway in a Flight Plan .......................................................................................... 31

User-Deﬁned Holding Patterns ............................................................................................ 31

Invert An Active Flight Plan .................................................................................................. 34

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 34

Store a Flight Plan .................................................................................................................. 34

Edit a Stored Flight Plan ....................................................................................................... 35

Delete a Waypoint from the Flight Plan ............................................................................ 35

Invert and Activate a Stored Flight Plan ........................................................................... 36

Copy a Flight Plan ................................................................................................................... 36

Delete a Flight Plan ................................................................................................................ 36

Graphical Flight Plan Creation ............................................................................................. 37

Export a Flight Plan to an SD Card ..................................................................................... 37

PROCEDURES ................................................................................................................................. 39

Load and Activate a Departure Procedure ....................................................................... 39

Activate A Departure Leg ..................................................................................................... 39

Load An Arrival Procedure .................................................................................................... 39

Activate An Arrival Leg ......................................................................................................... 40

Load and/or Activate an Approach Procedure ................................................................. 40

Activate An Approach in the Active Flight Plan ............................................................... 42

Activate a Vector to Final Approach Fix ............................................................................ 42

Activate A Missed Approach in the Active Flight Plan ................................................... 42

Temperature Compensated Altitude ................................................................................. 42

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

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

SiriusXM Weather (Optional) ............................................................................................... 45

Trafﬁc Systems ........................................................................................................................ 48

Terrain And Obstacle Proximity ........................................................................................... 52

Terrain-SVS ............................................................................................................................... 53

Terrain Awareness & Warning System (TAWS-B) Display (Optional) ........................... 55

ADDITIONAL FEATURES ........................................................................................................... 57

Synthetic Vision (Optional) ................................................................................................... 57

Terminal Procedure Charts ................................................................................................... 58

Airport Directory .................................................................................................................... 60

SiriusXM Radio Entertainment ............................................................................................ 61

Pilot Proﬁles............................................................................................................................. 64

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

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Table of Contents

ABNORMAL OPERATION..........................................................................................................69

Reversionary Mode ................................................................................................................ 69

Abnormal COM Operation .................................................................................................... 69

Hazard Displays with Loss of GPS Position ....................................................................... 69

Unusual Attitudes ................................................................................................................... 70

Dead Reckoning ...................................................................................................................... 70

ANNUNCIATIONS & ALERTS ................................................................................................... 73

G1000 System Annunciations ............................................................................................... 73

CAS Annunciations .................................................................................................................. 75

System Messages .................................................................................................................... 76

Voice Alerts .............................................................................................................................. 77

Terrain-SVT Alerts ................................................................................................................... 77

Terrain-SVT System Status Annunciations ........................................................................ 78

TAWS-B Alerts .......................................................................................................................... 79

TAWS-B System Status Annunciations ............................................................................... 80

GDL 69/69A Data Link Receiver Messages ........................................................................ 81

MFD & PFD Message Advisories .......................................................................................... 82

Database Message Advisories ............................................................................................. 83

GMA 1347 Message Advisories ............................................................................................ 86

GIA 63W Message Advisories ............................................................................................... 87

GEA 71 Message Advisories .................................................................................................. 90

GTX 33/33 w/ES Message Advisories .................................................................................. 90

GRS 77 Message Advisories .................................................................................................. 91

GMU 44 Message Advisories ................................................................................................ 92

GDL 69A Message Advisories ............................................................................................... 92

GTS 800 Message Advisories ................................................................................................ 92

GDC 74A Message Advisories ............................................................................................... 93

Miscellaneous Message Advisories ..................................................................................... 93

Flight Plan Import/Export Messages .................................................................................. 97

Pilot Proﬁle Import/Export Messages ................................................................................ 99

APPENDIX ..................................................................................................................................... 101

PFD Softkey Map .................................................................................................................. 101

MFD Softkey Map ................................................................................................................. 106

Loading Updated Databases .............................................................................................. 109

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

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

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Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

Instruments EIS

Flight

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

Press the PFD Softkey.

Press the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

Press the PFD Softkey to display the second-level softkeys.

Press the ALT UNIT Softkey.

Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).

Press the HPA Softkey to display the barometric pressure setting in hectopascals.

Press the BACK Softkey to return to the top-level softkeys.

CHANGE NAVIGATION SOURCES

Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD.

Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency.

Press the CDI Softkey a third time to return to GPS.

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Flight Instruments

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

Flight

InstrumentsEIS

Press the OBS Softkey to select OBS Mode.

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.

Press the OBS Softkey again to disable OBS Mode.

Nav/Com/

GENERIC TIMER

XPDR/AudioGPS Nav

Press the TMR/REF Softkey, then turn the large FMS Knob to select the time ﬁeld (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN ﬁeld is now highlighted.

Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS

Flight

PlanningProcedures

Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted.

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

Hazard

Avoidance

Press the TMR/REF Softkey.

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

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

Press the

Turn the large FMS Knob to highlight the Minimums ﬁeld.

Turn the small FMS Knob to select BARO, or TEMP COMP. OFF is selected

TMR/REF

Softkey.

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

190-01462-00 Rev. A

Flight Instruments

If TEMP COMP was selected, press the ENT Key or turn the large FMS Knob to highlight the next ﬁeld and then enter the destination airport temperature (-59˚C to 59˚C). The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value.

To remove the window, press the

DISPLAYING WIND DATA

Press the PFD Softkey.

Press the WIND Softkey to display wind data below the Selected Heading.

Press one of the OPTN softkeys to change how wind data is displayed.

To remove the Wind Data Window, press the OFF Softkey.

CLR

Key or the

TMR/REF

Softkey.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Flight Instruments

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

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ENGINE DISPLAY

ENGINE INDICATION

EIS

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Engine Display when

Engine Page is displayed

Engine Display

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

EIS

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Engine Manifold Pressure Gauge (MAN IN HG)

Tachometer (RPM)

Propeller Sync Indicator

Exhaust Gas Temperature

(EGT °F)

Fuel Flow Indicator (FFLOW GPH)

Oil Pressure Indicator (OIL PSI)

Oil Temperature Indicator (OIL °F)

Alternator Current(ALTR AMPS)

Voltage (VOLTS)

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.

Abnormal

OperationAnnun/AlertsAppendixIndex

Battery Current(BATT AMPS)

Fuel Quantity Indicator (FUEL QTY GAL)

Landing Gear Status

(LANDING GEAR)

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Displays the battery current in amperes

Displays the amount of fuel in gallons (gal) for each

side of a standard fuel tank.

Displays landing gear status

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EIS

ENGINE PAGE

Press the ENGINE Softkey or turn the large FMS Knob and select the EIS - Engine

Page.

