Cirrus SR22 Pilot's Information Manual

With cirrus perspective touch+ avionics system

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Pilot's operating handbook and flight manual (524 pages)

Pilot operating handbook (502 pages)

Maintenance manual (74 pages)

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PILOT'S INFORMATION

MANUAL

for the CIRRUS SR22

with Cirrus Perspective Touch+ Avionics System

This manual includes descriptions of the airplane and its systems.

P/N 44766-001

Cover Page-i

Revision 1

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Summary of Contents for Cirrus SR22

Page 1 PILOT’S INFORMATION MANUAL for the CIRRUS SR22 with Cirrus Perspective Touch+ Avionics System This manual includes descriptions of the airplane and its systems. P/N 44766-001 Cover Page-i Revision 1...
Page 3 ’ IRRUS ILOT NFORMATION ANUAL SR22 IST OF FFECTIVE AGES List of Effective Pages Use this page to determine the current effective date for each page in the PIM. Dates of original issue and revised pages are: Original Issue..04 Dec 2023 Revision 1...03 Apr 2025...
Page 4 ’ ILOT NFORMATION ANUAL IRRUS SR22 IST OF FFECTIVE AGES List of Effective Pages (Cont.) Page Status Page Status Page Status 15-1 Revision 1 18-6 Original Issue 15-2 Revision 1 18-7 Original Issue 15-3 Revision 1 18-8 Original Issue 15-4...
Page 5 RONT ATTER SR22 OREWORD Foreword This manual has been prepared by Cirrus Aircraft to familiarize operators with the aircraft. Read this manual carefully. It provides system descrip- tions, operational procedures, and basic information for maintaining the airplane. • N •...
Page 6 Issue” at this location. In the event that the majority of pages are revised, Cirrus Aircraft may determine that it is more effective to reissue the manual. Reissued pages will be identified by the word “Reissue” followed by a letter indicating the reissue level;...
Page 7 IRRUS RONT ATTER SR22 UPPLEMENTS Supplements The Supplements chapter contains supplementary information relating to optional equipment not provided with the standard airplane or not included in the manual. Supplements are essentially “mini-handbooks” and may contain data corresponding to most chapters of the manual. Data in a supplement either adds to, supersedes, or replaces similar data in the basic manual.
Page 8 RONT ATTER IRRUS SR22 ARNINGS AUTIONS OTES Intentionally Left Blank Front Matter-4 P/N 44766-001 Original Issue...
Page 9 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 1: Airframe Table of Contents Airframe....................3 Fuselage.................... 3 Overview ..................3 Wings ....................3 Overview ..................3 Empennage ..................4 Overview ..................4 P/N 44766-001 Original Issue...
Page 10 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ABLE OF ONTENTS Intentionally Left Blank P/N 44766-001 Original Issue...
Page 11 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 IRFRAME Airframe Fuselage Overview The airplane’s monocoque fuselage is constructed primarily of composite materials and is designed to be aerodynamically efficient. The cabin area is bounded on the forward side by the firewall at fuselage station 100, and on the rear by the aft baggage compartment bulkhead at fuselage station 222.
Page 12 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 IRFRAME Empennage Overview The empennage consists of a horizontal stabilizer, a two-piece elevator, a vertical stabilizer, and a rudder. All of the empennage components are conventional spar (shear web), rib, and skin construction.
Page 13 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 IRFRAME Figure 1-1: Equipment Locations LEGEND 1. Avionics Cooling Fan 2. ADAHRS 3. Integrated Avionics Unit 4. Stick Shaker Controller 5. Audio Panel 6. Engine Interface 7. Battery 1 8. Fire Extinguisher 9. MFD 10.
Page 14 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 IRFRAME Intentionally Left Blank P/N 44766-001 Original Issue...
Page 15 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 2: Flight Controls Table of Contents Flight Controls ..................3 Elevator System ................3 Overview ..................3 Operation..................3 Aileron System .................. 5 Overview ..................5 Operation..................5 Rudder System.................. 7 Overview ..................
Page 16 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ABLE OF ONTENTS Intentionally Left Blank P/N 44766-001 Original Issue...
Page 17 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LIGHT ONTROLS Flight Controls Conventional flight controls for ailerons, elevator, and rudder are used. The ailerons and elevator are controlled through either of two side sticks. The rudder is controlled through either of two sets of rudder pedals. The control system uses a combination of push rods, cables, and bell cranks for control of the surfaces.
