This manual reflects the operation of System Software 1705.00 or later for the AgustaWestland
AW119Kx. 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 G1000H™ 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.
Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.;
NavData® is a registered trademark of Jeppesen, Inc.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AC-U-KWIK® is a registered trademark of Penton Business Media 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.
March, 2013 190-01515-00 Rev. B Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000H GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74H Air Data Computer, or
other altimeters in the aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the G1000H PFD or
other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000H system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so entirely
at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: 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.
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
Warnings, Cautions & Notes
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.
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: The Garmin G1000H, as installed in the AgustaWestland AW119
rotorcraft, has a very high degree of functional integrity. However, the pilot
must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G1000H. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.
WARNING: For safety reasons, G1000H 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 Garmin G1000H utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000H can be misused or misinterpreted and,
therefore, become unsafe.
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
Warnings, Cautions & Notes
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000H Pilot’s Guide documentation and the
AgustaWestland AW119 Rotorcraft Flight Manual (RFM). Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare
indications from the G1000H to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use the
G1000H to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
WARNING: Lamp(s) inside this product may 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.
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
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 Garmin G1000H does not contain any user-serviceable
parts. Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the G1000H panel and displays, are subject to change and may not
reflect the most current G1000H system and aviation 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: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
NOTE: Do not rely solely 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: 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 G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
Warnings, Cautions & Notes
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: 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 G1000H system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000H Pilot’s Guide for this aircraft.
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
Warnings, Cautions & Notes
Blank Page
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
Record of Revisions
Part NumberChange Summary
190-01515-00Initial Release
RevisionDate of RevisionAffected PagesDescription
AMarch, 2013AllInitial Release
BMarch, 2013AllUpdated CAS messages
Clerical corrections
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
INDEX .........................................................................................................................................Index-1
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
iii
Table of Contents
Blank Page
iv
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
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.
Com/Nav/
XPDRGPS Nav
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
1
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 a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
XPDRGPS Nav
Com/Nav/
GENERIC TIMER
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
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 starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.
SET BAROMETRIC/RADAR ALTIMETER (OPTIONAL) MINIMUM DESCENT
Hazard
Avoidance
ALTITUDE
Features
Additional
Abnormal
OperationAnnun/AlertsAppendixIndex
1)
Press the
2)
Turn the large FMS Knob to highlight the Minimums field.
3)
Turn the small FMS Knob to select the barometric (BARO), TEMP COMP
TMR/REF
Softkey.
baro or radar altimeter (RAD ALT) altitude source. OFF is selected 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 (BARO or TEMP
COMP from zero to 16,000 feet, RAD ALT from zero to 2,500 feet ). If
TEMP COMP was selected, a field for entering the airport temperature and
altitude will appear. Press the ENT Key or turn the large FMS Knob to
highlight this field, and use the small FMS Knob to enter the temperature.
5)
To remove the window, press the
2
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
CLR
Key or press the
TMR/REF
190-01515-00 Rev. B
Softkey.
Flight Instruments
DISPLAYING WIND DATA
1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data to the left of the HSI.
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.
CHANGING HSI FORMAT
1)
Press the PFD Softkey.
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Or
:
Press the ARC HSI Softkey to display the arc style HSI.
ENABLE HEADING PRESET MODE
1)
Press the SET HDG Softkey on the PFD. The system is in Heading Preset
Mode (HPM) as indicated by displaying ‘SET’ to the left of the heading
value.
2)
Press the HDG + and/or HDG - Softkeys to slew the heading value to the
desired setting.
Or
:
Set the Selected Heading Bug to the desired heading value, then press the
HDG SYNC Softkey.
InstrumentsEIS
Flight
Com/Nav/
XPDRGPS Nav
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
OperationAnnun/AlertsAppendixIndex
Abnormal
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
3
Flight Instruments
DISABLE HEADING PRESET MODE
Flight
InstrumentsEIS
Press the HPM OFF Softkey on the PFD to manually disable Heading Preset
Mode.
Or
:
Heading Preset Mode automatically disables after eight minutes.
If there is more than 10° difference between the Heading Preset value and the
XPDRGPS Nav
magnetic heading when Heading Preset Mode is disabled, the heading value is
Com/Nav/
displayed in yellow and ‘ALN’ will be displayed to the left of the heading. When the
magnetic heading has properly aligned, the heading value will be displayed in white
and ‘ALN’ will no longer be displayed.