14 13 12

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Engine Page

Engine Manifold

Pressure Gauge

Displays manifold pressure in inches of Mercury (in Hg) to

indicate engine power

(MAN IN HG)

Tachometer (RPM)

Displays propeller speed in revolutions per minute

(rpm)

Propeller Sync

Indicator

Exhaust Gas Temperature

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

(EGT °F)

Fuel Flow Indicator

Displays fuel ﬂow in gallons per hour (gph)

(FFLOW GPH)

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Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

EIS

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Oil Pressure

Indicator (OIL PSI)

Oil Temperature

Indicator (OIL °F)

Landing Gear

Status (LANDING GEAR)

Fuel Calculations

Group (FUEL CALC)

Electrical Group

(ELECTRICAL)

Engine Hours

(TACH TIME)

Exhaust Gas Temperature

(EGT °F)

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 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

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Cylinder Head

Temperature Bar Graph (CHT °F)

Fuel Quantity

Gauges (L/R FUEL QTY GAL)

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

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

190-01462-00 Rev. A

EIS

Fuel Calculations

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), 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 aircraft’s heading and the wind direction and speed.

Adjusting 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.

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.

Set Fuel Remaining

Calculated Fuel Used

Calculated Endurance

Calculated Range

Fuel Efﬁciency

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

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Avoidance

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Features

Operation Annun/Alerts Appendix Index

Abnormal

Fuel Calculations Group

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

EIS

LANDING GEAR INDICATIONS

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Landing Gear statuses are shown using the indications in the following table.

Position EIS Engine Page

Up & Locked

In Transition

Down and

Locked

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Gear Failure

Landing Gear Indications

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ENTER A TRANSPONDER CODE

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

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

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

Press the DME Softkey.

Turn the large FMS to select the DME source ﬁeld.

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

Press the ENT Key to complete the selection.

Nav/Com/XPDR/Audio Panel

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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

To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).

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.

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Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Nav/Com/XPDR/Audio Panel

NAV/COM TUNING

Flight

InstrumentsEIS

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

Turn the respective tuning knobs to enter the desired frequency into the standby frequency ﬁeld. The large knob enters MHz and the small knob enters kHz.

Nav/Com/

XPDR/AudioGPS Nav

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

Flight

PlanningProcedures

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 begins playing the previously recorded

Hazard

Avoidance

memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block.

COM MIC

Key is recorded. Audio is

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Nav/Com/XPDR/Audio Panel

INTERCOM SYSTEM (ICS) ISOLATION

Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/

Com radios.

Mode

PILOT KEY

ANNUNCIATOR

ALL OFF OFF

PILOT ON OFF

COPILOT OFF ON

CREW ON ON

COPLT KEY

ANNUNCIATOR

Pilot Hears

Selected radios; pilot; copilot; passengers; music

Selected radios; pilot

Selected radios; pilot; passengers; music

Selected radios; pilot; copilot

Copilot

Hears

Selected radios; pilot; copilot; passengers; music

Copilot; passengers; music

Copilot

Selected radios; pilot; copilot

Passenger

Hears

Selected radios; pilot; copilot; passengers; music

Copilot; passengers; music

Selected radios; pilot; passengers; music

Passengers; music

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Planning Procedures

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Operation Annun/Alerts Appendix Index

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Nav/Com/XPDR/Audio Panel

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Nav/Com/

XPDR/AudioGPS Nav

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PlanningProcedures

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Avoidance

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OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation using the MFD

Press the Direct-to

Enter the waypoint identiﬁer.

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

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

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

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 9.

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

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

10)

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

11)

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

12)

Press the ENT Key to activate.

Direct-to Navigation using the PFD

( )

Key on the MFD.

GPS Navigation

Instruments EIS

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XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

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Features

Operation Annun/Alerts Appendix Index

Abnormal

Press the Direct-to Key

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

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

( )

on the PFD.

etc.

Press the ENT Key.

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.

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

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

GPS Navigation

Turn the small FMS Knob to enter the desired altitude.

Flight

InstrumentsEIS

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

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

10)

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

11)

Turn the small FMS Knob to enter the desired target altitude offset from

Nav/Com/

XPDR/AudioGPS Nav

the selected Direct-to.

12)

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

highlight the ‘CRS’ ﬁeld.

13)

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

14)

Press the ENT Key to highlight ‘ACTIVATE?’.

15)

Flight

PlanningProcedures

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

ACTIVATE A STORED FLIGHT PLAN

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

Hazard

Avoidance

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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.

Abnormal

OperationAnnun/AlertsAppendixIndex

ACTIVATE A FLIGHT PLAN LEG

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.

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.

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190-01462-00 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

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

Press the MENU Key to display the Page Menu Window.

Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT

Instruments EIS

Flight

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.

XPDR/Audio GPS Nav

Nav/Com/

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.

Planning Procedures

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

Large White

Insertion

Point

Indicator

Text

Large Light

Blue Text

Flight

Avoidance

Hazard

Additional

Features

Small Light

Blue Text

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Operation Annun/Alerts Appendix Index

Abnormal

GPS Navigation

Altitudes associated with approach procedures are “auto-designated”. This means

the system will automatically use the altitudes loaded with the approach for giving

Flight

InstrumentsEIS

vertical ﬂight path guidance outside the FAF. 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

Nav/Com/

XPDR/AudioGPS Nav

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 to

Flight

PlanningProcedures

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

Hazard

shifts in wind direction, aircraft power management, pitch angle, and course changes.

Avoidance

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

Features

Additional

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.

Abnormal

OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

GPS Navigation

White Text Light Blue Text Light Blue

Subdued Text

Instruments EIS

Flight

Large Text

Small Text

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

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

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

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

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

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

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Operation Annun/Alerts Appendix Index

Abnormal

190-01462-00 Rev. A 19

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

GPS Navigation

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Nav/Com/

XPDR/AudioGPS Nav

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PlanningProcedures

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OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Flight Planning

Instruments EIS

Flight

Entering Weight Parameters

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

FMS

Knob to select the Weight Planning Pge.

Press the EMPTY WT Softkey to place the cursor in the Basic Empty Weight

FMS

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

ﬁeld.

Enter the desired aircraft empty weight.

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

Enter the desired weight of Pilot & Stores.

Press the ENT Key.

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

Entering Fuel Parameters

Press the FMS Knob to activate the cursor.

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

Turn the small FMS Knob to enter the desired fuel quantity.

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

Turn the small FMS Knob to enter the desired reserve fuel quantity.

Press the FMS Knob to remove the cursor.

Press the ENT Key.

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

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Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

TRIP PLANNING

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

Turn the small FMS Knob to select the Trip Planning Page.

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.

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Flight Planning

For Direct-to planning:

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

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Abnormal

OperationAnnun/AlertsAppendixIndex

Or:

For point-to-point planning:

Or:

For ﬂight plan leg 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.

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.

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

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

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

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

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

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

190-01462-00 Rev. A

Flight Planning

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

The ﬂashing cursor moves to the ground speed (GS) ﬁeld. Enter the ground speed. Press the mode, ground speed is provided by the system.

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.

The ﬂashing cursor moves to the fuel onboard 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 AIR TEMP) ﬁeld. Enter

the desired air temperature. Press the ENT Key when ﬁnished. Note that in ‘AUTOMATIC’ page mode, air temperature is provided by the system outside air temperature.

