Garmin SR20, SR22 User Manual

Page 1
®
Cirrus SR20 & SR22
Integrated Avionics System
Cockpit Reference Guide
System Software 0764.06 or later
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Page 3
FLIGHT INSTRUMENTS
EIS
NAV/COM/TRANSPONDER/AUDIO PANEL
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Page 4
Page 5
Copyright © 2008, 2009 Garmin Ltd. or its subsidiaries. All rights reserved.
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.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
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.
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.
Page 6
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
Page 7
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.”
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Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Page 8
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
Page 9
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.
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Warnings, Cautions & Notes
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Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
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Record of Revisions
Part Number Change Summary
190-00821-00
Rev A
Initial release
Rev B
Rev C
Made clerical changes
Made clerical changes to pages 8 and 91
190-00821-01 Added 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
190-00821-02 Added SR20 engine display operation
Added FIKI Anti-icing system GDU 9.12
190-00821-03 Added AOPA Airport Directory
Added dual navigation database capability Added database synchronization Added GDU 10.0 parameters
Revision Date of Revision Affected Pages Description
A July, 2009 All Production release
190-00821-03 Rev. A RR-1
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Record of Revisions
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RR-2
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Table of Contents
FLIGHT INSTRUMENTS ................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting ...................................................... 1
Selecting Standard Barometric Pressure ............................................................................. 1
Change Altimeter Barometric Pressure Setting Units ...................................................... 1
Change Navigation Sources ................................................................................................... 1
Enable/Disable OBS Mode While Navigating with GPS .................................................... 1
Generic Timer ............................................................................................................................. 2
Configure V-speed Bugs ........................................................................................................... 2
Set Barometric Minimum Descent Altitude ........................................................................ 2
Displaying Wind Data ..............................................................................................................3
ENGINE INDICATION SYSTEM ................................................................................................. 5
Engine Page................................................................................................................................ 6
System Display ........................................................................................................................ 11
NAV/COM/TRANSPONDER/AUDIO PANEL ....................................................................... 13
DME Tuning............................................................................................................................... 13
Enter a Transponder Code..................................................................................................... 13
Selecting a COM Radio .......................................................................................................... 13
Selecting a NAV Radio ........................................................................................................... 14
NAV/COM Tuning ..................................................................................................................... 14
Intercom System (ICS) Isolation .......................................................................................... 14
Digital Clearance Player ........................................................................................................ 15
AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................................... 17
GFC 700 AFCS ........................................................................................................................... 17
S-TEC Fifty Five X Autopilot (Optional) .............................................................................. 20
GPS NAVIGATION ........................................................................................................................ 21
Direct-to Navigation .............................................................................................................. 21
Activate a Stored Flight Plan ............................................................................................... 22
Activate a Flight Plan Leg ..................................................................................................... 22
Stop Navigating a Flight Plan .............................................................................................. 23
Vertical Navigation (VNAV)................................................................................................... 23
FLIGHT PLANNING ...................................................................................................................... 27
Trip Planning ............................................................................................................................ 27
Create a New User Waypoint Defined by Latitude & Longitude ................................. 29
Create a New User Waypoint Defined by Radials from Other Waypoints ................. 29
Create a New User Waypoint Defined by a Radial & Distance from Another
Waypoint .............................................................................................................................. 31
Delete a User Waypoint ......................................................................................................... 32
Create a New Flight Plan ...................................................................................................... 33
Import a Flight Plan from an SD Card ................................................................................ 34
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Table of Contents
Insert a Waypoint in the Active Flight Plan ...................................................................... 35
Enter an Airway in a Flight Plan .......................................................................................... 35
Invert An Active Flight Plan .................................................................................................. 36
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 36
Store a Flight Plan .................................................................................................................. 37
Edit a Stored Flight Plan ....................................................................................................... 37
Delete a Waypoint from the Flight Plan ............................................................................ 37
Invert and Activate a Stored Flight Plan ........................................................................... 38
Copy a Flight Plan ................................................................................................................... 38
Delete a Flight Plan ................................................................................................................ 38
Graphical Flight Plan Creation ............................................................................................. 39
Export a Flight Plan to an SD Card ..................................................................................... 39
PROCEDURES ................................................................................................................................. 41
Load and Activate a Departure Procedure ....................................................................... 41
Activate A Departure Leg ..................................................................................................... 41
Load An Arrival Procedure .................................................................................................... 41
Activate An Arrival Leg ......................................................................................................... 42
Load and/or Activate an Approach Procedure ................................................................. 42
Activate An Approach in the Active Flight Plan ............................................................... 43
Activate a Vector to Final Approach Fix ............................................................................ 43
Activate A Missed Approach in the Active Flight Plan ................................................... 44
HAZARD AVOIDANCE ................................................................................................................45
Customizing the Hazard Displays on the Navigation Map ............................................ 45
STORMSCOPE® (Optional) ..................................................................................................... 45
XM Weather (Optional) .......................................................................................................... 47
Traffic Advisory Systems ....................................................................................................... 48
Terrain And Obstacle Proximity ........................................................................................... 50
Terrain-SVS ............................................................................................................................... 51
Terrain Awareness & Warning System (TAWS) Display ................................................... 52
ADDITIONAL FEATURES ........................................................................................................... 55
Synthetic Vision ....................................................................................................................... 55
Enhanced Vision System ........................................................................................................ 56
Terminal Procedure Charts ...................................................................................................57
AOPA Airport Directory ......................................................................................................... 59
XM® Radio Entertainment..................................................................................................... 60
Electronic Checklists .............................................................................................................. 62
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Table of Contents
ABNORMAL OPERATION..........................................................................................................65
Reversionary Mode ................................................................................................................ 65
Abnormal COM Operation .................................................................................................... 65
Hazard Displays with Loss of GPS Position ....................................................................... 65
Unusual Attitudes ................................................................................................................... 66
Dead Reckoning ...................................................................................................................... 67
ANNUNCIATIONS & ALERTS ................................................................................................... 69
WARNING Alerts ...................................................................................................................... 69
CAUTION Alerts ........................................................................................................................ 70
Advisory Annunciations......................................................................................................... 71
Comparator Annunciations ................................................................................................... 72
Reversionary Sensor Annunciations (SR22 Only) ............................................................. 72
Message Advisory Alerts ....................................................................................................... 72
GFC 700 AFCS Alerts ...............................................................................................................73
Terrain-SVS Alerts ................................................................................................................... 74
Terrain-SVS System Status Annunciations ........................................................................ 74
TAWS Alerts .............................................................................................................................. 75
Aural Alerts .............................................................................................................................. 77
CO Guardian Messages (Optional) ...................................................................................... 77
MFD & PFD Message Advisories .......................................................................................... 77
Database Message Advisories ............................................................................................. 79
GMA 347 Message Advisories .............................................................................................. 81
GIA 63W Message Advisories ............................................................................................... 82
GEA 71 Message Advisories .................................................................................................. 84
GTX 32 & GTX 33 Message Advisories ................................................................................ 85
GRS 77 Message Advisories .................................................................................................. 85
GMU 44 Message Advisories ................................................................................................ 87
GDL 69/69A Message Advisories .........................................................................................87
GDC 74A Message Advisories ............................................................................................... 88
GCU 478 Message Advisories ............................................................................................... 88
GMC 705 Message Advisories .............................................................................................. 89
Miscellaneous Message Advisories ..................................................................................... 89
Flight Plan Import/Export Messages .................................................................................. 93
APPENDIX ....................................................................................................................................... 95
PFD Softkey Map .................................................................................................................... 95
MFD Softkey Map ................................................................................................................. 100
Dual Navigation Databases ................................................................................................ 103
Automatic Database Synchronization ............................................................................. 103
INDEX .........................................................................................................................................Index-1
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190-00821-03 Rev. A
Page 17

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

Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
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.
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Operation
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Annun/
Alerts Appendix Index
Page 18
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
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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.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
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Annun/
Alerts Appendix Index
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Flight Instruments
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
4
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Page 21

ENGINE INDICATION SYSTEM

EIS
Instruments EIS
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/Audio AFCS GPS Nav
2
3
4
5
6
7
8
9
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
11
SR20
1
Percent Power Indicator
2
Tachometer
3
Manifold Pressure
4
Gallons Used Indicator
5
Fuel Flow Indicator
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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/
Alerts Appendix Index
Page 22
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.
1 32 4 5
Nav/Com/
XPDR/AudioAFCSGPS Nav
9
Flight
PlanningProcedures
(SR20)
Hazard
Avoidance
1 32 4 5
6
7
8
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
6
9
7
10
8
(SR22)
6
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EIS
9
10
11
1
Percent Power Indicator
2
Tachometer
3
Manifold Pressure
4
Fuel Flow Indicator
1 32 4 5
(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
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
6
7
8
Planning Procedures
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.
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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
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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
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Temperature Deviation from Peak
Leaning Assist Mode
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Page 26
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:
Nav/Com/
• Theleftandrighttanktanklevelimbalanceisgreaterthan0.25gallons(low
XPDR/AudioAFCSGPS Nav
tankwillbecloseduntillevelbalanceiswithin0.15gallons)
• The uid quantity is empty (indicated from the uid level sensor and level
switch)
• Theuidquantityisunreliable(amiscomparebetweenthelevelsensorandlevel
switch or an out of range level sensor value)
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
Page 27
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 Mode System Operation Comments
OFF System Off No modes selected
NORMAL Both pumps operate on a timed,
repeating cycle – 30 seconds ON
Provides 50% flow rate for light/ moderate icing
and 90 seconds OFF
HIGH A 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 BKUP A 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

Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
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.
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Additional
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Alerts Appendix Index
Page 28
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
Page 29

