This manual reflects the operation of System Software version 0435.09 or later for the Cessna
Citation Mustang. 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® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH™,
FliteCharts™, and SafeTaxi™ are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM
Satellite Radio, Inc.
May, 2007 190-00600-01 Rev. C Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain function. The G1000 Terrain Proximity feature is NOT
intended to be used as a primary reference for terrain avoidance and does not
relieve the pilot from the responsibility of being aware of surroundings during
flight. The Terrain Proximity feature is only to be used as an aid for terrain
avoidance and is not certified for use in applications requiring a certified
terrain awareness system. Terrain data is obtained from third party sources.
Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B 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: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on the G1000 Multi Function Display
is provided as an aid in visually acquiring traffic. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition of
conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
Warnings, Cautions & Notes
WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: The Garmin G1000, as installed in the Cessna Citation Mustang
aircraft, has a very high degree of functional integrity. However, the pilot
must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.
WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
CAUTION: The GDU 1040A PFDs and GDU 1500 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.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system. Depictions of equipment may differ
slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Lamp(s) inside this product may contain mercury (HG) and must be
recycled or disposed of according to local, state, or federal laws. For more
information, refer to our website at www.garmin.com/aboutGarmin/environment/disposal.jsp.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
Part NumberChange Summary
190-00600-00
Rev A
Initial release
Rev B
Added Additional Features section
190-00600-01
Rev A
Rev B
Production release
Added CAS INOP system messages
RevisionDate of RevisionAffected PagesDescription
CMay, 2007Pages 6
Pages 36, 37
Page 51
Added COM 3 function for HF.
Added TAS.
Removed automatic Reversionary
Mode operation.
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
RR-1
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
SD Card Use .............................................................................................................................. 86
Index ...........................................................................................................................................Index-1
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
iii
Table of Contents
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the STD BARO Softkey.
OR
Push the BARO Knob to select standard pressure.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
OR
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Press the BACK Softkey to return to the top-level softkeys.
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
1)
Press the MENU Key to display the PFD Setup Menu.
2)
Turn the
3)
Turn the
4)
Press the MENU Key to remove the window.
large
FMS Knob to highlight the ‘Baro Sync’ ON/OFF field.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
SYNCHRONIZE CDI
1)
Press the MENU Key to display the PFD Setup Menu.
2)
Turn the large FMS Knob to highlight ‘CDI SYNC OFF’.
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
1
Flight Instruments
3)
Turn the small FMS Knob in the direction of the green arrowhead to select
ON.
4)
Press the MENU Key to remove the window.
CHANGE NAVIGATION SOURCES
1)
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.
3)
Press the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Press the OBS Softkey to select OBS Mode.
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
GENERIC TIMER
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
CONFIGURE VSPEED BUGS INDIVIDUALLY
1)
Press the TMR/REF Softkey.
2)
Turn the
2
large
FMS Knob to highlight the desired Vspeed.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
speed has been changed from a default value, an asterisk appears next to
the speed).
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
TURN VSPEED BUGS ON OR OFF BY CATEGORY
1)
Press the TMR/REF Softkey.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Press the TMR/REF Softkey to remove the window.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to BARO.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Flight Instruments
DISPLAYING WIND DATA
1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data below the Selected Heading.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
3
Flight Instruments
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER OR CHANGE FLIGHT ID
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
2)
Turn the small FMS Knob to enter the first character.
3)
Turn the large FMS Knob to select the next field.
4)
Turn the small FMS Knob to enter the next desired character.
5)
Repeat steps 3 and 4 until the desired Flight ID is entered.
6)
Press the ENT Key to update the Flight ID.
ADF TUNING (OPTIONAL)
1)
Press the ADF/DME Softkey.
2)
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
3)
Turn the large FMS Knob to select the next desired field.
4)
Turn the small FMS Knob to enter the desired number.
5)
Repeat steps 3 and 4 until the desired ADF frequency is entered.
6)
Press the ENT Key to accept the new frequency.
7)
Press the ENT Key again to transfer the frequency to the active field.
8)
Turn the large FMS Knob to select the MODE field.
9)
Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10)
Press the ENT Key to complete the selection.
Nav/Com/XPDR/Audio Panel
DME TUNING
1)
Press the ADF/DME or DME Softkey.
2)
Turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired DME tuning.
4)
Press the ENT Key to complete the selection.
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
5
Nav/Com/XPDR/Audio Panel
ENTER A TRANSPONDER CODE
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the XPDR1 or XPDR2 Softkey to select the active transponder.
3)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
4)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
SELECTING A COM RADIO
Transmit
Press the COM1 MIC, COM2 MIC
the audio panel.