ENT

Key when ﬁnished. Note that in ‘automatic’ page

Instruments EIS

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Planning Procedures

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Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

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. 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.

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Flight Planning

Turn the large FMS Knob one click to the left to highlight

Flight

InstrumentsEIS

‘TEMPORARY’.

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).

Nav/Com/

XPDR/AudioGPS Nav

Press the ENT Key.

CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS

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.

Flight

PlanningProcedures

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

Hazard

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Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

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.

Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.

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.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ ﬁeld. With the ﬁrst

waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Flight Planning

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.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

Repeat step 10 to enter the next waypoint name.

14)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld for the

second waypoint. Enter the desired radial from the reference waypoint.

15)

Press the ENT Key.

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Features

Operation Annun/Alerts Appendix Index

Abnormal

16)

Press the FMS Knob to remove the ﬂashing cursor.

CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM

ANOTHER WAYPOINT

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.

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Flight Planning

Press the NEW Softkey. A waypoint is created at the current aircraft

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

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PlanningProcedures

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Avoidance

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Abnormal

OperationAnnun/AlertsAppendixIndex

position.

Enter the desired waypoint name.

Press the ENT Key.

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.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ ﬁeld. With the ﬁrst

waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:

Or:

Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.

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.

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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.

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.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Flight Planning

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) ﬁeld. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

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

distance from the reference waypoint.

14)

Press the ENT Key.

15)

Press the FMS Knob to remove the ﬂashing cursor.

CREATE A USER WAYPOINT USING THE MAP POINTER

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.

Instruments EIS

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XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

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Avoidance

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Additional

Features

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) a new 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.

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Operation Annun/Alerts Appendix Index

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Flight Planning

If desired, change the storage method of the waypoint to “TEMPORARY” or

Flight

InstrumentsEIS

“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

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PlanningProcedures

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

Hazard

Avoidance

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

leg is activated automatically after it is created.

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Creating an active ﬂight plan:

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 select 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.

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190-01462-00 Rev. A

Flight Planning

Creating a stored ﬂight plan:

Press the FPL Key.

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

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.

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.

Repeat step numbers 4 and 5 to enter each additional ﬂight plan waypoint.

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

Instruments EIS

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Planning Procedures

Flight

IMPORT A FLIGHT PLAN FROM AN SD CARD

Insert the SD card containing the ﬂight plan in the top card slot on the MFD.

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

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

Press the FMS Knob to activate the cursor.

Turn either FMS Knob to highlight an empty or existing ﬂight plan.

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.

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Abnormal

Flight Planning

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

Flight

InstrumentsEIS

Press the ENT Key.

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

Press the FPL Key to display the active ﬂight plan.

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

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PlanningProcedures

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Avoidance

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OperationAnnun/AlertsAppendixIndex

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).

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

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

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.

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190-01462-00 Rev. A

Turn the large FMS Knob to select the desired user waypoint.

Press the ENT Key.

Press the

ENT

Key again to “accept” the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

Press the FPL Key.

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

Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. 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.

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).

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.

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

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

Flight Planning

Instruments EIS

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Avoidance

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Operation Annun/Alerts Appendix Index

Abnormal

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:

Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).

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.

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Flight Planning

Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key.

Flight

InstrumentsEIS

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.

Nav/Com/

XPDR/AudioGPS Nav

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.

Flight

10)

PlanningProcedures

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:

Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).

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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.

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190-01462-00 Rev. A

Flight Planning

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

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).

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 activate the Direct To with the user-deﬁned hold deﬁned at the Direct To waypoint.

Instruments EIS

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Planning Procedures

Flight

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

Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).

Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the HOLD waypoint.

Press the CLR Key. A ‘Remove Holding Pattern?’ conﬁrmation window is displayed.

Select ‘OK’ and press the ENT Key. The holding pattern is removed from the active ﬂight plan. Select ‘CANCEL’ and press the ENT Key to cancel the removal of the holding pattern.

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

Press the Direct To Key to display the DIRECT TO Window (PFD or MFD).

Press the MENU Key to display the PAGE MENU with the cursor on the ‘Cancel Direct To NAV’ selection.

Press the ENT Key. The holding pattern is removed.

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Flight Planning

INVERT AN ACTIVE FLIGHT PLAN

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XPDR/AudioGPS Nav

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

PLAN

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

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Or, for a stored ﬂight plan:

Press the MFD FPL Key and 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 desired ﬂight plan.

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

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.

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190-01462-00 Rev. A

EDIT A STORED FLIGHT PLAN

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

Press the FMS Knob to activate the cursor.

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

Press the EDIT Softkey.

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

Enter the changes, then press the ENT Key.

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

Flight Planning

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Nav/Com/

DELETE A WAYPOINT FROM THE FLIGHT PLAN

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

Or, for a stored ﬂight plan:

Press the FPL Key of the MFD and 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 desired ﬂight plan.

Press the EDIT Softkey.

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

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

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

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

Planning Procedures

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Flight Planning

INVERT AND ACTIVATE A STORED FLIGHT PLAN

Flight

InstrumentsEIS

Press the FPL Key for 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 desired ﬂight plan.

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

Nav/Com/

XPDR/AudioGPS Nav

displayed.

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

Flight

PlanningProcedures

Press the FPL Key for 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 copied.

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

Hazard

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Features

Additional

DELETE A FLIGHT PLAN

Abnormal

OperationAnnun/AlertsAppendixIndex

displayed.

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.

Press the FPL Key for 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 deleted.

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

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

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190-01462-00 Rev. A

GRAPHICAL FLIGHT PLAN CREATION

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 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

Flight Planning

ABOVE

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Planning Procedures

Flight

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 to conﬁrm the export.

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190-01462-00 Rev. A

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

Press the PROC Key.

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

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

Turn the large FMS Knob to highlight the desired departure.

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.

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

Turn the large FMS Knob to highlight the desired transition.

Press the ENT Key.

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

Procedures

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ACTIVATE A DEPARTURE LEG

Press the FPL Key for the MFD 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 departure.

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

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AN ARRIVAL PROCEDURE

Press the PROC Key.

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

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

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Procedures

Turn the large FMS Knob to highlight the desired arrival.

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InstrumentsEIS

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

Turn either FMS Knob to select the desired transition.

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

Turn the large FMS Knob to highlight the desired runway.

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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

Flight

Hazard

PlanningProcedures

Avoidance

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

Features

Additional

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

Abnormal

OperationAnnun/AlertsAppendixIndex

in the list of available approaches.

Press the PROC Key.

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

Select the airport and approach:

Use the FMS Knob to select an airport and press the ENT Key.

Select an approach from the list and press the ENT Key.

Or:

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190-01462-00 Rev. A

Procedures

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.

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.

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

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

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

If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small direction of the green arrow to change the display from OFF to BARO, or TEMP COMP.

Press the

FMS

ENT

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

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

procedure.

FMS

Knob in the

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Avoidance

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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.

10)

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

highlighted.