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
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
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. A 13
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
, or
COM3 Key (optional COM radio, if installed) on
Alerts Appendix Index
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Page 30
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
Page 31
PILOT KEY
Annunciator
OFF OFF
ON OFF
OFF ON
ON ON
COPLT KEY
Annunciator
Pilot Hears
Selected radios, aural alerts, pilot, copilot, passengers, music
Selected radios, aural alerts, pilot
Selected radios, aural alerts, pilot; passengers, music
Selected radios, aural alerts, pilot, copilot
Nav/Com/XPDR/Audio Panel
Copilot
Hears
Passenger Hears
Selected radios, aural alerts, pilot, copilot, passengers,
Selected radios, aural alerts, pilot, copilot, passengers, music
music Copilot,
passengers, music
Copilot, passengers, music
Selected radios,
Copilot
aural alerts, pilot, passengers, music
Selected radios, aural alerts, pilot,
Passengers, music
copilot
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
ICS Isolation Modes

DIGITAL CLEARANCE PLAYER

NOTE: Only the audio for the selected
COM MIC
Key is recorded. Audio is
not recorded for COM3 MIC.
• PressingthePLAY Key once plays the latest recorded memory block, then returns to normal operation.
• PressingtheMKR/MUTE Key while playing a memory block stops play.
• Pressingthe PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block.
190-00821-03 Rev. A 15
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Annun/
Alerts Appendix Index
Page 32
Nav/Com/XPDR/Audio Panel
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
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190-00821-03 Rev. A
Page 33

AUTOMATIC FLIGHT CONTROL SYSTEM

GFC 700 AFCS

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 autopilot 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 flight director in the listed modes.
Control Pressed
Lateral Vertical FD Key Roll Hold (default) ROL Pitch Hold (default) PIT AP Key Roll Hold (default) ROL Pitch Hold (default) PIT
GA Switch Go Around GA Go Around GA
A LT Key Roll Hold (default) ROL Altitude Hold A LT
VS Key Roll Hold (default) ROL Vertical Speed VS
VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH
NAV Key Navigation**
APR Key Approach**
HDG Key Heading Select HDG Pitch Hold (default) PIT
LV L Key Level Hold LVL Level Hold LV L
Modes Selected
GPS
VOR
LOC
Pitch Hold (default) PIT
BC
GPS
VOR
LOC
Pitch Hold (default)
Glidepath
Glideslope
AFCS
PIT GP GS
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
*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.
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Page 34
AFCS
Vertical Modes
Flight
InstrumentsEIS
Vertical Mode Description Control Annunciation
Holds the current aircraft pitch attitude;
Pitch Hold
Nav/Com/
XPDR/AudioAFCSGPS Nav
Selected Altitude Armed
Altitude Hold Holds the current Altitude Reference ALT Key A LT nnnnn f T
Vertical Speed
VNAV
Flight
PlanningProcedures
VNAV Target Altitude Armed
Glidepath
Hazard
Avoidance
Glideslope
Features
Additional
Takeoff
Abnormal
Operation
Go Around
AlertsAppendixIndex
Annun/
Level Hold
* ALTS armed automatically when PIT, VS, or GA active, and under VPTH when Selected Altitude is
to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
may be used to climb/descend to the Selected Altitude
AFCS armed to capture the altitude displayed in the Selected Altitude window
Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude
Captures and tracks the VNAV flight path
AFCS armed to capture the altitude displayed in the VNAV Target Altitude window
Captures and tracks the WAAS glidepath on approach
Captures and tracks the ILS glideslope on approach
Commands constant pitch angle and wings level on ground in preperation for takeoff.
Disengages the autopilot and commands a constant pitch attitude and wings level
Engages the autopilot and levels the aircraft in pitch and roll attitudes.
(default) PIT
* ALTS
VS Key VS nnnn f p m
VNV
Key
** ALTV
APR Key
GA
Switch
LV L Key LV L
VPTH
GP
GS
TO
GA
18
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-03 Rev. A
Page 35
AFCS
Lateral Modes
Lateral Mode Description Control Annunciation
Holds current aircraft roll attitude
Roll Hold
Heading Select Captures and tracks Selected Heading
Navigation, GPS Arm/Capture/Track
Navigation, VOR Enroute Arm/ Capture/Track
Navigation, LOC Arm/Capture/Track (No Glideslope)
Navigation Backcourse
Capture/Track Approach, GPS
Arm/Capture/Track Approach, VOR
Arm/Capture/Track Approach, ILS Arm/
Capture/Track (Glideslope Mode automatically armed)
Takeoff
Go Around
Level Hold
or rolls wings level, depending on commanded bank angle
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)
Commands constant pitch angle and wings level on ground in preperation for takeoff.
Disengages autopilot and commands a constant pitch angle and wings level
Engages the autopilot and levels the aircraft in pitch and roll attitudes.
(default) ROL
HDG
Key
HDG
GPS
VOR
NAV
Key
LOC
BC
GPS
VAPP
APR Key
LOC
TO
GA
Switch
GA
LV L Key LVL
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
190-00821-03 Rev. A 19
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Page 36
AFCS
Level
Flight
Pressing the LV L Key engages the autopilot and levels the aircraft in pitch (to arrest
InstrumentsEIS
a climb or descent) and roll. No other lateral or vertical modes are engaged, therefore, the aircraft will not hold a course or heading and will not hold a selected altitude.

S-TEC FIFTY FIVE X AUTOPILOT (OPTIONAL)

Nav/Com/
XPDR/AudioAFCSGPS Nav
NOTE: This status annunciation is not analogous to both Perspective® and the
S-TEC Fifty Five X. Refer to the approved S-TEC Fifty Five X Pilot’s Operating Handbook (POH) for comprehensive list of annunciations and operating instructions.
In addition to the status and mode annunciations that are simultaneously displayed on both the Perspective® system AFCS Status Box and the S-TEC Fifty Five X Autopilot Display and/or Remote Annunciator Display, the Perspective® sysetm displays an
Flight
additional status annunciation of ‘AP’ when the autopilot is engaged. This provides the
PlanningProcedures
pilot with a dedicated annunciation showing the status of the autopilot engagement.
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
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20
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190-00821-03 Rev. A
Page 37

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation using the MFD
1)
Press the Direct-to
2)
Enter the 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. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 9.
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 (-) the waypoint.
11)
Press the ENT Key. The ‘Activate?’ field is highlighted.
12)
Press the ENT Key to activate.
( )
Key on the Control Unit.
GPS Navigation
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Direct-to Navigation using 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 ‘ALT’ altitude field.
190-00821-03 Rev. A 21
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
( )
on the PFD.
Operation
Abnormal
Annun/
Alerts Appendix Index
Page 38
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav

ACTIVATE A STORED FLIGHT PLAN

Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
10)
Press the ENT Key. The cursor is placed in the ‘OFFSET’ 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 ‘CRS’ 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 Key again to activate the Direct-to.
1)
Press the FPL Key on the Control Unit 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)
Press 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

Abnormal
Operation
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
AlertsAppendixIndex
Annun/
and turn the large FMS Knob to highlight the desired waypoint.
2)
Press the ACT LEG Softkey.
OR
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.
3)
With ‘Activate’ highlighted, press the ENT Key.
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Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
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Page 39
GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)
Press the FPL Key on the Control Unit 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 (VNAV)

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
Small Light
Blue Text
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Small Light
Blue Subdued
Text
Small White Text
with Altitude
Restriction Bar
Cross AT or ABOVE 5,000 ft
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
190-00821-03 Rev. A 23
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Additional
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Operation
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Annun/
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Page 40
GPS Navigation
Altitudes associated with approach procedures are “auto-designated”. This means
the system automatically uses the altitudes loaded with the approach for giving vertical
Flight
InstrumentsEIS
flight path guidance outside the FAF. Note these altitudes are displayed as small light blue text.
Altitudes associated with arrival procedures are “manually-designated”. This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot. Note that these altitudes are initially displayed as white text. These altitudes may be “designated” by placing the
Nav/Com/
XPDR/AudioAFCSGPS Nav
cursor over the desired altitude and pressing the ENT Key. After designation, the text changes to light blue.
Altitudes that have been designated for use in vertical navigation 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 flight path 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.
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
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24
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190-00821-03 Rev. A
Page 41
GPS Navigation
White Text Light Blue Text Light Blue
Subdued Text
Instruments EIS
Flight
Large Text
Small Text
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 flight path guidance.
Altitude is not designated to be used in determining vertical flight path guidance. Altitude has been retrieved from the navigation database and is provided as a reference.
Altitude has been entered by the pilot. Altitude is designated for use in giving vertical flight path. Altitude does not match the published altitude in navigation database or no published altitude exists.
Altitude is designated for use in giving vertical flight path 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 flight path guidance.
The system cannot use this altitude in determining vertical flight path guidance.
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
190-00821-03 Rev. A 25
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GPS Navigation
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
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Features
Additional
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Operation
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Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
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Page 43

TRIP PLANNING

1)
Turn the large FMS Knob on the Control Unit to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the Trip Planning Page.
3)
The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL Softkey.
4)
For Direct-to planning:
a)
Press the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position).
b)
If necessary, press the MENU Key on the Control Unit and select ‘Set WPT to Present Position’ to display ‘P.POS’.
c)
Press the ENT Key and the flashing cursor moves to the ending waypoint field.
d)
Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint.
Or:
For point-to-point planning:
a)
Enter the identifier of the starting waypoint.
b)
Once the waypoint’s identifier is entered, press the ENT Key to accept the waypoint. The flashing cursor moves to the ending waypoint.
c)
Again, enter the identifier of the ending waypoint.
d)
Press the ENT Key to accept the waypoint.
Or:
For flight plan leg planning:
a)
Press the FPL Softkey (at the bottom of the display).
b)
Turn the small FMS Knob to select the desired flight plan (already stored in memory), by number.
c)
Turn the large FMS Knob to highlight the ‘LEG’ field.
d)
Turn the 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.

