This manual reflects the operation of System Software version 0464.00 or later for the Tiger AG-5B. 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® is a registered trademark of L-3 Communications; and XM® is a
registered trademark of XM Satellite Radio, Inc.
July 2005 190-00616-00 Rev. A Printed in the U.S.A.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 3
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 Garmin G1000, as installed in Tiger AG-5B 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 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 non-navigational situational awareness. Any basemap indication should be compared with other navigation sources.
CAUTION: 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.”
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
i
Page 4
WARNINGS,
CAUTIONS, & NOTES
CAUTION: 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.
CAUTION: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation. 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.
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.
CAUTION: The GDU 1040 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.
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: 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.
Avoid the clusters to avoid the thunderstorms. In the cell display mode, even a single discharge point may
represent thunderstorm activity and should therefore be avoided.
ii
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 5
RECORD OF REVISIONS
Part NumberChange Summary
190-00616-00
Initial Release.
(Rev. A)
RevisionDate of RevisionAffected PagesDescription
A7/05i-Index-2Initial release
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
iii
Page 6
RECORD OF REVISIONS
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iv
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 7
TABLE OF CONTENTS
SECTION 1: SYSTEM OVERVIEW .................................... 1-1
INDEX ...................................................................................Index-1
TABLE OF CONTENTS
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
vii
Page 10
TABLE OF CONTENTS
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viii
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 11
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 operat
ing 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 Tiger AG-5B Pilot’s Guide:
This Cockpit Reference Guide gives the pilot abbrevi
ated 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 Tiger AG-5B Pilot’s Operating
Handbook (POH) and Pilot’s Operating Handbook
Supplement (POHS) for limitations, procedures
and operational information not contained in
this Cockpit Reference Guide. The Tiger AG-5B
POH and POHS always takes precedence over the
information found in this guide.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
1-1
1-1
Page 12
SECTION 1
SYSTEM OVERVIEW
1.1 PFD/MFD CONTROLS
3
4216
5
7
8
9
1-2
17
Figure 1-1 PFD/MFD Controls
10
11
12
13
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
14
15
16
Page 13
SECTION 1
SYSTEM OVERVIEW
(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.
(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.
(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.
(14) MENU Key – Displays a context-sensitive list of op-
tions. 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, avail
able 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.
(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.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
1-3
Page 14
OBS
TMR/REF
NRST
INSET
IDENT
XPDR
CDI
PFD
ALERTS
SECTION 1
SYSTEM OVERVIEW
1.2 PFD SOFTKEYS
INSET – Press to display the Inset Map in the lower
left corner of the PFD.
OFF
DCLTR
• No declutter: All map features are visible
• Declutter – 1: Declutters land data
• Declutter – 2: Declutters land and SUA data
• Declutter – 3: Declutters large NAV data remaining
TRAFFIC
TOPO
TERRAIN
STRMSCP (optional)
NEXRAD (optional)
XM LTNG (optional)
BACK
PFD – Press to display the additional softkeys for
additional configurations to the PFD.
METRIC
1-4
Softkey ON
Figure 1-2 PFD Top Level Softkeys
Softkey OFF
– Press to remove the Inset Map
(3) – Press momentarily to select the
desired amount of map detail. The declutter
level appears adjacent to the DCLTR softkey.
(removes everything except the active flight plan)
– Press to display TIS traffic on the map.
– Press to display topographical data (i.e.,
coastlines, terrain, rivers, lakes, etc.) and
elevation scale on the inset map.
– Press to display terrain information
on the inset map.
– Press to display the Stormscope lightning data on the inset map (within
a 200 nm radius of the aircraft).
– Press to display NEXRAD
precititation data on the inset map.
– Press to display the XM
Radio lightning data on the inset map.
– Press to return to the previous level
softkey configuration.
– 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.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
DFLTS
– Press to reset default settings on the PFD.
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.
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.
OFF
– Removes the BRG1 inf o rmation
window.
360 HSI
ARC HSI
BRG2 (bearing)
– Press to display the 360° compass rose.
– Press to display the 140° viewable arc.
– 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.
OFF
– Removes th e BRG2 information
window.
STD BARO
– Press to set the barometric pressure
to 29.92 inches of mercury (1013 hPa by
pressing the
BACK
– Press to return to the previous level
METRIC softkey).
softkeys.
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.
XPDR – Press to display the transponder mode selec-
tion softkeys.
STBY
– Press to select standby mode.
ON
– Press to select mode A.
Page 15
ALT
INSET
OFF
TOPO
TRAFFIC
TERRAIN
DCLTR
DCLTR-2
DCLTR-3
DCLTR-1
NEXRAD
Press the BACK or OFF softkey
to return to the top leve
l
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
– 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).
BKSP
– Press to remove numbers entered one
at a time.
BACK
– Press to return to the previous level
softkeys.
SECTION 1
SYSTEM OVERVIEW
IDENT
– Press to provide special aircraft position
identification to Air Traffic Control (ATC).
BACK
– Press to return to the previous level
softkeys.
Figure 1-3 PFD Softkey Flow Chart – 1
Figure 1-4 PFD Softkey Flow Chart – 2
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
1-5
Page 16
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
softke
y
to return to
the top level
softkeys
ALERTS
ALERTS
CDI
CDI (VOR1)
CDI (VOR2)
GPS
SYSTEM OVERVIEW
1-6
Figure 1-5 PFD Softkey Flow Chart – 3
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.
1.3 MFD SOFTKEYS
ENGINE – Pressing this softkey makes available
the LEAN and SYSTEM and softkeys which in
turn access the Lean Page and the System Page,
respectively.
MAP – pressing this softkey enables the following
softkeys:
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
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.
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.
Page 17
BACK – pressing this softkey displays the
MAP
DCLTR
TRAFFIC
TOPO
TERRAIN
DCLTR-2
DCLTR-3
DCLTR-1
BACK
Press to return to the
top softkey leve
l
CHKLIST
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)
BACK
SYSTEM
ENGINE
LEAN
ENGINE
BACK
SYSTEM
LEAN
ENGINE
ENGINE
LEAN
BACK
SYSTEM
Press the BACK softkey on this level to
return to the top softkey leve
l
ASSIST
CYL SLCT
Press the ENGINE or BACK softkey on any level to
return to the default page leve
l
(optional)
ENGINE and MAP top level softkeys.
DCLTR (declutter) – pressing this softkey removes
map information in three levels.
SECTION 1
SYSTEM OVERVIEW
Figure 1-6 MFD Softkeys
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
1-7
Page 18
SECTION 1
SYSTEM OVERVIEW
1.4 MFD PAGE GROUPS
1. Turn the
large FMS
knob until the desired page
group is selected.
2. Turn the
small FMS
knob to select pages within
the group. See Figure 1-7.
Nearest Group
Auxiliary Page Group
Waypoint Page Group
Map Page Group
1.5 BACKLIGHTING
To manually adjust the backlight for the
PFD and MFD:
1. Press the
PFD Setup Menu window.
MENU key on the PFD to display the
Number of Pages in Current
Figure 1-7 Page Group Icon
Group
Selected Page
1-8
2. Press the small FMS knob to activate the
cursor. ‘PFD DSPL > AUTO’ is now high
lighted.
3. Turn the small FMS knob to display the
selection window.
4. Turn the
FMS knob to select ‘MANUAL’, then
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.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
-
Figure 1-8 PFD Setup Menu Window
Page 19
SECTION 2: FLIGHT INSTRUMENTS
SECTION 2
FLIGHT INSTRUMENTS
1
2
3
4
5
6
1
NAV Frequency Window
2
Airspeed Indicator
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 Tiger AG-5B
11
Vertical Speed Indicator
12
Altimeter
13
Altitude Reference Box
14
COM Frequency Window
15
Navigation Status Bar
16
Slip/Skid Indicator
2-1
Page 20
SECTION 2
FLIGHT INSTRUMENTS
1
10
9
8
2
3
4
1
Traffic Annunciation
2
Selected Heading Box
3
Inset Map
4
BRG1 Information Window
5
BRG2 Information Window
6
Alerts Window
Figure 2-2 Additional PFD Information
7
Selected Course Box
8
Annunciation Window
9
Vertical Deviation/Glideslope Indicator
10
Marker Beacon Annunciation
5
7
6
2-2
Distance to Next Waypoint
Next Waypoint
Desired Track to
Next Waypoint
Figure 2-3 PFD Navigation Status Window (default)
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Current Track
Page 21
SECTION 2
FLIGHT INSTRUMENTS
2.1 AIRSPEED INDICATOR
Airspeed Trend
Vector
Actual Airspeed
Vspeed
References
Speed Ranges
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.
Figure 2-5 Red Pointer at Vne
Vspeed References
Vspeeds are set using the TMR/REF softkey. Glide, Vr,
Vx and Vy are shown on the References window. When
active (ON), the Vspeeds are displayed at their respective
locations to the right of the airspeed scale.
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 tra
ditional slip/skid indicator.
10
1
2
3
4
-
9
8
7
6
5
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 Pilot’s Operating Handbook (POH)
and Pilot’s Operating Handbook Supplement (POHS) 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 Tiger AG-5B
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 Index
2-3
Page 22
SECTION 2
FLIGHT INSTRUMENTS
2.3 ALTIMETER
Altitude Reference
Box
Altitude Trend
Vector
Altitude Reference Bug
Figure 2-7 Altimeter
Altitude Reference Bug
The Altitude Reference Bug can be set to any desired
altitude. The bug acts as a visual reference to indicate the
desired altitude is approaching.
To set the altitude reference bug:
ALT
1. Turn the
bug. The
the
large ALT
altitude also appears in the altitude reference
box above the altimeter.
knobs to set the altitude reference
small ALT
knob sets the hundreds and
knob sets the thousands. This
Current Altitude
Barometric Setting
Box
Barometric Setting Box
To set barometric pressure, turn the BARO knob to
select the desired setting.
2.4 VERTICAL DEVIATION/GLIDESLOPE
INDICATOR
The Vertical Deviation/Glideslope Indicator appears
when an ILS is tuned in the active NAV field.
2.5 MARKER BEACON ANNUNCIATIONS
Marker Beacon
Annunciation
Vertical
Deviation/Glideslope
Indicator
Figure 2-8 Marker Beacon and Vertical Deviation
2-4
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.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 23
SECTION 2
FLIGHT INSTRUMENTS
2.6 VERTICAL SPEED INDICATOR
Vertical Speed Pointer
Figure 2-9 Vertical Speed Indicator
The actual vertical speed is displayed inside the pointer.
2.7 HORIZONTAL SITUATION INDICATOR
(HSI)
The HSI compass can be displayed as a 360° rose or
140° arc by pressing the PFD softkey, followed by the 360 HSI or the ARC HSI softkey.
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
Figure 2-10 Horizontal Situation Indicator
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
2-5
Page 24
SECTION 2
FLIGHT INSTRUMENTS
Turn Rate Indicator and Heading Trend Vector
Each tick mark is at 9 (half standard rate tick mark)
and 18 (standard rate tick mark) degrees to the left and
right of the lubber line. A wide magenta line displays the
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.
current turn rate, up to 24 degrees. A magenta arrowhead appears at 25 degrees. This trend vector provides
the pilot with a prediction of what the heading will be in
6 seconds at the present turn rate.
Figure 2-14 Turn Rate Indicator and Heading Trend Vector
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.
Bearing 1
Pointer
Bearing 1
Information
Window
Figure 2-14 HSI with Bearing Information
Distance to
Bearing Source
Bearing 2
Pointer
Bearing 2
Information
Window
2-6
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 the MFD Section
for more detail.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Waypoint
Identifier
Bearing
Source
Figure 2-15 BRG1 Information Window
Figure 2-16 BRG2 Information Window
Pointer
Icon
Distance to
Bearing Source
Pointer
Icon
Waypoint
Identifier
Bearing
Source
Page 25
SECTION 2
FLIGHT INSTRUMENTS
Navigation Source
To change between navigation sources:
1. Press the
VOR1/LOC1.