11)

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

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

12)

Press the ENT Key.

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Procedures

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

Flight

InstrumentsEIS

Press the PROC Key.

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

Press the ENT Key.

ACTIVATE A VECTOR TO FINAL APPROACH FIX

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Press the PROC Key.

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

Press the ENT Key.

The ﬁnal approach course becomes the active leg.

Flight

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

PlanningProcedures

Press the PROC Key.

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

Press the ENT Key. A conﬁrmation window is displayed.

Hazard

Avoidance

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the Go-around Switch.

Features

Additional

TEMPERATURE COMPENSATED ALTITUDE

When temperature compensated altitude is enabled for the loaded approach, the

altitudes associated with the approach waypoints are displayed in slanted text.

Abnormal

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Altitudes Displayed Without

Temperature Compensation

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Altitudes Displayed With

Temperature Compensation

190-01462-00 Rev. A

Procedures

Enabling temperature compensated altitude:

From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed.

Turn the FMS Knob to highlight ‘Temperature Compensation’.

Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed.

Use the small FMS Knob to select the temperature at the <airport>. The

compensated altitude is computed as the temperature is selected.

Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.

Press the ENT Key. The compensated altitudes for the approach are

shown in the ﬂight plan.

Disabling temperature compensated altitude:

From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed.

Turn the FMS Knob to highlight ‘Temperature Compensation’.

Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed.

Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.

Press the ENT Key. The temperature compensated altitude at the FAF

is cancelled.

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Hazard Avoidance

HAZARD AVOIDANCE

Customizing THE HAZARD DISPLAYS ON THE NAVIGATION MAP

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.

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.

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 accurately depict current weather conditions.

Displaying SiriusXM Weather on the Navigation Map Page

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Abnormal

Press the MAP Softkey.

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

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

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

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

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Hazard Avoidance

Displaying Weather on the SiriusXM Weather Data Link Page

Flight

Nav/Com/

InstrumentsEIS

XPDR/AudioGPS Nav

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

Push in the Joystick to display the panning arrow.

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

Flight

PlanningProcedures

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

Hazard

Avoidance

ENT Key when panning over a TFR displays TFR speciﬁc information.

Enabling/disabling winds aloft data display in Proﬁle View:

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Select the Navigation Map Page.

Press the MENU Key.

With Map Setup highlighted, press the

Turn the small FMS Knob to select the Proﬁle Group and press the ENT Key

Turn the large

Turn the small

Press the FMS Knob or CLR Key to return to the Navigation Map Page with

FMS

Knob to select ‘Proﬁle Winds’.

FMS

Knob to select ‘On’ or ‘Off’.

ENT

Key

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

190-01462-00 Rev. A

SiriusXM Weather Products and Symbols

Hazard Avoidance

Instruments EIS

Flight

Wx Product

Status Icons

Description

NEXRAD - Available for the US and Canada. The age of the displayed data

for each is shown at the right.

ECHO TOP - The age of the displayed data is shown at the right. Not displayed when CLOUD TOP is displayed.

CLOUD TOP - The age of the displayed data is shown at the right. Not displayed when ECHO TOP is displayed.

XM LIGHTNING - The age of the displayed data is shown at the right.

CELL MOVEMENT - The age of the displayed data is shown at the right.

SIGMET & AIRMET - The age of the displayed data for each is shown at the

right.

METAR - Available for the US and Canada. The age of the displayed data for each is shown at the right.

SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts Surface Analysis. The lower symbol depicts City Forecast. The age of the displayed data for each is shown at the right. The selected forecast period is shown at the bottom.

FREEZING LEVEL - The age of the displayed data is shown at the right.

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Hazard Avoidance

InstrumentsEIS

XPDR/AudioGPS Nav

Wx Product

Status Icons

Flight

Nav/Com/

No Status Icon

Flight

TRAFFIC SYSTEMS

PlanningProcedures

Hazard

Avoidance

Features

Additional

Description

PIREP - The age of the displayed data is shown at the right. Urgent Pireps

are displayed in yellow.

TURBULENCE - The age of the displayed data is shown at the right. The altitude selection is shown at the bottom.

ICING POTENTIAL - The age of the displayed data is shown at the right. The altitude selection is shown at the bottom.

TFR- Depicted as an area outlined in yellow

Abnormal

OperationAnnun/AlertsAppendixIndex

• If Trafﬁc information Service (TIS) is conﬁgured, a STANDBY, OPERATE, and TNA MUTE Softkey are displayed.

• If a Trafﬁc Advisory System (TAS) is conﬁgured, a STANDBY, NORMAL, TEST, and ALT MODE Softkey are displayed.

• If an ADS-B trafﬁc system is conﬁgured, only the ALT MODE Softkey is displayed.

Trafﬁc Symbol Description

(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)

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Non-Threat Trafﬁc

190-01462-00 Rev. A

Hazard 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

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

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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

Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Press the TNA MUTE Softkey to mute the “Trafﬁc Not Available” aural alert, (if desired)

Displaying Trafﬁc on the Navigation Map

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

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

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Hazard Avoidance

GTS 800 (Optional)

Flight

InstrumentsEIS

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.

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

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

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 “Trafﬁc 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

Turn the large

Turn the small

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

FMS

Knob to select the Map Page Group.

FMS

Knob to select the Trafﬁc Map Page.

190-01462-00 Rev. A

Hazard Avoidance

Turn the RANGE Knob clockwise to display a larger area or counterclockwise to display a smaller area.

Displaying Trafﬁc on the Navigation Map

Ensure TAS is operating.

With the Navigation Map displayed, press the MAP Softkey.

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

NOTE: A 1090 MHz extended squitter transponder is required to display

ADS-B symbology for aircraft providing ADS-B data.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Aircraft Identiﬁcation (tail number or Flight

ID number)

Intruder Aircraft

Ground Track (extends

in the direction of the

Relative Altitude (in this case 1200 feet above own aircraft)

Altitude Trend (up arrow indicates climbing, down arrow indicates descending)

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)

Non-threat trafﬁc with ADS-B directional information. Points in the direction of the intruder aircraft track. (GTS 800 only)

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Non-threat trafﬁc with no directional information.

Trafﬁc with ADS-B directional information, but positional accuracy is degraded. Points in the direction of the aircraft track. (GTS 800 only)

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Hazard Avoidance

TERRAIN AND OBSTACLE PROXIMITY

Flight

InstrumentsEIS

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

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Turn the large

Turn the small

If desired, press the When the the

360

Rotate the clockwise to display a smaller area.

FMS

Knob to select the Map Page Group.

FMS

Knob to select the Terrain Proximity Page.

VIEW

ARC

Softkey is pressed, a radar-like 120° view is displayed. Press

Softkey to return to the 360° default display.

Joystick

clockwise to display a larger area or rotate counter-

Color Terrain/Obstacle Location

Red

Yellow

Black

Softkey to access the

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

ARC

and

360

Softkeys.