Receive
Press the COM1, COM2
, or
, or
COM3 MIC Key (HF, if installed) on
COM3 Key (HF, if installed) on the audio panel.
SELECTING A NAV RADIO
1)
Press the CDI Softkey to select NAV1 (VOR1/LOC1) or NAV2 (VOR2/LOC2).
2)
Pressing the NAV1, NAV2, DME, or ADF Key selects and deselects the
navigation radio audio source. All radio keys can be selected individually or
together.
NAV/COM TUNING
1)
Press the small tuning knob to select the desired radio for tuning.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
6
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
Nav/Com/XPDR/Audio Panel
DIGITAL CLEARANCE RECORDER AND PLAYER
NOTE: Only the audio for the selected
not recorded for COM3 MIC.
COM MIC
Record
1)
Press the REC Key to begin recording.
2)
Press the REC Key again to stop recording.
Play
1)
Press the PLAY Key once to play the latest recorded memory block.
2)
Press the PLAY Key once while playing to stop.
3)
Press the PLAY Key twice quickly while playing to begin playing the
previously recorded block.
Each subsequent two presses will skip back to
the previously recorded block.
Key is recorded. Audio is
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
7
Nav/Com/XPDR/Audio Panel
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8
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the flight director automatically disengages.
FLIGHT DIRECTOR ACTIVATION
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
AFCS
Control Pressed
Modes Selected
LateralVertical
FD KeyRoll Hold (default)ROLPitch Hold (default)PIT
AP KeyRoll Hold (default)ROLPitch Hold (default)PIT
CWS ButtonRoll Hold (default)ROLPitch Hold (default)PIT
GA Switch
ALT Key
Takeoff (on ground)
Go Around (in air)
TO
GA
Roll Hold (default)ROLAltitude HoldALT
Takeoff (on ground)
Go Around (in air)TOGA
VS KeyRoll Hold (default)ROLVertical SpeedVS
VNV KeyRoll Hold (default)ROLVertical Path Tracking*VPTH
GPS
NAV Key
Navigation**
VOR
Pitch Hold (default)PIT
LOC
BC KeyBackcourse***BCPitch Hold (default)PIT
GPS
APR KeyApproach**
VOR
Pitch Hold (default)PIT
LOC
HDG KeyHeading SelectHDGPitch Hold (default)PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV
or
APR
Key press activates flight director.
BC
***The selected navigation receiver must have a valid LOC signal before
director.
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Key press activates flight
9
AFCS
VERTICAL MODES
Vertical ModeDescriptionControlAnnunciation
Holds the current aircraft pitch attitude;
Pitch Hold
Selected Altitude
Capture
Altitude HoldHolds the current Altitude ReferenceALT KeyALTnnnnn FT
Vertical Speed
Flight Level Change,
IAS Hold
Flight Level Change,
Mach Hold
Vertical Path
Tracking
VNV Target Altitude
Capture
Glidepath
Glideslope
Takeoff (on ground)
Go Around (in air)
* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected
Altitude is to be captured instead of VNV Target Altitude
** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of
Selected Altitude
may be used to climb/descend to the
Selected Altitude
Captures the Selected Altitude
Maintains the current aircraft vertical
speed; may be used to climb/descend
to the Selected Altitude
Maintains the current aircraft airspeed
(in IAS or Mach) while the aircraft is
climbing/descending to the Selected
Altitude
Captures and tracks descent legs of an
active vertical profile
Captures the Vertical Navigation (VNV)
Target Altitude
Captures and tracks the WAAS
glidepath on approach
Captures and tracks the ILS glideslope
on approach
Disengages the autopilot and
commands a constant pitch angle and
wings level in the air on the ground in
preparation for takeoff
Disengages the autopilot and
commands a constant pitch angle and
wings level in the air
(default)PIT
*ALTS
VS KeyVSnnnn FPM
FLCnnn KT
FLC Key
FLCM .nnn
VNV
Key
VPTH
**ALTV
GP
APR Key
GS
TO
GA
Switch
GA
10
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
AFCS
LATERAL MODES
Lateral ModeDescriptionControlAnnunciation
Holds current aircraft roll attitude
Roll Hold
Low Bank
Heading Select
Navigation, GPS Arm/
Capture/Track
Navigation, VOR Enroute
Arm/Capture/Track
Navigation, LOC Arm/
Capture/Track
(No Glideslope)
Backcourse Arm/Capture/
Track
Approach, GPS Arm/
Capture/Track
Approach, VOR Arm/
Capture/Track
Approach, ILS Arm/
Capture/Track
(Glideslope Mode
automatically armed)
Takeoff (on ground)
Go Around (in air)
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
or rolls wings level, depending
on commanded bank angle
Limits maximum commanded
roll angle
Captures and tracks Selected
Heading
Captures and tracks selected
navigation source (GPS, VOR,
LOC)
Captures and tracks a localizer
signal for backcourse approaches
Captures and tracks selected
navigation source (GPS, VOR,
LOC)
Disengages autopilot and
commands a constant pitch
angle and wings level in
preparation for takeoff
Disengages autopilot and
commands a constant pitch
angle and wings level in the air
(default)ROL
BANK
Key
HDG
Key
*
HDG
GPS
NAV
VOR
Key
LOC
BC KeyBC
GPS
VAPP
APR Key
LOC
TO
GA
Switch
GA
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
11
AFCS
Roll Hold Mode (ROL)
Bank AngleFlight Director Response
< 6 degRolls wings level
6 to 30 degMaintains current aircraft roll attitude
> 30 degLimits bank to 30 degrees
Roll Hold Mode Responses
12
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
GPS NAVIGATION
DIRECT-TO NAVIGATION
Direct-to Navigation from the MFD
1)
Press the Direct-to
2)
Enter the destination waypoint identifier.