2. Press the
VOR1/LOC1 to VOR2/LOC2.
3. Press the
GPS.
When using GPS as the navigation source, the follow-
ing may appear:
• INTEG – RAIM is not available
• WARN – GPS detects a position error
• SUSP – Displayed when in OBS Mode indicating
GPS navigation is suspended.
CDI softkey to change from GPS to
CDI softkey again to change from
CDI
softkey a third time to return to
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.
Figure 2-17 GPS INTEG, GPS SUSP, LOC1 and VOR2
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
2-7
Page 26
SECTION 2
FLIGHT INSTRUMENTS
.
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2-8
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 27
SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
SECTION 3: ENGINE INDICATION
SYSTEM (EIS)
3.1 ENGINE DISPLAY
In all cases green indicates normal operation, yellow
indicates caution, and red indicates warning.
Pressing the
LEAN and SYSTEM softkeys which in turn provide access the Lean Page and the System Page, respectively.
Fuel Pressure
Indicator
Oil Temperature
Indicator
ENGINE softkey makes available the
RPM Gauge
Cylinder Head
Temperature
Indicator
Oil Pressure
Indicator
3.2 LEAN ENGINE DISPLAY
Cylinder Select
The CYL SLCT softkey can be utilized to obtain infor-
mation 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.
Hollow Bar
Representing Peak
EGT Readout
For Selected
Cylinder
Exhaust Gas
Temperature
Bar Graph
Temperature
Deviation
From Peak
Ammeter
Fuel Quantity
Indicator
Figure 3-1 Default Engine Page
Voltmeter
CHT Readout
For Selected
Cylinder
Figure 3-3 LEAN Engine Page
Pressing the ASSIST softkey causes the first cylinder
EGT that peaks to become highlighted and information
for that cylinder to be displayed.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Cylinder Head
Temperature
Bar Graph
3-1
Page 28
SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
3.3 ENGINE SYSTEM DISPLAY
System
Information
3-2
Aircraft Total
Time in Service
Figure 3-5 SYSTEM Engine Page
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 29
SECTION 4: NAV/COM AND
TRANSPONDER
The Nav/Com controls and frequency windows are located on the Primary Flight Display and the Multi-Function Display in the same locations.
SECTION 4 – NAV/COM &
TRANSPONDER
NAV
Controls
NAV Frequency WindowCOM Frequency Window
COM
Controls
Figure 4-1 G1000 VHF NAV/COM Interface (
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
PFD)
4-1
Page 30
SECTION 4 – NAV/COM &
TRANSPONDER
Standby NAV
Frequency Field
Tuning Box
Selected NAV
Frequency
Active NAV
Frequency Field
Frequency Toggle Arrow
Figure 4-3 Frequency Toggle Arrow and Tuning Box
NAV ControlsCOM Controls
Navigation Status Window
Figure 4-2 Frequency Fields
VOL/PUSH
ID Knob
VOL/PUSH
SQ Knob
Selected COM
Frequency
Tuning Box
Active COM
Frequency Field
Standby COM
Frequency Field
Tuning Box
4-2
Frequency Toggle Key
Dual NAV
Knob
• Turn to tune in desired
frequencies.
• Press to change tuning box
positions.
Figure 4-4 NAV/COM Controls
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Dual COM
Knob
Page 31
SECTION 4 – NAV/COM &
TRANSPONDER
4.1 RADIO STATUS INDICATIONS
• TX – When a COM radio is keyed, a white TX
indication appears to the right of the corresponding
COM frequency.
• ID – When the Morse code identifier is ON for a
NAV radio, a
of the corresponding active NAV frequency. The
Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel.
white ID indication appears to the left
Figure 4-5 Radio Status Indications
4.2 VOLUME
‘VOLUME’ is displayed in place of the associated radio
name (i.e., ‘COM1’ or ‘NAV2’) for two seconds after the
volume level is last changed.
4.5 FREQUENCY AUTO-TUNING
Auto-tuning on the PFD
Figure 4-7 Nearest Airports Window (PFD)
1. Press the
Airports Window.
2. Turn the
frequency.
3. Press the
standby field of the active COM.
4. Press the
frequency in the active field.
NRST
softkey to display the Nearest
FMS
knobs to highlight the desired
ENT
key to place the frequency in the
Frequency Toggle
key to place the
Figure 4-6 COM Volume Level
4.3 AUTOMATIC SQUELCH
Automatic squelch can be disabled for a COM radio by
pressing the COM knob to select the desired COM subwindow, then by pressing the VOL/PUSH SQ knob.
4.4 QUICKLY ACTIVATING 121.500 MHZ
Pressing and holding the COM Frequency Toggle key
for approximatelytwo (2) seconds automatically tunes the
selected COM radio to the emergency frequency.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
NAV frequencies are entered automatically in the NAV
window upon approach loading or approach activation.
Auto-tuning on the MFD
Auto-tuning on the MFD is done in much the same
way as on the PFD. Use the FMS knobs to select the desired frequency on any of the information pages. Pressing
the ENT key then loads the selected frequency into the
standby frequency window of the appropriate radio.
4-3
Page 32
SECTION 4 – NAV/COM &
TRANSPONDER
4.6 TRANSPONDER
Mode Selection
The STBY, ON and ALT softkeys can be accessed by
pressing the
Ground Mode (Automatic)
GND is displayed when the aircraft is on the ground.
Reply Status
When the transponder sends replies to interrogations,
an “R” indication appears momentarily in the reply status
field.
XPDR softkey.
Figure 4-8 Ground Mode
Figure 4-9 Reply Indication
Following is a list of important codes:
• 1200 – VFR code in the U.S. (please refer to the
ICAO standards for VFR codes in other countries).
• 7000 – VFR code commonly used in Europe
(please refer to the ICAO standards).
• 7500 – Hijack code.
• 7600 – Loss of communication code.
• 7700 – Emergency code.
• 7777 – Military interceptor operations code
(NEVER ENTER THIS CODE).
• 0000 – Code for military use (in the U.S.).
Flight ID Reporting
If so configured, the Flight ID may be entered in the
Timer/Reference window. If configuration is set to “SAME
AS TAIL” the aircraft tail number will always be displayed.
4-4
Code Selection
1. Press the
XPDR
softkey to display the transpon-
der Mode Selection softkeys.
CODE
2. Press the
softkey to display the transponder Code Selection softkeys, which includes the
digit softkeys.
3. Press the appropriate digit softkeys to enter
the code in the four-digit code field of the
Transponder Status bar. Five seconds after the
fourth digit has been entered, the transponder
code becomes activated.
BKSP
When entering a code, press the
softkey as needed to back up and change code
digits.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Flight ID
Figure 4-10 Timer/References Window
Page 33
SECTION 5: AUDIO PANEL
SECTION 5 – AUDIO PANEL
(COM3 MIC is unavailable)
Transmitters
Split COM
(Not recommended for use in
the Tiger AG-5B)
Passenger Address
Marker Beacon/Mute
Aircraft Navigation Radio
Audio (ADF, DME and, AUX
unavailable on Tiger AG-5B)
Manual Squelch
Transceiver Audio
(COM 3 is unavailable)
Telephone (Unavailable)
Speaker
Marker Beacon Signal Sensitivity
Aircraft Navigation Radio Audio
Recorded COM Audio Playback
ICS Isolation
VOL/SQ
Volume/Squelch
VOL Annunciation
Figure 5-1 Audio Panel Controls
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
SQ Annunciation
Reversionary Mode
5-1
Page 34
SECTION 5 – AUDIO PANEL
5.1 COM RADIO SELECTION
Pressing the COM1 MIC or COM2 MIC key selects
the active transmitter (i.e., microphone). The associated
receiver audio (COM1 or COM2) also becomes selected
when the COM MIC key is pressed.
To prevent deselecting the desired received audio
when pressing another COM MIC key, press the already
selected COM1 or COM2 key before pressing the other
COM MIC key.
Figure 5-2 Transceivers
5.2 MARKER BEACON RECEIVER
The marker beacon receiver is always ON. Figure 5-3
shows the marker beacon annunciators on the PFD
Inner Marker
Annunciator
Middle Marker
Annunciator
Marker Beacon Signal Sensitivity
The HI SENS key can be pressed for increased marker
beacon signal sensitivity.
Figure 5-4 Marker Beacon
5.3 NAV RADIO AUDIO SELECTION
Pressing DME, ADF, NAV1, or NAV2 selects and
deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the
speakers. These four keys can be selected individually or
together.
Outer Marker
Annunciator
5-2
Figure 5-3 Marker Beacon Signal Indicator Lights on the PFD
When the MKR/MUTE key is pressed, the key annunciator is lit and the audio tone can be heard over the
speaker or headsets during marker reception.
When the tone is active, pressing the
MKR/MUTE key
mutes the audio but does not affect the annunciator. The
audio returns when the next marker signal is received.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 35
SECTION 5 – AUDIO PANEL
5.5 INTERCOM SQUELCH CONTROL
Select manual squelch for intercom audio by pressing
the MAN SQ key to light the annunciator.
Figure 5-5 Navigation Radios
5.4 INTERCOM SYSTEM (ICS) ISOLATION
Press the PILOT and/or COPLT key to select who is
isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1.
Figure 5-6 ICS Isolation
Mode
PILOT KEY
ANNUNCIATOR
ALLOFFOFF
PILOT
ONOFF
COPLT KEY
ANNUNCIATOR
Pressing the
smallVOL/SQ knob now toggles between volume and squelch adjustment by lighting VOL
or SQ respectively.
Figure 5-7 Volume/Squelch Control
Pilot HearsCopilot Hears
Selected radios;
pilot; copilot;
passengers;
MUSIC 1
Selected radios;
pilot
Selected radios;
pilot; copilot;
passengers;
MUSIC 1
Copilot;
passengers;
MUSIC 1
Passenger
Selected radios;
pilot; copilot;
passengers;
MUSIC 2
Copilot;
passengers;
MUSIC 2
Hears
COPILOT
OFFON
CREWONON
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Selected radios;
pilot; passengers;
MUSIC 1
Selected radios;
pilot; copilot
Table 5-1 ICS Isolation Modes
Copilot
Selected radios;
pilot; copilot
Selected radios;
pilot; passengers;
MUSIC 2
Passengers;
MUSIC 2
5-3
Page 36
SECTION 5 – AUDIO PANEL
5.6 DIGITAL CLEARANCE RECORDER
WITH PLAYBACK CAPABILITY
Each reception of primary active COM audio is automatically recorded in a memory block. When the next
transmission is received, it is recorded in the next memory
block, and so on. Once the 2.5 minutes of recording time
has been reached, the recorder begins recording over the
stored memory blocks, starting from the oldest block.
Powering off the unit automatically clears all recorded
blocks.
Figure 5-8 Playback
• Pressing PLAY once plays back the latest recorded
memory block, then returns to normal operation.
• Pressing PLAY during playback of a memory block
halts the playback of this block and plays back the
preceding recorded block. The PLAY key can be
used to backtrack through the recorded memory
blocks to reach and play back any desired block.
Pressing the MKR/MUTE key during playback
halts playback and returns the recorder/playback
to normal operation.
5-4
If a COM input signal is detected during playback,
playback is halted and the new COM input signal is re
corded as the latest block.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
-
Page 37
SECTION 6: AUTOMATIC FLIGHT
CONTROL
Refer to the pilot’s guide for the installed autopilot system.
