This manual reflects the operation of System Software version 0424.20 or later for the Mooney M20M, M20R, and M20TN. Some
differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
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® is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000® is a trademark 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® and SkyWatch® are registered trademarks of L-3
Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.
July 2006 190-00450-02 Rev. D Printed in the U.S.A
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
WARNINGS,
CAUTIONS, & NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function.
.
The G1000 Terrain Proximity 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
Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications
requiring a certified terrain awareness system. 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 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: The Jeppesen database used in the G1000 system must be updated regularly in order to ensure
that its information remains current. Updates are released every 28 days. A database information packet is
included in the G1000 package. Pilots using an outdated database do so entirely at their own risk.
WARNING: The basemap (land and water data) must not be used for navigation, but rather only for nonnavigational situational awareness. Any basemap indication should be compared with other navigation
sources.
WARNING: Traffic information shown on the G1000 Multi Function Display 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: Use of the Stormscope® interface is not intended for hazardous weather penetration (thunderstorm
penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance,
not penetration.
WARNING: The GDL 69 Weather Interface should not be used for hazardous weather penetration. Weather
information provided by the GDL 69 is approved only for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
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 Mooney M20M, M20R, and M20TN 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 G1000 Flight Manual Supplement. 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 Airman’s Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense
radar echo.”
CAUTION: The GDU 1040 & 1042 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 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.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
WARNINGS,
CAUTIONS, & NOTES
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: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
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 cleared.
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. 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 Mooney M20M, M20R, & M20TN
RECORD OF REVISIONS
Part NumberChange Summary
190-00450-01Reformat of manual
Added WX 500 Stormscope
Added XM Weather
Added ADF/DME
Added extended range fuel tanks
Changes in EIS softkey labels
190-00450-02Added TAWS-B
Added Automatic Flight Control System
Changed System Software Revision
RevisionDate of RevisionAffected PagesDescription
A12/05i-Index-2Initial release
B4/062-4
11-2
12-1
C6/063-1 – 3-2
5-1
6-1
D7/06RR-1
2-4
12-7
Added Altitude Alert and Barometric Minimums info.
Added Hazard Displays with Loss of GPS info.
Added inactive alerts info.
Direct-to Navigation from the MFD .............................. 7-1
Enter a Direct-to Destination
Select a Direct-to Destination to a Flight Plan
Waypoint or Nearest Airport
To Re-center the CDI to the Destination Waypoint
To Manually Define the Direct-to Course
Canceling Direct-to Navigation
Direct-to Navigation from the PFD ............................... 7-2
Cancelling Direct-to Navigation
7.3 Airport Information ............................................... 7-3
Select the Airport Information Page ............................. 7-3
Enter a Waypoint Facility Name or City Location
Access Runway Information
Access Frequency Information
7.4 Intersection Information ...................................... 7-4
Select the Intersection Information Page ...................... 7-4
Access Information on an Intersection
7.5 NDB Information ..................................................... 7-4
Select the NDB Information Page .................................7-4
View Information on a Specific NDB
7.6 VOR Information ..................................................... 7-5
Select the VOR Information Page .................................7-5
Access Information on a VOR
7.7 User Waypoint Information Page ....................... 7-5
Index ..................................................................................... Index-1
iv
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
SECTION 1
SYSTEM OVERVIEW
SECTION 1: SYSTEM OVERVIEW
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
complete system are found in the G1000 Mooney M20M,
M20R, and M20TN Pilot’s Guide (190-00647-00).
This guide gives the pilot abbreviated operating
instructions for the Primary Flight Display (PFD), Multi
Function Display (MFD), and the GMA 1347 Audio Panel
System.
NOTE: The pilot should read and thoroughly
understand the Mooney M20M/M20R/M20TN
Airplane Flight Manual Supplement (AFMS)
for limitations, procedures, and operational
information not contained in this Cockpit
Reference Guide. The Mooney M20M/M20R/
M20TN Airplane Flight Manual Supplement
always takes precedence over the information
found in this guide.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
1-1
1-1
SECTION 1
SYSTEM OVERVIEW
1.1 PFD/MFD CONTROLS
3
4216
5
7
8
9
1-2
18
19
20
21
22
23
17
Figure 1-1 PFD/MFD Controls
10
24
25
26
27
11
12
13
MFD Only
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
14
15
16
SECTION 1
SYSTEM OVERVIEW
Functionality of the PFD and MFD controls are the
same with the exception of the dedicated autopilot keys
located only on the MFD bezel.