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Displaying Terrain and Obstacles on the Navigation Map

With the Navigation Map displayed, press the

Press the

TERRAIN

Softkey. Terrain and obstacle proximity will now be

displayed on the map.

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

MAP

Softkey.

190-01462-00 Rev. A

TERRAIN-SVS

NOTE: Terrain-SVS is only available when the Synthetic Vision Technology (SVT) option is installed and the TAWS-B option has not been installed.

Hazard Avoidance

Instruments EIS

Flight

NOTE: Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area.

Display Terrain on the TERRAIN-SVS Page

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

Turn the small FMS Knob to select the Terrain-SVS Page.

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.

Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Color Terrain/Obstacle Location

Red

Yellow

Black

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Enable/Disable Aviation Data

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

While the Terrain-SVS Page is displayed, press the MENU Key.

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

Press the ENT Key.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Hazard Avoidance

Terrain-SVS Inhibit

Flight

InstrumentsEIS

Inhibit Terrain

While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.

Press the MENU Key.

Nav/Com/

XPDR/AudioGPS Nav

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

Press the ENT Key.

Enable Terrain

While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.

Flight

Hazard

PlanningProcedures

Avoidance

While the Terrain-SVS Page is displayed, press the MENU Key.

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

Press the ENT Key.

NOTE: If Terrain-SVS 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.

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Hazard Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY (OPTIONAL)

NOTE: Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area.

NOTE: TAWS-B operation is only available when the G1000 is conﬁgured for a TAWS-B installation.

Manual System Test

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

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

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.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Display Terrain on the TAWS-B Page

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

Turn the small FMS Knob to select the TAWS-B Page.

Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.

Color Terrain/Obstacle Location

Red

Yellow

Black

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Hazard Avoidance

Enable/Disable Aviation Data

Flight

InstrumentsEIS

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

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

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.

Press the MENU Key.

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

Press the ENT Key.

Enable TAWS

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

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

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

Press the ENT Key.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION (OPTIONAL)

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

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 pilot’s perspective. SVT information is shown on the primary ﬂight display (PFD).

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

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

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Trafﬁc

• Airport Signs

• Runway Display

Displaying SVT Terrain

Press the PFD Softkey.

Press the SYN VIS Softkey.

Press the SYN TERR Softkey.

Press the BACK Softkey to return to the previous page.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Operation Annun/Alerts Appendix Index

Abnormal

Additional Features

Displaying Pathways

Flight

InstrumentsEIS

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Press the PATHWAY Softkey.

Press the BACK Softkey to return to the previous page.

Nav/Com/

XPDR/AudioGPS Nav

Displaying Heading on the Horizon

Press the PFD Softkey.

Press the SYN VIS Softkey.

If not already enabled, press the SYN TERR Softkey.

Flight

PlanningProcedures

Press the HRZN HDG Softkey.

Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

Press the PFD Softkey.

Press the SYN VIS Softkey.

Hazard

Avoidance

Features

Additional

If not already enabled, press the SYN TERR Softkey.

Press the APTSIGNS Softkey.

Press the BACK Softkey to return to the previous page.

TERMINAL PROCEDURE CHARTS

Abnormal

OperationAnnun/AlertsAppendixIndex

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 airport. The airport display on the map reveals runways with numbers, taxiways identiﬁers, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. The aircraft symbol provides situational awareness while taxiing.

Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and airport identiﬁcation labels. Pressing the DCLTR Softkey twice removes VOR station ID, the VOR symbol, and intersection names if within the airport plan view. Pressing

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Additional Features

Instruments EIS

the DCLTR Softkey a third time removes the airport runway layout, unless the airport

Flight

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

XPDR/Audio GPS Nav

Nav/Com/

on the ground. This database is updated on a 56-day cycle.

ChartView (Optional)

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

Planning Procedures

Flight

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

Avoidance

Hazard

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.

Additional

Features

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.

Operation Annun/Alerts Appendix Index

Abnormal

View Charts from the Navigation Map Page

Press the SHW CHRT Softkey when displayed.

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

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.

Press the GO BACK Softkey to return to the previous page.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional Features

View Charts from the Active Flight Plan Page

Flight

InstrumentsEIS

While viewing the Active Flight Plan Page, press the FMS Knob to activate the cursor.

Turn the large FMS Knob to select the departure airport, destination airport, departure, arrival, or approach.

Press the SHW CHRT Softkey. The appropriate chart is displayed, if

Nav/Com/

XPDR/AudioGPS Nav

available for the item selected.

Press the GO BACK Softkey to return to the previous page.

Change Day/Night View

While viewing a chart press the MENU Key to display the Page Menu OPTIONS.

Flight

PlanningProcedures

Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and press the ENT Key.

Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR SCHEME’ Options.

Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen Options.

Hazard

Avoidance

Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’ Options.

In Auto Mode, turn the large FMS Knob to select the percentage ﬁeld and

Features

Additional

change percentage with the small FMS Knob. The percentage of change is the day/night crossover point based on backlighting intensity.

Press the FMS Knob when ﬁnished to remove the Chart Setup Menu.

Abnormal

OperationAnnun/AlertsAppendixIndex

AIRPORT DIRECTORY

The Aircraft Owners and Pilots Association (AOPA) or AC-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.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

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.

Instruments EIS

Flight

SIRIUSXM RADIO ENTERTAINMENT

XPDR/Audio GPS Nav

Nav/Com/

The XM Radio Page provides information and control of the audio entertainment

features of the SiriusXM Satellite Radio.

Selecting the XM Radio Page

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

Turn the small FMS Knob to select XM Radio.

Press the RADIO Softkey to show the XM Radio Page where audio

Planning Procedures

Flight

entertainment is controlled.

Active Channel and Channel List

The Active Channel Box on the XM Radio Page displays the currently selected

Avoidance

channel. The Channels List Box of the XM Radio Page shows a list of the available

Hazard

channels for the selected category.

Selecting a Category

Additional

Features

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

of audio.

Operation Annun/Alerts Appendix Index

Press the CATGRY Softkey on the XM Radio Page.

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

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

Abnormal

desired category with the small FMS Knob.

Press the ENT Key.

Select an Available Channel within the Selected Category

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

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

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional Features

Flight

InstrumentsEIS

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

With the desired channel highlighted, press the ENT Key.

Entering a Channel Directly

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

Nav/Com/

XPDR/AudioGPS Nav

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

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

Press the ENT Key to activate the selected channel.

Flight

PlanningProcedures

Assigning Channel Presets

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

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

Press the MORE Softkey to access the next ﬁve channels (PS6 – PS10),

Hazard

Avoidance

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

Press the SET Softkey.

Features

Additional

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

Abnormal

OperationAnnun/AlertsAppendixIndex

Adjusting Volume

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

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

Select the XM Radio Page or XM Information Page.

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

190-01462-00 Rev. A

Additional Features

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 PFD. 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.

Entering a Scheduler Message

Select the AUX - Utility Page.

Press the FMS Knob momentarily to activate the ﬂashing cursor.

Turn the large FMS Knob to highlight the ﬁrst empty scheduler message

naming ﬁeld.

