Garmin PA-34-220T Reference Guide

®

G1000

Cockpit Reference Guide for the Piper PA-34-220T Seneca

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

Copyright © 2013 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 1578.01 or later for the Piper
PA-34-220T Seneca. Some differences in operation may be observed when comparing the
information in this manual to earlier or later software versions.

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

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

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

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

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. WATCH®,
FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; 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.

May, 2013 190-01405-00 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-34-220T Seneca

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-34-220T Seneca

190-01405-00 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-34-220T Seneca

Warnings, Cautions & Notes

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

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

NOTE: 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.

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.

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

190-01405-00 Rev. A

Record of Revisions

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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Record of Revisions

Part Number Change Summary

190-01405-00 Initial release

Revision Date of Revision Affected Pages Description

A May, 2013 All Production release

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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

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

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

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

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

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

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

Turn ALL Vspeed Bugs On or Off ............................................................................................ 3

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

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

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

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

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

Flap Indications ....................................................................................................................... 10

Landing Gear Indications ...................................................................................................... 11

NAV/COM/TRANSPONDER/AUDIO PANEL ....................................................................... 13

Enter a Transponder Code..................................................................................................... 13

DME Tuning...............................................................................................................................13

Selecting a COM Radio .......................................................................................................... 13

Selecting a NAV Radio ........................................................................................................... 13

NAV/COM Tuning ..................................................................................................................... 14

Digital Clearance Recorder and Player .............................................................................. 14

Intercom System (ICS) Isolation .......................................................................................... 15

GPS NAVIGATION ........................................................................................................................ 17

Direct-to Navigation .............................................................................................................. 17

Activate a Stored Flight Plan ............................................................................................... 18

Activate a Flight Plan Leg ..................................................................................................... 18

Stop Navigating a Flight Plan .............................................................................................. 19

Vertical Navigation (VNAV)................................................................................................... 19

FLIGHT PLANNING ...................................................................................................................... 23

Weight Planning ...................................................................................................................... 23

Trip Planning ............................................................................................................................ 23

Create a User Waypoint Defined by Latitude & Longitude ........................................... 25

Create a User Waypoint Defined by Radials from Other Waypoints ........................... 26

Create a User Waypoint Defined by a Radial & Distance from Another Waypoint .. 28

Create a User Waypoint using the Map Pointer............................................................... 29

Delete a User Waypoint ......................................................................................................... 30

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Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

Table of Contents

Create a Flight Plan ................................................................................................................ 30

Import a Flight Plan from an SD Card ................................................................................ 31

Insert a Waypoint in the Active Flight Plan ...................................................................... 32

Enter an Airway in a Flight Plan .......................................................................................... 33

Creating a User-Defined Hold at an Active Flight Plan Waypoint ................................ 33

Creating a User-Defined Hold at the Aircraft Present Position ....................................34

Removing a User-Defined Hold (Created at the Aircraft P.POS) .................................. 34

Removing a User-Defined Hold (Created at an Active Waypoint) ............................... 35

Invert An Active Flight Plan .................................................................................................. 35

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 35

Store a Flight Plan .................................................................................................................. 36

Edit a Stored Flight Plan ....................................................................................................... 36

Delete a Waypoint from the Flight Plan ............................................................................ 36

Invert and Activate a Stored Flight Plan ........................................................................... 37

Copy a Flight Plan ................................................................................................................... 37

Delete a Flight Plan ................................................................................................................ 37

Graphical Flight Plan Creation ............................................................................................. 38

Export a Flight Plan to an SD Card ..................................................................................... 38

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 ............................................................... 41

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

STORMSCOPE® (Optional) ..................................................................................................... 45

SiriusXM Weather (Optional) ............................................................................................... 47

Connext Weather (Optional) ................................................................................................ 50

Traffic Advisory System (TAS) .............................................................................................. 62

Terrain And Obstacle Proximity ........................................................................................... 64

Terrain-SVS ............................................................................................................................... 64

Terrain Awareness & Warning System (TAWS-B) Display (Optional) ........................... 66

Airborne Color Weather Radar ............................................................................................ 68

ADDITIONAL FEATURES ........................................................................................................... 71

Synthetic Vision (Optional) ................................................................................................... 71

Terminal Procedure Charts ................................................................................................... 72

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Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

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Table of Contents

Airport Directory .................................................................................................................... 74