Page 18 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT ONTROLS Figure 2-1: Elevator System LEGEND 1. RH Elevator 2. LH Elevator 3. Spring Cartridge 4. Pulley 5. Cable 6. Side Stick 7. Ground Adjustable Trim Tab SR22_PM02_1005 P/N 44766-001 Original Issue...
Page 19 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LIGHT ONTROLS Aileron System Overview The ailerons provide airplane roll control. The ailerons are of conventional design with skin, spar and ribs manufactured of aluminum. Each aileron is attached to the wing shear web at two hinge points.
Page 20 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT ONTROLS Figure 2-2: Aileron System LEGEND 1. RH Aileron 2. Pulley 3. LH Aileron 4. Spring Cartridge 5. Cable 6. Side Stick SR22_PM02_1011 P/N 44766-001 Original Issue...
Page 21 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LIGHT ONTROLS Rudder System Overview The rudder provides directional (yaw) control. The rudder is of conven- tional design with skin, spar and ribs manufactured of aluminum. The rudder is attached to the aft vertical stabilizer shear web at three hinge points and to the fuselage tailcone at the rudder control bell crank.
Page 22 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT ONTROLS Figure 2-3: Rudder System LEGEND 1. Spring Cartridge 2. Pulley 3. Rudder SR22_PM02_1014 P/N 44766-001 Original Issue...
Page 23 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 3: Instrument Panel Table of Contents Instrument Panel ................. 3 Overview ................... 3 Pilot Instrument Panel Arrangement ..........3 Overview ..................3 Operation..................3 Center Console Arrangement............4 Overview ..................4 Operation..................
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Page 25 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NSTRUMENT ANEL Instrument Panel Overview The instrument panel is installed in sections so equipment can be easily removed for maintenance. The surrounding glareshield projects over the instrument panel to reduce reflections on the windshield from lighted equipment and to shield the panel equipment from glare.
Page 26 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NSTRUMENT ANEL Center Console Arrangement Overview A center console contains the autopilot controls, flap system control, fuel pump switch, fuel selector valve, Automatic Fuel Selector System (AFSS), environmental system controls, power and mixture levers, headset jacks, and USB power.
Page 27 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NSTRUMENT ANEL Figure 3-1: Instrument Panel and Console (1 of 2) LEGEND 1. Magnetic Compass (if installed) 13. Center Storage Compartment 2. CAPS 14. Left Side Console 3. Safe Return Autoland Panel • ELT Remote (if installed) •...
Page 28 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NSTRUMENT ANEL Figure 3-1: Instrument Panel and Console (2 of 2) BOOST FUEL PUMP PRIME LEGEND 22. Audio Jacks 27. Flap Selector Switch 23. Fuel Tank Selector 28. Throttle 24. Fuel Pump Switch 29.
Page 29 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NSTRUMENT ANEL Bolster Panel Arrangement Overview A switch panel located in the bolster below the instrument panel contains switches and controls for the batteries (BAT 1 and BAT 2), alternators (ALT 1 and ALT 2), exterior lighting (STRB, LAND, and ICE), oxygen...
Page 30 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NSTRUMENT ANEL Figure 3-2: Bolster Switch Panel Arrangement HIGH BAT1 ALT1 PROBE INST ALT2 STRB LAND NORM BKUP BAT2 HEAT LIGHTS CHECKLIST LIGHTS ELECTRICAL ICE PROTECT LEGEND 1. Oxygen Switch (if installed) 2. Instrument Panel Dimmer Knob 3.
Page 31 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NSTRUMENT ANEL Engine Start and Ignition Control Arrangement Overview The engine start controls are located on the left side of the instrument panel and contains the following: • Engine PUSH TO START button •...
Page 32 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NSTRUMENT ANEL Figure 3-4: Center Console Switch Panel FLAPS BOOST FUEL PUMP PRIME 100% LEGEND 1. Enviromental System Controls 2. Flap Selector Switch 3. Fuel Pump Switch SR22_PM03_1029 System Circuit Breaker Panel Arrangement Overview System circuit breakers are located on the left side of the center console.
Page 33 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NSTRUMENT ANEL Safe Return Autoland Panel Arrangement (If Installed) Overview Safe Return Autoland panel is located aft of CAPS panel. Refer to “Figure 20-1: Safe Return Autoland”. Operation For specific Safe Return Autoland operation details refer to Chapter 20: Safe Return Autoland (Optional), "Safe Return Autoland (If Installed)"...