FLIGHT PLANNING

Flight Planning
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
190-00821-03 Rev. A 27
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
Page 44
Flight Planning
Flight
InstrumentsEIS
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
6)
Enter the departure time. Press the ENT Key when finished. Departure time may be entered in local or UTC time, depending upon system settings.
7)
The flashing cursor moves to the ground speed (GS) field. Enter the ground speed. Press the mode, ground speed is provided by the system.
8)
The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow is provided by the system.
9)
The flashing cursor moves to the fuel onboard field. Enter the fuel onboard. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel onboard is provided by the fuel totalizer.
10)
The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
11)
The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, altitude is provided by the system.
12)
The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered on the PFD.
13)
The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, air temperature is provided by the system outside air temperature.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan.
NOTE: The page mode must be set to ‘MANUAL’ to perform the following steps.
NOTE: The departure time on the Trip Planning Page is used for preflight planning. Refer to the Utility Page for the actual flight departure time.
ENT
Key when finished. Note that in ‘automatic’ page
28
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190-00821-03 Rev. A
Page 45
Flight Planning

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.
a)
Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.
b)
Press the ENT Key to place a check-mark in the box.
7)
The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob to display a list of waypoint types.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER
WAYPOINTS
1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.
a)
Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.
b)
Press the ENT Key to place a check-mark in the box.
Instruments EIS
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7)
The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob
Flight
InstrumentsEIS
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XPDR/AudioAFCSGPS Nav
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Features
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Operation
AlertsAppendixIndex
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to display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
10)
The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:
a)
b)
c)
Or:
a)
b)
c)
d)
Or:
a)
b)
c)
d)
Or:
a)
b)
c)
d)
11)
Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
Turn the small FMS Knob to the right to display the ‘NRST’ waypoints to the aircraft’s current position.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
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Flight Planning
12)
Press the ENT Key.
13)
Repeat step 10 to enter the next waypoint name.
14)
Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
15)
Press the ENT Key.
16)
Press the FMS Knob to remove the flashing cursor.
CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7.
a)
Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’.
b)
Press the ENT Key to place a check-mark in the box.
7)
The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob to display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/DIS (radial/distance).
9)
Press the ENT Key.
10)
The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows:
a)
When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints.
b)
Turn the large FMS Knob to select the desired waypoint.
c)
Press the ENT Key.
Or:
Instruments EIS
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a)
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Operation
b)
c)
d)
Or:
a)
b)
c)
d)
Or:
a)
b)
c)
d)
11)
Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
12)
Press the ENT Key.
13)
The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
14)
Press the ENT Key.
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
Turn the small FMS Knob to the right to display the ‘NRST’ waypoints to the aircraft’s current position.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Turn the large FMS Knob to select the desired waypoint.
Press the ENT Key.
15)
Press the FMS Knob to remove the flashing cursor.
AlertsAppendixIndex
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DELETE A USER WAYPOINT

1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
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Flight Planning
4)
Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’ field.
5)
Turn the small FMS Knob to highlight the desired waypoint.
6)
Press the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With ‘YES’ highlighted, press the ENT Key.

CREATE A NEW FLIGHT PLAN

NOTE: When creating a new flight plan in the Active Flight Plan Window,
the first leg is activated automatically after it is created.
Using the MFD
1)
Press the FPL Key on the Control Unit.
2)
Turn the small FMS Knob to display the Flight Plan Catalog Page.
3)
Press the NEW Softkey to display a blank flight plan for the first empty storage location.
4)
Turn the small FMS Knob to display the Waypoint Information Window.
5)
Enter the identifier of the departure waypoint.
6)
Press the ENT Key.
7)
Repeat step number 4, 5, and 6 to enter the identifier for each additional flight plan waypoint.
Instruments EIS
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XPDR/Audio AFCS GPS Nav
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Planning Procedures
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Avoidance
Hazard
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Features
8)
When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list.
Using the PFD
NOTE: If a flight plan is active, an additional flight plan cannot be entered
using the PFD.
1)
Press the FPL Key on the PFD.
2)
Turn the small FMS Knob on the PFD to display the Waypoint Information Page.
3)
Turn the small FMS Knob to enter the first letter of the destination waypoint identifier.
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Flight Planning
4)
Turn the large FMS Knob to the right to move the cursor to the next character
Flight
InstrumentsEIS
position.
5)
Repeat step 3 and 4 to spell out the rest of the waypoint identifier.
6)
Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint.
7)
Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint.
Nav/Com/
XPDR/AudioAFCSGPS Nav
8)
Once all waypoints have been entered, press the FMS Knob to remove the cursor. The new flight plan is now active.

IMPORT A FLIGHT PLAN FROM AN SD CARD

NOTE: See the Annunciations & Alerts section for flight plan import message
descriptions.
1)
Flight
PlanningProcedures
Insert the SD card containing the flight plan in the top card slot on the MFD.
2)
Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
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34
4)
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Press the IMPORT Softkey.
If an empty flight plan is selected, a list of the available flight plans on the SD card will be displayed.
Or:
If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card. If overwriting the existing flight plan is not desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select another existing or empty flight plan, and again press the IMPORT Softkey.
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key.
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Flight Planning

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

1)
Press the FPL Key on the Control Unit to display the active flight plan.
2)
If necessary, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The new waypoint is inserted before the highlighted waypoint.
4)
Turn the small FMS Knob. The Waypoint Information Window is now displayed.
5)
Enter the new flight plan waypoint by one of the following:
a)
Enter the user waypoint identifier, facility, or city.
b)
Press the ENT Key.
Or:
a)
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
b)
Turn the small FMS Knob to the right to display the ‘NRST’ airport waypoints to the aircraft’s current position.
c)
Turn the large FMS Knob to select the desired waypoint.
d)
Press the ENT Key.
Or:
a)
Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed.
b)
Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints.
c)
Turn the large FMS Knob to select the desired waypoint.
d)
Press the ENT Key.
e)
Press the ENT Key again to “accept” the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

Instruments EIS
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1)
Press the FPL Key on the Control Unit.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not a valid airway entry point, a valid entry point should be entered at this time.
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4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Flight
InstrumentsEIS
Softkey, or press the MENU Key and select “Load Airway” (required on the PFD). The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when an acceptable airway entry waypoint has been chosen (the waypoint ahead of the cursor position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the
Nav/Com/
XPDR/AudioAFCSGPS Nav
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the new airway inserted.

INVERT AN ACTIVE FLIGHT PLAN

Flight
1)
PlanningProcedures
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
4)
Press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location.
Hazard
Avoidance
5)
With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
PLAN
1)
Press the FPL Key to display the active flight plan. Press the FMS Knob to activate the cursor.
Or, for a stored flight plan:
a)
Press the FPL Key on the Control Unit and turn the small FMS Knob to select the Flight Plan Catalog Page.
b)
Press the FMS Knob to activate the cursor.
c)
Turn the large FMS Knob to highlight the desired flight plan.
d)
Press the EDIT Softkey.
2)
Turn the large FMS Knob to highlight the title for the approach, departure, arrival, or airway to be deleted. Titles appear in white directly above the procedure’s waypoints.
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Flight Planning
3)
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure or airway.

STORE A FLIGHT PLAN

1)
After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key.
2)
Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
3)
With ‘OK’ highlighted, press the ENT Key to store the flight plan.

EDIT A STORED FLIGHT PLAN

1)
Press the FPL Key on the Control Unit 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)
Press the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
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Avoidance
Hazard

DELETE A WAYPOINT FROM THE FLIGHT PLAN

1)
Press the FPL Key to display the active flight plan. Press the FMS Knob to activate the cursor.
Or, for a stored flight plan:
a)
Press the FPL Key on the Control Unit and turn the small FMS Knob to select the Flight Plan Catalog Page.
b)
Press the FMS Knob to activate the cursor.
c)
Turn the large FMS Knob to highlight the desired flight plan.
d)
Press the EDIT Softkey.
2)
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation window.
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4)
With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
Flight
InstrumentsEIS
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
5)
Once all changes have been made, press the FMS Knob to remove the cursor.

INVERT AND ACTIVATE A STORED FLIGHT PLAN

Nav/Com/
XPDR/AudioAFCSGPS Nav
1)
Press the FPL Key on the Control Unit.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
Flight
PlanningProcedures
inverted and activated. The original flight plan remains intact in its flight plan catalog storage location.

COPY A FLIGHT PLAN

1)
Press the FPL Key on the Control Unit.
Hazard
Additional
Avoidance
Features
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is displayed.
Abnormal
Operation
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
AlertsAppendixIndex
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DELETE A FLIGHT PLAN

1)
Press the FPL Key on the Control Unit.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
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5)
Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

GRAPHICAL FLIGHT PLAN CREATION

1)
Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.
2)
Press the Joystick to activate the map pointer. Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan.
3)
The default insertion point is at the end of the flight plan. If the selected waypoint is to be placed anywhere other than the end of the flight plan, press the FMS Knob to activate the cursor. Waypoints are inserted the cursor. Turn the large FMS Knob to select the desired insertion point.
4)
Press the LD WPT Softkey. The selected waypoint is inserted at the selected point. The default user waypoint naming is USR000, USR001, USR002, and so on.
5)
To change the user waypoint name, follow the procedure for modifying a user waypoint.
ABOVE
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Avoidance
Hazard

EXPORT A FLIGHT PLAN TO AN SD CARD

NOTE: See the Annunciations & Alerts section for flight plan export message
descriptions.
1)
Insert the SD card into the top card slot on the MFD.
2)
Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
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PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when the flight plan is active.
Procedures
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Flight

ACTIVATE A DEPARTURE LEG

1)
Press the FPL Key on the Control Unit to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AN ARRIVAL PROCEDURE

1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list of available arrivals.
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Procedures
4)
Turn the large FMS Knob to highlight the desired arrival.
5)
Flight
InstrumentsEIS
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways may be displayed for the selected arrival.
8)
Turn the large FMS Knob to highlight the desired runway.
9)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Press the ENT Key.
10)
With ‘LOAD?’ highlighted, press the ENT Key.
11)
The arrival becomes part of the active flight plan.