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
6-1
Page 38
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
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6-2
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 39
SECTION 7 – NAVIGATION
SECTION 7: NAVIGATION
7.1 NAVIGATION MAP PAGE
Select the MAP Page Group
1. Turn the
lighted in the page group window in the lower
right of the MFD display.
2. Turn the
page (indicated by a solid rectangular icon).
3. Press the
available information which may be displayed
on the map.
WARNING: The map display should only be
used for situational awareness. Any map display
indication should be compared with approved
navigation sources.
large FMS
small FMS
MAP
softkey to display softkeys for the
knob until
knob to select the first
MAP
is high-
MAP
7.2 DIRECT-TO NAVIGATION
Direct-to Navigation from the MFD
Identifier
Facility Name
Flight Plan Field
City
Map of the
Selected
Waypoint
Bearing
Distance
Direct-to
Course
Figure 7-2 MFD Direct-to Window
To enter a Direct-to destination:
1. Press the
2. Turn the
Direct-to ()
small FMS
knob to enter the first letter
of the destination waypoint identifier. Turn the
large FMS
knob to the right to move the cursor
to the next character position.
Symbol
Nearest Airport
Map Orientation
Map Range
Region
Latitude/
Longitude
Activate Field
key.
Figure 7-1 Navigation Map Page
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
3. Repeat step 2 to spell out the rest of the way
point identifier.
ENT
4. Press the
key to confirm the identifier. The
‘Activate?’ field is highlighted.
ENT
5. Press the
key to activate.
To select a Direct-to destination to a flight
plan waypoint or nearest airport:
1. Press the
2. Turn the
Direct-to ()
large FMS
knob to highlight the Flight
key.
Plan Field or Nearest Airport Field.
3. Turn the
small FMS
knob to display a list way-
points or airports.
-
7-1
Page 40
SECTION 7 – NAVIGATION
4. Continue turning the
small FMS
knob to scroll
through the list and highlight the desired
waypoint or airport.
ENT
5. Press the
Press
ENT
key to confirm the selection.
again to activate a Direct-to.
To re-center the CDI (HSI) needle to the
same destination waypoint:
()
1. Press the Direct-to
pressing the
ENT
key twice. NOTE: If a missed
key, followed by
approach point (MAP) is the current destination, the approach will be canceled.
To manually define the Direct-to course:
1. Press the
2. Turn the
Direct-to ()
FMS
knobs to select the destination
key.
waypoint.
ENT
3. Press the
point, then turn the
key to confirm the selected way-
large FMS
knob to highlight
the Direct-to Course field.
FMS
4. Turn the
and press the
5. Press the
knobs to select the desired course
ENT
key.
ENT
key again to begin navigation
using the selected destination and course.
Canceling Direct-to Navigation:
1. Press the
Direct-to ()
key.
Direct-to Navigation from the PFD
WPT Symbol
Identifier
Facility Name
Flight Plan WPT
Bearing to WPT
Distance from WPT
Course to Selected WPT
Figure 7-4 PFD Direct-to Window
1. Press the Direct-to key
2. Turn the
large FMS
the desired selection field.
3. Turn the
small FMS
desired identifier, location, etc.
ENT
4. Press the
key.
5. The cursor is now flashing on ‘ACTIVATE?’.
Press the
ENT
key again to activate.
Cancelling Direct-to Navigation:
1. Press the Direct-to
2. Press the
MENU
Window. The cursor will be flashing on ‘Cancel
Direct-to NAV’.
ENT
3. Press the
key to cancel the direct-to.
()
.
knob to place the cursor in
knob to begin selecting the
()
key.
key to display the Options
WPT Location
Nearest WPT
Lat/Lon
7-2
MENU
2. Press the
key to display the Direct-to
options menu.
3. With ‘Cancel Direct-To NAV’ highlighted, press
the
ENT
key. If a flight plan is still active, the
G1000 resumes navigating the flight plan
along the closest leg.
Figure 7-3 Canceling Direct-to Navigation
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 41
SECTION 7 – NAVIGATION
7.3 AIRPORT INFORMATION
Figure 7-5 Airport Information Page
Select the Airport Information Page
1. Turn the
group. Turn the
rectangular page icon.
Enter a Waypoint Facility Name or City
Location:
large FMS
small FMS
knob to select the ‘WPT’ page
knob to select the first
7. To remove the flashing cursor, press the
knob.
Access Runway Information
1. Press the
2. Turn the
the Runways field.
3. Turn the
runway for the selected airport.
4. Continue turning the
the desired runway.
5. To remove the flashing cursor, press the
knob.
FMS
knob to activate the cursor.
large FMS
small FMS
knob to place the cursor on
knob to display the next
small FMS
knob to select
Access Frequency Information
1. Press the
2. Turn the
the Frequencies window.
3. Turn either
placing the cursor on the desired frequency.
4. Press the
quency in the standby field of the ‘COM’ or
‘NAV’ window.
FMS
knob to activate the cursor.
large FMS
ENT
knob to move the cursor to
FMS
knob to scroll through the list,
key to place the selected fre-
FMS
FMS
1. Press the
2. Turn the
FMS
knob to activate the cursor.
large FMS
knob to select the facility
name or location (city) field.
3. Turn the
small FMS
knob to select the desired
character.
4. Turn the
large FMS
knob to select the next
character field.
5. Repeat steps 3 and 4 until the facility name or
location is selected, then press
the ENT key. If
there are duplicate names in the database, a
list is displayed from which to chose the desired
location.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
5. To remove the flashing cursor, press the
knob.
• ‘TX’ – transmit only, RX - receive only
• ‘PT’ – part time frequency
• ‘i’ – additional information exists, press the ENT
key
If a listed frequency has sector or altitude restrictions,
the frequency is preceded by an info designation.
FMS
7-3
Page 42
SECTION 7 – NAVIGATION
7.4 INTERSECTION INFORMATION
Select the Intersection Information Page
1. Turn the
group.
2. Turn the
rectangular page icon.
large FMS
small FMS
knob to select the WPT page
knob to select the second
7.5 NDB INFORMATION
Figure 7-7 NDB Information Page
Select the NDB Information Page
1. Turn the
group.
large FMS
knob to select the WPT page
7-4
Figure 7-6 Intersection Information Page
Access Information on an Intersection
1. With the Intersection Information Page displayed, press the
cursor.
2. Turn the
identifier and press the
3. Press the
cursor.
FMS
FMS
FMS
knob to activate the
knobs to enter a name for the
ENT
key.
knob to remove the flashing
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
2. Turn the
rectangular page icon
small FMS
knob to select the third
View Information on a Specific NDB:
1. With the NDB Information Page displayed,
press the
2. Turn the
desired selection field (identifier, name or closest city).
3. Turn the
or city and press the
4. Press the
cursor.
FMS
knob to activate the cursor.
large FMS
FMS
knobs to enter an identifier, name
FMS
knob to highlight the
ENT
key.
knob to remove the flashing
Page 43
SECTION 7 – NAVIGATION
7.6 VOR INFORMATION
Figure 7-8 VOR Information Page
Select the VOR Information Page
1. Turn the
group.
2. Turn the
rectangular page icon.
Access Information on a VOR:
large FMS
small FMS
knob to select the WPT page
knob to select the fourth
7.7 USER WAYPOINT INFORMATION
PAGE
See the Flight Planning section for a discussion on cre-
ating and modifying user defined waypoints.
7.8 NEAREST AIRPORTS
Figure 7-9 Nearest Airports Page
Nearest Airport Information on the MFD
Select the Nearest Airports Page
1. With the VOR Information Page displayed, press
the
FMS
knob to activate the cursor.
2. Turn the
desired selection field (identifier, name or closest city).
3. Turn the
or city and press the
4. Press the
cursor.
large FMS
FMS
knobs to enter an identifier, name
FMS
knob to highlight the
ENT
key.
knob to remove the flashing
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
1. Turn the
page group.
2. Turn the
rectangular page icon.
Access Information on a Specific Airport
1. Press the
of the display. The first airport in the nearest
airports list is highlighted.
2. Turn the
desired airport.
large FMS
small FMS
APT
large FMS
knob to select the NRST
knob to select the first
softkey located at the bottom
knob to highlight the
7-5
Page 44
SECTION 7 – NAVIGATION
Access Runway Information for the
Selected Airport
RNWY
1. Press the
softkey located at the bottom
of the display.
2. Turn the
small FMS
knob to select the desired
runway.
Quickly Tune the COM Transceiver to a
Nearby Airport Frequency
FREQ
1. Press the
softkey located at the bottom
of the display.
FMS
2. Turn either
knob to select the desired
frequency.
ENT
3. Press the
key. The selected frequency is
placed in the standby frequency tuning box.
4. Press the
Frequency Toggle
key to place the
frequency in the active field.
Nearest Airports Information on the PFD
Bearing TO
Airport Symbol
Distance
2. Press the
ENT
key to display airport informa-
tion.
ENT
3. Press the
key again (cursor is on ‘BACK’)
to return to the list.
Load an Airport COM Frequency into the
Active COM
1. Turn the
large FMS
knob to place the cursor
on the desired airport frequency shown in the
window.
ENT
2. Press the
key and the selected frequency
will become the standby frequency for the
active COM.
3. Press the
Frequency Toggle
key to make the
frequency the active frequency.
7.9 NEAREST INTERSECTIONS
7-6
Identifier
Primary COM Frequency
Figure 7-10 Nearest Airports Window
1. Press the
NRST
softkey to display the PFD Near-
Runway Length
est Airports Window.
View Information on a Specific Airport in
the List
1. Turn the
large FMS
knob to place the cursor on
the desired airport identifier.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Figure 7-11 Nearest Intersections Page
Select the Nearest Intersections Page
1. Turn the
page group.
large FMS
knob to select the NRST
Page 45
SECTION 7 – NAVIGATION
2. Turn the
rectangular page icon.
small FMS
knob to select the second
View Information on the Nearest Intersection
1. Press the
2. Turn either
intersection. Press the
FMS
knob to activate the cursor.
FMS
knob to select the desired
ENT
key.
7.10 NEAREST NDB
7.11 NEAREST VOR
Select the Nearest VOR Page
1. Turn the
page group.
2. Turn the
rectangular page icon.
large FMS
small FMS
knob to select the NRST
knob to select the fourth
Figure 7-12 Nearest NDB Page
Select the Nearest NDB Page
1. Turn the
page group.
2. Turn the
rectangular page icon.
large FMS
small FMS
knob to select the NRST
knob to select the third
Access Information on a Specific NDB
1. Press the
2. Turn either
Press the
on the Nearest NDB Page pertains to the
selected NDB.
FMS
knob to activate the cursor.
FMS
knob to select the desired NDB.
ENT
key. The remaining information
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Figure 7-13 Nearest VOR Page
View Information on the Nearest VOR:
1. With the Nearest VOR Page selected, press the
VOR
softkey.
FMS
2. Turn either
the
ENT
key.
OR Press the
Window option and press the
either
FMS
knob to select a VOR. Press
MENU
key. Select the Select VOR
ENT
knob to select a VOR.
key. Turn
7-7
Page 46
SECTION 7 – NAVIGATION
Select and Load a VOR Frequency
1. With the Nearest VOR Page selected, press the
FREQ
softkey to highlight the VOR frequency
for the selected VOR.
ENT
2. Press the
is placed in the NAV standby frequency field.
OR Press the
quency Window option and press the
Press the
field is highlighted to place the selected VOR
frequency in the NAV standby field.
key. The selected VOR frequency
MENU
key. Select the Select Fre-
ENT
ENT
key again when the frequency
7.12 NEAREST USER WAYPOINT
key.
Select a Nearest User Waypoint
1. With the Nearest User Waypoint Page selected,
press the
2. Press the
Waypoint.
3. The remaining information on the Nearest User
Waypoint Page pertains to the selected Nearest
User Waypoint.
FMS
knob to activate the cursor.