3)
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
4)
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
5)
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
6)
Enter the desired altitude.
7)
Press the ENT Key. The option to select MSL or AGL is now displayed.
8)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
9)
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
10)
Enter the desired offset distance before (-) or after (+) the waypoint.
11)
Press the ENT Key. The ‘Activate?’ field is highlighted.
12)
Press the ENT Key to activate.
()
Key.
GPS Navigation
Direct-to Navigation from the PFD
1)
Press the Direct-to Key
2)
Turn the large FMS Knob to place the cursor in the desired selection field.
3)
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
4)
Press the ENT Key.
5)
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
6)
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
7)
Turn the small FMS Knob to enter the desired VNV altitude.
190-00600-01 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
()
.
13
GPS Navigation
8)
Press the ENT Key. The option to select MSL or AGL is now displayed.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
10)
Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance field.
11)
Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
12)
Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘COURSE’ field.
13)
Turn the small FMS Knob to enter the desired course to the waypoint.
14)
Press the ENT Key to highlight ‘ACTIVATE?’.
15)
Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key and turn the small FMS Knob to display the Flight Plan
Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Select the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired destination waypoint.
2)
Select the ACT LEG Softkey.
OR
3)
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the
ENT Key. This step must be used when activating a leg from
the PFD.
4)
With ‘Activate’ highlighted, press the ENT Key.
14
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-01 Rev. C
GPS Navigation
STOP NAVIGATING A FLIGHT PLAN
1)
Press the FPL Key to display the Active Flight Plan Page.
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.
VERTICAL NAVIGATION
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Large White
Text
Large Light
Blue Text
190-00600-01 Rev. C
Small Light
Blue Text
Small Light
Blue Subdued
Text
Small White Text
with Altitude
Restriction Bar
Stay AT or ABOVE 5,000 ft
Stay AT 2,300 ft
Stay AT or BELOW 3,000 ft
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
15
GPS Navigation
Altitudes associated with arrival and approach procedures are “auto-designated”.
This means the system will automatically use the altitudes loaded with the arrival or
approach for giving vertical speed and deviation guidance. Note that these altitudes
will be displayed as blue text up to, but not including the FAF. The FAF will always be
a “reference only” altitude and cannot be designated, unless the selected approach does
not provide vertical guidance. In this case, the FAF altitude can be designated.
Altitudes that have been designated for use in vertical guidance may also be made
“non-designated” by placing the cursor over the desired altitude and pressing the CLR
Key. The altitude is now displayed only as a reference. It will not be used to give
vertical guidance. Other displayed altitudes may change due to re-calculations or
rendered invalid as a result of manually changing an altitude to a non-designated
altitude.
White TextLight Blue TextLight Blue
Subdued Text
Large Text
Small Text
16
Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
speed and deviation
guidance.
Altitude is not
designated to be used
in determining vertical
speed and deviation
guidance. Altitude has
been retrieved from the
navigation database
and is provided as a
reference.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Altitude has been
entered by the pilot.
Altitude is designated
for use in giving vertical
speed and deviation
guidance. Altitude
does not match the
published altitude in
navigation database or
no published altitude
exists.
Altitude is designated
for use in giving vertical
speed and deviation
guidance. Altitude has
been retrieved from the
navigation database
or has been entered by
the pilot and matches
a published altitude
in the navigation
database.
The system cannot
use this altitude in
determining vertical
speed and deviation
guidance.
The system cannot
use this altitude in
determining vertical
speed and deviation
guidance.
190-00600-01 Rev. C
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