(1) NAV VOL/ID Knob – Controls the NAV audio level.
Press to toggle the Morse code identifier ON and OFF.
Volume level is shown in the field as a percentage.
(2) NAV Frequency Toggle Key – Toggles the standby
and active NAV frequencies.
(3) Dual NAV Knob – Tunes the MHz (large knob)
and kHz (small knob) standby frequencies for the NAV
receiver. Press to toggle the tuning cursor (light blue box)
between the NAV1 and NAV2 fields.
(4) Heading Knob – Turn to manually select a heading
on the HSI. When pressed, it synchronizes the Heading
Bug with the compass lubber line. Selected Heading
provides the heading reference to the Flight Director while
operating in Heading Select Mode.
(5)Joystick – Changes the map range when rotated.
Activates the map pointer when pressed.
(6)CRS/BARO Knob – The large knob sets the altimeter
barometric pressure and the small
knob adjusts the
course. The course is only adjustable when the HSI is in
VOR1, VOR2, or OBS/SUSP Mode. Pressing this knob
centers the CDI on the currently selected VOR.
Selected
Course provides course reference to the Flight Director
when operating in Navigation and Approach modes.
(7)Dual COM Knob – Tunes the MHz (large knob)
and kHz (small knob) standby frequencies for the COM
transceiver. Pressing this knob toggles the tuning cursor
(light blue box) between the COM1 and COM2 fields.
(8)COM Frequency Toggle Key – Toggles the standby
and active COM frequencies. Pressing and holding this
key for two seconds automatically tunes the emergency
frequency (121.5 MHz) in the active frequency field.
(9) COM VOL/SQ Knob – Controls COM audio level.
Pressing this knob turns the COM automatic squelch ON
and OFF. Audio volume level is shown in the field as a
percentage.
(10) Direct-to Key – Allows the user to enter a destination
waypoint and establish a direct course to the selected
destination (specified by the identifier, chosen from the
active route, or taken from the map cursor position).
(11)FPL Key – Displays the active Flight Plan Page for
creating and editing the active flight plan, or for accessing
stored flight plans.
(12) CLR Key (DFLT MAP) – Erases information,
cancels an entry, or removes page menus. To display the
Navigation Map Page immediately, press and hold CLR
(MFD only).
(13)Dual FMS Knob – Used to select the page to be
viewed (only on the MFD). The large knob selects a page
group (MAP, WPT, AUX, NRST), while the small
knob
selects a specific page within the page group. Pressing the
small knob turns the selection cursor ON and OFF. When
the cursor is ON, data may be entered in the different
windows using the small and large knobs. The large
knob is used to move the cursor on the page, while the
small knob is used to select individual characters for the
highlighted cursor location. When the G1000 displays
a list that is too long for the display screen, a scroll bar
appears along the right side of the display, indicating the
availability of additional items within the selected category.
Press the Small FMS Knob to activate the cursor and turn
the Large FMS Knob to scroll through the list.
(14) MENU Key – Displays a context-sensitive list of
options. This list allows the user to access additional
features, or to make setting changes that relate to certain
pages.
(15) PROC Key – Selects approaches, departures and
arrivals from the flight plan. If a flight plan is used,
available procedures for the departure and/or arrival
airport are automatically suggested. If a flight plan is not
used, the desired airport and the desired procedure may be
selected. This key selects IFR departure procedures (DPs),
arrival procedures (STARs), and approaches (IAPs) from
the database and loads them into the active flight plan.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
1-3
SECTION 1
OBS
TMR/REF
NRST
INSET
IDENT
XPDR
CDI
PFD
ALERTS
ADF/DME
(optional)
SYSTEM OVERVIEW
(16) ENT Key – Accepts a menu selection or data entry.
This key is used to approve an operation or complete data
entry. It is also used to confirm selections and information
entries.
(17) Dual ALT Knob – Sets the reference altitude in the
box located above the Altimeter. The large knob selects
the thousands, while the small knob selects the hundreds.