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
OperationAnnun/AlertsAppendixIndex
4
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
Engine Indication System
ENGINE INDICATION SYSTEM
NOTE: Refer to the Rotorcraft Flight Manual (RFM) for limitations.
InstrumentsEIS
Flight
The G1000H Engine Indication System (EIS) displays critical engine, electrical,
fuel, and other system parameters on the left side of the Primary Flight Display (PFD)
Com/Nav/
XPDRGPS Nav
and Multi Function Display (MFD) during normal operations (Figure 3-1). EIS
information can be fully expanded to an entire page (EIS - Engine Page) using the
ENGINE Softkey on the MFD or using the START/AUTOROT pushbutton on the
Cyclic.
PFD
PlanningProcedures
Flight
EIS Strip
Avoidance
Hazard
Additional
Features
MFD
OperationAnnun/AlertsAppendixIndex
Abnormal
EIS Strip
190-01515-00 Rev. B
EIS (Normal)
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
5
Engine Indication System
Flight
InstrumentsEIS
XPDRGPS Nav
Com/Nav/
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
OperationAnnun/AlertsAppendixIndex
Fuel Quantity Indicator
1
(FUEL QTY KG)
2
Inter Turbine Temperature
(ITT)
3
Gas Generator Speed (N1)
4
Torque (TRQ)
5
Power Turbine Speed (N2)
6
Rotor Speed (NR)
Oil Pressure Indicator
7
(ENG OIL PSI)
8
Oil Temperature Indicator
(ENG OIL ºC)
9
Transmission Oil Pressure
(XMSN OIL PSI)
10
Transmission Oil
Temperature (XMSN
OIL ºC)
Hydraulic Pressure
11
(HYD PSI)
12
Fuel PSI
Displays the quantity of fuel in each fuel tank
as well as the total fuel.
Displays the current Inter Turbine Air
Temperature (˚ Celsius).
Displays a digital readout of the Gas Generator
Compressor Speed as a percentage.
Displays current fuel engine Torque as a
percentage.
Displays current Power Turbine Speed as a
percentage on a round dial, a digital readout
is shown to the side.
Displays Rotor Speed as a percentage, a digital
readout is shown to the side.
Displays the oil pressure supplied to the engine
in pounds per square inch
Displays engine oil temperature (˚ Celsius).
Display the pressure of oil supplied to the
transmission in pounds per square inch.
Displays the transmission oil temperature (˚
Celsius).
Displays the current Hydraulic Pressure for
both hydraulic systems (1 and 2) in pounds
per square inch.
Displays the current Fuel Pressure in pounds
per square inch
Generator Ammeter
13
(AMP)
14
Generator Voltmeter
(VDC)
6
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
Displays the generator load in amperes
Displays the generator voltage.
190-01515-00 Rev. B
Engine Indication System
InstrumentsEIS
Flight
1
7
2
8
Com/Nav/
XPDRGPS Nav
9
3
10
PlanningProcedures
Flight
4
Avoidance
Hazard
11
Additional
Features
5
6
OperationAnnun/AlertsAppendixIndex
Abnormal
12
13
14
190-01515-00 Rev. B
EIS Display (PFD)
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
EIS Display (MFD)
7
Engine Indication System
ENGINE PAGE
Flight
Pressing the ENGINE Softkey or the START/AUTOROT pushbutton on the
InstrumentsEIS
Cyclic, displays the EIS - ENGINE Page which provides a full screen view of all
engine instruments. The EIS-Engine Page is automatically displayed when N1 <
51%.
Engine Parameters
1
XPDRGPS Nav
Com/Nav/
2
3
Flight
PlanningProcedures
4
5
Fuel System
Hazard
Avoidance
6
Features
Additional
7
Power Turbine Speed
(N2)
Rotor Speed (NR)
Torque (TRQ)
Gas Generator Speed
(N1)
Inter Turbine
Temperature (ITT)
Fuel Quantity
Indicator
(FUEL QTY KG)
Fuel PSI
Displays current Power Turbine Speed as a
percentage on a round dial, a digital readout is
shown to the side.
