This manual reflects the operation of System Software version 1162.00 or later for the Cessna
CitationJet Model 525. Some differences in operation may be observed when comparing the
information in this manual to earlier or later software versions.
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied,
transmitted, disseminated, downloaded or stored in any storage medium, for any purpose
without the express written permission of Garmin. Garmin hereby grants permission to
download a single copy of this manual and of any revision to this manual onto a hard drive or
other electronic storage medium to be viewed for personal use, provided that such electronic
or printed copy of this manual or revision must contain the complete text of this copyright
notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.
Garmin® is a registered trademark 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.; and XM® is a registered trademark of
XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell
International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.
May, 2010 190-01130-00 Rev. A Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by the 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 the aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the PFD or other
pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the system must be updated regularly in order to ensure that the information
remains current. Pilots using any outdated database do so entirely at their
own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based upon
TCAS II Resolution Advisories (if installed), 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 CitationJet Model 525
190-01130-00 Rev. A
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 G1000 Integrated Flight Deck, as installed in the Cessna
CitationJet Model 525 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 system. 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, system 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 system utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the system 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 CitationJet Model 525 Airplane Flight Manual. Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare
indications from the system 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 system 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.”
190-01130-00 Rev. A
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Warnings, Cautions & Notes
WARNING: Lamp(s) inside this product may contain mercury (HG) and must
be recycled or disposed of according to local, state, or federal laws. For
more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
WARNING: Because of variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications. North of 72° North latitude at all longitudes. South of
70° South latitude at all longitudes. North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude
between longitude 70° W and 128° W. (Northern Canada). North of 70° North
latitude between longitude 85° E and 114° E. (Northern Russia). South of
55° South latitude between longitude 120° E and 165° E. (Region south of
Australia and New Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are
derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean,
lint-free cloth and an eyeglass lens cleaner that is specified as safe for antireflective coatings.
CAUTION: The system 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 panel and displays, are subject to change and may not reflect
the most current system and databases. Depictions of equipment may differ
slightly from the actual equipment.
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
Warnings, Cautions & Notes
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot
a resource with which to find operating instructions on the major features
of the G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Integrated Flight Deck Pilot’s Guide.
190-01130-00 Rev. A
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Warnings, Cautions & Notes
Blank Page
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
Record of Revisions
Part NumberChange Summary
190-01130-00Initial release
RevisionDate of Revision Affected PagesDescription
AMay, 2010AllProduction release
190-01130-00 Rev. ARR-1
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Record of Revisions
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RR-2
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
INDEX .........................................................................................................................................Index-1
iv
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE
Press the BARO Knob.
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
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION
Window.
4)
Turn the
small
FMS Knob clockwise to ON or counterclockwise to OFF.
SYNCHRONIZE CDI
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the
190-01130-00 Rev. A1
small
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Flight Instruments
CHANGE NAVIGATION SOURCES
Flight
1)
InstrumentsEIS
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
Nav/Com/
XPDR/AudioAFCSGPS Nav
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 the CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to slew the CDI Course Pointer to a course bearing directly
to the waypoint.
Flight
PlanningProcedures
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
Hazard
Avoidance
Features
Additional
Abnormal
Operation
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
CONFIGURE VSPEED BUGS INDIVIDUALLY
AlertsAppendixIndex
Annun/
1)
Press the TMR/REF Softkey.
2)
Turn the
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
large
FMS Knob to highlight the desired Vspeed.
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field.
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
TURN 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/RADAR ALTIMETER (RA OPTIONAL) MINIMUM DESCENT
ALTITUDE
1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the
right of ‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to select BARO or RAD ALT.
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.
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
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.
190-01130-00 Rev. A3
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Operation
Abnormal
Annun/
AlertsAppendixIndex
Flight Instruments
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
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Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
4
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
ENGINE INDICATION SYSTEM
NOTE: Refer to the Airplane Flight Manual (AFM) for engine limitations.