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Page 35 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 4: Flight Instruments Table of Contents Flight Instruments................3 Attitude Indicator ................6 Overview ..................6 Operation..................6 Airspeed Indicator ................6 Overview ..................6 Operation..................6 Altimeter .................... 7 Overview ..................
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Page 37 On the MFD, these can be used only when in reversionary mode. Refer to Chapter 17: Avionics, "Cirrus Perspective Touch+ Avionics System" for more details. For additional information on PFD and MFD operation, refer to Cirrus Perspective Touch+ Integrated Avionics System Pilot’s Guide. P/N 44766-001 Original Issue...
Page 38 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT NSTRUMENTS Figure 4-1: Primary Flight Instruments (1 of 2) COM1 136.97 USING AHRS2 3000 Power -450 360° 250° 250° FEET BARO 29.92 2100 LOLCU laf 0207 2.00 9° 1900 0:17:33 GAGL 48°...
Page 39 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LIGHT NSTRUMENTS Figure 4-1: Primary Flight Instruments (2 of 2) 360° HDG 360° 360° 2.00 __._ __:__ HSI DETAIL LEGEND 1. Lubber Line 10. To/From Indicator 2. Current Heading 11. Course Pointer 3.Turn Rate and Heading Trend Vector 12.
Page 40 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT NSTRUMENTS Attitude Indicator Overview The primary attitude indicator is shown on the upper center of the PFD and displays pitch, roll, and slip/skid information provided by the Air Data, Attitude, and Heading Reference System (ADAHRS).
Page 41 • N • To change altimeter barometric pressure setting units and/or to display selected attitude in meters, refer to Cirrus Perspective Touch+ Avionics System Pilot Cockpit Reference Guide. Additionally, a standby altimeter indicator is provided by the air data source available for display on GTC 1 by selecting the DISPLAY BACKUP push button on the center instrument panel.
Page 42 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT NSTRUMENTS Horizontal Situation Indicator Overview The Horizontal Situation Indicator (HSI) is displayed along the lower center of the PFD. Heading data is provided by ADAHRS and the onboard magnetometers. The HSI displays a rotating compass card in a heading-up orientation.
Page 43 Once the failure condition(s) are resolved, GTC1 may be returned to normal operation by twice pressing the red Display Backup Button mounted between the PFD and MFD. For additional SFD operational details, refer to Cirrus Perspective Touch+ Avionics System Pilot's Guide. Standby Airspeed Indicator The standby airspeed indicator displays the current indicated airspeed (IAS).
Page 44 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LIGHT NSTRUMENTS The barometer window shows the currently set barometric pressure located at the bottom of the altitude tape. Setting the current barometric pressure compensates the altitude for the appropriate environmental conditions. When the LH touchscreen controller is transitioned to the standby flight display, the current barometric setting from the PFD syncs to the standby flight display.
Page 45 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 5: Wing Flaps Table of Contents Wing Flaps ..................3 Flap Control System................3 Overview ..................3 Operation..................5 Controls ................... 5 Indications ..................7 Power Source .................. 7 Alerts ....................
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Page 47 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LAPS Wing Flaps Flap Control System Overview The electrically controlled, single-slotted flaps provide low-speed lift enhancement. Each flap is manufactured of aluminum and connected to the wing structure at three hinge points. Rub strips are installed on the top leading edge of each flap as an intentional wear item between the flap and wing flap cove.
Page 48 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LAPS Figure 5-1: Wing Flaps LEGEND 1. RH Flap 2. Torque Tube 3. Flap Actuator 4. LH Flap SR22_PM05_1035 P/N 44766-001 Original Issue...
Page 49 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LAPS Operation The flaps are selectively set to three positions: UP, 50%, and 100% by oper- ating the flaps selector switch. The flaps selector switch positions the flaps through a motorized linear actuator mechanically connected to both flaps by a torque tube.
Page 50 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LAPS Figure 5-2: Flaps Selector Switch FLAPS 100% LEGEND 1. Flaps Selector Switch SR22_PM05_1038 P/N 44766-001 Original Issue...