ENT
key to select the Nearest User
7.13 NEAREST FREQUENCIES
7-8
Figure 7-14 Nearest User Waypoints Page
Select the Nearest User Waypoint Page
1. Turn the
page group.
2. Turn the
rectangular page icon.
large FMS
small FMS
knob to select the NRST
knob to select the fifth
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Figure 7-15 Nearest Frequencies Page
Select the Nearest Frequencies Page
1. Turn the
page group.
2. Turn the
rectangular page icon.
large FMS
small FMS
knob to select the NRST
knob to select the sixth
Page 47
SECTION 7 – NAVIGATION
Select and Load the Nearest ARTCC, FSS, or
Weather Frequency
1. With the Nearest Frequencies Page selected,
press the
2. Turn the
quency.
3. Press the
the ‘COM’ frequency standby field.
ARTCC, FSS, or Wx
large FMS
ENT
key to load the frequency into
softkey.
knob to select the fre-
7.14 NEAREST AIRSPACES
displayed.
• If the aircraft is within two nautical miles of an
airspace and the current course takes the aircraft
inside, ‘Ahead < 2 nm’ is displayed.
• If the aircraft is within two nautical miles of an
airspace and the current course will not take the
aircraft inside, ‘Within 2 nm’ is displayed.
• If the aircraft has entered an airspace, ‘Inside’ is
displayed.
View Additional Details for a Listed Airspace
1. Select the Nearest Airspace Page.
FMS
2. Press the
3. Turn the
list, highlighting the desired airspace.
4. Press the
knob to select the desired airspace.
5. Press the
cursor.
knob to activate the cursor.
large FMS
ALERTS
FMS
knob to scroll through the
softkey and turn either
knob to remove the flashing
FMS
View and Quickly Load the Frequency for a
Controlling Agency
Figure 7-16 Nearest Airspaces Page
Select the Nearest Airspaces Page
1. Turn the
page group.
2. Turn the
rectangular page icon.
large FMS
small FMS
knob to select the NRST
knob to select the seventh
Airspace Alerts Box
• If the projected course takes the aircraft inside an
airspace within the next ten minutes, ‘Ahead’ is
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
1. Select the Nearest Airspaces Page.
FREQ
2. Press the
knob to select the desired frequency. Press the
ENT
key to load the frequency into the ‘COM’
frequency standby field.
softkey and turn either
FMS
7-9
Page 48
SECTION 7 – NAVIGATION
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7-10
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 49
SECTION 8 – FLIGHT PLANNING
SECTION 8: FLIGHT PLANNING
8.1 USER DEFINED WAYPOINTS
Figure 8-1 User WPT Information Page
Select the User WPT Information Page
1. Turn the
page group.
large FMS
knob to select the NRST
3. Turn the
latitude/longitude field or the Reference Waypoints field, depending on how the waypoint
is to be defined.
4. Turn the
coordinates or the radial and distance from
the reference waypoint.
5. Press the
point.
6. Press the
cursor.
large FMS
FMS
ENT
FMS
knob to highlight the
knobs to enter the position
key to accept the new way-
knob to remove the flashing
Create User Waypoints from the Navigation
Map Page
1. With the Navigation Map Page displayed, push
the
joystick
The target pointer is displayed at the present
aircraft position.
2. After placing the pointer at the desired posi
tion, press the
Information Page is now displayed with the
captured position.
to activate the panning function.
ENT
key. The User Waypoint
-
2. Turn the
rectangular page icon.
small FMS
knob to select the fifth
Create a New User Waypoint
1. With the User Waypoint Information Page
displayed, press the
cursor.
FMS
2. Turn the
waypoint and press the
‘Are you sure you want to create the new user
waypoint’ is displayed. With ‘YES’ highlighted,
press the
knobs to enter a name for the new
ENT
key.
FMS
knob to activate the
ENT
key. The message
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
FMS
3. Turn the
name.
4. Press the
name. The first reference waypoint field is
highlighted.
5. If desired, turn the
identifier of the reference waypoint and the
radial and distance to the reference waypoint.
Press the
6. Press the
cursor.
knobs to select a waypoint
ENT
key to accept the selected
FMS
knobs to enter the
ENT
key to accept.
FMS
knob to remove the flashing
8-1
Page 50
SECTION 8 – FLIGHT PLANNING
Modify a User Waypoint
1. With the User Waypoint Information Page
displayed, press the
cursor.
FMS
knob to activate the
2. Turn the
the desired field and turn the
to make changes.
3. Press the
4. Press the
cursor.
large FMS
ENT
FMS
knob to move the cursor to
small FMS
key to accept the changes.
knob to remove the flashing
knob
Delete a User Waypoint
1. Select the User Waypoint Information Page
MENU
and press
Information Page Options or press the
softkey.
2. Turn the
Waypoint’ and press the
‘Would you like to delete the user waypoint’
is displayed. With ‘YES’ highlighted, press the
ENT
large FMS
key.
to display the User Waypoint
DELETE
knob to select ‘Delete User
ENT
key. The message
8.2 VIEWING THE ACTIVE FLIGHT PLAN
1. Press the
FPL
key.
Figure 8-3 Active Flight Plan Window on the PFD
8.3 ACTIVATE A STORED FLIGHT PLAN
1. Press the
to display the Flight Plan Catalog Page.
2. Press the
3. Turn the
flight plan and press the
FPL
key and turn the
Figure 8-4 Flight Plan Catalog Page
FMS knob
large FMS
to activate the cursor.
knob to highlight the desired
small FMS
ACTIVE
softkey.
knob
8-2
Figure 8-2 Active Flight Plan Page on the MFD
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
ENT
4. With OK highlighted, press the
activate the flight plan. To cancel the flight
plan activation, turn the
highlight ‘CANCEL’ and press the
large FMS
key to
knob to
ENT
key.
8.4 ACTIVATE A FLIGHT PLAN LEG
1. From the Active Flight Plan Page, press the
knob to activate the cursor and turn the
FMS
knob to highlight the desired destination
waypoint.
FMS
large
Page 51
SECTION 8 – FLIGHT PLANNING
2. Press the
ACT LEG
softkey (using MFD only).
OR
MENU
3. Press the
option from the page menu and press the
key, select the ‘Activate Leg’
ENT
key. This step must be used when activating a
leg from the PFD.
4. With ‘Activate’ highlighted, press the
ENT
key.
Figure 8-5 Activate Flight Plan Leg Confirmation
8.5 STOP NAVIGATING A FLIGHT PLAN
1. Press the
to display the Active Flight Plan Page.
2. Press the
window.
FPL
key and turn the
ENT
key to display the Page Menu
small FMS
knob
8.6 INVERT ACTIVE FLIGHT PLAN
1. From the Active Flight Plan Page, press the
MENU
key to display the Page Menu.
2. Turn the
large FMS
Flight Plan’ and press the
nal flight plan remains intact in its flight plan
catalog storage location.
3. With ‘OK’ highlighted, press the
invert the flight plan.
Figure 8-8 Invert Flight Plan
knob to highlight ‘Invert
ENT
key. The origi-
ENT
key to
Figure 8-6 Delete Flight Plan
3. Turn the
Flight Plan’ and press the
highlighted, press the
large FMS
knob to highlight ‘Delete
ENT
key. With ‘OK’
ENT
key to deactivate
the flight plan. This will not delete the stored
flight plan, only the active flight plan.
Figure 8-7 Delete Flight Plan Confirmation
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Figure 8-9 Invert Flight Plan Confirmation
8.7 CREATE A NEW FLIGHT PLAN
To create a new flight plan using the MFD:
FPL
1. Press the
key and turn the
to display the Flight Plan Catalog Page.
NEW
2. Press the
softkey to display a blank flight
plan page for the first empty storage loca
tion.
small FMS
knob
-
8-3
Page 52
SECTION 8 – FLIGHT PLANNING
Figure 8-10 Create FPL on MFD
3. Turn the
point Information Page. Turn the
small FMS
knob to display the Way-
small FMS
knob to enter the first character of the identifier
of the departure waypoint. Turn the
large FMS
knob to move the cursor to the next character
field. Repeat using the
FMS
knobs until the
desired identifier has been entered.
Figure 8-11 Waypoint Info Window
4. Press the
ENT
key.
5. Repeat step number 3 to enter the identifier
for each additional flight plan waypoint.
6. When all waypoints have been entered, press
FMS
the
knob to return to the Flight Plan
Catalog Page. The new flight plan is now in
the list.
1. Press the
FPL
key and press the
to activate the cursor.
2. Turn the
small FMS
character of the flight plan starting identifier.
3. Turn the
large FMS
the next character field.
4. Turn the
small FMS
acter. Continue this process until the desired
identifier is entered.
5. Press the
ENT
key and the cursor is now ready
for entering of the next flight plan waypoint.
6. Repeat steps 2 through 5 to enter the identifier
for each additional flight plan waypoint.
7. Once all waypoints have been entered, press
FMS
the
knob to return to the Active Flight Plan
Window.
Figure 8-12 Creating Flight Plan on the PFD
8.8 LOAD A DEPARTURE
See the Procedures section for a discussion on loading
and activating departure procedures.
small FMS
knob
knob to enter the first
knob to move the cursor to
knob to enter the next char-
8-4
Create a new flight plan using the PFD
NOTE: A flight plan cannot be entered using the
PFD if another flight plan is active.
NOTE: After the first leg is entered (using the
PFD only), it is immediately activated.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
8.9 LOAD AN ARRIVAL
See the Procedures section for a discussion on loading
and activating arrival procedures.
8.10 LOAD AN APPROACH
See the Procedures section for a discussion on loading
and activating approach procedures.
Page 53
8.11 REMOVE A DEPARTURE, ARRIVAL,
OR APPROACH FROM A FLIGHT PLAN
1. With the Active or Stored Flight Plan Page dis-
played, press the small FMS knob to activate
the cursor.
2. Turn the large FMS knob to highlight the title
for the approach, departure or arrival to be
deleted. Titles appear in white directly above
the procedure’s waypoints.
3. Press the
window. With ‘OK’ highlighted, press the ENT
key to remove the selected procedure.
CLR key to display a confirmation
SECTION 8 – FLIGHT PLANNING
FMS
4. Turn the
changes, then press the
5. Press the
Catalog Page.
knobs to make the desired
ENT
key.
FMS knob
to return to the Flight Plan
8.14 DELETE A WAYPOINT FROM THE
FLIGHT PLAN
1. Press the
to display the Flight Plan Catalog Page.
2. Press the
3. Turn the
desired flight plan and press the
FPL
key and turn the
FMS
knob to activate the cursor.
large FMS
knob to highlight the
small FMS
ENT
key.
knob
8.12 STORE A FLIGHT PLAN
1. From the Flight Plan Page, press the
to activate the cursor.
2. Turn the
desired flight plan and press the
display the Flight Plan Page options.
3. Turn the
Flight Plan’ and press the
4. With ‘OK’ highlighted, press the
store the flight plan.
Figure 8-13 Store Flight Plan Confirmation
large FMS
large FMS
knob to highlight the
knob to highlight ‘Store
ENT
FMS knob
MENU
key.
ENT
8.13 EDIT A STORED FLIGHT PLAN
1. Press the
to display the Flight Plan Catalog Page.
2. Press the
3. Turn the
desired flight plan and press the
FPL
key and turn the
FMS knob
large FMS
to activate the cursor.
knob to highlight the
small FMS
ENT
key.
key to
key to
knob
4. Turn the
to be deleted and press the
‘REMOVE WAYPOINT’ confirmation window.
5. With ‘OK’ highlighted, press the
remove the waypoint. To cancel the delete
request, turn the
‘CANCEL’ and press the
6. Once all changes have been made, press the
FMS
Figure 8-14 Remove Waypoint Confirmation
large FMS
knob to return to the Flight Plan Page.
knob to select the waypoint
CLR
key to display a
large FMS
knob to highlight
ENT
key.