EIS
InstrumentsEIS
Flight
1
XPDR/AudioAFCSGPS Nav
Nav/Com/
2
PlanningProcedures
Flight
3
4
Avoidance
Hazard
Additional
Features
5
Operation
Abnormal
EIS Display (Engine Run)
Engine Fan Rotation Speed
1
Interturbine Temperature
2
Engine High Pressure Turbine Rotation
3
4
Engine Oil Pressure and Temperature
Fuel Display
5
Speed
When an unsafe operating condition occurs, the pointer and readout color change to
indicate a caution (yellow) or warning (red). If the time limit for an unsafe condition is
exceeded, the color of the sliders, pointers, and digits may change to denote an increase
190-01130-00 Rev. A5
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
AlertsAppendixIndex
Annun/
EIS
in priority level, even if the parameter is still within the lower priority condition range.
If sensor data for a parameter becomes invalid or unavailable, a red “X” is displayed
Flight
InstrumentsEIS
across the indicator and/or readout.
Exceedance
Levels
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Slider
(Normal)
Pointer
(Normal)
Exceedance
Levels
Slider
(Exceedance)
Normal Band
Pointer
(Exceedance)
Indicators and Exceedance Levels
INTER-TURBINE TEMPERATURE
When either engine is not running, red triangles indicate the ITT limits which must
Hazard
not be exceeded while starting. When the respective engine ignitors are on, ‘IGN’
Avoidance
appears in green text at the top of the ITT scales.
When both engines are running, the ITT scale is reduced and the red triangles are
Features
removed from display.
Additional
During an ITT exceedance, pointer(s) are displayed in yellow or red, and readout(s)
are provided for each engine below the scale showing an exceedance.
Abnormal
Operation
AlertsAppendixIndex
Annun/
Ignitor On
Indication
Never
Exceed
Inter-Turbine Temperature Display
(Right Engine Start)
6
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Inter-Turbine Temperature Display
(Both Engines Running)
190-01130-00 Rev. A
EIS
GROUND OAT SET WINDOW
When the aircraft is parked or is taxiing, the reported ground Outside Air
Temperature (OAT) for the airport can be set in the Ground OAT Set Window.
Ground OAT Set Window
Setting Outside Air Temperature (OAT)
1)
Select the TARGT N1 Softkey.
2)
Select the GND OAT Softkey to display the Ground OAT Set Window.
3)
To adjust the temperature in 1 °C increments, use the OAT and OAT
softkeys,
4)
To confirm the selected takeoff settings and close the Ground OAT Set
Window, select the ACCEPT Softkey,
Or
:
To cancel the operation, select the BACK Softkey.
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
ENGINE SPOOL ROTATION SPEEDS (N1 AND N2)
The N1 display ranges from 20 to 110% of maximum rotational speed. If N1
drops below 20%, the sliders are removed from the scale while the readouts remain
displayed below.
Caution or warning conditions cause the exceedance pointer(s) and readout(s) to
be displayed in yellow or red respectively.
190-01130-00 Rev. A7
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
AlertsAppendixIndex
Annun/
EIS
The N2 readouts are located beneath the ITT display. Readouts normally appear in
green. An N2 exceedance readout will appear in red. If the readout is out of range,
Flight
InstrumentsEIS
dashes will be displayed instead of a readout.
Target Thrust Mode
Warning
Line
N1 Target Value
Readout
N1 Target
Bug
Nav/Com/
XPDR/AudioAFCSGPS Nav
N1 Readout
N1 Display
Flight
PlanningProcedures
N2 Display
TARGET N1 THRUST MODE
When the system is powered up on the ground, the TO/GA target thrust mode
is shown in light blue subdued text, and the N1 target readout box displays dashes.
Hazard
Avoidance
After the ground OAT is accepted, the target thrust mode is shown in light blue, the
N1 target readout box contains the target N1 percentage, and the target N1 bugs are
displayed along the vertical scale for each engine.
Features
Additional
If the flight conditions or air data are out of range, the selected target thrust mode
is shown in light blue subdued text, the N1 target readout is replaced with dashes, and
Abnormal
the N1 target bugs are removed from display.
Operation
AlertsAppendixIndex
Annun/
IndicationTarget Thrust Mode
TO/GATakeoff/Go Around
CLBClimb
CRUCruise
MANManual
Thrust Mode Indications
8
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
NOTE: The system automatically selects a target thrust mode under certain
flight conditions; refer to the Airplane Flight Manual Supplement (AFMS) for
a detailed discussion of automatic thrust mode transitions.
Selecting Takeoff, Climb, or Cruise Target N1 Thrust Mode
1)
Select the TARGT N1 Softkey
2)
Select one of the following Softkeys:
TO
/GA: Selects the Takeoff/Go Around target N1 thrust mode.