Use the FMS Knob to enter the message text to be displayed in the Messages Window and press the

Press the ENT Key again or use the large FMS Knob to move the cursor to

ENT

Key.

the ﬁeld next to Type.

Turn the small FMS Knob to select the message type:

• Event—Message issued at the speciﬁed date/time

• One-time—Message issued when the message timer reaches zero (default setting)

• Periodic—Message issued each time the message timer reaches zero

Press the ENT Key again or use the large FMS Knob to move the cursor to the next ﬁeld.

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.

For event-based messages:

Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key.

Press the ENT Key again or use the large FMS Knob to move the cursor to the next ﬁeld.

Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key.

10)

Press the ENT Key again or use the large FMS Knob to move the cursor to

enter the next message.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional Features

Deleting a Scheduler Message

Flight

InstrumentsEIS

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

Nav/Com/

XPDR/AudioGPS Nav

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

Flight

PlanningProcedures

the scheduler message is deleted from the message queue.

PILOT PROFILES

Creating a proﬁle:

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

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 ‘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

190-01462-00 Rev. A

Additional Features

With ‘CREATE’ highlighted, press the ENT Key to create the proﬁle

Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the

ENT Key to activate the new proﬁle.

To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key.

Selecting an active proﬁle:

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 the active proﬁle ﬁeld in the Pilot Proﬁle Box.

Turn the small FMS Knob to display the pilot proﬁle list and highlight the desired proﬁle.

Press the ENT Key. The system loads and displays the system settings for the selected proﬁle.

Renaming a proﬁle:

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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 ‘RENAME’ in the Pilot Proﬁle Box.

Press the ENT Key.

In the ‘Rename Proﬁle’ window, turn the FMS Knob to select the proﬁle to rename.

Press the ENT Key.

Use the FMS Knob to enter a new proﬁle name up to 16 characters long and press the ENT Key.

With ‘RENAME’ highlighted, press the ENT Key.

To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Additional Features

Deleting a proﬁle:

Flight

InstrumentsEIS

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’ in the Pilot Proﬁle Box.

Press the ENT Key.

Nav/Com/

XPDR/AudioGPS Nav

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.

Flight

PlanningProcedures

Importing a proﬁle:

Insert the SD card containing the Pilot Proﬁle into the top card slot on the MFD.

Use the FMS Knob to select the AUX - System Setup Page.

Hazard

Additional

Abnormal

Avoidance

Features

OperationAnnun/AlertsAppendixIndex

Press the IMPORT softkey. If the correct Pilot Proﬁle ﬁle is selected; with ‘IMPORT’ highlighted press the ENT Key.

Or:

If the SD card contains more than one Pilot Proﬁle:

Turn the large FMS Knob to highlight the select ﬁle ﬁeld in the Pilot Proﬁle Importing Box.

Turn the small FMS Knob to display the pilot proﬁle list and highlight the desired proﬁle to import and press the ENT Key.

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

190-01462-00 Rev. A

Additional Features

Exporting a proﬁle:

Insert the SD card for storing the Pilot Proﬁle into the top card slot on the MFD.

Use the FMS Knob to select the AUX - System Setup Page.

Activate the desired Pilot Proﬁle to export. Only the active Pilot Proﬁle can be exported.

Press the EXPORT softkey.

With ‘EXPORT’ highlighted press the ENT Key.

“Pilot proﬁle export succeeded.” is shown in the export results box. Press the ENT Key to exit the Pilot Proﬁle Exporting Box.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Additional Features

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Abnormal Operation

Instruments EIS

ABNORMAL OPERATION

Flight

REVERSIONARY MODE

In reversionary mode, critical ﬂight instrumentation is combined with engine

instrumentation on the remaining displays.

When a system detected failure occurs, the display reversionary modes are as

XPDR/Audio GPS Nav

Nav/Com/

follows:

• PFD failure – MFD does not automatically enter reversionary mode,

reversionary mode must be activated manually.

• MFD failure – PFD automatically enters reversionary mode.

Planning Procedures

• Reversionary display mode can be manually activated by pressing the

Flight

DISPLAY BACKUP Button on the audio panel. When the DISPLAY

BACKUP Button is selected both displays enter reversionay display mode.

NOTE: The PA-44-180 Seminole Pilot’s Operating Handbook (POH) always takes precedence over the information found in this section.

Avoidance

Hazard

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

Additional

Features

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.

Operation Annun/Alerts Appendix Index

Abnormal

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

If GPS position is lost, or becomes invalid, selected hazards being displayed on the

Navigation Map Page are removed until GPS position is again established.

Loss of Hazard Functions with Loss of GPS

Position

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Abnormal Operation

UNUSUAL ATTITUDES

Flight

InstrumentsEIS

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary functions are displayed in these situations.

The following information is removed from the PFD (and corresponding softkeys are disabled) when the aircraft experiences unusual attitudes:

• Trafﬁc Annunciations

• AFCS Annunciations

Nav/Com/

XPDR/AudioGPS Nav

• Flight Director Command Bars

• Inset Map

• Temperatures

• DME Information

Flight

PlanningProcedures

Window

• Wind Data

• Selected Heading Box

• Selected Course Box

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

• Transponder Status Box

• System Time

• PFD Setup Menu

• Windows displayed in the lower right corner of the PFD:

– Timer/References – Nearest Airports – Flight Plan – Messages – Procedures

Extreme Pitch Indication

• Barometric Minimum Descent Altitude Box

• Glideslope, Glidepath, and Vertical Deviation Indicators

• Altimeter Barometric Setting

• Selected Altitude

• VNV Target Altitude

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 aircraft’s current estimated position.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Abnormal Operation

Instruments EIS

Flight

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.

XPDR/Audio GPS Nav

DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’

Nav/Com/

superimposed in yellow over the ‘own aircraft’ symbol as shown in the following ﬁgure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following ﬁgure. 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.

Planning Procedures

Flight

Normal navigation using GPS/SBAS source data resumes automatically once a valid

GPS solution is restored.

It is important to note that estimated navigation data supplied by the 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,

Avoidance

Hazard

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 heading and/or airspeed data available should not be used for

Additional

Features

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

Operation Annun/Alerts Appendix Index

Abnormal

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

190-01462-00 Rev. A 71

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Abnormal Operation

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

Flight

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

InstrumentsEIS

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

Nav/Com/

• All Bearing Pointer Distances

XPDR/AudioGPS Nav

• 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

Flight

PlanningProcedures

degraded accuracy.

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Annunciations & Alerts

ANNUNCIATIONS & 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 Pilot’s Operating Handbook (POH) for additional information regarding pilot responses to these annunciations

System Annunciation Comment

Attitude and Heading Reference System is aligning.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

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.

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Annunciations & Alerts

System Annunciation Comment

Flight

InstrumentsEIS

Display system is not receiving airspeed input from air data computer.

Nav/Com/

XPDR/AudioGPS Nav

Display system is not receiving altitude input from the air data computer.