Page 51 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LAPS Indications Flap position is indicated in the left side of the MFD on the Engine Indica- tion System (EIS) section displayed as UP, 50%, and 100%. Selected flap position is highlighted in a cyan box. When the flaps reach a given position the text is highlighted green and the flap symbol is colored cyan.
Page 52 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LAPS Alerts A FLAPS AIRSPEED INHIBIT Caution CAS message will be displayed, and flaps will not actuate, under the following conditions: • Airspeed is less than 74 KIAS, and flaps are then selected to 0%.
Page 53 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 6: Landing Gear Table of Contents Landing Gear..................3 Main Gear..................3 Overview ..................3 Nose Gear ..................3 Overview ..................3 Brake System ..................3 Overview ..................3 Operation..................
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Page 55 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ANDING Landing Gear Main Gear Overview The main landing gear are bolted to composite wing structure between the wing spar and shear web. The landing gear struts are constructed of composite material for fatigue resistance. The main wheels and wheel pants are bolted to the struts.
Page 56 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ANDING Operation Braking pressure is initiated by depressing the top half of a rudder pedal (toe brake). The brakes are plumbed so that depressing either the pilot’s or copilot’s left or right toe brake will apply the respective (left or right) main wheel brake.
Page 57 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 7: Seats Table of Contents Seats ....................3 Crew Seats..................3 Overview ..................3 Operation..................3 Controls ................... 3 Passenger Seats ................5 Overview ..................5 Operation..................5 Controls ................... 5 Seat Belt and Shoulder Harness ............
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Page 59 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 EATS Seats Crew Seats Overview This airplane has two individual front crew seats. The front seats are adjust- able fore and aft, and the seat backs can be reclined for passenger comfort or folded forward for rear seat access. Integral headrests are provided.
Page 60 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 EATS Figure 7-1: Crew Seats LEGEND 1. Co-pilot Seat 2. Pilot Seat 3. Seat Back Control Lever 4. Position Control Handle DETAIL SR22_PM07_1044 P/N 44766-001 Original Issue...
Page 61 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 EATS Passenger Seats Overview The rear seats employ a one-piece bench seat and two seat backs configured in 60/40 split. This “2+1” seating configuration provides for a center seat/restraint area for a third passenger on the wider left hand seat.
Page 62 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 EATS Figure 7-2: Rear Seats Location LEGEND 1. Passenger Seats 2. Recline Lock Mechanism 3. Seat Back Control Lever SR22_PM07_1047 P/N 44766-001 Original Issue...
Page 63 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 EATS Seat Belt and Shoulder Harness Overview Integrated seat belt and shoulder harness assemblies with inertia reels are provided for the pilot and each passenger. Seats belts must be worn and tightened snug and low on the waist. The seat belts are designed to accommodate an approximately 5th percentile female and 95th percentile male.
Page 64 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 EATS To use aft restraints Slip arm into the harness so that the harness extends over the occu- pant’s respective shoulder. Hold the buckle and firmly insert the link. Tighten lap belt by pulling excess shoulder belt through the tongue.
Page 65 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 EATS Operation To install child seat Fasten lower seat attachments to bench seat: LATCH Compliant Outboard Seat: Fasten lower seat attachment to the outboard anchors in the bench seat. Non-LATCH Compliant Center Seat: Using the center seat belt, fasten lower seat attachments to the bench seat as described by the manufacturer’s instructions.
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Page 67 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 8: Doors and Windows Table of Contents Doors and Windows ................3 Cabin Doors ..................3 Overview ..................3 Operation..................3 Control ..................... 3 Indications ..................3 Baggage Compartment Door ............3 Overview ..................
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Page 69 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 OORS AND INDOWS Doors and Windows Cabin Doors Overview Two large forward hinged doors allow crew and passengers to enter and exit the cabin. The door handles use two over center latches that engage a striker pin on the fuselage door opening.