Altitude Select is used by the Automatic Flight Control
System in certain modes, in addition to the standard
G1000 Altitude Alerter function.
(18) AP Key – Engages/disengages the Autopilot and
Flight Director in the default vertical and lateral modes.
(19) FD Key – Activates/deactivates the Flight Director
only. Pressing the
FD Key turns on the Flight Director in
the default pitch axis and roll axis modes. Pressing the
FD Key again deactivates the Flight Director and removes
the command bars, unless the Autopilot is engaged. If the
Autopilot is engaged, the FD Key is disabled.
(20) NAV Key
– Selects/deselects the Navigation Mode.
(21) ALT Key – Selects/deselects the Altitude Hold
Mode.
(22) VS Key – Selects/deselects the Vertical Speed Mode.
(23) FLC Key – Selects/deselects the Flight Level Change
Mode.
(24) HDG Key – Selects/deselects the Heading Select
Mode.
(25) APR Key – Selects/deselects the Approach Mode.
(26, 27) NOSE UP/NOSE DN Keys – Controls the
active pitch reference for the Pitch Hold, Vertical Speed,
and Flight Level Change modes.
1.2 PFD SOFTKEYS
Softkey ON
Figure 1-2 PFD Top Level Softkeys
INSET – Press to display the Inset Map in the lower
left corner of the PFD.
OFF
– Press to remove the Inset Map.
DCLTR
(3) – Press momentarily to select the
desired amount of map detail. The declutter
level appears adjacent to the DCLTR Softkey.
• No declutter: All map features are visible
• Declutter – 1: Declutters land data
• Declutter – 2: Declutters land and SUA data
• Declutter – 3: Removes everything except the active
flight plan
TRAFFIC
TOPO
– Press to display traffic on the map.
– Press to display topographical data (i.e.,
coastlines, terrain, rivers, lakes, etc.) and
elevation scale on the Inset Map
TERRAIN
– Press to display terrain information
on the Inset Map.
STRMSCP (optional)
– Press to display the
Stormscope lightning data on the Inset Map
(within a 200 nm radius of the aircraft).
NEXRAD (optional)
– Press to display NEXRAD
precipitation data on the Inset Map.
XM LTNG (optional)
– Press to display the XM®
Radio lightning data on the Inset Map.
BACK
– Press to return to the previous level
softkey configuration.
ALERTS
– Press to display the Alerts Window.
Softkey OFF
1-4
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
PFD – Press to display the additional softkeys for
INSET
OFF
TOPO
TRAFFIC
TERRAIN
DCLTR
DCLTR-2
DCLTR-3
DCLTR-1
NEXRAD
Press the BACK or OFF softkey
to return to the top level
softkeys
XM LTNG
STRMSCP
BACK
ALERTS
(optional)(optional)(optional)
PFD
Press the STD BARO or BACK softkeys
to return to the top level softkey
s
Press the DFLTS softkey to change the PFD
metric values to standard
ARC HSI
360 HSI
STD BARO
BACK
ALERTS
BRG2
BRG1
METRIC
DFLTS
DME
(optional)
additional configurations of the PFD.
METRIC
– Press to display the current and
reference altitudes in meters, in addition
to feet. Pressing the METRIC Softkey also
changes the barometric setting to hectopascals.
DFLTS
– Press to reset default settings on the PFD.
DME
(optional) – Press to display the DME
Information Window.
BRG1 (bearing)
– Press to cycle through the
following Nav sources, making the pointer the
indicator for the corresponding source and
displaying the the appropriate information.
SECTION 1
SYSTEM OVERVIEW
NAV1
– Displays NAV1 waypoint frequency or
identifier and DME information in the BRG1
Information Window.
GPS
– Displays GPS waypoint identifier and GPS
distance information in the BRG1 Information
Window.
ADF
– Displays ADF waypoint frequency in
the BRG1 Information Window.
OFF
– Remove s th e BR G1 Informat ion
Window.
360 HSI
ARC HSI
– Press to display the 360° compass rose.
– Press to display the 140° viewable arc.