Flight

PlanningProcedures

Display system is not receiving vertical speed input from the air data computer.

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

Other Various Red X

Indications

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

A red ‘X’ through any other display ﬁeld (such as engine instrumentation display) indicates that the ﬁeld is not receiving valid data.

190-01462-00 Rev. A

Annunciations & Alerts

Instruments EIS

CAS ANNUNCIATIONS

Flight

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 pilot responses.

Warning Annunciations

Annunciation

Window Text

L ENG CHT R ENG CHT L ALTR FAIL R ALTR FAIL L FUEL QTY

R FUEL QTY

L START ENGD

R START ENGD

GEAR SYS

Left engine CHT in warning range Right engine CHT in warning range Left Alternator failure

Right Alternator failure Left fuel quantity in warning range Right fuel quantity in warning range Left starter motor energized when engine is

running Right starter motor energized when engine is

running A failure of a gear system component has been

detected Landing gear are not down and locked

CHECK GEAR

or Landing gear is selected UP on the ground

HTR OVERHEAT

Heater unit has sensed an overheat condition

Description Audio Alert

Triple Chime

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Annunciations & Alerts

Caution Annunciations

Flight

InstrumentsEIS

Annunciation

Window Text

L FUEL QTY

R FUEL QTY

PITOT HEAT FAIL

Nav/Com/

PITOT HEAT OFF

XPDR/AudioGPS Nav

GEAR SYS

CHECK GEAR

HYDR PUMP ON

Flight

PlanningProcedures

Advisory Annunciations

Description Audio Alert

Left fuel quantity in caution range Right fuel quantity in caution range Pitot heat failure Pitot heat selected OFF A failure of a gear system component has been

detected Landing gear are not down and locked Hydraulic pump is running when it should not be

running

Double Chime

Annunciation Window Text

EMERG BATT ON

Hazard

Avoidance

FUEL IMBAL

MAINT MODE ON

PFD FAN FAIL

Features

Additional

MFD FAN FAIL

AV FAN FAIL

Abnormal

OperationAnnun/AlertsAppendixIndex

SYSTEM MESSAGES

Alerts Window Text Description

WOW MISCOMPARE

Description Audio Alert

Emergency power in use Fuel imbalance (left vs. right tank quantity) Maintenance Mode ON

Single Chime

PFD display fan is inoperative MFD display fan is inoperative

Avionics fan fail

Left and right squat switches do not agree

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Annunciations & Alerts

VOICE ALERTS

Message Priority Description

“Stall”

“Airspeed” Airspeed exceeds VNE

“Minimums, minimums”

Warning

“Check Gear” Landing gear are not down and locked

“Trafﬁc”

“Trafﬁc, (distance, bearing, altitude)” TAS Trafﬁc Alert

Caution

“Check Gear” Landing gear are not down and locked

“TAS System Test Passed”

“TAS System Test Failed” TAS system initiated test failed

“Vertical track”

Advisory

“TIS Not Available” Aircraft is outside TIS coverage area

“Timer Expired” Countdown timer on the PFD has reached zero

Imminent stall is sensed by stall vane

Aircraft has descended below the preset barometric minimum descent altitude

TIS Trafﬁc Alert

TAS system initiated test passed

Aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled.

TERRAIN-SVT ALERTS

PFD/MFD

Alert Type

Reduced Required Terrain Clearance Warning (RTC)

Imminent Terrain Impact Warning (ITI)

Reduced Required Obstacle Clearance Warning (ROC)

Imminent Obstacle Impact Warning (IOI)

Reduced Required Terrain Clearance Caution (RTC)

Imminent Terrain Impact Caution (ITI)

Reduced Required Obstacle Clearance Caution (ROC)

TERRAIN-SVT

Page

Annunciation

MFD

Pop-Up Alert

Aural

Message

“Warning; Terrain,

Terrain”

“Warning; Terrain,

Terrain”

“Warning; Obstacle,

Obstacle”

“Warning; Obstacle,

Obstacle”

“Caution; Terrain,

Terrain”

“Caution; Terrain,

Terrain”

“Caution; Obstacle,

Obstacle”

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Annunciations & Alerts

Flight

InstrumentsEIS

Alert Type

PFD/MFD

TERRAIN-SVT

Page

Pop-Up Alert

Annunciation

Imminent Obstacle Impact Caution (IOI)

TERRAIN-SVT SYSTEM STATUS ANNUNCIATIONS

Nav/Com/

XPDR/AudioGPS Nav

Alert Type

PFD/MFD Alert

Annunciation

System Test in Progress

Flight

System Test Pass None None

PlanningProcedures

Terrain Alerting is disabled

MFD Terrain or Obstacle database unavailable or invalid.

Hazard

Terrain-SVS operating

Avoidance

None TERRAIN DATABASE FAILURE None

with PFD Terrain or Obstacle databases

Terrain System Test

Features

Additional

Fail

Terrain or Obstacle database unavailable

Abnormal

OperationAnnun/AlertsAppendixIndex

or invalid, invalid software conﬁguration, system audio fault

No GPS position NO GPS POSITION

Excessively degraded GPS signal, Out of database coverage area

Sufﬁcient GPS signal received after loss

None None

TERRAIN-SVT Page

Annunciation

TERRAIN TEST None

TERRAIN FAIL

MFD

None

Aural

Message

“Caution; Obstacle,

Obstacle”

Aural Message

“Terrain System

Test OK”

None

“Terrain System

Failure”

“Terrain System

Failure”

“Terrain System

Not Available”

“Terrain System

Not Available”

“Terrain System

Available”

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

TAWS-B ALERTS

Annunciations & Alerts

Instruments EIS

Flight

Alert Type

Excessive Descent Rate Warning (EDR)

Reduced Required Terrain Clearance Warning (RTC)

Imminent Terrain Impact Warning (ITI)

Reduced Required Obstacle Clearance Warning (ROC)

Imminent Obstacle Impact Warning (IOI)

Reduced Required Terrain Clearance Caution (RTC)

Imminent Terrain Impact Caution (ITI)

Reduced Required Obstacle Clearance Caution (ROC)

PFD/MFD TAWS-B Page Annunciation

MFD

Pop-Up Alert

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up, Pull Up”

“Terrain Ahead, Pull Up; Terrain

Ahead, Pull Up”

Terrain Ahead, Pull Up; Terrain

Ahead, Pull Up”

“Terrain, Terrain; Pull Up, Pull Up”

“Obstacle, Obstacle; Pull Up, Pull

Up”

“Obstacle Ahead, Pull Up; Obstacle

Ahead, Pull Up”

“Obstacle Ahead, Pull Up; Obstacle

Ahead, Pull Up”

“Obstacle, Obstacle; Pull Up, Pull

Up”

“Caution, Terrain; Caution, Terrain”

“Terrain Ahead; Terrain Ahead”

“Caution, Terrain; Caution, Terrain”

“Caution, Obstacle; Caution,

Obstacle”

“Obstacle Ahead; Obstacle Ahead”

