This manual reflects the operation of System Software version 0720.13 or later for the Piper PA46 Meridian. 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. 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; and SiriusXM™ is a registered trademark of SiriusXM Satellite Radio,
Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell International, 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.
July, 2011 190-00764-03 Rev. C 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 G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74A 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 G1000
PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000 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: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.
WARNING: XM WX Satellite Weather should not be used for hazardous
weather penetration. Weather information provided by the GDL 69A is
approved only for weather avoidance, not penetration.
190-00764-03 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
Warnings, Cautions & Notes
WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: The Garmin G1000, as installed in the Piper PA-46 Meridian
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. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G1000. 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, G1000 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 G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Piper PA-46 Meridian Pilot’s Operating Handbook. Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the G1000 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 G1000 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.”
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
Warnings, Cautions & Notes
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.
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 G1000 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 G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.
190-00764-03 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
Warnings, Cautions & Notes
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: 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: 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.
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
Record of Revisions
Part NumberChange Summary
190-00764-00
Rev AInitial release
190-00764-01
Rev AAdded Synthetic Vision System and GDU 9.05
190-00764-02
Rev A
Added temporary user waypoints
Added import/export flight plans
Added CDI availability during Dead Reckoning mode
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization
Added GDU 10.01
INDEX .........................................................................................................................................Index-1
190-00764-03 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
iii
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1)
Select the PFD Softkey to display the second-level softkeys.
2)
Select the STD BARO Softkey.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Select the PFD Softkey to display the second-level softkeys.
2)
Select the ALT UNIT Softkey.
3)
Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or
:
Select the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Select the BACK Softkey to return to the top-level softkeys.
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
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.
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
190-00764-03 Rev. C
small
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
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1
Flight Instruments
CHANGE NAVIGATION SOURCES
Flight
InstrumentsEICAS
1)
Select 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)
Select 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
Nav/Com/
XPDR/AudioAFCSGPS Nav
frequency.
3)
Select the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Select 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.
Flight
PlanningProcedures
3)
Select the OBS Softkey again to disable OBS Mode.
GENERIC TIMER
1)
Select 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
Hazard
Avoidance
Features
Additional
Abnormal
Operation
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.
CONFIGURE VSPEED BUGS INDIVIDUALLY
AlertsAppendixIndex
Annun/
1)
Select the TMR/REF Softkey.
2)
Turn the
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
large
FMS Knob to highlight the desired Vspeed.
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
TURN ALL VSPEED BUGS ON OR OFF
1)
Select the TMR/REF Softkey.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Select the TMR/REF Softkey to remove the window.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1)
Select the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to BARO.
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.
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
DISPLAYING WIND DATA
1)
Select the PFD Softkey.
2)
Select the WIND Softkey to display wind data below the Selected Heading.
3)
Select one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, select the OFF Softkey.
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Operation
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AlertsAppendixIndex
3
Flight Instruments
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
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4
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
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EICAS
ENGINE INDICATION & CREW ALERTING SYSTEM
InstrumentsEICAS
Flight
1
1
8
XPDR/AudioAFCSGPS Nav
2
2
Nav/Com/
9
10
11
12
13
14
15
10
3
4
PlanningProcedures
Flight
5
6
8
Avoidance
Hazard
9
Additional
11
Features
3
4
5
6
7
12
13
Operation
Abnormal
14
EICAS Display (Normal Mode)
1
Torque
2
Interturbine
Temperature
3
Propeller Speed
4
Generator Speed
5
Oil Pressure
190-00764-03 Rev. C
15
EIS Display (Reversionary Mode)
6
Oil Temperature
7
CAS Display
8
Cabin Pressure Altitude
and Change Rate
9
Differential Pressure
11
Fuel Flow
12
Fuel Temperature
13
Generator and
Alternator Current
14
Emergency Bus
Voltages
10
Fuel Quantity
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
15
Vacuum
Annun/
AlertsAppendixIndex
5
EICAS
CREW ALERTING SYSTEM (CAS)
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
CAS Display
NOTE: Refer to the Annunciations and Alerts section for specific CAS
messages.
NOTE: Refer to the Pilot’s Operating Handbook (POH) for emergency
procedures.
CAS
Window
Normal Mode
Reversionary Mode
CAS Message Displays
Hazard
Avoidance
Message Prioritization
Features
Additional
NOTE: Red warning messages cannot be scrolled through and remain at the
top of the CAS display. The scroll bar changes to yellow if more than ten
caution messages exist to be scrolled through.
• Caution (yellow) – Immediate crew awareness and possible future corrective
AlertsAppendixIndex
Annun/
action required; Master Caution triggered
• Advisory (white) – Advisory information; no immediate action required
When a new red CAS warning message appears, it flashes (inversely red on white)
in conjunction with the Master Warning Indicator. Pressing the Master Warning
Indicator acknowledges all flashing red messages, extinguishing the master warning
lights, and stops warning message flashing.
6
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
EICAS
When a new yellow caution message appears on the CAS display, it appears as black
InstrumentsEICAS
Flight
text on a yellow background. Pressing the Master Caution Indicator acknowledges
all unacknowledged yellow messages, extinguishing the master caution light. The
caution message is displayed as yellow text on black after it is acknowledged.