SiriusXM Radio Entertainment (Optional) ........................................................................ 75

ABNORMAL OPERATION..........................................................................................................77

Reversionary Mode ................................................................................................................ 77

Abnormal COM Operation .................................................................................................... 77

Hazard Displays with Loss of GPS Position ....................................................................... 78

Unusual Attitudes ................................................................................................................... 78

Dead Reckoning ...................................................................................................................... 79

ANNUNCIATIONS & ALERTS ................................................................................................... 81

G1000 System Annunciations ............................................................................................... 81

G1000 System Annunciations (Cont.) ................................................................................. 82

CAS Annunciations .................................................................................................................. 83

System Messages .................................................................................................................... 85

Comparator Annunciations ................................................................................................... 85

Reversionary Sensor Annunciations ................................................................................... 85

Voice Alerts .............................................................................................................................. 86

Terrain-SVS Alerts ................................................................................................................... 87

Terrain-SVS System Status Annunciations ........................................................................ 87

TAWS-B Alerts .......................................................................................................................... 88

TAWS-B System Status Annunciations ............................................................................... 90

MFD & PFD Message Advisories .......................................................................................... 91

Database Message Advisories ............................................................................................. 93

GMA 1347 Message Advisories ............................................................................................ 96

GIA 63W Message Advisories ............................................................................................... 97

GEA 71 Message Advisories ................................................................................................ 100

GTX 33 & 33 w/ES Message Advisories ............................................................................ 100

GRS 77 Message Advisories ................................................................................................ 101

GMU 44 Message Advisories .............................................................................................. 102

GDL 69A Message Advisories ............................................................................................. 103

GDC 74A Message Advisories ............................................................................................. 103

GWX 68 Alert Messages ....................................................................................................... 104

Miscellaneous Message Advisories ................................................................................... 104

Flight Plan Import/Export Messages ................................................................................ 108

APPENDIX ..................................................................................................................................... 111

PFD Softkey Map .................................................................................................................. 111

MFD Softkey Map ................................................................................................................. 117

Loading Updated Databases .............................................................................................. 120

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

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190-01405-00 Rev. A

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 BARO Knob.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

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

2)

Press the ALT UNIT Softkey.

3)

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

Or

:

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

4)

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

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION
Window.

4)

Turn the

small

FMS Knob clockwise to ON or counterclockwise to OFF.

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

SYNCHRONIZE CDI

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.

4)

Turn the

190-01405-00 Rev. A 1

small

FMS Knob clockwise to ON or counterclockwise to OFF.

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

Flight Instruments

CHANGE NAVIGATION SOURCES

Flight

1)

InstrumentsEIS

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

2)

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

Nav/Com/

XPDR/AudioGPS Nav

3)

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

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)

Press the OBS Softkey to select OBS Mode.

2)

Turn a CRS Knob to select the desired course to/from the waypoint. Press

Flight

PlanningProcedures

the CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.

3)

Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1)

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

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

2)

Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.

3)

Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.

TURN INDIVIDUAL VSPEED BUGS ON OR OFF

1)

Press the TMR/REF Softkey.

2)

Turn the

3)

Turn the

4)

To remove the window, press the CLR Key or the TMR/REF Softkey.

2

large

FMS Knob to highlight the desired Vspeed.

small

FMS Knob clockwise to ON or counterclockwise to OFF.

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

190-01405-00 Rev. A

Flight Instruments

TURN ALL VSPEED BUGS ON OR OFF

1)

Press the TMR/REF Softkey.

2)

Press the MENU Key.

3)

Turn the FMS Knob to highlight the desired option.

4)

Press the ENT Key. Press the TMR/REF Softkey to remove the window.

SET BAROMETRIC ALTIMETER MINIMUM DESCENT ALTITUDE

1)

Press the TMR/REF Softkey.

2)

Turn the large FMS Knob to highlight the OFF/BARO/TEMP COMP field to
the right of ‘MINIMUMS’.

3)

Turn the small FMS Knob clockwise to select BARO or TEMP COMP.
Selecting TEMP COMP will allow the system to use an altitude
compensated for temperature.

4)

Press the ENT Key.

5)

Use the small FMS Knob to enter the desired altitude.

6)

Press the ENT Key.

7)

To remove the window, press the CLR Key or the TMR/REF Softkey.

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

DISPLAYING WIND DATA

1)

Press the PFD Softkey.