ACTIVATE AN ARRIVAL LEG

1)
Press the FPL Key on the Control Unit to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Flight
PlanningProcedures
Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Hazard
Avoidance

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

Features
Additional
NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed in the list of available approaches.
Abnormal
Annun/
Operation
AlertsAppendixIndex
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
3)
Press the ENT Key. A list of available approaches for the destination airport is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach procedure is now displayed.
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Procedures
6)
Turn either FMS Knob to select the desired transition. 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.
7)
Press the ENT Key. The cursor moves to the MINIMUMS field.
8)
If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small
FMS
Knob in the
direction of the green arrow to change the display from OFF to BARO.
9)
Press the
FMS
ENT
Key. The cursor moves to the altitude field. Turn the small
Knob to enter the published DA/MDA for the selected approach
procedure.
10)
Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
11)
Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Selecting ‘LOAD?’ enters the selected approach procedure into the active flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the selected approach procedure into the active flight plan and is immediately activated.
12)
Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

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1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.

ACTIVATE A VECTOR TO FINAL APPROACH FIX

1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
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Procedures

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Or:
Press the go-around button.
5)
After activating the missed approach procedure, another approach procedure may be loaded.
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
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Hazard Avoidance

HAZARD AVOIDANCE

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.
2)
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select ‘Weather’ to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.

STORMSCOPE® (OPTIONAL)

Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
WARNING: The Stormscope is not intended to be used for hazardous
thunderstorm penetration. Weather information on the Perspective® 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 MAP Softkey.
2)
Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page.
Lightning Age Symbol
Strike is less than 6 seconds old
Strike is between 6 and 60 seconds old
Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old
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’.
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
2)
Turn the large FMS Knob to select ‘STRMSCP MODE’.
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Hazard Avoidance
3)
Turn the small FMS Knob to display the ‘Cell/Strike’ window.
4)
Flight
InstrumentsEIS
Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
5)
Push the FMS Knob to return to the Navigation Map Page.
Clear Stormscope Lightning Data from the Navigation Map Page
1)
Press the MENU Key (with the Navigation Map Page displayed).
2)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field and press the ENT Key.
Stormscope Page
Flight
1)
PlanningProcedures
2)
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
1)
2)
Hazard
Avoidance
Features
Additional
Abnormal
Operation
Change the Viewing Mode Between 360˚ and 120˚
1)
AlertsAppendixIndex
Annun/
2)
NOTE:
If heading input 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.
Turn the large FMS Knob until the Map Page group is selected.
Turn the small FMS Knob select the Stormscope Page.
Select the Stormscope Page.
Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed. Press the CELL Softkey to display ‘CELL’ data or press the 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.
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical activity that indicate cells.
Select the Stormscope Page.
Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area.
Press the CLEAR Softkey to remove all Stormscope lightning data from the display.
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Hazard Avoidance

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.
Displaying XM Weather on the Navigation Map Page
1)
Press the MAP Softkey.
2)
Press the NEXRAD
and/or
XM LTNG Softkey to display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page.
Display METAR and TAF information on the Airport Information Page
1)
Turn the large FMS Knob to select the WPT Page Group.
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes).
Displaying Weather on the Weather Data Link Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Press the available softkeys to select the desired XM weather product.
4)
Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Map Panning Information – Weather Data Link Page
1)
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs.
3)
Press the ENT Key to display pertinent information for the selected product.
Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report. Panning over an airport with METAR information does not display more
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Hazard Avoidance
information but allows the user to press the ENT Key and select that
Flight
InstrumentsEIS
Airport’s Information Page to display the text of the report. Pressing the ENT Key when panning over a TFR displays TFR specific information.
Weather Products and Symbols
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
Icing Potential
Nav/Com/
XPDR/AudioAFCSGPS Nav
Turbulence PIREPs
AIREPs
NEXRAD
Cloud Top
Cell Movement
XM Lightning
SIGMETs/AIRMETs

TRAFFIC ADVISORY SYSTEMS

Flight
PlanningProcedures
Traffic Symbol Description
Hazard
Avoidance
Features
Additional
Abnormal
Operation
WARNING: Traffic information shown on the Perspective® 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.
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Proximity Advisory (PA)
(intruder is within 5 nm and less than 1200’ vertical separation)
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
City Forecast
METARs
Cyclone Warnings
Freezing Levels
Surface Analysis
Winds Aloft
County Warnings
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48
Traffic Advisory Off Scale
Traffic Symbol Description
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Hazard Avoidance
Avidyne TAS600 Series Traffic Advisory System (Optional)
Displaying Traffic on the Traffic Map Page
1)
Turn the large
2)
Turn the small
3)
Turn the RANGE Knob clockwise to display a larger area or counter-
FMS
Knob to select the Map Page Group.
FMS
Knob to select the Traffic Map Page.
clockwise to display a smaller area.
5)
Press the MUTE Softkey once to mute TAS voice alerts. Press twice rapidly to replay the last voice alert.
Displaying Traffic on the Navigation Map
1)
Ensure TAS is operating.
2)
With the Navigation Map displayed, press the MAP Softkey.
3)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
L-3 Skywatch HP (SKY497)(Optional)
System Self Test
1)
Set the range to 2/6 nm.
2)
Press the STANDBY Softkey.
3)
Press the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed successfully, traffic symbols display and a voice alert “Traffic Advisory System Test Passed” is heard. If the self test fails, the system reverts to Standby Mode and a voice alert “Traffic Advisory System Test Failed” is heard.
Displaying Traffic on the Traffic Map Page
1)
Turn the large
2)
Turn the small
3)
Press the OPERATE Softkey to begin displaying traffic. OPERATING is displayed in the Traffic mode field.
4)
Press the ALT MODE Softkey to change the altitude volume.
5)
Press the STANDBY Softkey to place the system in the Standby mode. STANDBY is displayed in the Traffic mode field.
6)
Turn the RANGE Knob clockwise to display a larger area or counter­clockwise to display a smaller area.
FMS
Knob to select the Map Page Group.
FMS
Knob to select the Traffic Map Page.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
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Hazard Avoidance
Displaying Traffic on the Navigation Map
Flight
1)
InstrumentsEIS
Ensure TAS is operating.
2)
With the Navigation Map displayed, press the MAP Softkey.
3)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.

TERRAIN AND OBSTACLE PROXIMITY

Nav/Com/
XPDR/AudioAFCSGPS Nav
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Displaying Terrain and Obstacles on the Terrain Proximity Page
1)
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
Turn the large
2)
Turn the small
3)
If desired, press the When the the
360
4)
Rotate the clockwise to display a smaller area.
FMS
Knob to select the Map Page Group.
FMS
Knob to select the Terrain Proximity Page.
VIEW
Softkey to access the
ARC
Softkey is pressed, a radar-like 120° view is displayed. Press
ARC
Softkey to return to the 360° default display.
Joystick
clockwise to display a larger area or rotate counter-
Color Terrain/Obstacle Location
Red
Yellow
Black
Terrain/Obstacle above or within 100’ below current aircraft altitude.
Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.
Terrain/Obstacle is more than 1000’
below aircraft altitude.
and
360
Softkeys.
Displaying Terrain and Obstacles on the Navigation Map
AlertsAppendixIndex
Annun/
1)
With the Navigation Map displayed, press the
2)
50
Press the displayed on the map.
Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
TERRAIN
Softkey. Terrain and obstacle proximity will now be
MAP
Softkey.
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Hazard Avoidance

TERRAIN-SVS

NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS) option is installed and the TAWS option has not been installed.
NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
Display Terrain on the TERRAIN-SVS Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Terrain-SVS Page.
3)
If desired, press the VIEW Softkey to access the ARC and 360 softkeys. When the ARC Softkey is selected, a radar-like 120° view is displayed. Press the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to display a larger area or rotate counter­clockwise to display a smaller area.
Color Terrain/Obstacle Location
Red
Yellow
Black
Terrain/Obstacle above or within 100’ below current aircraft altitude.
Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Enable/Disable Aviation Data
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
1)
While the Terrain-SVS Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
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Hazard Avoidance
Terrain-SVS Inhibit
Flight
Nav/Com/
Inhibit Terrain
InstrumentsEIS
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or
1)
2)
XPDR/AudioAFCSGPS Nav
3)
:
Press the MENU Key.
Turn the small FMS Knob to select ‘Inhibit Terrain’.
Press the ENT Key.
Enable Terrain
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or
:
1)
While the Terrain-SVS Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Enable Terrain’.
3)
Flight
PlanningProcedures
Press the ENT Key.
NOTE: If Terrain-SVS alerts are inhibited when the Final Approach Fix is the
active waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix.
Hazard
Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
NOTE: TAWS operation is only available when the Perspective® system is configured for a TAWS-B installation.
Manual System Test
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Test TAWS System’.
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Hazard Avoidance
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS-B Page.
When all is in working order, “TAWS System Test, OK” is heard.
Display Terrain on the TAWS-B Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, press the VIEW Softkey to access the ARC and 360 softkeys. When the ARC Softkey is selected, a radar-like 120° view is displayed. Press the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to display a larger area or rotate counter­clockwise to display a smaller area.
Color Terrain/Obstacle Location
Red
Yellow
Black
Terrain/Obstacle above or within 100’ below current aircraft altitude.
Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Enable/Disable Aviation Data
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
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TAWS Inhibit
Flight
InstrumentsEIS
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix.
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
Inhibit TAWS
While the TAWS-B Page is displayed, press the INHIBIT Softkey.
Or
:
1)
Press the MENU Key.
2)
Turn the small FMS Knob to select ‘Inhibit TAWS’.
3)
Press the ENT Key.
Enable TAWS
While the TAWS-B Page is displayed, press the INHIBIT Softkey.
Or
:
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Enable TAWS’.
3)
Press the ENT Key.
AlertsAppendixIndex
Annun/
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Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION

WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVS is intended as an aid to situational awareness only and may not provide the accuracy and/or fidelity upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
WARNING: Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing.
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the Perspective® Integrated Avionics System.
SVS is primarily comprised of a computer-generated forward-looking, attitude aligned view of the topography immediately in front of the aircraft from the pilot’s perspective. SVS information is shown on the primary flight display (PFD).
In addition to SVS enhancement to the PFD, the following features have been added to the PFD:
• Pathways
• Flight Path Marker
• Horizon Heading Marks
• Terrain and Obstacle Alerting
• Three-dimensional Traffic
• Airport Signs
• Runway Display
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Displaying SVS Terrain
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
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Additional Features
Displaying Pathways
Flight
Nav/Com/
Flight
Hazard
1)
InstrumentsEIS
XPDR/AudioAFCSGPS Nav
PlanningProcedures
Avoidance
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
Displaying Airport Signs
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.