8.15 INVERT AND ACTIVATE A STORED
FLIGHT PLAN
1. From the Flight Plan Catalog Page, press the
FMS
knob to activate the cursor.
2. Turn the
desired flight plan and press the
display the Page Menu options.
large FMS
knob to highlight the
ENT
MENU
key to
key to
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
8-5
Page 54
SECTION 8 – FLIGHT PLANNING
3. Turn the
Flight Plan’ and press the
nal flight plan remains intact in its flight plan
catalog storage location.
4. With ‘OK’ highlighted, press the
invert the flight plan.
large FMS
Figure 8-15 Invert Flight Plan
knob to highlight ‘Invert
ENT
key. The origi-
ENT
8.16 COPY A FLIGHT PLAN
1. From the Flight Plan Catalog press the
knob to activate the cursor, turn the
knob to highlight the flight plan to be copied,
MENU
then press the
Plan Catalog Options.
2. Turn the
Flight Plan #’ and press the
3. A ‘Copy to flight plan?’ confirmation window
is displayed. With ‘OK’ highlighted, press the
ENT
the
press the
large FMS
key to copy the flight plan. To cancel, turn
large FMS
knob to highlight ‘CANCEL’ and
ENT
key.
key to display the Flight
knob to highlight ‘Copy
ENT
large FMS
key.
key to
FMS
MENU
2. Press the
Catalog options.
3. Turn the
Flight Plan’ and press the
4. A ‘Delete flight plan?’ confirmation window
is displayed. With ‘OK’ highlighted, press the
ENT
key to delete the flight plan. To cancel,
turn the
and press the
large FMS
key to display the Flight Plan
large FMS
knob to highlight ‘Delete
ENT
key.
knob to highlight ‘CANCEL’
ENT
key.
8.18 GRAPHICAL FLIGHT PLAN CREATION
1. Press the
Plan Page.
2. Press the
Use the
desired point on the map to be inserted as a
waypoint in the flight plan.
3. Press the
point will be inserted at the end of the flight
plan.
4. If the selected waypoint is to be placed else
where in the flight plan, press the
to activate the cursor. Waypoints are inserted
ABOVE
5. After placing the cursor at the desired point
in the list of waypoints, press the
key.
FPL
key to display the Active Flight
Joystick
Joystick
LD WPT
the cursor.
to activate the map pointer.
to move the pointer to the
softkey. The selected way-
LD WPT
8.19 TRIP PLANNING
FMS
-
knob
soft-
8-6
8.17 DELETE A FLIGHT PLAN
1. From the Flight Plan Catalog Page, press the
FMS
knob to activate the cursor, turn the
FMS
knob to highlight the flight plan to be
deleted.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
large
1. Turn the
group.
2. Turn the
rectangular page icon.
large FMS
knob to select the AUX page
small FMS
knob to select the first
Page 55
SECTION 8 – FLIGHT PLANNING
3. The current page mode is displayed at the
top of the page: ‘AUTOMATIC’ or ‘MANUAL’.
To change the page mode, press the
MANUAL
softkey.
Figure 8-16 Trip Planning Page
4. For Direct-to planning, press the
WPTS
AUTO
or
softkey
and verify that the ‘from’ waypoint field indicates P.POS (present position). If necessary,
press the
MENU
key and select ‘Set WPT to
Present Position’ to display P.POS. Press the
ENT
key and the flashing cursor moves to the
‘to’ waypoint field. Turn the
FMS
knobs to enter
the identifier of the ‘to’ waypoint and press the
ENT
key to accept the waypoint. OR,
FMS
5. For point-to-point planning, turn the
knobs
to enter the identifier of the ‘from’ waypoint.
Once the waypoints identifier is entered, press
the
ENT
key to accept the waypoint. The
flashing cursor moves to the ‘to’ waypoint.
FMS
Again, turn the
fier of the ‘to’ waypoint and press the
knobs to enter the identi-
ENT
key
to accept the waypoint.
6. For flight plan leg planning, press the
FPL
softkey (at the bottom of the display) and turn
the
small FMS
knob to select the desired flight
plan (already stored in memory), by number.
Turn the
large FMS
field and turn the
knob to highlight the ‘LEG’
small FMS
knob to select the
desired leg of the flight plan, or select ‘CUM’
to apply trip planning calculations to the entire
flight plan.
7. Turn the
large FMS
knob to highlight the depar-
ture time (DEP TIME) field.
FMS
8. Turn the
Press the
knobs to enter the departure time.
ENT
key when finished. (Departure
time may be entered in local or UTC time,
depending upon unit settings).
FMS
9. Turn the
Press the
knobs to enter the fuel flow.
ENT
key when finished. Note that in
automatic page mode, fuel flow is provided by
the system.
10. The flashing cursor moves to the fuel on board
FMS
field. Turn the
board. Press the
knobs to modify the fuel on
ENT
key when finished. Note
that in automatic mode this is provided by the
system.
11. The flashing cursor moves to the calibrated
FMS
airspeed field. Turn the
calibrated airspeed. Press the
knobs to enter an
ENT
key when
finished.
OR,
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
8-7
Page 56
SECTION 8 – FLIGHT PLANNING
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8-8
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 57
SECTION 9: PROCEDURES
9.1 ARRIVALS AND DEPARTURES
Load and Activate a Departure Procedure
SECTION 9 – PROCEDURES
1. With the Navigation Map Page displayed, press
the
FPL
key.
LD DP
2. Press the
the departure airport will be displayed as the
default. A list of available departures is also
displayed.
3. If no flight plan is active, use the
enter the identifier of the desired airport. Press
the
ENT
4. Turn the
ture field. Turn the
a list of available departures.
5. Turn either
departure and press the
softkey. If a flight plan is active,
key.
large FMS
knob to highlight the Depar-
small FMS
FMS
knob to select the desired
knob to display
ENT
key.
FMS
knobs to
Figure 9-2 Select Departure Transition
8. With ‘LOAD?’ highlighted, press the
The departure will be active when the flight
plan is active.
ENT
Load and Activate An Arrival Procedure
1. With the Navigation Map Page displayed, press
the
FPL
key.
ENT
LD STAR
key.
large FMS
2. Press the
active, the destination airport will be displayed
as the default. A list of available arrivals is also
displayed.
3. If no flight plan is active, use the
enter the identifier of the desired airport. Press
the
4. Turn the
field. Turn the
of available arrivals.
softkey. If a flight plan is
FMS
knobs to
knob to highlight the Arrival
small FMS
knob to display a list
key.
Figure 9-1 Select Departure
6. A list of runways may be displayed for the
FMS
departure. Turn either
desired runway and press the
7. A list of available transitions is displayed for the
departure. Turn either
the desired transition waypoint and press the
ENT
key.
knob to select the
ENT
key.
FMS
knob to highlight
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
5. Turn either
arrival and press the
Figure 9-3 Select Arrival
FMS
knob to select the desired
ENT
key.
9-1
Page 58
SECTION 9 – PROCEDURES
6. A second window is displayed listing available
transitions for the arrival. Turn either
FMS
knob
to highlight the desired transition waypoint and
press the
ENT
key.
Figure 9-4 Select Arrival Transition
7. A third window is displayed listing the available
runways. Turn either
desired runway and press the
FMS
knob to select the
ENT
key.
9.2 APPROACHES
Load and/or Activate an Approach Procedure
1. With the Navigation Map Page displayed, press
the
FPL
key.
LD APR
2. Press the
active, the destination airport will be displayed
as the default. A list of available approaches
is also displayed.
3. If no flight plan is active, use the
enter the identifier of the desired airport. Press
the
ENT
key.
4. Turn the
large FMS
Approach field. Turn the
display a list of available approaches.
softkey. If a flight plan is
FMS
knobs to
knob to highlight the
small FMS
knob to
9-2
Figure 9-5 Select Arrival Runway
8. With ‘LOAD?’ highlighted, press the
If a flight plan is active, the selected arrival
procedure is inserted after the destination
airport and becomes part of the active flight
plan. If no flight plan is active when the arrival
is loaded, the arrival procedure will become the
active flight plan.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
ENT
key.
Figure 9-6 Selecting an Approach Procedure
5. Turn the
approach. Press the
FMS
knobs to highlight the desired
ENT
key.
6. The cursor will move to the TRANSITIONS
field. Turn the
large FMS
desired transition waypoint and press the
knob to highlight the
ENT
key. (The “Vectors” option assumes vectors will
be received to the final course segment of the
approach and will provide navigation guidance
relative to the final approach course.)
Page 59
Figure 9-7 Selecting an Approach Transition
SECTION 9 – PROCEDURES
7. Turn the
and press the
large FMS
ENT
knob to highlight ‘Activate?’
key to activate the approach.
Selecting ‘Load?’ will add the procedure to the
flight plan without immediately using it for
navigation guidance.
Activate An Approach in the Active Flight Plan
1. With the Navigation Map Page displayed, press
the
PROC
key.
2. Turn the
APPROACH’.
3. Press the
now active.
large FMS
ENT
knob to highlight ‘ACTIVATE
key. The approach procedure is
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
9-3
Page 60
SECTION 9 – PROCEDURES
This page intentionally left blank.
9-4
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 61
SECTION 10 – HAZARD
AVOIDANCE
SECTION 10: HAZARD AVOIDANCE
10.1 CUSTOMIZING THE HAZARD
DISPLAYS ON THE NAVIGATION MAP
1. With the Navigation Map Page displayed, press
the
MENU
key to display the Navigation Map
Page Menu. The cursor flashes on the ‘Map
Setup’ option.
ENT
2. Press the
displayed. Turn the
the ‘Weather’ or ‘Traffic’ group to customize
the display of weather features. Select ‘Traffic’
to customize the display of traffic.
3. Press the
Navigation Map Page.
key. The Map Setup Menu is
small FMS
small FMS
knob to return to the
knob to select
10.2 STORMSCOPE® (OPTIONAL)
WARNING: Use of the Stormscope system for
hazardous thunderstorm penetration is prohibited. Weather information on the G1000 MFD
is approved for weather avoidance only. Refer
to the WX-500 Pilot’s Guide for detailed operation.
Displaying Stormscope Lightning Data on the
Navigation Map Page
1. Press the
2. Press the
softkey again to remove Stormscope Lightning
Data from the Navigation Map Page.
MAP
softkey.
STRMSCP
softkey. Press the
STRMSCP
Figure 10-1 Page Menu
Figure 10-2 Map Setup Menu
Figure 10-3 Map Setup Group List
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The
presence of Stormscope lightning data is indicated by the
annunciation ‘LTNG < 25 nm’ in the upper right corner.
Figure 10-5 Lightning Display Range Annunciation
To select ‘cell’ or ‘strike’ as the Stormscope
lightning mode:
1. With the Weather Group selected, press the
ENT
key. The cursor flashes on ‘STRMSCP
LTNG’.
2. Turn the
large FMS
knob to select ‘STRMSCP
MODE’.
FMS
3. Turn either
knob to display the ‘Cell/Strike’
window.
FMS
4. Turn either
Press the
5. Push the
knob to select ‘Cell’ or ‘Strike’.
ENT
key.
FMS
knob to return to the Navigation
Map Page.
To clear Stormscope lightning data from
the Navigation Map Page:
MENU
1. Press the
key (with the Navigation Map
Page displayed).
2. Turn the
small FMS
knob until the Stormscope
Page is selected. This is the third rectangular
page icon.