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Annunciations & Alerts

Flight

InstrumentsEIS

Alert Type

PFD/MFD TAWS-B Page Annunciation

Imminent Obstacle Impact Caution (IOI)

Premature Descent

Nav/Com/

XPDR/AudioGPS Nav

Alert Caution (PDA)

Altitude Callout

None None “Five-Hundred”

“500”

Excessive Descent Rate Caution

Flight

PlanningProcedures

(EDR)

Negative Climb Rate Caution (NCR)

TAWS-B SYSTEM STATUS ANNUNCIATIONS

Hazard

Avoidance

Alert Type

PFD/MFD Alert

Annunciation

MFD

Pop-Up Alert

Aural Message

“Obstacle Ahead; Obstacle Ahead”

“Caution, Obstacle; Caution,

Obstacle”

“Too Low, Terrain”

“Sink Rate”

“Don’t Sink”

“Too Low, Terrain”

TAWS-B Page Annunciation Aural Message

System Test in Progress TAWS TEST None

Features

Additional

System Test Pass None None

TAWS Alerting is disabled

Abnormal

OperationAnnun/AlertsAppendixIndex

None

MFD Terrain or Obstacle database unavailable or invalid. TAWS operating

None TERRAIN DATABASE FAILURE None with PFD Terrain or Obstacle databases

TAWS-B System Test Fail TAWS FAIL

Terrain or Obstacle database unavailable or invalid, invalid software

TAWS FAIL

conﬁguration, system audio fault

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

“TAWS System

Test OK”

None

“TAWS System

Failure”

“TAWS System

Failure”

190-01462-00 Rev. A

Annunciations & Alerts

Alert Type

No GPS position NO GPS POSITION

Excessively degraded GPS signal, Out of database coverage area

Sufﬁcient GPS signal received after loss

PFD/MFD Alert

Annunciation

TAWS-B Page Annunciation Aural Message

None

None None “TAWS Available”

GDL 69/69A DATA LINK RECEIVER MESSAGES

“TAWS Not

Available”

“TAWS Not

Available”

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Message Message Location Description

CHECK ANTENNA

UPDATING

NO SIGNAL

LOADING XM Radio Page (MFD)

OFF AIR XM Radio Page (MFD) Channel not in service

-------- XM Radio Page (MFD) Missing channel information

WEATHER DATA LINK FAILED

ACTIVATION REQUIRED

DETECTING ACTIVATION

WAITING FOR DATA...

XM Information Page

(MFD)

XM Information Page

(MFD))

XM Information Page

Weather Datalink Page

(MFD)

Weather Datalink Page

(MFD)

XM Information Page

(MFD)

Weather Datalink Page

(MFD)

Weather Datalink Page

(MFD)

Data Link Receiver antenna error; service required

Data Link Receiver updating encryption code

Loss of signal; signal strength too low for receiver

Acquiring channel audio or information

No communication from Data Link Receiver within last 5 minutes

SiriusXM subscription is not activated

SiriusXM subscription is activating.

SiriusXM subscription conﬁrmed downloading weather data.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Flight

InstrumentsEIS

DATA LOST

Message Comments

– Pilot stored data

was lost. Recheck settings.

XTALK ERROR

Nav/Com/

XPDR/AudioGPS Nav

crosstalk error has occurred.

PFD1 SERVICE

– A ﬂight display

– PFD1 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

service. Return unit for repair.

Flight

PlanningProcedures

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– MFD1 software

mismatch, communication halted.

PFD1 CONFIG

Conﬁg service req’d.

Hazard

Avoidance

MFD1 CONFIG

error. Conﬁg service req’d.

Features

Additional

SW MISMATCH

version mismatch. Xtalk is off.

Abnormal

OperationAnnun/AlertsAppendixIndex

PFD1 COOLING

– PFD1 conﬁg error.

– MFD1 conﬁg

– GDU software

– PFD1 has poor

cooling. Reducing power usage.

MFD1 COOLING

– MFD1 has poor

cooling. Reducing power usage.

PFD1 KEYSTK

– PFD1 [key name]

Key is stuck.

MFD1 KEYSTK

– MFD [key name]

Key is stuck.

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

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

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

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

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

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

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

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

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.

Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole

190-01462-00 Rev. A

Garmin PA-44-180 Reference Guide

Specifications and Main Features

Frequently Asked Questions

User Manual

Flight Instruments

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

CHANGE NAVIGATION SOURCES

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

GENERIC TIMER

TURN ALL VSPEED BUGS ON OR OFF

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

DISPLAYING WIND DATA

ENGINE DISPLAY

ENGINE INDICATION

ENGINE PAGE

LANDING GEAR INDICATIONS

NAV/COM/TRANSPONDER/AUDIO PANEL

ENTER A TRANSPONDER CODE

DME TUNING

SELECTING A COM RADIO

SELECTING A NAV RADIO

NAV/COM TUNING

DIGITAL CLEARANCE RECORDER AND PLAYER

INTERCOM SYSTEM (ICS) ISOLATION

GPS NAVIGATION

DIRECT-TO NAVIGATION

ACTIVATE A STORED FLIGHT PLAN

ACTIVATE A FLIGHT PLAN LEG

STOP NAVIGATING A FLIGHT PLAN

VERTICAL NAVIGATION (VNAV)

FLIGHT PLANNING

WEIGHT PLANNING

TRIP PLANNING

CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS

CREATE A USER WAYPOINT USING THE MAP POINTER

DELETE A USER WAYPOINT

CREATE A FLIGHT PLAN

IMPORT A FLIGHT PLAN FROM AN SD CARD

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

ENTER AN AIRWAY IN A FLIGHT PLAN

USER-DEFINED HOLDING PATTERNS

INVERT AN ACTIVE FLIGHT PLAN

STORE A FLIGHT PLAN

EDIT A STORED FLIGHT PLAN

DELETE A WAYPOINT FROM THE FLIGHT PLAN

INVERT AND ACTIVATE A STORED FLIGHT PLAN

COPY A FLIGHT PLAN

DELETE A FLIGHT PLAN

GRAPHICAL FLIGHT PLAN CREATION

EXPORT A FLIGHT PLAN TO AN SD CARD

PROCEDURES

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

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

ACTIVATE A VECTOR TO FINAL APPROACH FIX

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

TEMPERATURE COMPENSATED ALTITUDE

Hazard Avoidance

Customizing THE HAZARD DISPLAYS ON THE NAVIGATION MAP

SIRIUSXM WEATHER (OPTIONAL)

TRAFFIC SYSTEMS

TERRAIN AND OBSTACLE PROXIMITY

TERRAIN-SVS

TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY (OPTIONAL)

Additional Features

SYNTHETIC VISION (OPTIONAL)

TERMINAL PROCEDURE CHARTS

AIRPORT DIRECTORY

SIRIUSXM RADIO ENTERTAINMENT

PILOT PROFILES

Abnormal Operation

REVERSIONARY MODE

ABNORMAL COM OPERATION

HAZARD DISPLAYS WITH LOSS OF GPS POSITION