ENHANCED VISION SYSTEM

Features
Additional
The Perspective® system provides a control and display interface to an Enhanced Vision System. EVS is designed to provide an aid to situational awareness while operating in low visibility environments.
Abnormal
Operation
Accessing the EVS System
AlertsAppendixIndex
Annun/
56
1)
Turn the large FMS Knob to select the AUX Page Group.
2)
Turn the small FMS Knob to select the VIDEO Page.
3)
Pressing the VID ZM + and VID ZM - softkeys switches the EVS display magnification between 1x and 2x.
4)
Pressing the HIDE MAP Softkey removes the map from the display and increases the EVS display to full screen.
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Additional Features
Adjusting the EVS Display
1)
Turn the large FMS Knob to select the AUX Page Group.
2)
Turn the small FMS Knob to select the VIDEO Page.
3)
Press the SETUP Softkey. The EVS display adjustment softkeys are now displayed.
4)
Pressing the CNTRST - and CNTRST + Softkeys adjust display contrast in five percent increments from 0 to 100%.
5)
Pressing the BRIGHT - and BRIGHT + Softkeys adjust display brightness in five percent increments from 0 to 100%.
6)
Pressing the SAT - and SAT + Softkeys adjust display saturation in five percent increments from 0 to 100%.
7)
Pressing the RESET Softkey returns all video adjustments options to the default settings
8)
Press the BACK Softkey to return to the previous softkey level, or after 45 seconds of softkey inactivity, the system reverts to the top level AUX ­VIDEO Page softkeys.

TERMINAL PROCEDURE CHARTS

NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts® in electronic form, it is still advisable to carry another source of charts on-board the aircraft.
SafeTaxi
®
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
SafeTaxi® is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport. The airport display on the map reveals runways with numbers, taxiways identifiers, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and airport identification labels. Pressing the DCLTR Softkey twice removes VOR station ID, the VOR symbol, and intersection names if within the airport plan view. Pressing the DCLTR Softkey a third time removes the airport runway layout, unless the airport in view is part of an active route structure. Pressing the DCLTR Softkey again cycles back to the original map detail.
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Additional Features
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams aid in following ground control instructions by accurately displaying
Flight
InstrumentsEIS
the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and
services.Thisdatabaseisupdatedona56-daycycle.
ChartView
ChartView resembles the paper version of Jeppesen terminal procedures charts. The
charts are displayed in full color with high-resolution. The MFD depiction shows the
Nav/Com/
XPDR/AudioAFCSGPS Nav
aircraft position on the moving map in the plan view of most approach charts and on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database is
notupdatedwithin70daysoftheexpirationdate,ChartView will no longer function.
FliteCharts
®
FliteCharts® resemble the paper version of National Aeronautical Charting Office
(NACO) terminal procedures charts. The charts are displayed with high-resolution
Flight
PlanningProcedures
and in color for applicable charts. Current aircraft position is not displayed on FliteCharts.
The FliteCharts database contains procedure charts for the United States only.
Thisdatabaseisupdatedona28-daycycle. Ifnotupdatedwithin 180daysofthe
expiration date, FliteCharts will no longer function.
Hazard
View Charts from the Navigation Map Page
Avoidance
1)
Press the SHW CHRT Softkey when displayed.
Or
Features
Additional
:
Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.
Abnormal
Operation
2)
Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
AlertsAppendixIndex
Annun/
are only available with ChartView.
3)
Press the GO BACK Softkey to return to the previous page.
View Charts from the Active Flight Plan Page
58
1)
While viewing the Active Flight Plan Page, press the FMS Knob to activate the cursor.
2)
Turn the large FMS Knob to select the departure airport, destination airport, departure, arrival, or approach.
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Additional Features
3)
Press the SHW CHRT Softkey. The appropriate chart is displayed, if available for the item selected.
4)
Press the GO BACK Softkey to return to the previous page.
Change Day/Night View
1)
While viewing a chart press the MENU Key to display the Page Menu OPTIONS.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and press the ENT Key.
3)
Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR SCHEME’ Options.
4)
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen Options.
5)
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’ Options.
6)
In Auto Mode, turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob. The percentage of change is the day/night crossover point based on backlighting intensity.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.

AOPA AIRPORT DIRECTORY

AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT-Airport Information Page.
This database is updated four times per year. Check fly.garmin.com for the current database.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
View Airport Directory Information
While viewing the WPT-Airport Information Page, if necessary, press the INFO-1 Softkey to change the softkey label to display INFO-2. AOPA airport information is displayed on the right half of the display.
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Additional Features

XM® RADIO ENTERTAINMENT

Flight
The XM® Radio Page provides information and control of the audio entertainment
InstrumentsEIS
features of the XM Satellite Radio.
Selecting the XM Radio Page
1)
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Turn the small FMS Knob to select the XM Radio Page.
3)
If necessary, press the RADIO Softkey to display the XM Radio Page where audio entertainment is controlled.
Active Channel and Channel List
The Active Channel Box on the XM Radio Page displays the currently selected channel. The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category.
Flight
Selecting a Category
PlanningProcedures
The Category Box of the XM Radio Page displays the currently selected category of audio.
1)
Press the CATGRY Softkey on the XM Radio Page.
2)
Press the CAT + and CAT - softkeys to cycle through the categories.
Hazard
Additional
Avoidance
Features
Or
:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the desired category with the small FMS Knob.
3)
Press the ENT Key.
Select an Available Channel within the Selected Category
Abnormal
Operation
1)
While on the XM Radio Page, press the CHNL Softkey.
2)
AlertsAppendixIndex
Annun/
60
Press the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey.
Or
:
Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels.
3)
With the desired channel highlighted, press the ENT Key.
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190-00821-03 Rev. A
Page 77
Additional Features
Entering a Channel Directly
1)
While on the XM Radio Page, press the CHNL Softkey.
2)
Press the DIR CH Softkey. The channel number in the Active Channel Box is highlighted.
3)
Press the numbered softkeys located on the bottom of the display to directly select the desired channel number. The number keys on the PFD/ MFD Control Unit may also be used.
4)
Press the ENT Key to activate the selected channel.
Assigning Channel Presets
Upto15channelsfromanycategorycanbeassignedapresetnumber.
1)
On the XM Radio Page, with the desired channel active, press the PRESETS Softkey to access the first five preset channels (PS1 - PS5).
2)
Press the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five channels (PS11 – PS15). Pressing the MORE Softkey repeatedly cycles through the preset channels.
3)
Press any one of the (PS1 - PS15) softkeys to assign a number to the active channel.
4)
Press the SET Softkey on the desired channel number to save the channel as a preset.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Adjusting Volume
1)
With the XM Radio Page displayed, press the VOL Softkey.
2)
Press the VOL – Softkey to reduce volume or press the VOL + Softkey to increase volume. (Once the VOL Softkey is pressed, the volume can also be adjusted using the small FMS Knob.)
3)
Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to unmute the audio.
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Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
Page 78
Additional Features

ELECTRONIC CHECKLISTS

Flight
The system accesses the checklists from an SD card inserted into the bezel slot.
InstrumentsEIS
If the SD card contains an invalid checklist file or no checklist, the Power-up Page messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the CHKLIST Softkey is not available.
Accessing and Navigating Checklists
Nav/Com/
XPDR/AudioAFCSGPS Nav
1)
From any page on the MFD, press the CHKLIST Softkey.
2)
Turn the large FMS Knob to select the ‘GROUP’ field.
3)
Turn the small FMS Knob to select the desired procedure and press the ENT Key.
4)
Turn the large FMS Knob to select the ‘CHECKLIST’ field.
5)
Turn the FMS Knob to select the desired checklist and press the ENT Key. The selected checklist item is indicated with white text surrounded by a
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
white box.
6)
Press the ENT Key or CHECK Softkey to check the selected checklist item. The line item turns green and a checkmark is placed in the associated box. The next line item is automatically selected for checking.
Either FMS Knob can be used to scroll through the checklist and select the desired checklist item.
Press the CLR Key or UNCHECK Softkey to remove a check mark from an item.
The following colors are used for checklist items:
Blue - Items not selected
White - Item is selected
Green - Item has been checked
Yellow - Caution notes
Red - Warning notes
7)
When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window. If all items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’ will be displayed in yellow text.\
8)
Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor.
62
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Page 79
Additional Features
9)
Press the ENT Key to advance to the next checklist.
10)
Press the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.
Immediately Accessing Emergency Procedures
1)
From any page on the MFD, press the CHKLIST Softkey.
2)
Press the EMERGCY Softkey.
3)
Turn the FMS Knob to select the desired emergency checklist and press the ENT Key.
4)
Press the ENT Key or CHECK Softkey to check the selected emergency checklist item. The line item turns green and a checkmark is placed in the box next to it. The next line item is automatically highlighted for checking.
Either FMS Knob can be used to scroll through the checklist and select the desired checklist item.
Press the CLR Key or UNCHECK Softkey to remove a check mark from an item.
5)
When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window. If all items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’ will be displayed in yellow text.\
6)
Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor.
7)
Press the ENT Key to advance to the next checklist.
8)
Press the RETURN Softkey to return to the previous checklist.
9)
Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
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Alerts Appendix Index
Annun/
Page 80
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
64
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Abnormal Operation

ABNORMAL OPERATION

REVERSIONARY MODE

Should a system detected failure occur in either display, the Perspective® system automatically enters reversionary mode. In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display.
Reversionary display mode can be manually activated by pressing the DISPLAY
BACKUP Button on the instrument panel between the PFD and MFD.
NOTE: The Cirrus SR20/SR22 Airplane Flight Manual (AFM) always takes precedence over the information found in this section.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/

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 eld of the COM radio for which the tuning failure was detected.