Figure 10-6 Stormscope Page
To change the Stormscope lightning mode
between ‘cell’ and ‘strike’:
1. Select the Stormscope Page.
MODE
2. Press the
softkey. The
softkeys are displayed. Press the
to display ‘CELL’ data or press the
CELL
and
STRIKE
CELL
softkey
STRIKE
softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’
is displayed in the mode box located in the
upper left corner of the Stormscope Page.
10-2
2. Turn either
Lightning Data’ field and press the
Stormscope Page
1. Turn the
group is selected.
large FMS
FMS
knob to highlight the ‘Clear
ENT
knob until the Map Page
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
key.
NOTE: “Cell mode” uses a clustering program to
identify clusters of electrical activity that indicate
cells.
To change the viewing mode between 360˚
and 120˚:
1. Select the Stormscope Page.
Page 63
SECTION 10 – HAZARD
AVOIDANCE
2. Press the
VIEW
softkey. The
360
and
keys are displayed. Press the 360 softkey to
display a 360˚ viewing are or press the ARC
softkey to display a 120˚ viewing area.
CLEAR
Press the
softkey to remove all Storm-
scope lightning data from the display.
10.3 XM WEATHER (OPTIONAL)
WARNING: Use of XM weather for hazardous weather penetration is not recommended.
Weather information provided by XM Radio
Service is approved only for weather avoidance,
not penetration.
1. Press the
2. Press the
play the desired weather. Press the applicable
softkey again to remove weather data from the
Navigation Map Page.
MAP
softkey.
NEXRAD or XM LTNG
softkey to dis-
ARC
soft-
Displaying METAR and TAF information on the
Airport Information Page
To display METAR and TAF text on the Airport Information Page:
1. Turn the
large FMS
Group.
2. Turn the
small FMS
Information Page.
3. Press the WX softkey to display METAR and TAF
text (METAR and TAF information is updated
every 12 minutes).
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
TAF
Text
WX
Softkey
Figure 10-8 METAR and TAF Text Displayed on the
Airport (Weather) Information Page
10-3
Page 64
SECTION 10 – HAZARD
AVOIDANCE
Displaying Weather on the Weather Data Link
Page
To select the Weather Data Link Page:
1. Turn the
large FMS
Group.
2. Turn the
small FMS
rectangular page icon.
3. Press the available softkeys to select the desired
XM weather product.
4. Press the
LEGEND
for the selected products. If necessary, turn the
FMS
knobs to scroll through the list. Press the
small FMS
knob or the
the map.
knob to select the Map Page
knob to select the fourth
softkey to view the legends
ENT
softkey to return to
NEXRAD Limitations
Certain limitations exist regarding the NEXRAD radar
displays. Some, but not all, are listed here:
• NEXRAD base reflectivity does not provide suf
ficient information to determine cloud layers or
precipitation characteristics (hail vs. rain, etc).
• An individual NEXRAD site cannot depict high altitude storms at close ranges, and has no information
about storms directly over the site.
• The resolution of displayed NEXRAD data is 2 kilometers. Therefore, when zoomed in on the display,
each square block is 2 kilometers. The intensity
level reflected by the square will be the highest level
sampled within the 2 kilometer square area.
ECHO TOP – press the ECHO TOP softkey to show
the location, elevation, and direction the highest radar echo. This may not indicate the top of
a storm or clouds, only the highest radar return
echo. ECHO TOPS cannot be displayed along
with NEXRAD and CLOUD TOPS. When ECHO
TOPS is activated, NEXRAD and CLOUD TOPS
are removed. Refer to the Legend for a description of the ECHO TOPS coding. The display is
updated every 7.5 minutes.
-
10-4
Figure 10-9 Weather Data Link Page
NEXRAD – press the NEXRAD softkey to show
NEXRAD weather and radar coverage information.
Areas where radar coverage is not available will be
shown in grayish-purple. The display is updated
every five minutes.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
CLD TOP – press the CLD TOP softkey to show the
cloud top altitude determined from satellite imagery.
The display is updated every 15 minutes.
LTNG – pressing the LTNG softkey shows the location
of cloud-to-ground lightning strikes. The display is
updated every five minutes.
NOTE: Strikes depicted represent cloud to ground
strikes within a 2 km radius of the actual strike
location. Therefore, the exact location of the
strike is not displayed.
Page 65
SECTION 10 – HAZARD
AVOIDANCE
CELL MOV – pressing the CELL MOV softkey shows
storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The
display is updated every 12 minutes.
SIG/AIR – pressing the SIG/AIR softkey shows
SIGMET and AIRMET information.
updated every 12 minutes.
METAR – press the METAR softkey to graphically dis
play METARs. METARS are shown as colored flags
at airports providing METAR reports. The display
is updated every 12 minutes.
MORE WX – press the MORE WX softkey to display
the following group of softkeys for additional
weather control:
SFC – pressing the SFC softkey for Surface Analysis
shows current or forecast conditions. Forecasts
are available for intervals of Current, 12, 24, 36,
and 48 hours. Press the softkey corresponding
to the desired forecast. The closest city forecast
information is displayed in the legend. The display is updated every 12 minutes.
FRZ LVL – press the FRZ LVL softkey to display
contour lines for freezing levels.
updated every 12 minutes.
WIND – press the WIND softkey to show wind
speed and direction at a selected altitude from
the ground up to 42,000 feet in 3,000 foot incre
ments. After pressing the WIND softkey, press
the softkey corresponding to the desired winds
aloft altitude. The display is updated every 12
minutes.
COUNTY – pressing the COUNTY softkey provides
specific public awareness and protection
warnings for Tornado, Severe Thunderstorm,
and Flood conditions provided by the National
Weather Service (NWS). The display is updated
every 5 minutes.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
The display is
-
The display is
-
weather
CYCLONE – pressing the CYCLONE softkey shows
the current location of cyclones (hurricanes and
tropical storms) and their projected track at vari
ous time intervals.
12 minutes.
The display is updated every
-
Map Panning Information – Weather Data Link
Page
1. Push in the
arrow.
2. Move the
on AIRMETs, TFRs, METARs, or SIGMETs. Press
the ENT key to display pertinent information
for the selected product.
Note that pressing the ENT key when pan
ning over an AIRMET or a SIGMET displays an
information box that displays the text of the
report. Panning over an airport with METAR
information does not display more information
but allows the user to press the ENT key and
select that Airport’s Information Page to display
the text of the report. Pressing the ENT key
when panning over a TFR displays TFR specific
information.
joystick
joystick
to display the panning
to place the panning arrow
-
Weather Products and Symbols
Figure 10-10 depicts the symbol for each weather
product (read from left to right) . When a weather product is active, the product symbol is displayed in the lower
right of the screen.
• NEXRAD
• Cloud Top/Echo Top
• XM Lightning
• Cell Movement
• SIGMETs/AIRMETs
• METARs
• City Forecast
10-5
Page 66
SECTION 10 – HAZARD
AVOIDANCE
• Surface Analysis
• Freezing Levels
• Winds Aloft
• County Warnings
• Cyclone Warnings
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
Figure 10-10 Weather Product Symbols
The XM Information Page in the AUX Page Group will
display the weather products available for the current sub
scription. A green box by the weather product means that
it is available.
NOTE: The DONE softkey on the AUX - XM INFORMATION page is used to save the GDL 69(A) activation data when the XM services are initially set
up. It is not used during normal operation of the
GDL 69(A), and it should have no adverse effects
if inadvertently selected during flight. Refer to
the GDL 69/69A XM Satellite Radio Activation
Instructions (190-00355-04, Rev E or later) for
further information.
Weather Product Age
The age for each of the enabled products is displayed
on the right side of the display. Times are based on Zulu
time when the data was assembled on the ground, not the
time the data was received by the FIS sensor. When the age
of a weather product has exceeded half of the expiration
time, the product time will change from light blue to amber
in color.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 67
SECTION 10 – HAZARD
AVOIDANCE
10.4 TRAFFIC INFORMATION SERVICE (TIS)
NOTE: Traffic Information Service (TIS) is only
available when the aircraft is within the service
volume of a TIS capable terminal radar site.
Displaying Traffic on the Traffic Map Page
1. Turn the
Group.
2. Turn the
rectangular page icon.
3. Press the
traffic. ‘TIS OPERATIING’ is displayed in the
Traffic mode field.
4. Press the
in the Standby mode. ‘TIS STANDBY’ will be
displayed in the Traffic mode field.
5. Rotate the
area or rotate counter-clockwise to display a
smaller area.
If data is not received for a period longer than 6 seconds, the age of the present data will be displayed in the
lower left of of the screen along with the annuciation that
the system has entered Coast mode. The system will
maintain the traffic display (up to 60 seconds) until the
next data reception. If no data is received after 60 seconds, traffic will be removed from the display.
large FMS
small FMS
OPERATE
STANDBY
Joystick
knob to select the Map Page
knob to select the second
softkey to begin displaying
softkey to place the system
clockwise to display a larger
Traffic Mode
Last data update
is older than 6
sec. resulting in
Coast mode
descending, moving in the direction of the line
Traffic Advisory, aircraft is 400’ above &
Proximity Traffic at same
altitude, level flight & moving
in the direction of the line
Figure 10-11 Traffic Map Page
Traffic 1600’ above &
climbing, moving in the
Traffic out of
range
direction of the line
Displaying Traffic on the Navigation Map
1. Ensure TIS is operating. With the Navigation
Map displayed, press the
2. Press the
TRAFFIC
softkey. Traffic will now be
MAP
softkey.
displayed on the map.
TIS Audio Alert
When a Traffic Advisory (TA) is displayed, an audio
alert “Traffic” is given.
“Traffic Not Available” will be heard whenever TIS ser-
vice becomes unavailable.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
10-7
Page 68
SECTION 10 – HAZARD
1000' AGL
Aircraft Altitude
100' Threshold
AVOIDANCE
10.5 TERRAIN AND OBSTACLE PROXIMITY
NOTE: Terrain data is not displayed when the
aircraft latitude is greater than 75 degrees (north
or south).
Displaying Terrain and Obstacles on the Terrain
Proximity Page
1. Turn the
Group.
2. Turn the
rectangular page icon.
3. If desired, press the
ARC
is pressed, a radar-like 120° view is displayed.
Press the
default display.
4. Rotate the
area or rotate counter-clockwise to display a
smaller area.
and
large FMS
small FMS
360
360
knob to select the Map Page
knob to select the last
VIEW
softkey to access the
softkeys. When the
softkey to return to the 360°
Joystick
clockwise to display a larger
ARC
softkey
ColorIndication
RED
YELLOW
WARNING: Terrain/Obstacle at or within
100’ below current aircraft altitude.
CAUTION: Terrain/Obstacle between 100’
and 1000’ below current aircraft altitude.
Displaying Terrain and Obstacles on the
Navigation Map
1. With the Navigation Map displayed, press the
MAP
softkey.
2. Press the
TERRAIN
proximity will now be displayed on the map.
softkey. Terrain and obstacle
Maximum
elevation of
topography presently
displayed on-screen
Minimum
elevation of
topography presently
displayed on-screen
10-8
Figure 10-12 Terrain Proximity Page
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Range of
topography eleva-
tion presently dis
played on-screen
Figure 10-13 Topography Scale
Aircraft altitude
Ground elevation
-
at present aircraft
position
Page 69
SECTION 10 – HAZARD
AVOIDANCE
Unlighted Obstacle
(Height is less than
1000’ AGL)
Lighted Obstacle
(Height is less than
1000’ AGL)
Figure 10-14 Obstacle Symbols
Unlighted Obstacle
(Height is greater than
1000’ AGL)
Lighted Obstacle
(Height is greater than
1000’ AGL)
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
10-9
Page 70
SECTION 10 – HAZARD
AVOIDANCE
This page intentionally left blank.
10-10
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 71
SECTION 11 – ABNORMAL
OPERATION
SECTION 11: ABNORMAL
OPERATION
11.1 REVERSIONARY MODE
Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode.
