This manual reflects the operation of System Software version 0764.06 or later for the Cirrus SR20,
SR22 and SR22TN. 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.
Perspective® is a registered trademark of Cirrus Design Corporation.
Garmin® is a registered trademarks of Garmin Ltd. or its subsidiaries. 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.
July, 2009 190-00821-03 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 Perspective®GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the 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 Perspective® PFD
or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the Perspective® system must be updated regularly in order to ensure that
the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 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 Perspective® system, as installed in the Cirrus SR20/SR22
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 Perspective® 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, Perspective® 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 Perspective® system utilize GPS as
a precision electronic NAVigation AID (NAVAID). Therefore, as with all
NAVAIDs, information presented by the Perspective® 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 Perspective® Pilot’s Guide documentation and
the Cirrus SR20/SR22 Airplane Flight Manual. Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the Perspective® 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
Perspective® 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.”
190-00821-03 Rev. A
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
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).
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 Perspective® 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 Perspective® panel and displays, are subject to change and
may not reflect the most current Perspective® system and aviation databases.
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.
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
Warnings, Cautions & Notes
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 Perspective® system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found in
the Perspective® Pilot’s Guide for this aircraft.
190-00821-03 Rev. A
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Warnings, Cautions & Notes
Blank Page
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
Record of Revisions
Part NumberChange Summary
190-00821-00
Rev A
Initial release
Rev B
Rev C
Made clerical changes
Made clerical changes to pages 8 and 91
190-00821-01Added Enhanced Vision System
Added changes in page navigation
Added new procedures for creating user waypoints
Added importing and exporting flight plans
Updated Warning Alerts, Caution Alerts, and Advisory Annunciations
Added new XM Weather product symbols
Added other GDU 9.10 parameters
INDEX .........................................................................................................................................Index-1
190-00821-03 Rev. Aiii
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Table of Contents
Blank Page
iv
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 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.
CHANGE NAVIGATION SOURCES
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
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
the CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
190-00821-03 Rev. A1
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Flight Instruments
GENERIC TIMER
Flight
1)
InstrumentsEIS
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
Nav/Com/
XPDR/AudioAFCSGPS Nav
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 V-SPEED BUGS
NOTE: V-speed values cannot be adjusted on SR22TN.
Flight
PlanningProcedures
1)
Press the TMR/REF Softkey.
2)
Turn the
3)
Use the small FMS Knob to change the V-speed in 1-kt increments. Vx
large
FMS Knob to highlight the desired V-speed.
may be adjusted up to 89 knots and Vy may be adjusted down to 89 knots.
Vglide and Vrotate cannot be adjusted. When a speed has been changed
Hazard
Avoidance
from a default value, an asterisk appears next to the value.
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
Features
Additional
Abnormal
Operation
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.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
AlertsAppendixIndex
Annun/
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.
2
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
Flight Instruments
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
DISPLAYING WIND DATA
1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data below the Selected Heading.
3)
Press the OPTN 1 or OPTN 2 Softkey to change how wind data is
displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
190-00821-03 Rev. A3
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Flight Instruments
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
4
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
ENGINE INDICATION SYSTEM
EIS
InstrumentsEIS
Flight
10
1
2
3
4
5
6
7
8
9
10
1
2
3
4
5
6
7
8
9
12
10
1
XPDR/AudioAFCSGPS Nav
2
3
4
5
6
7
8
9
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
11
SR20
1
Percent Power Indicator
2
Tachometer
3
Manifold Pressure
4
Gallons Used Indicator
5
Fuel Flow Indicator
190-00821-03 Rev. A5
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
11
6
Oil Temperature
7
Oil Pressure
8
Ammeter
9
Voltmeter
10
Cylinder Head
Temperature
SR22
11
SR22TN
11
Exhaust Gas
Temperature
Exhaust Gas
Temperature/Turbine
Inlet Temperature
(SR22TN)
12
Target Cruise Power
Fuel Flow
Operation
Abnormal
Annun/
AlertsAppendixIndex
EIS
ENGINE PAGE
Flight
Pressing the ENGINE Softkey accesses the EIS - Engine Page, which displays all
InstrumentsEIS
engine, fuel, fuel calculation, electrical, and air data information. Pressing the FUEL
Softkey accesses the second-level softkeys.
13245
Nav/Com/
XPDR/AudioAFCSGPS Nav
9
Flight
PlanningProcedures
(SR20)
Hazard
Avoidance
13245
6
7
8
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
6
9
7
10
8
(SR22)
6
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
EIS
9
10
11
1
Percent Power
Indicator
2
Tachometer
3
Manifold Pressure
4
Fuel Flow Indicator
13245
(SR22TN)
5
Oil Temperature
6
Electrical Group
7
Fuel Calculation
Group
8
Air Data
9
Engine Temperature
Group
10
TKS FIKI or TKS
NH Fluid Quantity
(optional)
11
Oxygen Pressure
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
6
7
8
PlanningProcedures
Flight
Avoidance
Hazard
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and
are calculated from the last time the fuel was reset.
Adjusting the fuel totalizer quantity:
1)
Press the ENGINE Softkey to display the Engine Page.
2)
Press the FUEL Softkey to access the Initial Usable Fuel Page.
3)
Turn the small FMS Knob increase or decrease the initial usable fuel
displayed.
190-00821-03 Rev. A7
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Flight
EIS
Calculated
InstrumentsEIS
Set Fuel
Remaining
Calculated
Range
Fuel Used
Calculated Time
Remaining
Calculated
Economy
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
Fuel Calculations Group
Full Fuel (SR20)
Initial Usable Fuel Page
AlertsAppendixIndex
Annun/
Fuel to TABS (SR22)
Initial Usable Fuel Page
8
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
EIS
Leaning Assist Mode
NOTE: The pilot should follow the engine manufacturer’s recommended
leaning procedures in the Pilot’s Operating Handbook (POH).