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

If GPS position is lost, or becomes invalid, selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established.
Loss of Hazard Functions with Loss of GPS
Position
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
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Page 82
Abnormal Operation

UNUSUAL ATTITUDES

Flight
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
InstrumentsEIS
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• TrafcAnnunciations
• AFCSAnnunciations
Nav/Com/
XPDR/AudioAFCSGPS Nav
• FlightDirector
Command Bars
• InsetMap
• Temperatures
• DMEInformation
Window
• WindData
• SelectedHeadingBox
Flight
PlanningProcedures
• SelectedCourseBox
• TransponderStatus
• SystemTime
• PFDSetupMenu
• Windowsdisplayedin
the lower right corner
of the PFD: – Timer/References – Nearest Airports – Flight Plan – Messages – Procedures
• BarometricMinimum
Descent Altitude Box
Box
Hazard
Avoidance
• Glideslope,Glidepath,
and Vertical Deviation Indicators
• Altimeter Barometric Setting
• SelectedAltitude
• VNV Target Altitude
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
66
Extreme Pitch Indication
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190-00821-03 Rev. A
Page 83
Abnormal Operation

DEAD RECKONING

While in Enroute or Oceanic phase of flight, if the Perspective® system detects an invalid GPS solution or is unable to calculate a GPS position, the system automatically reverts to Dead Reckoning (DR) Mode. In DR Mode, the system uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position.
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the system stops navigating in GPS Mode.
DR Mode is indicated by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own aircraft’ symbol as shown in the following figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure. Also, the CDI deviation bar is displayed in yellow. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message appears on the PFD.
Normal navigation using GPS/WAAS source data resumes automatically once a valid GPS solution is restored.
It is important to note that estimated navigation data supplied by the system in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or not available, the DR function is not be capable of estimating your position and, consequently, the system may display a path that is different than the actual movement of the aircraft. Estimated position information displayed by the system through DR while there is no heading and/or airspeed data available should not be used for navigation.
DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the lack of satellite measurements needed to determine a position. Changes in wind speed and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this degraded accuracy, the crew must maintain position awareness using other navigation equipment until GPS-derived position data is restored.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
190-00821-03 Rev. A 67
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Page 84
Abnormal Operation
Flight
InstrumentsEIS
CDI ‘DR’ Indication on PFD
Symbolic Aircraft
(Map pages and Inset Map)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Dead Reckoning Indications
As a result of operating in DR Mode, all GPS-derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information. This data includes the following:
• NavigationStatusBoxeldsexceptActiveLeg,TAS,andDTK
• CourseDeviationIndicator
• GPSBearingPointer
Flight
• WinddataandpointersintheWindDataBoxonthePFD
PlanningProcedures
• TrackIndicator
• AllBearingPointerDistances
• ActiveFlightPlandistances,bearings,andETEvalues
Also, while the system is in DR Mode, the autopilot will not couple to GPS, and
Hazard
Terrain Proximity, TERRAIN-SVS, and TAWS are disabled. Additionally, the accuracy
Avoidance
of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy.
Features
Additional
Abnormal
Operation
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Annun/
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Page 85

WARNING ALERTS

Annunciations & Alerts

ANNUNCIATIONS & ALERTS
Instruments EIS
Flight
Annunciation
Alerts Window Text Audio Alert
Window Text
ANTI ICE CTL
ANTI ICE FLO
ANTI ICE QTY
ANTI ICE QTY
AOA OVERHEAT
Tank valves cannot be controlled (closed) (TKS).
Flow rate is low (TKS). Repeating Double Chime Left and right fluid quantities are
unknown (TKS) Fluid quantity is low (TKS). Repeating Double Chime
AOA probe is overheated. Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
BRAKE TEMP Brake termperature is high. Repeating Double Chime
CHT Cylinder head temperature is high. Repeating Double Chime
CO LVL HIGH
Carbon monoxide level is too high Repeating Double Chime
ESS BUS Check essential power bus voltage. Repeating Double Chime
FUEL FLOW Check fuel flow. None
FUEL QTY Check fuel tank levels. Repeating Double Chime
M BUS 1 Check main power bus 1 voltage. Repeating Double Chime M BUS 2 Check main power bus 2 voltage. Repeating Double Chime
MAN PRESSURE* Check manifold pressure.
Repeating Double Chime
(after 30 seconds)
OIL PRESSURE Oil pressure is out of range. Repeating Double Chime
OIL TEMP Oil temperature is high. Repeating Double Chime
OXYGEN FAULT
OXYGEN QTY
Oxygen system fault. Repeating Double Chime
Oxygen quantity is low. Repeating Double Chime
RPM Check engine RPM. Repeating Double Chime
STALL Stall warning. Tone
START ENGAGE Starter is engaged. Repeating Double Chime
TIT* TIT temperature is high. Repeating Double Chime
Optional / * SR22TN only / TKS NH (optional) / TKS FIKI (optional) /
1
In air only
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
1
Avoidance
Hazard
Additional
Features
Operation
1
Abnormal
Annun/
Alerts Appendix Index
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Page 86
Annunciations & Alerts

CAUTION ALERTS

Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
Annunciation
Alerts Window Text Audio Alert
Window Text
ALT 1 Check alternator 1 current. Double Chime ALT 2 Check alternator 2 current. Double Chime
ALT AIR OPEN* Alternate air door is open. Double Chime
ANTI ICE HTR
ANTI ICE LVL
ANTI ICE LVL
ANTI ICE PSI
ANTI ICE PSI
ANTI ICE QTY
ANTI ICE QTY
ANTI ICE SPD
ANTI ICE SPD
AP MISCOMP
AP/PFD ADC
AP/PFD AHRS
Stall warning/AoA heater has failed. Double Chime
Left tank fluid quantity is unreliable (TKS). Double Chime
Right tank fluid quantity is unreliable (TKS). Double Chime
Tail pressure is low (TKS). Double Chime
Pressure is high (TKS). Double Chime
Fluid quantity imbalance has been detected (TKS) Double Chime
Fluid quantity is low (TKS) Double Chime
Airspeed is too low for ice protection (TKS). Double Chime
Airspeed is to high for ice protection (TKS). Double Chime Autopilot miscompare, autopilot is not available. Double Chime Autopilot and PFD are using different ADCs. Double Chime Autopilot and PFD are using different AHRSs. Double Chime
AVIONICS OFF Avionics master switch is off. Double Chime
BATT 1 Check battery 1 current. Double Chime
BRAKE TEMP Brake termperature is high. Double Chime
CHT Cylinder head temperature is high. Double Chime
FLAPS Flaps are extended beyond airspeed limitations. Double Chime
FUEL FILTER Fuel filter in bypass Double Chime
FUEL QTY Check fuel tank levels. Double Chime
M BUS 1 Check main power bus 1. Double Chime M BUS 2 Check main power bus 2. Double Chime
MAN PRESSURE* Check manifold pressure. None
NO ADC MODES
NO VERT MODES
Autopilot air data modes are not available. Double Chime
Autopilot vertical modes are not available. Double Chime
OIL PRESSURE Oil pressure is out of range. Double Chime
1
1
1
1
1
1
1
1
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Page 87
Annunciations & Alerts
Annunciation
Alerts Window Text Audio Alert
Window Text
OIL TEMP Oil temperature is high. Double Chime
OXYGEN QTY
OXYGEN RQD
Oxygen quantity is low. Double Chime
Oxygen is required. Double Chime
PARK BRAKE Parking break is set. None
PITOT HEAT Pitot heat failure. Double Chime
PITOT HT OFF Pitot heat is turned off. None
PITOT HT RQD Pitot heat is required. Double Chime
START ENGAGE Starter is engaged. Double Chime
Optional / * SR22TN only / TKS NH (optional) / TKS FIKI (optional) /
1
In air only

ADVISORY ANNUNCIATIONS

Annunciation
Window Text
ALTITUDE SEL
ALTITUDE SEL
Climbing away from selected altitude.
Descending away from selected altitude.
Alerts Window Text Audio Alert
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
1
Planning Procedures
Flight
Avoidance
Hazard
V
AOA FAIL
COURSE SEL
HIGH MP FF*
L FUEL QTY
OXYGEN QTY
PUMP BACKUP
R FUEL QTY
bug is not available.
REF
Current track will not intercept selected course.
Avoid fuel flow 18 to 30 GPH and MP above 26”.
Check left fuel tank level.
Oxygen quantity is low. Anti-ice backup pump mode has been selected
(TKS). Check right fuel tank level.
None
Optional / * SR22TN only / TKS FIKI (optional) / GFC 700 AFCS only
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Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
Page 88
Annunciations & Alerts