CL
B: Selects the Climb target N1 thrust mode.
CR
U: Selects the Cruise target N1 thrust mode.
3)
To return to the top level of Softkeys without changing the target thrust
mode, select the BACK Softkey.
Manually Entering Target N1 Speed
1)
Select the TARGT N1 Softkey.
2)
Select the MAN Softkey.
3)
Select the following Softkeys to adjust the target N1% readout and bugs.
+1
: Increases the target N1 speed by 1%..
+0
.1: Increases the target N1 speed by 0.1%.
-1
: Decreases the target N1 speed by -1%.
-.
01: Decreases the target N1 speed by -0.1%
4)
Select the BACK Softkey to return to the top level of Softkeys.
Removing N1 Target Speed Display
EIS
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
1)
Select the TARGT N1 Softkey.
2)
Select the OFF Softkey.
190-01130-00 Rev. A9
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
AlertsAppendixIndex
Annun/
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
EIS
Blank Page
Hazard
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Features
Additional
Abnormal
Operation
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10
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
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)
Tune the ADF using the remote ADF control head.
2)
If two ADF systems are installed, press the AUX Key on the desired audio
panel to monitor ADF2 audio.
DME TUNING
Nav/Com/XPDR/Audio Panel
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
1)
Press the DME Softkey.
2)
If two DMEs are installed, turn the large FMS to select the DME source
field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
5)
If two DMEs are installed, press the AUX Key on the desired audio panel to
monitor DME2 audio.
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.
190-01130-00 Rev. A11
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Nav/Com/XPDR/Audio Panel
SELECT TRANSPONDER MODE
Flight
1)
InstrumentsEIS
Press the XPDR Softkey.
2)
If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder.
3)
Press the desired transponder mode softkey (STBY, ON, ALT, or GND).
SELECTING A COM RADIO
Nav/Com/
XPDR/AudioAFCSGPS Nav
Transmit/Receive
Press the COM1 MIC, COM2 MIC
the audio panel.
Receive Only
Press the COM1, COM2
Flight
PlanningProcedures
SELECTING A NAV RADIO
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
Hazard
Avoidance
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
, or
COM3 MIC Key (HF, if installed) on
, or
COM3 Key (HF, if installed) on the audio panel.
NAV/COM TUNING
Features
Additional
1)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
Abnormal
Operation
AlertsAppendixIndex
Annun/
enters kHz.
2)
Press the appropriate Frequency Transfer Key to place the frequency into
the active frequency field.
Or
:
1)
Press the COM or NAV Key on the MFD/PFD Control Unit to select the
desired COM or NAV frequency box.
2)
Turn the FMS Knob to tune the desired frequency (large knob for MHz;
small knob for kHz).
3)
Press the
12
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Frequency Transfer
Key to transfer the frequency to the active field.
190-01130-00 Rev. A
Nav/Com/XPDR/Audio Panel
INTERCOM SYSTEM (ICS) ISOLATION
Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.
The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.
the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the
VOL/SQ selection).
•Whenthe MANSQAnnunciatorisilluminated(ManualSquelch),theICS
Knob controls either volume or squelch (selected by pressing the ICS Knob and
indicated by the VOL or SQ annunciation).
Cabin Address
The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.
When the flight crew wants to communicate with the passengers, the pilot or
copilot presses the CABIN Key to signal that communication is desired.
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
PASSENGER ADDRESS (PA) SYSTEM
A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the headset only if the
PA Key is enabled on both audio panels. PA messages are one way from the flight deck
to the passengers.
190-01130-00 Rev. A13
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Nav/Com/XPDR/Audio Panel
CLEARANCE RECORDER AND PLAYER
Flight
InstrumentsEIS
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.
Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes
Nav/Com/
of recording time have been reached, the recorder begins recording over the stored
XPDR/AudioAFCSGPS Nav
memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator is illuminated to
indicate when play is in progress. The PLAY annunciator extinguishes after playback
is finished.
Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
Flight
block, play is halted.
PlanningProcedures
Pressing the PLAY Key twice within one-half second while audio is playing plays
the previous block of recorded audio. Each subsequent two presses of the PLAY Key
within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
14
Garmin G1000® Cockpit Reference Guide for the Cessna CitationJet Model 525
190-01130-00 Rev. A
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