Displays Rotor Speed as a percentage, a digital
readout is shown to the side.
Displays current fuel engine Torque as a
percentage.
Displays a digital readout of the Gas Generator
Compressor Speed as a percentage.
Displays the current Inter Turbine Air Temperature
(˚ Celsius).
Displays the quantity of fuel in each fuel tank as
well as the total fuel in KG.
Displays the current Fuel Pressure in pounds per
square inch
Electrical System
Abnormal
OperationAnnun/AlertsAppendixIndex
Generator Voltmeter
8
9
Generator Ammeter
Hydraulic System
10
Hydraulic Pressure
8
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
(VOLT)
(AMP)
(HYD PSI)
Displays the primary generator voltage.
Displays the generator load in amperes
Displays the current Hydraulic Pressure for both
hydraulic systems in pounds per square inch.
190-01515-00 Rev. B
Engine/Transmission Oil
Oil Pressure Indicator
11
(ENG OIL PSI)
12
Oil Temperature
Indicator
(ENG OIL ºC)
13
Transmission Oil
Pressure (XMSN
OIL PSI)
14
Transmission Oil
Temperature (XMSN
OIL ºC)
12
11
13
Engine Indication System
Displays the oil pressure supplied to the engine in
pounds per square inch
Displays engine oil temperature (˚ Celsius).
Display the pressure of oil supplied to the
transmission in pounds per square inch.
Displays the transmission oil temperature
(˚ Celsius).
14
1
2
InstrumentsEIS
Flight
Com/Nav/
XPDRGPS Nav
PlanningProcedures
Flight
Avoidance
Hazard
10
9
190-01515-00 Rev. B
78
65
Engine Page Display (MFD)
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
Additional
Features
3
OperationAnnun/AlertsAppendixIndex
Abnormal
4
9
Engine Indication System
Flight
InstrumentsEIS
XPDRGPS Nav
Com/Nav/
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
OperationAnnun/AlertsAppendixIndex
10
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
COM/NAV TUNING
1)
Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
2)
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)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
Com/Nav/Transponder
COM/NAV/TRANSPONDER
Active
Fields
Tuning Box
Standby
Fields
InstrumentsEIS
Flight
Com/Nav/
XPDRGPS Nav
PlanningProcedures
Flight
Avoidance
Hazard
Selecting a COM Radio for Transmit
Features
SELECTING A NAV RADIO
A NAV radio is selected for navigation by pressing the CDI Softkey located on the
OperationAnnun/AlertsAppendixIndex
PFD. Pressing the CDI Softkey once selects NAV1 as the navigation radio. Pressing
the CDI Softkey a second time selects NAV2 as the navigation radio. Pressing the CDI
Softkey a third time activates GPS mode. Pressing the CDI Softkey again cycles back
to NAV1.
While cycling through the CDI Softkey selections, the NAV Tuning Box and the
Frequency Transfer Arrow are placed in the active NAV Frequency Field.
190-01515-00 Rev. B
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
11
Additional
Abnormal
Com/Nav/Transponder
The three navigation modes that can be cycled through are:
Flight
• VOR1 (or LOC1) – If NAV1 is selected, a green single line arrow (not shown)
InstrumentsEIS
labeled either VOR1 or LOC1 is displayed on the HSI.
• VOR2 (or LOC2) – If NAV2 is selected, a green double line arrow (shown) labeled
either VOR2 or LOC2 is displayed on the HSI.
• GPS – If GPS Mode is selected, a magenta single line arrow (not shown) appears
on the HSI and neither NAV radio is selected.
XPDRGPS Nav
Com/Nav/
Flight
PlanningProcedures
Standby
Fields
Tuning Box
The NAV Radio is Selected
Active
Fields
by Pressing the
CDI
Softkey
Selecting a NAV Radio for Navigation
Hazard
Avoidance
NAV radios are selected for listening by switching the corresponding knob on the
remote Audio Panel to the “IN” position and by pressing the NAV VOL/ID Knob on
the PFD or MFD.
Features
Additional
ENTER A TRANSPONDER CODE
1)
Abnormal
OperationAnnun/AlertsAppendixIndex
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.
12
Garmin G1000H Cockpit Reference Guide for the AgustaWestland AW119Kx
190-01515-00 Rev. B
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