Figure 1-3 PFD Softkey Flow Chart – 1
Figure 1-4 PFD Softkey Flow Chart – 2
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
1-5
SECTION 1
NRST
OBS
TMR/REF
IDENT
ALERTS
XPDR
STBY
ON
BACK
VFR
ALT
CODE
IDENT
0
1
6
3
2
4
5
7
IDENT
BACK
BKSP
Press the BACK softkey
to return to the top level
softkeys
Press the BACK
softkey
to return to
the top level
softkey
s
ALERTS
ALERTS
ADF/DME
(optional)
CDI
CDI (VOR1)
CDI (VOR2)
GPS
SYSTEM OVERVIEW
BRG2 (bearing)
– Press to cycle through the
following Nav sources, making the pointer the
indicator for the corresponding source and
displaying the the appropriate information.
NAV2
– Displays NAV2 waypoint frequency or
identifier and DME information in the BRG2
Information Window.
GPS
– Displays GPS waypoint identifier and GPS
distance information in the BRG2 Information
Window.
ADF
– Displays ADF waypoint frequency in
the BRG2 Information Window.
OFF
– Remove s th e BRG2 Information
Window.
STD BARO
– Press to set the barometric pressure to
29.92 inches of mercury (1013 hPa by pressing
the METRIC Softkey).
BACK
– Press to return to the previous level
softkeys.
ALERTS
– Press to display the Alerts Window.
OBS – Press to select OBS Mode on the CDI when
navigating by GPS (only available with active leg).
CDI – Press to change navigation mode on the CDI
between GPS, VOR1, and VOR2.
ADF/DME (optional) – Press to display the ADF/DME
Tuning Window.
XPDR – Press to display the transponder mode
selection softkeys.
STBY
– Press to select Standby Mode.
ON
– Press to select Mode A.
ALT
– Press to select Altitude Reporting Mode.
VFR
– Press to automatically squawk 1200 (only
in the U.S.A., refer to ICAO standards for VFR
codes in other countries).
CODE
– Press to display transponder code selection
softkeys 0-7.
0 through 7
IDENT
– Press numbers to enter code.
– Press to provide special aircraft
position identification to Air Traffic Control
(ATC).
1-6
Figure 1-5 PFD Softkey Flow Chart – 3
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
BACK
DEC FUEL
SYSTEM
ENGINE
LEAN
ENGINE
MAP
DCLTR
BACK
SYSTEM
LEAN
ENGINE
ENGINE
LEAN
BACK
SYSTEM
TRAFFIC
TOPO
TERRAIN
DCLTR-2
DCLTR-3
DCLTR-1
Press the BACK softkey on this level to
return to the top softkey level
BACK
Press to return to the
top softkey level
CHKLIST
ASSIST
CYL SLCT
EXIT
EMERGCY
ENGINE
DCLTR
MAP
ENGINE
CHKLIST
CLR
DONE
The DONE softkey changes to UNDO when the checklist
item is already checked
STRMSCP
NEXRAD
XM LTNG
(optional)
(optional)(optional)
RST FUEL
INC FUEL
(optional)
Press the ENGINE or BACK softkey on any level to
return to the default page level
BKSP
– Press to remove numbers entered one
at a time.
BACK
– Press to return to the previous level
softkeys.
IDENT
– Press to provide special aircraft position
identification to Air Traffic Control (ATC).
BACK
– Press to return to the previous level
softkeys.
ALERTS
– Press to display the Alerts Window.
IDENT – Press to provide special aircraft position
identification to Air Traffic Control (ATC).
TMR/REF – Press to display the Timer/References
Window.
NRST – Press to display the Nearest Airports
Window.
ALERTS – Press to display the Alerts Window.
SECTION 1
SYSTEM OVERVIEW
1.3 MFD SOFTKEYS
ENGINE – Pressing this softkey makes available the
LEAN and SYSTEM softkeys which in turn access
the Lean Page and the System Page, respectively.
MAP – Pressing this softkey enables the following
softkeys:
TRAFFIC – Pressing this softkey displays/
removes Traffic on the Navigation Map.
TOPO – Pressing this softkey displays or
removes topographic information on the
Navigation Map.
TERRAIN – Pressing this softkey displays/
removes terrain and obstacle data on the
Navigation Map.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Figure 1-6 MFD Softkeys
1-7
SECTION 1
SYSTEM OVERVIEW
STRMSCP (optional) – Pressing this softkey
displays/removes Stormscope lightning
data on the Navigation Map.