Page 70 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 OORS AND INDOWS The baggage compartment extends from behind the rear passenger seat to the aft cabin bulkhead. The rear seats can be folded forward to provide additional baggage area for long or bulky items.
Page 71 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 OORS AND INDOWS Emergency Egress Hammer Overview A hammer is located in the center armrest. Operation In the event where the cabin doors are jammed or inoperable, the hammer may be used to break through the acrylic windows to provide an escape path.
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Page 73 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 9: Powerplant Table of Contents Powerplant ..................3 Engine ....................3 Overview ..................3 Operation..................3 Controls ................... 5 Indications ..................6 Propeller .................... 9 Overview ..................9 Operation..................9...
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Page 75 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 OWERPLANT Powerplant Engine Overview The airplane is powered by a Continental Motors IO-550-N, six-cylinder, normally aspirated, fuel-injected engine rated to 310 hp at 2700 RPM. Dual, conventional magnetos provide ignition. The engine is attached to the firewall by a six-point steel engine mount. The firewall attach points are structurally reinforced with gusset-type attach- ments that transfer thrust and bending loads into the fuselage shell.
Page 76 NFORMATION ANUAL HAPTER IRRUS SR22 OWERPLANT ON and starter disable switch is enabled, rotating the engine knob to the BOTH position and pressing the start button energizes the starter and acti- vates both magnetos. When the BAT1 switch is OFF and the engine knob is not in the OFF position, an intermittent aural warning tone will sound to alert the pilot that the magnetos are still hot.
Page 77 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 OWERPLANT Engine Cooling Engine cooling is accomplished by discharging heat to the oil and then to the air passing through the oil cooler, and by discharging heat directly to the air flowing past the engine. Cooling air enters the engine compartment through the two inlets in the cowling.
Page 78 For additional information on Engine Instrument Markings and Annunciations, refer to Section 2: Limitations in the AFM. For additional information on the System Annunciations and Alerts, refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide. P/N 44766-001 Original Issue...
Page 79 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 OWERPLANT Figure 9-1: Engine Controls and Indicating % Power 2500 28.0 19.0 FFlow GPH MAP inHg 1550 LEGEND 1500 1. Throttle Oil °F CHT °F EGT °F Oil PSI 2. Mixture Lever 3. Friction Knob (if installed) 4.
Page 80 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 OWERPLANT Tachometer Engine speed (RPM) is displayed on the EIS as a vertical bar and numeric display. Engine speed is displayed in revolutions per minute. During normal operating conditions, gauge pointer and display text appear in white.
Page 81 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 OWERPLANT Manifold Pressure Gauge Manifold pressure is displayed on the EIS as a vertical bar and numeric display. The pressure is displayed in inches of mercury to indicate engine power. The digital value is displayed in white numerals below the vertical bar.
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Page 83 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 10: Fuel Table of Contents Fuel ..................... 3 Fuel Storage System ................. 3 Overview ..................3 Operation..................3 Controls ................... 6 Indications ..................6 Alerts ....................8 Mixture Management............... 10 Overview ..................
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Page 85 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 Fuel Fuel Storage System Overview A 92-gallon usable wet-wing fuel storage system provides fuel for engine operation. The system consists of a 47.25-gallon capacity (46-gallon usable) vented integral fuel tank and a fuel collector tank in each wing, an Auto- matic Fuel Selection System (AFSS) with manual override, an electric fuel pump, and an engine-driven fuel pump.
Page 86 ANUAL HAPTER IRRUS SR22 Drain valves at the system low points allow draining the system for main- tenance and for examination of fuel in the system for contamination and grade. The fuel must be sampled prior to each flight. A sampler cup is provided to drain a small amount of fuel from the wing tank drains, the collector tank drains, and the gascolator drain.