In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining
display. Minimal navigation capability is available on the
reversionary mode display.
Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display
problem. The reversionary mode is activated manually
by pressing the red DISPLAY BACKUP button on the
bottom of the audio panel (GMA 1347). Pressing the red
DISPLAY BACKUP button again deactivates reversionary mode.
NOTE: The Tiger AG-5B Pilot’s Operating Handbook (POH) and Pilot’s Operating Handbook
Supplement (POHS) always takes precedence
over the information found in this section.
Normal PFD Display
MFD in Reversionary Mode
Figure 11-1 G1000 Reversionary Mode: Failed PFD
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Normal MFD Display
11-1
Page 72
SECTION 11 – ABNORMAL
OPERATION
11.2 ABNORMAL COM OPERATION
When a COM tuning failure is detected by the system,
the emergency frequency (121.500 MHz) is automatically
loaded into the active frequency field of the COM radio
for which the tuning failure was detected. In the event of
a dual display failure, the emergency frequency (121.500
MHz) automatically becomes the active frequency to the
pilot through the pilot headset.
11.3 UNUSUAL ATTITUDES
The PFD will ‘declutter’ when the aircraft enters an unusual attitude. Only the basic primary functions will be
displayed in these situations.
Red extreme pitch warning chevrons pointing toward
the horizon are displayed starting at 50 degrees above and
30 degrees below the horizon line.
11-2
Figure 11-2 Extreme Pitch Indication
11.4 STORMSCOPE OPERATION WITH
LOSS OF HEADING INPUT
If heading is lost, strikes and/or cells must be cleared
manually after the execution of each turn. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 73
SECTION 12 – ANNUNCIATIONS
& ALERTS
SECTION 12: ANNUNCIATIONS &
ALERTS
NOTE: The Pilot’s Operating Handbook Supple-
ment (POHS) supersedes information found in
this document.
The G1000 Alerting System conveys alerts to the pilot
using a combination of the following items:
• Annunciation Window: The Annunciation
window displays abbreviated annunciation text.
The Annunciation window is located to the right
of the Altitude and Vertical Speed windows on the
PFD display (or the MFD if system is in reversionary mode). All Tiger AG-5B annunciations can be
displayed simultaneously. A white horizontal line
separates annunciations that are acknowledged
from annunciations that are not yet acknowledged.
Acknowledged annunciations are always above the
line. Annuciations are displayed in order of priority
from top to bottom. The highest priority annunciation is displayed at the top of the Annunciation
Window.
• Alerts Window: The Alerts window displays alert
text messages. Up to 64 prioritized alerts can be displayed in the Alerts window. Pressing the ALERTS
softkey displays the Alerts window. Pressing the
ALERTS softkey again removes the Alerts window
from the display. When the Alerts window is displayed, the pilot may use the large FMS knob to
scroll through the alert list. Higher priority alerts are
displayed at the top of the window. Lower priority
alerts are displayed at the bottom of the window.
used as a flashing annunciation to accompany an
alert. During the alert, the ALERTS softkey assumes
a new label consistent with alert level (WARNING,
CAUTION, or ADVISORY). Pressing the softkey
annunciation acknowledges that the pilot is aware
of the alert. The softkey then returns to the previ
ous ALERTS label. The pilot can then press the
ALERTS softkey again to view alert text messages.
• System Annunciations: Typically, a large red ‘X’
appears in a window when a related LRU fails or
detects invalid data.
• Audio Alerting System: The G1000 system issues
audio alert tones when specific system conditions
are met. See the Alert Levels Definitions section for
more information.
System
Annunciation
Red ‘X’
Annunciation
Alerts Window
ALERTS Softkey
Annunciation
-
Window
• ALERTS Softkey Annunciation: When the Alert-
ing System issues an alert, the ALERTS softkey is
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Figure 12-1 G1000 Alerting System
12-1
Page 74
SECTION 12 – ANNUNCIATIONS
& ALERTS
12.1 ALERT LEVEL DEFINITIONS
The G1000 Alerting System, as installed in Tiger AG-
5B aircraft, uses three alert levels.
• WARNING: This level of alert requires immediate
pilot attention. A warning alert is accompanied
by an annunciation in the Annunciation window.
Warning text appearing in the Annunciation window
is RED. A warning alert is also accompanied by a
flashing WARNING softkey annunciation, as shown
in Figure 12-2. Pressing the WARNING softkey
acknowledges the presence of the warning alert and
stops the aural tone, if applicable.
• CAUTION: This level of alert indicates the existence of abnormal conditions on the aircraft that
may require pilot intervention. A caution alert is
accompanied by an annunciation in the Annunciation window. Caution text appearing in the
Annunciation window is YELLOW. A caution alert
is also accompanied by a flashing CAUTION softkey
annunciation, as shown in Figure 12-3. Pressing
the CAUTION softkey acknowledges the presence
of the caution alert.
Figure 12-2 WARNING Softkey
Annunciation
Figure 12-3 CAUTION Softkey
Annunciation
Figure 12-4 ADVISORY Softkey
Annunciation
12-2
• MESSAGE ADVISORY: This level of alert provides
general information to the pilot. A message advisory
alert does not issue annunciations in the Annunciation window. Instead, message advisory alerts only
issue a flashing ADVISORY softkey annunciation,
as shown in Figure 12-4. Pressing the ADVISORY
softkey acknowledges the presence of the message
advisory alert and displays the alert text message in
the Alerts window.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 75
SECTION 12 – ANNUNCIATIONS
& ALERTS
12.2 AIRCRAFT ALERTS
The following alerts are configured specifically for the
L FUEL LOWLeft fuel quantity is low.Single Aural Tone
R FUEL LOWRight fuel quantity is low.Single Aural Tone
LOW VOLTSPrimary bus voltage is below 24 VoltsSingle Aural Tone
LOW BATTERYEmergency battery voltage is low.Single Aural Tone
Message Advisory Alerts
Alerts Window MessageAudio Alert
PFD FAN FAIL – The cooling fan for the PFD is inoperative.
MFD FAN FAIL – The cooling fan for the MFD is inoperative.
GIA FAN FAIL – The cooling fan for the GIAs is inoperative.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
None
None
None
12-3
Page 76
SECTION 12 – ANNUNCIATIONS
& ALERTS
12.3 G1000 SYSTEM ANNUNCIATIONS
When an LRU or an LRU function fails, a large red ‘X’ is
typically displayed on windows associated with the failed
data. The following section describes various system annunciations. Refer to the Pilots Operating Handbook
Supplement (POHS) for additional information regarding
pilot responses to these annunciations.
Voice Alerts
Voice AlertAlert Trigger
“Traffic”Played when a Traffic Advisory (TA) is
issued.
“Traffic Not
Available”
Played when the traffic system fails or can
-
not communicate.
System AnnunciationComment
NOTE: Upon power-up of the G1000 system,
certain windows remain invalid as G1000 equipment begins to initialize. All windows should
be operational within one minute of power-up.
Should any window continue to remain flagged,
the G1000 system should be serviced by a
Garmin-authorized repair facility.
12-4
Attitude and Heading Reference System is aligning.
Display system is not receiving attitude information from the AHRS.
Display system is not receiving airspeed input from air data computer.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 77
SECTION 12 – ANNUNCIATIONS
System AnnunciationComment
Display is not receiving altitude input from the air data computer.
Display is not receiving vertical speed input from the air data computer.
Display is not receiving valid heading input from AHRS.
& ALERTS
Other Various Red X Indications
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
GPS information is either not present or is invalid for navigation use.
Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFMS).
Display is not receiving valid transponder information.
A red ‘X’ through any other display field, such as engine instrumentation
fields, indicates that the field is not receiving valid data.
12-5
Page 78
SECTION 12 – ANNUNCIATIONS
& ALERTS
A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-5 illustrates all possible flags
and the responsible LRUs.
12.4 G1000 SYSTEM MESSAGE
ADVISORIES
This section describes various G1000 system message
advisories. Certain messages are issued due to an LRU or an
LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown
previously in the G1000 System Annunciation section.
NOTE: This Section provides information regarding G1000 message advisories that may be displayed by the system. Knowledge of the aircraft,
systems, flight conditions, and other existing
operational priorities must be considered when
responding to a message. Always use sound
pilot judgment. The Pilot’s Operating Handbook
Supplement (POHS) takes precedence over any
conflicting guidance found in this section.
GIA 63 Integrated
Avionics Units
GEA 71 Engine
Airframe Unit
OR
GIA 63 Integrated
Avionics Unit
GDC 74A Air Data
Computer
Figure 12-5 G1000 System Failure Annunciations
GIA 63 Integrated
Avionics Units
GDC 74A Air Data
Computer
GRS 77 AHRS
OR
GMU 44
Magnetometer
GIA 63 Integrated
Avionics Units
GTX 33 Transponder
OR
GIA 63 Integrated
Avionics Units
12-6
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 79
MFD & PFD Message Advisories
MessageComments
DATA LOST – Pilot stored data was
lost. Recheck settings.
XTALK ERROR – A flight display
crosstalk error has occurred.
PFD1 SERVICE – PFD1 needs service.
Return unit for repair.
MFD1 SERVICE
service. Return unit for repair.
PFD1 CONFIG – PFD1 configuration
error. Config service req’d.
MFD1 CONFIG – MFD1 configuration
error. Config service req’d.
SW MISMATCH – GDU software
mismatch. Xtalk is off.
MANIFEST – PFD1 software mismatch.
Communication halted.
MANIFEST – MFD1 software
mismatch. Communication halted.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 “KEY” KEYSTK – Key is stuck.
MFD1 “KEY” KEYSTK – Key is stuck.
– MFD1 needs
SECTION 12 – ANNUNCIATIONS
& ALERTS
The pilot profile data was lost. System reverts to default pilot profile and settings.
The pilot may reconfigure the MFD & PFD with preferred settings, if desired.
The MFD and PFD are not communicating with each other. The G1000 system should
be serviced.
The PFD and/or MFD self-test has detected a problem. The G1000 system should be
serviced.
The PFD and/or MFD configuration settings do not match backup configuration
memory. The G1000 system should be serviced.
The MFD and PFD have different software versions installed. The G1000 system
should be serviced.
The PFD and/or MFD has incorrect software installed. The G1000 system should be
serviced.
The PFD and/or MFD is overheating and is reducing power consumption by dimming
the display. If problem persists, the G1000 system should be serviced.
A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The G1000 system should be serviced if the problem persists.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
12-7
Page 80
SECTION 12 – ANNUNCIATIONS
& ALERTS
Database Message Advisories
Alerts Window MessageComments
MFD1 DB ERR – MFD1 aviation
database error exists.
PFD1 DB ERR – PFD1 aviation
database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain database
error exists.
DB MISMATCH – Aviation database
version mismatch. Xtalk is off.
DB MISMATCH – Aviation database
type mismatch. Xtalk is off.
The MFD and/or PFD detected a failure in the aviation database. Attempt to reload
the aviation database. If problem persists, the G1000 system should be serviced.
The MFD and/or PFD detected a failure in the basemap database.
The MFD and/or PFD detected a failure in the terrain database. Ensure that the ter
rain card is properly inserted in display. Replace terrain card. If problem persists, The
G1000 system should be serviced.
The PFD and MFD have different aviation database versions installed. Crossfill is off.
Install correct aviation database version in both displays.
The PFD and MFD have different aviation database types installed (Americas, Euro
pean, etc.). Crossfill is off. Install correct aviation database type in both displays.
-
-
12-8
GMA 1347 Message Advisories
Alerts Window MessageComments
GMA1 FAIL – GMA1 is inoperative.The audio panel self-test has detected a failure. The audio panel is unavailable. The
G1000 system should be serviced.