NEXRAD (optional) – Pressing this softkey
displays/removes precipitation data on the
Navigation Map.
XM LTNG (optional) – Pressing this softkey
displays/removes XM Radio lightning data
on the Navigation Map.
BACK – Pressing this softkey displays the
ENGINE and MAP top level softkeys.
DCLTR (declutter) – Pressing this softkey removes
map information in three levels.
CHKLIST (checklist)(optional)– Pressing the
CHKLIST Softkey displays the Checklist Page.
1.4 MFD PAGE GROUPS
1) Turn the
group is selected.
2) Turn the
the group. See Figure 1-7.
Large FMS
Small FMS
Knob until the desired page
Knob to select pages within
1.5 BACKLIGHTING
To manually adjust the backlight for the
PFD and MFD:
1) Press the
PFD Setup Menu Window.
2) Press the Small FMS Knob to activate the cursor.
‘PFD DSPL > AUTO’ is now highlighted.
3) Turn the Small FMS Knob to display the
selection window.
4) Turn the
press the ENT Key.
5) With the intensity value now highlighted, turn
the Small FMS Knob to select the desired
backlighting.
6) Turn the Large FMS Knob to highlight ‘MFD
DSPL > AUTO’ and repeat steps 3 through 5.
MENU Key on the PFD to display the
FMS Knob to select ‘MANUAL’, then
1-8
Auxiliary Page Group
Waypoint Page Group
Map Page Group
Nearest Group
Number of Pages in Current
Group
Figure 1-7 Page Group Icon
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Figure 1-8 PFD Setup Menu Window
Selected Page
SECTION 2: FLIGHT INSTRUMENTS
The following discussions pertain to the Primary Flight
Display, unless otherwise indicated.
SECTION 2
FLIGHT INSTRUMENTS
1
2
3
4
5
6
1
NAV Frequency Window
2
Airspeed Indicator
17
16
15
9
Turn Rate Indicator
10
Barometric Setting Box
14
13
12
11
10
9
8
7
3
True Airspeed Box
4
Heading Box
5
Horizontal Situation Indicator
6
Outside Air Temperature Box
7
System Time Box
8
Transponder Status Bar
Figure 2-1 Default PFD Information
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
11
Vertical Speed Indicator
12
Altimeter
13
Altitude Reference Box
14
COM Frequency Window
15
Navigation Status Bar
16
Slip/Skid Indicator
17
Attitude Indicator
2-1
SECTION 2
FLIGHT INSTRUMENTS
1
10
9
2
3
4
1
Traffic Annunciation
2
Selected Heading Box
3
Inset Map
4
BRG1 Information Window
5
DME Information Window
5
6
BRG2 Information Window
7
Alerts Window
8
Selected Course Box
9
Vertical Deviation/Glideslope Indicator
10
Marker Beacon Annunciation
Figure 2-2 Additional PFD Information
6
8
7
2-2
Distance to Next Waypoint
Next Waypoint
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Desired Track to
Next Waypoint
Figure 2-3 PFD Navigation Status Window
Current Track
SECTION 2
FLIGHT INSTRUMENTS
2.1 AIRSPEED INDICATOR
Airspeed Trend
Vector
Actual Airspeed
True Airspeed
Box
Figure 2-4 Airspeed Indicator
Speed Indication
The indicated airspeed is displayed inside the black
pointer. The pointer will become red upon reaching
Vne.
Vspeed
References
Speed Ranges
Vspeed References
Vspeed References are turned on or off in the
Timer/References Window. Press the
TMR/REF Softkey
to display the widow. When active (ON), the Vspeeds are
displayed at their respective locations to the right of the
airspeed scale. To activate the Vspeed References, display
the Timer/References Window and turn the Large FMS
Knob to place the cursor in the ON/OFF field. Turn the
Small FMS Knob to select ON or OFF.
2.2 ATTITUDE INDICATOR
The Slip/Skid Indicator is located under the roll pointer
and moves laterally away from the pointer to indicate
lateral acceleration. One Slip/Skid indicator displacement
is equal to one ball displacement when compared to a
traditional slip/skid indicator.