Accessing Leaning Assist Mode:
1)
Press the ENGINE Softkey to display the Engine Page.
2)
Press the ASSIST Softkey to identify peaks.
When the ASSIST Softkey is pressed, the system initially highlights the number
and places a light blue box around the EGT readout of the cylinder with the hottest
EGT. The ∆ Peak temperature is the difference between the peak temperature and the
present temperature for the peaked cylinder. When the first peak is detected, “1st” is
annunciated below that cylinder’s EGT bar and the temperature is enclosed in a light
blue box.
The system continues to detect peak EGTs for each cylinder lean of peak as the
fuel flow is decreased, and the peak of each cylinder’s EGT is indicated by a light blue
marker on the graph. Once all cylinders are lean of peak, the last cylinder to peak is
denoted by the “Last” annunciation below its bar on the graph.
Light Blue Box
Represents Peak
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Temperature
Deviation
from Peak
Leaning Assist Mode
190-00821-03 Rev. A9
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
EIS
TKS FIKI Anti-ice System
Flight
In the default tank selection mode (AUTO), the system assures the fluid level in
InstrumentsEIS
the two tanks is kept relatively even by periodically closing the tank with the lowest
level. The system uses the TKS fluid tank quantity to control the tank shut-off valves.
When the system is on and operating in AUTO mode, the shut-off valves close under
the following conditions:
Manual tank mode allows the pilot to control either tank’s shut-off valve. Manual
may be selected by pressing the ANTI-ICE Softkey to access the second-level softkeys
Flight
LEFT, AUTO, and RIGHT.
PlanningProcedures
• LEFT Softkey – opens left tank valve and closes right tank valve
• AUTO Softkey – returns to AUTO tank mode
• RIGHT Softkey – opens right tank valve and closes left tank valve
While operating in manual tank mode, only the selected/open tank’s quantity is
used for the range and endurance calculations.
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
10
Manual Tank Mode (Left tank selected)
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
EIS
The TKS FIKI system consists of various operating modes, which are presented on
the Perspective® system. A white box highlights the active mode. Descriptions of the
various modes are listed in the following table:
Operating ModeSystem OperationComments
OFFSystem OffNo modes selected
NORMALBoth pumps operate on a timed,
repeating cycle – 30 seconds ON
Provides 50% flow rate for light/
moderate icing
and 90 seconds OFF
HIGHA single primary pump (#1)
operates continuously
MAX
(momentary)
Both primary pumps operate
continuously for 120 seconds
Provides 100% flow rate for
moderate icing
Provides 200% flow rate for severe
icing or to expedite the removal of
previous ice buildup
PUMP BKUPA single primary pump (#2)
operates continuously
This mode is used in the event of a
timer box failure or when BKUP mode
is selected. Pump #2 provides 100%
flow rate, bypassing the timer box
Refer to the AFM for pilot recommeneded actions
SYSTEM DISPLAY
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and
are calculated from the last time the fuel was reset.
NOTE: Refer to the Pilot’s Operating Handbook (POH) for limitations.
Accessing the EIS System Display:
1)
Press the ENGINE Softkey.
2)
Press the SYSTEM Softkey.
3)
To return to the default Engine Display, press the ENGINE or BACK
Softkey.
190-00821-03 Rev. A11
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
EIS
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
1
2
3
4
5
1
2
3
4
5
1
2
3
4
5
Blank Page
6
6
6
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
1
Percent Power
Indicator
2
Tachometer
3
Manifold Pressure
4
Fuel Calculation
Group
12
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
SR20
SR22
5
Electrical Group
6
Miscellaneous
‘Anti-Ice Gal’ and
‘Oxy PSI’ are optional
on the SR22TN
SR22TN
190-00821-03 Rev. A
NAV/COM/TRANSPONDER/AUDIO PANEL
DME TUNING
1)
Press the DME Softkey.
2)
Turn the large FMS Knob 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.
ENTER A TRANSPONDER CODE
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
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.
Or
:
1)
Press the XPDR Key on the PFD/MFD Control Unit to select the transponder
function.
2)
Enter a Code with the Numeric Keypad or FMS Knob on the PFD/MFD
Control Unit. Five seconds after the fourth digit has been entered, the
transponder code becomes active.
SELECTING A COM RADIO
Nav/Com/XPDR/Audio Panel
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Transmit/Receive
Press the COM1 MIC, COM2 MIC
, or
COM3 MIC Key (optional COM
radio, if installed) on the audio panel.
Receive Only
Press the COM1, COM2
the audio panel.
190-00821-03 Rev. A13
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
, or
COM3 Key (optional COM radio, if installed) on
AlertsAppendixIndex
Annun/
Nav/Com/XPDR/Audio Panel
SELECTING A NAV RADIO
Flight
1)
InstrumentsEIS
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
Nav/Com/
NAV/COM TUNING
XPDR/AudioAFCSGPS Nav
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
enters kHz.
2)
Press the appropriate Frequency Transfer Key to place the frequency into
the active frequency field.
Or
:
Flight
1)
PlanningProcedures
Press the COM or NAV Key on the PFD/MFD Control Unit to select the
desired COM or NAV frequency box.
2)
Turn the FMS/XPDR COM/NAV Knob to tune the desired frequency (large
knob for MHz; small knob for kHz).
3)
Press the
Hazard
Avoidance
INTERCOM SYSTEM (ICS) ISOLATION
Frequency Transfer
Key to transfer the frequency to the active field.
Press the PILOT and/or COPLT Key on the audio panel to select those isolated
Features
Additional
from hearing the Nav/Com radios and music.
Abnormal
Operation
AlertsAppendixIndex
Annun/
14
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
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