Page 87 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 Figure 10-1: Fuel System Schematic ANNUNCIATOR FUEL L MAN R INDICATION VENT FILLER FILLER VENT Fuel Gal R. WING TANK L. WING TANK AFSS COVER R. WING L. WING FUEL COLLECTOR COLLECTOR SELECTOR...
Page 88 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 Controls The AFSS integrates an automated fuel selector valve and handle. The auto- matic components include: a motor, a motor controller, logic circuit card assembly with I/O to avionics, proximity sensors, mechanical bracketry, and an intermittent motion mechanism. The selector valve is installed in the aft center console with a retractable cover over the manual selector handle.
Page 89 ILOT NFORMATION ANUAL HAPTER SR22 Fuel Quantity Gauge Fuel quantity gauges are displayed on the Engine & Fuel Synoptic Page and the EIS section. In the case of an electronic display failure (reversionary mode), essential fuel information is displayed on the EIS on the upper right corner of the PFD or MFD.
Page 90 Abnormal Procedures in the AFM. For additional information on Engine Instrument Markings and Annunciations, refer to Section 2: Limitations in the AFM. For additional information on the System Annunciations and Alerts, refer to Cirrus Perspective Touch+ Avionics System Pilot’s Guide. 10-8 P/N 44766-001...
Page 91 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 Figure 10-2: Fuel System Controls and Indicating Engine & Fuel 1460 1480 EGT °F CHT °F 1370 1435 1600 Cylinder Head Temperatures 1400 Exhaust Gas Temperatures 1200 1000 Induction Induction Fuel Flow MAP: 29.5 inHg System 18.3 GPH...
Page 92 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 Mixture Management Overview The mixture control needs to be carefully monitored and managed during all phases of flight to avoid damage to the engine or a possible loss of power. After engine start, and during taxiing operations, lean the mixture until maximum engine RPM is attained to prevent possible spark plug fouling and ensure smooth engine operation.
Page 93 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 11: Electrical Table of Contents Electrical....................3 Power Generation ................3 Overview ..................3 Operation..................3 Controls ................... 9 Indications ..................10 Alerts ..................... 11 P/N 44766-001 11-1 Original Issue...
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Page 95 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LECTRICAL Electrical Power Generation Overview The airplane is equipped with a two-alternator, two-battery, 28 volt direct current (VDC) electrical system designed to reduce the risk of electrical system faults. The system provides uninterrupted power for avionics, flight instrumentation, lighting, and other electrically operated and controlled systems during normal operation.
Page 96 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LECTRICAL Figure 11-1: Electrical System Schematic Master Control Unit ALT 1 BAT 1 CONSTANT POWER BUS STARTER MAIN CB ALT 2 PANEL SR22_PM11_1060 11-4 P/N 44766-001 Original Issue...
Page 97 ALT 1 and ALT 2 voltage regulation, the MCU also provides external power reverse polarity protection, alternator overvoltage protec- tion, as well as electrical system health annunciations to the Cirrus Perspec- tive Touch+ Avionics System. Power is distributed to the airplane circuit breaker panel buses through the Main and Essential buses in the MCU.
Page 98 NFORMATION ANUAL HAPTER IRRUS SR22 LECTRICAL Main Distribution Bus 2 The Main Distribution Bus 2 is powered by ALT 2 in the MCU through a 60-amp fuse. In the event of an ALT 2 failure, Main Distribution Bus 2 is powered by Main Distribution Bus 1 through an 80-amp fuse.
Page 99 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LECTRICAL Essential Buses The circuit breaker panel Essential Bus 1 and Essential Bus 2 are powered from the Essential Distribution Bus through individual 30-amp fuses in the MCU. The Essential Bus 1 is also powered directly by BAT 2 through a 30-amp circuit breaker near the battery which then backfeeds through the Essential Distribution Bus in the MCU to the Essential Bus 2.
Page 100 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 LECTRICAL Figure 11-2: Circuit Breaker Panel STARTER YAW SERVO PITCH TRIM AP SERVOS ENGINE PITOT ROLL AUTOBRK SERVOS HEAT TRIM STALL FUEL STALL WRN AP CTRL VANE HEAT VALVE STCK SHKR CONV FLAPS...
Page 101 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LECTRICAL Transient Voltage Suppressors Transient Voltage Suppressors (TVS) are installed in key areas of the elec- trical system to protect the system from lightning strikes. During lightning strikes, enormous energy spikes can be induced within the airplane elec- trical system.