10
9
1
2
8
Figure 2-5 Red Pointer at Vne
Speed Ranges
The color coded speed range strip denotes flaps
operating range, normal operating range, and never exceed
speed (Vne). A red range is also present for low speed
awareness. Refer to the Airplane Flight Manual (AFM) for
airspeed limitations and indicator markings.
Airspeed Trend Vector
The end of the trend vector displays approximately
what the airspeed will be in 6 seconds if the current rate
of acceleration/deceleration is maintained.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
3
4
1
Roll Pointer
2
Roll Scale
3
Horizon Line
4
Aircraft Symbol
5
Land Representation
Figure 2-6 Attitude Indicator
6
Aircraft Wing Tips
7
Pitch Scale
8
Slip/Skid Indicator
9
Sky Representation
10
Roll Scale Zero
7
6
5
2-3
SECTION 2
FLIGHT INSTRUMENTS
2.3 ALTIMETER
Selected Altitude
Box
Altitude Trend
Vector
Altitude Select Bug
Figure 2-7 Altimeter
Altitude Select Bug
The Altitude Select Bug is displayed at the selected
altitude or, if the selected altitude is beyond the altitudes
currently displayed, the bug is displayed at the top or
bottom of the display (whichever is closest to the selected
altitude).
To set the Selected Altitude Bug:
ALT
Turn the
Bug. The
the
Large ALT
Knob to set the Altitude Select
Small ALT
Knob sets the hundreds and
Knob sets the thousands. This
altitude also appears in the Selected Altitude
Box above the Altimeter.
Altitude Trend Vector
The end of the trend vector displays approximately
what the altitude will be in 6 seconds if the current rate of
vertical speed is maintained.
Barometric Setting Box
Current Altitude
Barometric Setting
Box
Altitude Alerting
Within 1000 ft
Figure 2-8 Altitude Alerting Visual Annunciations
Within 200 ft
(applicable to S-TEC
AFCS only)
Visual annunciations appear in the Selected Altitude
Box. Whenever the Selected Altitude is changed,
the Altitude Alerter is reset. The Altitude Alerter is
independent of the Automatic Flight Control System.
An aural tone is heard when the aircraft is within 1000
feet of acquiring the selected altitude or when deviating
beyond 200 feet of the acquired selected altitude. In
addition to the preceding tones, for S-TEC AFCS equipped
aircraft only, an aural tone is heard when the aircraft is
within 200 feet of acquiring the selected altitude.
Deviation of ±200 ft
Barometric Minimum Descent Altitude
The desired barometric minimum descent altitude
(MDA, or Decision Height, DH) can be set in the Timer/
References Window.
Visual annunciations alert the pilot when approaching
the MDA:
• When the aircraft altitude descends to within 2500
feet of the MDA setting, the Barometric Minimum
Box appears with the altitude in light blue text. The
bug appears on the tape in light blue once in range.
• When the aircraft passes through 100 feet of the
MDA, the bug and text turn white.
• Once the aircraft descends past the MDA, the
bug and text turn yellow and the aural alert,
“Minimums Minimums”, is generated.
2-4
To set barometric pressure, turn the BARO Knob to
select the desired setting.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Alerting is inhibited while the aircraft is on the ground.
If the aircraft climbs after having reached the MDA, once it
reaches 50 feet above the MDA, alerting is disabled.
SECTION 2
FLIGHT INSTRUMENTS
Within 2500 ft
Barometric Mini-
mum Bug
Barometric
Minimum Box
Altitude Reached
Figure 2-9 Barometric Minimum Descent Altitude
Alerting Visual Annunciations
Within 100 ft
2.4 VERTICAL DEVIATION/GLIDESLOPE
INDICATOR
2.5 MARKER BEACON ANNUNCIATIONS
Marker Beacon
Annunciation
Vertical
Deviation/Glideslope
Indicator
Figure 2-10 Marker Beacon and Vertical Deviation
2.6 VERTICAL SPEED INDICATOR
Selected Vertical Speed
Vertical Speed Bug
Vertical Speed Pointer
The Vertical Deviation/Glideslope Indicator appears
when an ILS is tuned in the active NAV field.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Figure 2-11 Vertical Speed Indicator
The actual vertical speed is displayed inside the
pointer.