GMA1 CONFIG – GMA1 configuration
error. Config service req’d.
MANIFEST – GMA1 software
mismatch. Communication halted.
GMA1 SERVICE
service. Return unit for repair.
BACKUP PATH – Audio panel using
backup data path.
– GMA1 needs
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
The audio panel configuration settings do not match backup configuration memory.
The G1000 system should be serviced.
The audio panel has incorrect software installed. The G1000 system should be
serviced.
The audio panel self-test has detected a problem in the unit. Certain audio functions
may still be available, and the audio panel may still be usable. The G1000 system
should be serviced when possible.
The audio panel is using a backup communication path. The G1000 system should
be serviced when possible.
Page 81
GIA 63 Message Advisories
Alerts Window MessageComments
GIA1 CONFIG – GIA1 configuration
error. Config service req’d.
GIA2 CONFIG – GIA2 configuration
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
MANIFEST – GIA1 software mismatch.
Communication halted.
MANIFEST – GIA2 software mismatch.
Communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.
– COM1 needs
SECTION 12 – ANNUNCIATIONS
& ALERTS
The GIA1 and/or GIA2 configuration settings do not match backup configuration
memory. The G1000 system should be serviced.
The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to
warm up to operating temperature.
The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000
system should be serviced.
The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000
system should be serviced.
The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should
be serviced.
The system has detected an over temperature condition in COM1 and/or COM2. The
transmitter will operate at reduced power. If the problem persists, the G1000 system
should be serviced.
The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may
still be usable. The G1000 system should be serviced when possible.
The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or
“pressed”) position. Press the PTT switch again to cycle its operation.
If the problem persists, the G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
12-9
Page 82
SECTION 12 – ANNUNCIATIONS
& ALERTS
GIA 63 Message Advisories (Cont.)
Alerts Window MessageComments
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
RAIM UNAVAIL
available from FAF to MAP waypoints.
RAIM UNAVAIL
available.
POSN ERROR – RAIM has determined
GPS position is in error.
DGRD GPS ACC – GPS position
accuracy degraded & RAIM unavailable.
GPS1 FAIL – GPS1 is inoperative.
GPS2 FAIL – GPS2 is inoperative.
GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
GPS2 SERVICE – GPS2 needs service.
Return unit for repair.
NAV1 SERVICE – NAV1 needs service.
Return unit for repair.
NAV2 SERVICE – NAV2 needs service.
Return unit for repair.
NAV1 RMTXFR – NAV1 remote
transfer key is stuck.
NAV2 RMTXFR – NAV2 remote
transfer key is stuck.
– RAIM is not
– RAIM is not
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) posi
tion. Press the transfer switch again to cycle its operation. If the problem persists,
the G1000 system should be serviced.
GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity
Monitoring (RAIM) from the FAF to the MAP waypoints.
GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity
Monitoring (RAIM) for the current phase of flight.
When a RAIM position error is detected, GPS is flagged and the system no longer
provides GPS-based guidance.
GPS position accuracy has been degraded and RAIM is not available.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is
unavailable. The G1000 system should be serviced.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be serviced.
A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be serviced.
The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”)
state. Press the transfer switch again to cycle its operation. If the problem persists,
the G1000 system should be serviced.
12-10
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 83
GIA 63 Message Advisories (Cont.)
Alerts Window MessageComments
G/S1 FAIL – G/S1 is inoperative.
G/S2 FAIL – G/S2 is inoperative.
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000
system should be serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver
may still be available. The G1000 system should be serviced when possible.
GEA 71 Message Advisories
Alerts Window MessageComments
GEA1 CONFIG – GEA1 configuration
error. Config service req’d.
MANIFEST – GEA1 software
mismatch. Communication halted.
BACKUP PATH
data path.
– EIS using backup
The GEA 71 configuration settings do not match those of backup configuration
memory. The G1000 system should be serviced.
The GEA 71 has incorrect software installed. The G1000 system should be serviced.
The GEA 71 is using a backup communication path. The G1000 system should be
serviced when possible.
SECTION 12 – ANNUNCIATIONS
& ALERTS
GTX 33 Message Advisories
Alerts Window MessageComments
XPDR1 CONFIG – XPDR1 config error.
Config service req’d.
MANIFEST – GTX1 software mismatch.
Communication halted.
BACKUP PATH – Transponder using
backup data path.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
The transponder configuration settings do not match those of backup configuration
memory. The G1000 system should be serviced.
The transponder has incorrect software installed. The G1000 system should be
serviced.
The transponder is using a backup communications path. The G1000 system should
be serviced when possible.
12-11
Page 84
SECTION 12 – ANNUNCIATIONS
& ALERTS
GRS 77 Message Advisories
Alerts Window MessageComments
AHRS TAS
airspeed.
AHRS GPS – AHRS using backup GPS
source.
AHRS GPS – AHRS not receiving GPS
information.
AHRS GPS – AHRS not receiving
backup GPS information.
AHRS GPS – AHRS operating
exclusively in no-GPS mode.
MANIFEST – GRS1 software mismatch.
Communication halted.
BACKUP PATH – AHRS using backup
data path.
AHRS SERVICE – AHRS Magnetic-field
model needs update.
GEO LIMITS – Too far North/South, no
magnetic compass.
– AHRS not receiving
The AHRS is not receiving true airspeed from the air data computer. The AHRS relies
on GPS information to augment the lack of airspeed. The G1000 system should be
serviced.
The AHRS is using the backup GPS path. Primary GPS path has failed. The G1000
system should be serviced when possible.
The AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The G1000 system should be serviced.
The AHRS is not receiving backup GPS information. The G1000 system should be
serviced.
The AHRS is operating exclusively in no-GPS mode. The G1000 system should be
serviced.
The AHRS has incorrect software installed. The G1000 system should be serviced.
The AHRS is using a backup communications data path. The G1000 system should
be serviced when possible.
The AHRS earth magnetic field model is out of date. Update magnetic field model
when practical.
The aircraft is outside geographical limits for approved AHRS operation. Heading is
flagged as invalid.
12-12
GMU 44 Message Advisories
Alerts Window MessageComments
HDG FAULT – A magnetometer fault
has occurred.
MANIFEST – GMU1 software
mismatch. Communication halted.
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
A fault has occurred in the GMU 44. Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000 system should be serviced.
The GMU 44 has incorrect software installed. The G1000 system should be serviced.
Page 85
SECTION 12 – ANNUNCIATIONS
GDC 74A Message Advisories
Alerts Window MessageComments
GDC1 CONFIG – GDC1 configuration
error. Config service req’d.
MANIFEST – GDC1 software
mismatch. Communication halted.
BACKUP PATH – Airdata using backup
data path.
GDC 74A configuration settings do not match those of backup configuration
memory. The G1000 system should be serviced.
The GDC 74A has incorrect software installed. The G1000 system should be
serviced.
The GDC 74A is using a backup communications data path. The G1000 system
should be serviced when possible.
Miscellaneous Message Advisories
Alerts Window MessageComments
FPL WPT LOCK – Flight plan waypoint
is locked.
FPL WPT MOVE
waypoint moved.
TIMER EXPIRD – Timer has expired.The system notifies the pilot that the timer has expired.
DB CHANGE – Database changed.
Verify user modified procedures.
FPL TRUNC
truncated.
APPR VPROF – Approaching VNAV
profile.
APPR TRG ALT – Approaching target
altitude.
– Flight plan
– Flight plan has been
Upon power-up, the G1000 system detects that a stored flight plan waypoint is
locked. This occurs when an aviation database update eliminates an obsolete way
point. The flight plan cannot find the specified waypoint and flags this message. This
can also occur with user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no longer exists in any database,
OR
update the waypoint name/identifier to reflect the new information.
The system has detected that a waypoint coordinate has changed due to a new
aviation database update. Verify that stored flight plans contain correct waypoint
locations.
This occurs when a stored flight plan contains procedures that have been manually
edited. This alert is issued only after an aviation database update. Verify that the
user-modified procedures in stored flight plans are correct and up to date.
This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan. The obsolete procedure is removed
from the flight plan. Update flight plan with current arrival or approach.
Aircraft is approaching VNAV profile. Prepare to climb or descend to meet VNAV
profile.
Aircraft is approaching target altitude. Prepare to level aircraft.
& ALERTS
-
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
12-13
Page 86
SECTION 12 – ANNUNCIATIONS
& ALERTS
Miscellaneous Message Advisories (Cont.)
Alerts Window MessageComments
LOCKED FPL – Cannot navigate locked
flight plan.
WPT ARRIVAL – Arriving at waypoint
-[xxxx]
STEEP TURN
INSIDE ARSPC – Inside airspace.The aircraft is inside the airspace.
ARSPC AHEAD – Airspace ahead less
than 10 minutes.
ARSPC NEAR – Airspace near and
ahead.
ARSPC NEAR – Airspace near – less
than 2 nm.
LEG UNSMOOTH
not be smooth.
APPR INACTV – Approach is not
active.
SLCT AUTOSEQ
sequence mode.
SLCT FREQ – Select appropriate
frequency for approach.
SLCT NAV – Select NAV on
approach.
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
TRAFFIC FAIL – Traffic device has
failed.
STRMSCP FAIL
failed.
BACKUP PATH – Stormscope using
backup path.
– Steep turn ahead.A steep turn is 15 seconds ahead. Prepare to turn.
– Flight plan leg will
– Select auto
CDI for
– Stormscope has
This occurs when the pilot attempts to activate a stored flight plan that contains
locked waypoint. Remove locked waypoint from flight plan. Update flight plan with
current waypoint.
Arriving at waypoint [xxxx], where [xxxx] is the waypoint name.
Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace
within 10 minutes.
Special use airspace is near and ahead of the aircraft position.
Special use airspace is within 2 nm of the aircraft position.
The approaching flight plan waypoints are too close to allow for smooth turns.
Prepare for steep turns ahead and expect noticeable course deviations.
The system notifies the pilot that the loaded approach is not active. Activate ap
-
proach when required.
The system notifies the pilot to select auto-sequence mode. Press the OBS softkey to
deactivate the OBS mode.
The system notifies the pilot to load the approach frequency for the appropriate NAV
receiver. Select the correct frequency for the approach.
The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI
to the correct NAV receiver.
The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position
with alternate navigation sources.
The traffic information system TIS has failed. The G1000 system should be serviced.
Stormscope has failed. The G1000 system should be serviced.
Stormscope is using the backup communication path. The G1000 system should be
serviced when possible.
12-14
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 87
INDEX
A
Abnormal COM operation 11-2
Activate a flight plan 8-2
Active flight plan 8-2
ADVISORY 12-1
Advisory alerts 12-3
Age 10-6
AHRS 12-12
Aircraft alerts 12-3
AIRMET 10-5
Airport frequency 7-6
Airport information 7-3
Airspace alerts 7-9
Airspeed indicator 2-3
Airspeed trend vector 2-3
Alerting System 12-1
Alerts 12-1
Alert levels 12-2
Altitude reference bug 2-4
Altitude trend vector 2-4
ALT knob 1-3
Annunciations 12-1
Approaches 9-2
Approach activation 4-3
Approach markers
Signal augmentation 5-2
Arrivals 9-1
Attitude indicator 2-3
Audio alerting system 12-1
Audio panel 4-3, 5-1
Audio panel controls
WARN 2-7
Warning 12-1, 12-2
Warnings i, ii
Weather data link page 10-4
Weather product symbol 10-5
Weather product symbols 10-6
Weather warnings 10-5
Wind direction 10-5
Wind speed 10-5
X
XPDR softkey 4-4
Index-2
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Page 89
Page 90
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd.
Unit 5, The Quadrangle
Abbey Park Industrial Estate
Romsey, SO51 9DL, U.K.
p: 44/0870.8501241 f: 44/0870.8501251