COMPARATOR ANNUNCIATIONS

Comparator
Flight
InstrumentsEIS
Window Text
ALT MISCOMP
IAS MISCOMP
Nav/Com/
XPDR/AudioAFCSGPS Nav
HDG MISCOMP
PIT MISCOMP
ROL MISCOMP
ALT NO COMP IAS NO COMP
HDG NO COMP
PIT NO COMP
Flight
PlanningProcedures
ROL NO COMP
Difference in altitude sensors is > 200 ft.
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts.
Difference in heading sensors is > 6 degrees.
Difference in pitch sensors is > 5 degrees.
Difference in roll sensors is > 6 degrees.
No data from one or both altitude sensors.
No data from one or both airspeed sensors.
No data from one or both heading sensors.
No data from one or both pitch sensors.
No data from one or both roll sensors..
Condition

REVERSIONARY SENSOR ANNUNCIATIONS (SR22 ONLY)

Reversionary
Sensor
Hazard
Window Text
Avoidance
The PFD is displaying data from the #2 Air Data Computer.
The PFD is displaying data from the #2 AHRS.
Features
Additional
USING ADC2
USING AHRS2

MESSAGE ADVISORY ALERTS

Abnormal
Operation
Alerts Window Message Audio Alert
EXIT ICING – Exit icing conditions.
AlertsAppendixIndex
Annun/
ANTI ICE QTY – Fluid quantity is low (TKS). PFD1 FAN FAIL – The cooling fan for PFD1 is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative.
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Condition
None
190-00821-03 Rev. A
Page 89
Annunciations & Alerts

GFC 700 AFCS ALERTS

Condition Annunciation Description
Pitch Failure Pitch axis control failure.
Roll Failure Roll axis control failure.
Pitch Trim Axis Control Failure
Yaw Damper Failure
System Failure AP and MET are unavailable. FD may still be available.
Elevator Mistrim Up
Elevator Mistrim Down
Aileron Mistrim Left
Aileron Mistrim Right
Rudder Mistrim Left
Rudder Mistrim Right
Preflight Test Performing preflight system test. Upon completion of the
If annunciated when AP is engaged, a failure has occurred in the pitch trim system.
YD control failure (SR22 only).
A condition has developed causing the pitch servo to provide a sustained force in the nose up direction.
A condition has developed causing the pitch servo to provide a sustained force in the nose down direction.
A condition has developed causing the roll servo to provide a sustained left force.
A condition has developed causing the roll servo to provide a sustained right force.
A condition has developed causing the yaw servo to provide a sustained force (SR22 only).
A condition has developed causing the yaw servo to provide a sustained force (SR22 only).
test, the aural alert will be heard.
Preflight system test has failed.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
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Alerts Appendix Index
Annun/
Page 90
Annunciations & Alerts

TERRAIN-SVS ALERTS

Flight
InstrumentsEIS
Alert Type
PFD/MFD
TERRAIN-SVS
Page
Annunciation
Reduced Required Terrain Clearance Warning (RTC)
Nav/Com/
Imminent Terrain Impact
XPDR/AudioAFCSGPS Nav
Warning (ITI)
Reduced Required Obstacle Clearance Warning (ROC)
Imminent Obstacle Impact Warning (IOI)
Reduced Required Terrain Clearance Caution (RTC)
Flight
Imminent Terrain Impact
PlanningProcedures
Caution (ITI)
Reduced Required Obstacle Clearance Caution (ROC)
Imminent Obstacle Impact Caution (IOI)
Hazard
Avoidance

TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS

MFD
Pop-Up Alert
Aural
Message
“Warning; Terrain,
Terrain”
“Warning; Terrain,
Terrain”
“Warning; Obstacle,
Obstacle”
“Warning; Obstacle,
Obstacle”
“Caution; Terrain,
Terrain”
“Caution; Terrain,
Terrain”
“Caution; Obstacle,
Obstacle”
“Caution; Obstacle,
Obstacle”
Features
Additional
Alert Type
PFD/MFD
TERRAIN-SVS Page
Aural Message
Annunciation
System Test fail “Terrain System Failure”
Abnormal
Operation
Terrain Alerting is disabled None
AlertsAppendixIndex
No GPS position or excessively
Annun/
degraded GPS signal
“Terrain System Not Available” “Terrain Available” will be heard when sufficient GPS signal is re-established.
System Test in progress None
System Test pass None Chime
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Page 91
Annunciations & Alerts

TAWS ALERTS

Alert Type
Excessive Descent Rate Warning (EDR)
Reduced Required Terrain Clearance Warning (RTC)
Imminent Terrain Impact Warning (ITI)
Reduced Required Obstacle Clearance Warning (ROC)
Imminent Obstacle Impact Warning (IOI)
Reduced Required Terrain Clearance Caution (RTC)
Imminent Terrain Impact Caution (ITI)
PFD/MFD TAWS-B Page Annunciation
MFD
Pop-Up Alert
or
or
or
or
or
or
Aural Message
“Pull Up”
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
“Caution, Terrain; Caution,
Terrain”
or
“Terrain Ahead; Terrain
Ahead”
“Terrain Ahead; Terrain
Ahead”
or
“Caution, Terrain; Caution,
Terrain”
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
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Page 92
Annunciations & Alerts
PFD/MFD
Flight
Alert Type
InstrumentsEIS
Reduced Required Obstacle Clearance Caution (ROC)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Imminent Obstacle Impact Caution (IOI)
Premature Descent Alert Caution (PDA)
Altitude Callout “500”
Flight
PlanningProcedures
Excessive Descent Rate Caution (EDR)
Negative Climb Rate Caution (NCR)
Hazard
Avoidance
TAWS-B Page
Annunciation
None None “Five-Hundred”
TAWS System Status Annunciations
MFD
Pop-Up Alert
or
or
or
Aural Message
“Caution, Obstacle; Cau-
tion, Obstacle”
or
“Obstacle Ahead; Obstacle
Ahead”
“Obstacle Ahead; Obstacle
Ahead”
or
“Caution, Obstacle;
Caution, Obstacle”
“Too Low, Terrain”
“Sink Rate”
“Don’t Sink”
or
“Too Low, Terrain”
Features
Additional
Alert Type
Abnormal
Operation
TAWS System Test Fail None “TAWS System Failure”
PFD/MFD TAWS-B Page Annunciation
MFD
Pop-Up Alert
Aural Message
TAWS Alerting is disabled None None
AlertsAppendixIndex
Annun/
No GPS position or excessively degraded GPS signal
None “TAWS Not Available”
“TAWS Available” will be heard when sufficient GPS signal is re-established.
System Test in progress None None
System Test pass None None Chime
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Annunciations & Alerts

AURAL ALERTS

Aural Alert Description
“Airspeed” Low airspeed when the autopilot is engaged (GFC 700 AFCS only).
“Minimums, minimums” The aircraft has descended below the preset minimum descent altitude or
decision altitude.
“Traffic, Traffic” Played when a Traffic Advisory (TA) is issued (optional).
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”
“Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical
Played when the Skywatch TAS system passes a pilot-initiated self test (optional).
Played when the Skywatch TAS system fails a pilot-initiated self test (optional).
navigation is enabled.

CO GUARDIAN MESSAGES (OPTIONAL)

Alerts Window Message Comments
CO DET SRVC
monoxide detector needs service.
CO DET FAIL
monoxide detector is inoperative.
– The carbon
– The carbon
There is a problem within the CO Guardian that requires service.
Loss of communication between the Perspective® system and the CO Guardian.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard

MFD & PFD MESSAGE ADVISORIES

Message Comments
DATA LOST
was lost. Recheck settings.
– Pilot stored data
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.
XTALK ERROR
crosstalk error has occurred.
– A flight display
The MFD and PFD are not communicating with each other. The Perspective® system should be serviced.
PFD1 SERVICE
service. Return unit for repair.
– PFD1 needs
The PFD and/or MFD self-test has detected a problem. The Perspective® system should be
MFD1 SERVICE
– MFD1 needs
serviced.
service. Return unit for repair.
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Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
Page 94
Annunciations & Alerts
MFD & PFD MESSAGE ADVISORIES (CONT.)
Flight
InstrumentsEIS
MANIFEST
Message Comments
– PFD1 software
mismatch, communication halted.
MANIFEST
– MFD1 software
mismatch, communication halted.
PFD1 CONFIG
Nav/Com/
XPDR/AudioAFCSGPS Nav
– PFD1 config error.
Config service req’d.
MFD1 CONFIG
– MFD1 config
error. Config service req’d.
SW MISMATCH
– GDU software
version mismatch. Xtalk is off.
Flight
PlanningProcedures
PFD1 COOLING
– PFD1 has poor
cooling. Reducing power usage.
MFD1 COOLING
– MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK
Hazard
Avoidance
Key is stuck.
MFD1 KEYSTK
Features
Key is stuck.
Additional
CNFG MODULE
– PFD1 [key name]
– MFD [key name]
– PFD1
configuration module is
Abnormal
Operation
inoperative.
PFD1 VOLTAGE
AlertsAppendixIndex
voltage. Reducing power usage
Annun/
MFD1 VOLTAGE
– PFD1 has low
– MFD1 has low
voltage. Reducing power usage
The PFD and/or MFD has incorrect software installed. The Perspective® system should be serviced.
The PFD configuration settings do not match backup configuration memory. The Perspective® system should be serviced.
The MFD configuration settings do not match backup configuration memory. The Perspective® system should be serviced.
The MFD and PFD have different software versions installed. The Perspective® system should be serviced.
The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the Perspective® 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 Perspective® system should be serviced if the problem persists.
The PFD1 configuration module backup memory has failed. The Perspective® system should be serviced.
The PFD1 voltage is low. The Perspective® system should be serviced.
The MFD voltage is low. The Perspective® system should be serviced.
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Annunciations & Alerts