When the Flight Director is placed in Vertical Speed
Mode (by pressing the VS Key) the Vertical Speed Bug
is displayed. Press the NOSE UP or NOSE DN Key to
adjust.
2-5
SECTION 2
FLIGHT INSTRUMENTS
2.7 HORIZONTAL SITUATION INDICATOR
(HSI)
14
13
1
2
3
4
5
6
1
Turn Rate Indicator
2
Lateral Deviation Scale
3
Navigation Source
4
Aircraft Symbol
5
Course Deviation Indicator
6
Rotating Compass Rose
7
OBS Mode
8
TO/FROM Indicator
9
Heading Bug
10
Course Pointer
11
Flight Phase
12
Turn Rate and Heading Trend Vector
13
Heading
14
Lubber Line
12
11
10
9
8
7
Arc HSI
The HSI compass can be displayed as a 360° rose or
140° arc (see Figure 2-15) by pressing the PFD Softkey,
followed by the 360 HSI or the ARC HSI Softkey.
NOTE: When the Arc HSI is displayed, the BRG1
and BRG2 information windows and pointers are
disabled.
NOTE: If the pilot makes a heading change
greater than 105˚ with respect to the course, the
CDI switches to the opposite side of the deviation
scale and displays reverse sensing.
Turn Rate Indicator and Heading Trend Vector
Tick marks to the left and right of the lubber line
denote half-standard and standard turn rates. A magenta
turn rate trend vector shows the current turn rate. The
end of the trend vector gives the heading predicted in six
seconds, based on the present turn rate. At rates greater
than 4 deg/sec, an arrowhead appears at the end of the
magenta trend vector and the prediction is no longer
valid.
Half-Standard Turn
Rate Tick Mark
Standard Turn
Rate Tick Mark
Figure 2-13 Turn Rate Indicator and Trend Vector
Turn Rate
Trend Vector
(rate > 4
deg/sec)
Turn Rate
Trend Vector
(standard rate)
2-6
Figure 2-12 Horizontal Situation Indicator
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Figure 2-14 Standard-Rate Turn Indication
SECTION 2
FLIGHT INSTRUMENTS
Course Pointer
The course pointer is a single line arrow (GPS, VOR1,
and LOC1) or double line arrow (VOR2 and LOC2) which
points in the direction of the set course.
Lateral Deviation
Scale
Figure 2-15 Arc CDI and Compass Rose CDI
Course Deviation
TO/FROM Indicator
Course Deviation Indicator (CDI)
The CDI scale automatically adjusts to the current
phase of flight (enroute 5.0 nm, terminal area 1.0 nm,
or approach 0.3 nm). Scaling may be selected manually
from the MFD System Setup Page. See Sytsem Setup in
the G1000 Pilot’s Guide for more detail.
Bearing Pointers and Information Windows
Pressing the PFD Softkey provides access to the BRG1
and BRG2 softkeys. The BRG1 pointer is a single line
pointer. The BRG2 pointer is a double line pointer.
DME
Information
Window
Bearing 1
Information
Figure 2-16 HSI with Bearing Information
Bearing 1
Window
Distance to
Bearing Source
Pointer
Bearing 2
Pointer
Bearing 2
Information
Window
Waypoint
Identifier
Bearing
Source
Figure 2-17 BRG1 Information Window
Figure 2-18 BRG2 Information Window
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Pointer
Icon
Distance to
Bearing Source
Pointer
Icon
Waypoint
Identifier
Bearing
Source
2-7
SECTION 2
FLIGHT INSTRUMENTS
DME (optional)
To display the DME Information Window, press the
PFD Softkey followed by the DME Softkey.
Figure 2-19 DME Information Window
Navigation Source
To change between navigation sources:
1) Press the
CDI
Softkey to change from GPS to
VOR1/LOC1.
2) Press the
CDI
Softkey again to change from
VOR1/LOC1 to VOR2/LOC2.
3) Press the
CDI
Softkey a third time to return to
GPS.
When using GPS as the navigation source, the following
may appear:
• INTEG – GPS information is either not present or
is invalid for navigation use
• WARN – GPS detects a position error
• SUSP – Displayed when in OBS Mode indicating
GPS waypoint sequencing is suspended.
