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.
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.
190-01462-00 Rev. A
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.
190-01462-00 Rev. A
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.
190-01462-00 Rev. A
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
190-01462-00 Rev. A
Record of Revisions
Part NumberChange Summary
190-01462-00Initial release
RevisionDate of RevisionAffected PagesDescription
AJune, 2013AllInitial release
190-01462-00 Rev. ARR-1
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
INDEX .........................................................................................................................................Index-1
190-01462-00 Rev. Aiii
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
190-01462-00 Rev. A
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
InstrumentsEIS
Flight
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1)
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or
:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Press the BACK Softkey to return to the top-level softkeys.
CHANGE NAVIGATION SOURCES
1)
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.
3)
Press the CDI Softkey a third time to return to GPS.
XPDR/AudioGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
190-01462-00 Rev. A1
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Flight Instruments
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
Flight
1)
InstrumentsEIS
Press the OBS Softkey to select OBS Mode.
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
Nav/Com/
GENERIC TIMER
XPDR/AudioGPS Nav
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Flight
PlanningProcedures
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
TURN ALL VSPEED BUGS ON OR OFF
Hazard
Avoidance
1)
Press the TMR/REF Softkey.
2)
Features
Additional
Abnormal
OperationAnnun/AlertsAppendixIndex
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 MINIMUM DESCENT ALTITUDE
1)
Press the
2)
Turn the large FMS Knob to highlight the Minimums field.
3)
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.
4)
Use the small FMS Knob to enter the desired altitude (from zero to 16,000
feet).
2
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
190-01462-00 Rev. A
Flight Instruments
5)
If TEMP COMP was selected, press the ENT Key or turn the large FMS
Knob to highlight the next field and then enter the destination airport
temperature (-59˚C to 59˚C). The temperature compensated altitude
minimum is displayed below the previously enter minimum altitude value.
6)
To remove the window, press the
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.
CLR
Key or the
TMR/REF
Softkey.
InstrumentsEIS
Flight
XPDR/AudioGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
190-01462-00 Rev. A3
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Additional
Features
OperationAnnun/AlertsAppendixIndex
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-44-180 Seminole
190-01462-00 Rev. A
ENGINE DISPLAY
ENGINE INDICATION
EIS
InstrumentsEIS
Flight
10
11
1
XPDR/AudioGPS Nav
Nav/Com/
2
3
4
PlanningProcedures
Flight
5
6
7
Avoidance
Hazard
8
Additional
9
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
12
Engine Display when
Engine Page is displayed
Engine Display
190-01462-00 Rev. A5
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
1
Engine Manifold
Pressure Gauge
(MAN IN HG)
2
Tachometer (RPM)
3
Propeller Sync
Indicator
4
Exhaust Gas
Temperature
(EGT °F)
5
Fuel Flow Indicator
(FFLOW GPH)
6
Oil Pressure
Indicator
(OIL PSI)
7
Oil Temperature
Indicator (OIL °F)
8
Alternator
Current(ALTR
AMPS)
9
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
10
Battery
Current(BATT
AMPS)
11
Fuel Quantity
Indicator (FUEL
QTY GAL)
12
Landing Gear Status
(LANDING GEAR)
6
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
190-01462-00 Rev. A
EIS
ENGINE PAGE
Press the ENGINE Softkey or turn the large FMS Knob and select the EIS - Engine
Page.
141312
1
2
3
4
5
6
7
8
11
10
9
InstrumentsEIS
Flight
XPDR/AudioGPS Nav
Nav/Com/
PlanningProcedures
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
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)
5
Fuel Flow Indicator
Displays fuel flow in gallons per hour (gph)
(FFLOW GPH)
190-01462-00 Rev. A7
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Additional
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
EIS
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
6
Oil Pressure
Indicator
(OIL PSI)
7
Oil Temperature
Indicator (OIL °F)
8
Landing Gear
Status (LANDING
GEAR)
9
Fuel Calculations
Group
(FUEL CALC)
10
Electrical Group
(ELECTRICAL)
11
Engine Hours
(TACH TIME)
12
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
13
Cylinder Head
Temperature Bar
Graph (CHT °F)
14
Fuel Quantity
Gauges
(L/R FUEL QTY
GAL)
8
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
InstrumentsEIS
Flight
XPDR/AudioGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
Fuel Calculations Group
190-01462-00 Rev. A9
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.
PositionEISEngine Page
Up & Locked
In Transition
Down and
Locked
Features
Additional
Abnormal
OperationAnnun/AlertsAppendixIndex
10
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
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
DME TUNING
1)
Press the DME Softkey.
2)
Turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
Nav/Com/XPDR/Audio Panel
InstrumentsEIS
Flight
XPDR/AudioGPS Nav
Nav/Com/
PlanningProcedures
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
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
190-01462-00 Rev. A11
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
Additional
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
Nav/Com/XPDR/Audio Panel
NAV/COM TUNING
Flight
1)
InstrumentsEIS
Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
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
12
Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
190-01462-00 Rev. A
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