Messages are displayed until the issue is corrected.
Once acknowledged, CAS warning messages are shown in red text and are displayed
until the issue is corrected.
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
190-00764-03 Rev. C
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
Additional
Features
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Annun/
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7
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
EICAS
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8
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER A TRANSPONDER CODE
1)
Select the XPDR Softkey to display the transponder mode selection
softkeys.
2)
Select the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Use the digit keys 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.
SELECTING A COM RADIO
Nav/Com/XPDR/Audio Panel
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
Transmit/Receive
Press the COM1 MIC, COM2 MIC
installed) on the audio panel.
Receive Only
Press the COM1, COM2
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.
, or
COM3 MIC Key (optional COM, if
, or
COM3 Key (optional COM, if installed) on the
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
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Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
9
Nav/Com/XPDR/Audio Panel
NAV/COM TUNING
Flight
InstrumentsEICAS
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)
Nav/Com/
XPDR/AudioAFCSGPS 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
not recorded for COM3 MIC.
Flight
• PressingthePLAY Key once plays the latest recorded memory block, then returns
PlanningProcedures
to normal operation.
• PressingtheMKR/MUTE Key while playing a memory block stops play.
• Pressingthe PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next
previously recorded block.
Hazard
Avoidance
COM MIC
Key is recorded. Audio is
Features
Additional
Abnormal
Operation
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Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
Nav/Com/XPDR/Audio Panel
INTERCOM SYSTEM (ICS) ISOLATION
Press the PILOT and/or COPLT Key on either audio panel to select those isolated
from hearing the Nav/Com radios and music.
PILOT KEY
Annunciator
OFFOFF
COPLT KEY
Annunciator
Pilot Hears
Selected
Radios, Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Copilot
Hears
Selected
Radios,
Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Passenger
Hears
Selected
Radios,
Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Selected
Radios,
ONOFF
Selected
Radios, Aural
Alerts, Pilot
Aural
Alerts,
Copilot,
Copilot,
Passengers,
Music
Passengers,
Music
Selected
Radios,
Aural
Alerts, Pilot,
Passengers,
Music
Passengers,
Music
OFFON
ONON
Selected
Radios, Aural
Alerts, Pilot,
Passengers,
Music
Selected
Radios, Aural
Alerts, Pilot,
Copilot
Selected
radios,
Aural
Alerts,
Copilot
Selected
Radios,
Aural
Alerts, Pilot,
Copilot
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
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Avoidance
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Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
11
Nav/Com/XPDR/Audio Panel
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
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Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
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AFCS
AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
FLIGHT DIRECTOR ACTIVATION
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
Control Pressed
Modes Selected
LateralVertical
FD KeyRoll Hold (default)ROLPitch Hold (default)PIT
AP KeyRoll Hold (default)ROLPitch Hold (default)PIT
CWS ButtonRoll Hold (default)ROLPitch Hold (default)PIT
GA SwitchGo AroundGAGo AroundGA
ALT KeyRoll Hold (default)ROLAltitude HoldALT
VS KeyRoll Hold (default)ROLVertical SpeedVS
VNV KeyRoll Hold (default)ROLVertical Path Tracking*VPTH
GPS
NAV KeyNavigation**
VOR
Pitch Hold (default)PIT
LOC
BC KeyBackcourse***BCPitch Hold (default)PIT
APR KeyApproach**
GPS
VOR
LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT
GP
GS
HDG KeyHeading SelectHDGPitch Hold (default)PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV
or
APR
Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
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PlanningProcedures
Flight
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AFCS
VERTICAL MODES
Flight
InstrumentsEICAS
Vertical ModeDescriptionControlAnnunciation
Holds the current aircraft pitch attitude;
Pitch Hold
Nav/Com/
XPDR/AudioAFCSGPS Nav
Selected Altitude
Armed
Altitude HoldHolds the current Altitude ReferenceA LT KeyALTnnnnn fT
Vertical Speed
Flight Level Change,
Flight
IAS Hold
PlanningProcedures
Flight Level Change,
Mach Hold
VNAV
Hazard
Avoidance
VNAV Target
Altitude Armed
Features
Additional
Glidepath
Glideslope
Abnormal
Operation
Go Around
AlertsAppendixIndex
Annun/
* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude
is to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
may be used to climb/descend to the
(default)PIT
Selected Altitude
AFCS armed to capture the altitude
displayed in the Selected Altitude
*ALTS
window
Maintains the current aircraft vertical
speed; may be used to climb/descend
VS KeyVSnnnn fpm
to the Selected Altitude
Maintains the current aircraft airspeed
(in IAS or Mach) while the aircraft is
climbing/descending to the Selected
FLC Key
Altitude
Captures and tracks the VNAV flight
path
VNV
Key
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
**ALTV
window
Captures and tracks the SBAS glidepath
on approach
APR Key
Captures and tracks the ILS glideslope
on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level
GA
Switch
FLCnnn kT
FLCM .nnn
VPTH
GP
GS
GA
14
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
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