Figure 2-20 GPS INTEG, GPS SUSP, LOC1 and VOR2
To enable/disable OBS Mode while navigating
with GPS:
1) Press the
OBS Softkey to select OBS Mode.
2) Turn the CRS Knob to select the desired course
TO/FROM the waypoint.
3) Press the OBS Softkey again to return to
normal operation.
NOTE: The OBS Softkey is only displayed when
navigating an active leg using GPS.
2-8
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
SECTION 3: ENGINE INDICATION
SYSTEM (EIS)
3.1 ENGINE DISPLAY
The Mooney M20R Default Engine Page is shown in
Figure 3-1. The M20TN display is similar, but shows
Turbine Inlet Temperature (TIT) instead of Exhaust Gas
Temperature (EGT). The M20M display is also similar to
Figure 3-1, but shows TIT and Fuel Pressure (instead of
EGT and Fuel Flow). In all cases green indicates normal
operation, yellow indicates caution, and red indicates
warning.
Pressing the ENGINE Softkey makes available the
LEAN and SYSTEM softkeys which in turn provide access
to the Lean Page and the System Page, respectively.
Manifold
Pressure
Gauge
RPM Gauge
Fuel Quantity
Indicator
3.2 LEAN ENGINE DISPLAY
The Mooney M20R Lean Engine Page is shown in
Figure 3-2. The M20M/M20TN display is similar, but also
shows Turbine Inlet Temperature (TIT).
Fuel Flow
Readout
Exhaust Gas
Temperature
Bar Graph
EGT Readout
For Selected
Cylinder
Cylinder Head
Temperature
Bar Graph
CHT Readout
For Selected
Cylinder
Figure 3-2 M20R LEAN Engine Page
Fuel Flow
Indicator
Oil Pressure
Indicator
Cylinder Head
Temperature
Indicator
Voltmeter
Ammeter
Figure 3-1 M20R Default Engine Page
Oil Temperature
Indicator
In aircraft with the extended range 55 gallon tanks option,
the fuel quantity will still show 45 gallons when full.
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
Cylinder Select
The CYL SLCT Softkey can be utilized to obtain
information about a particular cylinder.
The CYL SLCT Softkey becomes disabled when
a particular cylinder turns yellow or red, until the
temperature decreases and returns to normal or when the
ASSIST Softkey is pressed.
Pressing the
that peaks to become highlighted and information for that
cylinder to be displayed.
Any exceedance of default Engine Page parameters,
while viewing the Lean Engine Page, will cause the display
to automatically switch back to the default Engine Page.
ASSIST Softkey causes the first cylinder
3-1
SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
3.3 ENGINE SYSTEM DISPLAY
The Mooney M20R System Engine display is shown in
Figure 3-3. The M20TN display is similar, but also shows
Turbine Inlet Temperature (TIT). The M20M display is
also similar to Figure 3-3, but shows Fuel Pressure instead
of Exhaust Gas Temperature (EGT), and also shows TIT.
If desired, use the DEC FUEL, INCFUEL softkeys to adjust the amount of fuel remaining for
totalizer calculations.
NOTE: Fuel calculations do not use the aircraft
fuel quantity indicators, and are calculated from
the last time the fuel was reset.
FUEL, and RST
Any exceedance of default Engine Page parameters,
while viewing the System Engine Page, will cause the
display to automatically switch back to the default Engine
Page.
3.4 FLAP & TRIM INDICATIONS
The flap and trim indicators are located on the MFD
next to the engine indicating displays.
Rudder Trim Indicator
Actual trim position is shown using a blue inverted
triangle. The ‘takeoff’ rudder trim position is shown in
white.
Elevator Trim Indicator
Trim position is shown by a blue triangle. A white
block indicates ‘takeoff’ elevator trim position.
Flaps Position Indicator
The Flaps Position Indicator shows the current
position of the flaps. The three possible positions, up,
take-off, and down, are depicted in cyan as ‘UP’, ‘T/O’,
and ‘DN’, respectively. During flaps position transition,
‘///’ is displayed in the window.
3-2
Fuel Remaining
Figure 3-3 M20R SYSTEM Engine Page
Aircraft Total
Time in Service
Flap
Position
Elevator Trim
Takeoff Position
Trim Position
Indicator
Rudder Trim
Takeoff Position
Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
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