DATABASE MESSAGE ADVISORIES

Message Comments
MFD1 DB ERR
database error exists.
PFD1 DB ERR
database error exists.
MFD1 DB ERR
database error exists.
PFD1 DB ERR
– MFD1 navigation
– PFD1 navigation
– MFD1 basemap
– PFD1 basemap
The MFD and/or PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the Perspective® system should be serviced.
The MFD and/or PFD detected a failure in the basemap database.
database error exists.
MFD1 DB ERR
database error exists.
PFD1 DB ERR
database error exists.
– MFD1 terrain
– PFD1 terrain
The MFD and/or PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, The Perspective® system should be serviced.
MFD1 DB ERR
database missing.
PFD1 DB ERR
– MFD1 terrain
– PFD1 terrain
The terrain database is present on another LRU, but is missing on the specified LRU.
database missing.
MFD1 DB ERR
database error exists.
PFD1 DB ERR
database error exists.
– MFD1 obstacle
– PFD1 obstacle
The MFD and/or PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, The Perspective® system should be serviced.
MFD1 DB ERR
database missing.
PFD1 DB ERR
– MFD1 obstacle
– PFD1 obstacle
The obstacle database is present on another LRU, but is missing on the specified LRU.
database missing.
MFD1 DB ERR
terrain database error exists.
PFD1 DB ERR
terrain database error exists.
– MFD1 airport
– PFD1 airport
The MFD and/or PFD detected a failure in the airport terrain database. Ensure that the data card is properly inserted. Replace data card. If problem persists, The Perspective® system should be serviced.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
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Page 96
Annunciations & Alerts
DATABASE MESSAGE ADVISORIES (CONT.)
Flight
InstrumentsEIS
MFD1 DB ERR
Message Comments
– MFD1 airport
terrain database missing.
PFD1 DB ERR
– PFD1 airport
terrain database missing.
MFD1 DB ERR
Nav/Com/
XPDR/AudioAFCSGPS Nav
– MFD1 Safe Taxi
database error exists.
PFD1 DB ERR
– PFD1 Safe Taxi
database error exists.
MFD1 DB ERR
– MFD1 Chartview
database error exists.
Flight
PlanningProcedures
MFD1 DB ERR
– MFD1 FliteCharts
database error exists.
Hazard
Avoidance
MFD1 DB ERR
Directory database error exists.
Features
Additional
DB MISMATCH
Abnormal
Operation
– MFD1 Airport
– Navigation
database mismatch. Xtalk is off.
AlertsAppendixIndex
Annun/
DB MISMATCH
– Standby
Navigation database mismatch.
The airport terrain database is present on another LRU, but is missing on the specified LRU.
The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, The Perspective® system should be serviced.
The MFD and/or PFD detected a failure in the ChartView database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, The Perspective® system should be serviced.
The MFD and/or PFD detected a failure in the FliteCharts database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, The Perspective® system should be serviced.
The MFD detected a failure in the Airport Directory database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced.
The PFDs and MFD have different navigation database versions or types (Americas, European, etc.) installed. Crossfill is off. Install correct navigation database version or type in all displays.
The PFDs and MFD have different standby navigation database versions or types (Americas, European, etc.) installed. Install correct standby navigation database version or type in all displays.
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DATABASE MESSAGE ADVISORIES (CONT.)
Message Comments
DB MISMATCH
mismatch.
– Terrain database
The PFDs and MFD have different terrain database versions or types installed. Install correct terrain database version or type in all displays.
DB MISMATCH
database mismatch.
– Obstacle
The PFDs and MFD have different obstacle database installed. Install correct obstacle database in all displays.
DB MISMATCH
database mismatch.
– Airport Terrain
The PFDs and MFD have different airport terrrain databases installed. Install correct airport terrain database in all displays.
NAV DB UPDATED
navigation database updated.
TERRAIN DSP
MFD1] Terrain awareness display unavailable.
– Active
– [PFD1 or
System has updated the active navigation database from the standby navigation database.
One of the terrain, airport terrain, or obstacle databases required for TAWS in the PFD or MFD is missing or invalid.

GMA 347 MESSAGE ADVISORIES

Message Comments
GMA1 FAIL
– GMA1 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The Perspective® system should be serviced.
GMA1 CONFIG
error. Config service req’d.
– GMA1 config
The audio panel configuration settings do not match backup configuration memory. The Perspective® system should be serviced.
MANIFEST – GMA1 software
mismatch, communication halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
The audio panel has incorrect software installed. The
Perspective
The audio panel self-test has detected a problem. Certain audio functions may still be available, and the audio panel may still be usable. The system should be serviced when possible.
®
system should be serviced.
Perspective
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
®
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Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES

Flight
InstrumentsEIS
GIA1 CONFIG
Message Comments
– GIA1 config error.
Config service req’d.
GIA2 CONFIG
– GIA2 config error.
Config service req’d.
GIA1 CONFIG
Nav/Com/
XPDR/AudioAFCSGPS Nav
– GIA1 audio config
error. Config service req’d.
GIA2 CONFIG
– GIA2 audio config
error. Config service req’d.
GIA1 COOLING
– GIA1
temperature too low.
GIA2 COOLING
– GIA2
temperature too low.
Flight
PlanningProcedures
GIA1 COOLING
– GIA1 over
temperature.
GIA2 COOLING
– GIA2 over
temperature.
GIA1 SERVICE
Hazard
service. Return the unit for repair.
Avoidance
GIA2 SERVICE
– GIA1 needs
– GIA2 needs
service. Return the unit for repair.
Features
Additional
HW MISMATCH
– GIA hardware mismatch. GIA1 communication halted.
Abnormal
Operation
HW MISMATCH
– GIA hardware mismatch. GIA2 communication
AlertsAppendixIndex
Annun/
halted.
MANIFEST
– GIA1 software
mismatch, communication halted.
MANIFEST
– GIA2 software
mismatch, communication halted.
MANIFEST
– GFC software
mismatch, communication halted.
The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The Perspective® system should be serviced.
The GIA1 and/or GIA2 have an error in the audio configuration. The Perspective® 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 Perspective® system should be serviced.
The GIA1 and/or GIA2 self-test has detected a problem in the unit. The Perspective® system should be serviced.
A GIA mismatch has been detected, where only one is WAAS capable.
The GIA1 and/or GIA 2 has incorrect software installed. The Perspective® system should be serviced.
Incorrect servo software is installed, or gain settings are incorrect.
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GIA 63W MESSAGE ADVISORIES (CONT.)
Message Comments
COM1 TEMP
Reducing transmitter power.
COM2 TEMP
Reducing transmitter power.
– COM1 over temp.
– COM2 over temp.
The system has detected an over temperature condition in COM1 and/or COM2. The transmitter is operating at reduced power. If the problem persists, the Perspective® system should be serviced.
COM1 SERVICE
service. Return unit for repair.
COM2 SERVICE
service. Return unit for repair.
COM1 PTT
key is stuck.
COM2 PTT
key is stuck.
– COM1 needs
– COM2 needs
– COM1 push-to-talk
– COM2 push-to-talk
The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The Perspective® 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 Perspective® system should be serviced.
COM1 RMT XFR
transfer key is stuck.
COM2 RMT XFR
transfer key is stuck.
– COM1 remote
– COM2 remote
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, the Perspective® system should be serviced.
LOI
– GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST
– Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST
– Loss of GPS
navigation. Position error.
GPS NAV LOST
– Loss of GPS
navigation. GPS fail.
ABORT APR
– Loss of GPS
navigation. Abort approach.
APR DWNGRADE
– Approach
downgraded.
GPS integrity is insufficient for the current phase of flight.
Loss of GPS navigation due to insufficient satellites.
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Vertical guidance generated by WAAS is unavailable, use LNAV only minimums.
Instruments EIS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
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Page 100
Annunciations & Alerts
GIA 63W MESSAGE ADVISORIES (CONT.)
Flight
InstrumentsEIS
TRUE APR
Message Comments
– True north approach.
Change HDG reference to TRUE.
GPS1 SERVICE
– GPS1 needs
service. Return unit for repair.
Nav/Com/
GPS2 SERVICE
XPDR/AudioAFCSGPS Nav
– 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 RMT XFR
transfer key is stuck.
Flight
PlanningProcedures
NAV2 RMT XFR
– NAV1 remote
– NAV2 remote transfer key is stuck.
Hazard
Avoidance
G/S1 FAIL
G/S2 FAIL
– G/S1 is inoperative.
– G/S2 is inoperative.
Displayed after passing the first waypoint of a true north approach when the nav angle is set to ‘AUTO’.
A failure has been detected in the GPS1 and/ or GPS2 receiver. The receiver may still be available. The Perspective® system should be serviced.
A failure has been detected in the NAV1 and/ or NAV2 receiver. The receiver may still be available. The Perspective® 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 Perspective® system should be serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The Perspective® system should be serviced.
G/S1 SERVICE
service. Return unit for repair.
Features
Additional
G/S2 SERVICE
– G/S1 needs
– G/S2 needs
service. Return unit for repair.
Abnormal
Operation

GEA 71 MESSAGE ADVISORIES

AlertsAppendixIndex
Annun/
GEA1 CONFIG
Message Comments
– GEA1 config error.
Config service req’d.
MANIFEST
– GEA1 software
mismatch, communication halted.
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Cirrus Perspective® by Garmin – Cockpit Reference Guide for the SR20/SR22
A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The Perspective® system should be serviced when possible.
The GEA1 configuration settings do not match those of backup configuration memory. The Perspective® system should be serviced.
The #1 GEA 71 has incorrect software installed. The Perspective® system should be serviced.
190-00821-03 Rev. A
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