2)

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

3)

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

4)

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

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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

4

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

190-01405-00 Rev. A

ENGINE DISPLAY

ENGINE INDICATION

EIS

Instruments EIS

Flight

10

11

12

1

XPDR/Audio GPS Nav

Nav/Com/

2

3

4

Planning Procedures

Flight

5

6

7

Avoidance

Hazard

8

9

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

13

Engine Display when

Engine Page is displayed

Engine Display

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Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

EIS

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

1

Engine Manifold
Pressure Gauge
(MAN IN HG)

2

Tachometer (RPM)

3

Propeller Sync
Indicator

4

Turbo Inlet
Temperature
Indicator (TIT °F)

5

Fuel Flow Indicator
(FFLOW GPH)

6

Oil Pressure
Indicator
(OIL PSI)

7

Oil Temperature
Indicator (OIL °F)

8

Alternator
Current(ALTR
AMPS)

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 turbo

inlets 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

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

9

Voltage (VOLTS)

10

Battery
Current(BATT
AMPS)

11

Fuel Quantity
Indicator (FUEL
QTY GAL)

12

Flap Position

(FLAPS)

13

Landing Gear Status

(LANDING GEAR)

6

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

Displays the bus voltage.

Displays the battery current in amperes

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

side of a standard fuel tank.

Displays flap position in degrees

Displays landing gear status

190-01405-00 Rev. A

EIS

ENGINE PAGE

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

Page.

1415 13

1

2

3

4

5

6

7

8

9

12

11

10

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Engine Page

1

Engine Manifold

Pressure Gauge

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

indicate engine power

(MAN IN HG)

2

Tachometer (RPM)

Displays propeller speed in revolutions per minute

(rpm)

3

Propeller Sync

Indicator

4

Turbo Inlet

Temperature

Points towards the higher-speed propeller when the

propellers are out of sync.

Displays the temperature for the right and left turbo

inlets in °F

Indicator (TIT °F)

190-01405-00 Rev. A 7

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

EIS

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

5

Fuel Flow Indicator

(FFLOW GPH)

6

Oil Pressure

Indicator
(OIL PSI)

7

Oil Temperature

Indicator (OIL °F)

8

Flap Position

(FLAPS)

9

Landing Gear

Status (LANDING
GEAR)

10

Fuel Calculations

Group
(FUEL CALC)

11

Systems Group

(SYSTEMS)

12

Engine Hours

(TACH TIME)

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 flap position in degrees

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 oxygen in pounds per square inch (OXYGEN

PSI), vacuum in inches of Mercury (VACUUM IN
HG), and propeller heat in amperes (PROP HEAT
AMPS)

Displays the total time in hours the engine has been

in service

Abnormal

OperationAnnun/AlertsAppendixIndex

13

Cylinder Head

Temperature Bar
Graph (CHT °F)

14

Electrical Group

(ELECTRICAL)

15

Fuel Quantity

Gauges
(L/R FUEL QTY
GAL)

8

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

Displays head temperatures for all cylinders in °F

Displays alternator (ALTR AMPS) and battery (BATT

AMPS) currents in amperes and bus voltage (VOLTS)

Displays the total amount of fuel and the amount of

fuel in gallons (gal) for each side of a standard fuel
tank

190-01405-00 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 nautical miles per gallon, NMPG) 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

Flight

Avoidance

Hazard

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Fuel Calculations Group

190-01405-00 Rev. A 9

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

EIS

FLAP INDICATIONS

Flight

InstrumentsEIS

played as ‘--’.

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Flap positions are labeled 0°, 10°, 25°, and 40°. An invalid flap position is dis-

Indication Description

Flaps normal (EIS)

Flaps normal (Engine Page
displayed)

Invalid flap position (EIS)

Invalid flap position
(Engine Page displayed)

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

10

Flap Indications

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

190-01405-00 Rev. A

EIS

LANDING GEAR INDICATIONS

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

Position EIS Engine Page

Up &

Locked

In Transition

Down and

Locked

Instruments EIS

Flight

XPDR/Audio GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Warning

Landing Gear Indications

190-01405-00 Rev. A 11

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

Additional

Features

Operation Annun/Alerts Appendix Index

Abnormal

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioGPS Nav

Flight

PlanningProcedures

EIS

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

OperationAnnun/AlertsAppendixIndex

12

Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

190-01405-00 Rev. A