Page 102 Abnormal Procedures in the AFM. For additional information on Engine Instrument Markings and Annunciations, refer to Section 2: Limitations in the AFM. For additional information on the System Annunciations and Alerts, refer to Cirrus Perspective Touch+ Avionics System Pilot’s Guide. 11-10 P/N 44766-001...
Page 103 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 LECTRICAL Figure 11-3: Electrical Indication ESS Bus V 28.5 NOTE Essential (ESS) Bus V Bat 1 Amps Bat 1 1 Alt 2 Alt 1 Amps Alt 2 Amps SR22_PM11_1068 Alerts • N •...
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Page 105 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 12: Lighting Table of Contents Lighting....................3 Instrument Lights................3 Overview ..................3 Operation..................3 Power Source .................. 3 Convenience Lighting................ 4 Overview ..................4 Operation..................4 Power Source .................. 5 Landing Lights ...................
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Page 107 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 IGHTING Lighting Interior lighting consists of overhead task lights for the pilots and passen- gers, select backlit overlays, and instrument/controls area lighting. The flight instrumentation and avionics equipment lights are dimmable. The airplane wing tips have integrated exterior lighting components including integral position lights, anti-collision lights, mounted landing assist lights, and wingtip, ground illumination, and halo lights.
Page 108 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 IGHTING Convenience Lighting Overview Standard convenience lighting consists of a pilot, copilot, and two aft passenger task lights and an overhead baggage compartment light. Serials w/ Convenience Lighting option: The convenience lighting option...
Page 109 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 IGHTING When the cabin light switch is in the OFF position: • Task, baggage, accent, footwell, storage pockets, cubby and armrest lights will turn OFF. When the cabin light switch is in the AUTO position: •...
Page 110 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 IGHTING Figure 12-1: Interior Lighting Locations 17 18 LEGEND 1. Circuit Breaker Panel Overlays 10. Headliner Microspot Lights 2. Center Console Switch Panel 11. CAPS Instructions Overlay 3. Bolster Switch Panel 12. CAPS Handle Overlay 4.
Page 111 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 IGHTING Landing Lights Overview An LED landing light mounted in the lower engine cowl is controlled through the LAND light switch on the bolster switch panel. The wing tip mounted landing assist/taxi lights are controlled through the LAND light switch on the bolster switch panel.
Page 112 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 IGHTING Halo Lights Overview The wing tip halo lights provide additional lighting during preflight inspec- tion. Power Source 28 VDC for the wing tip halo lights is provided through the 5-amp CONV SYS 1 circuit breaker on Constant Power Bus.
Page 113 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 IGHTING • Unlocking the cabin doors using the key fob will turn the ground illu- mination and the entry step lights ON. Lights will turn OFF after 1 minute of inactivity. • Locking the cabin doors using the key fob will turn the ground illumi- nation and the entry step lights OFF.
Page 114 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 IGHTING Figure 12-2: Exterior Lighting Locations LEGEND 1. Landing Light 2. Ice Light 3. Wingtip/Landing Lights 4. Fwd Position/Anti-Collision Lights 5. Halo Lights 6. Aft Position/Anti-Collision Lights SR22_PM12_1071B 12-10 P/N 44766-001 Revision 1...
Page 115 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 13: Environmental Control Table of Contents Environmental Control................. 3 Heating and Cooling................3 Overview ..................3 Operation..................6 Controls ................... 7 Power Source .................. 9 Alerts ....................9 P/N 44766-001...
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Page 117 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NVIRONMENTAL ONTROL Environmental Control The Environmental Control System (ECS) supplies conditioned air to ventilate and regulate the temperature and distribution of air in the cabin compartment. Heating and Cooling Overview Cabin heating and ventilation is accomplished by supplying warmed ambient air from the exhaust heat exchanger for heating and windshield defog, and fresh outside air for ventilation.
Page 118 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NVIRONMENTAL ONTROL Figure 13-1: Standard Environmental System EXHAUST HEAT RAM AIR RAM AIR EXCHANGER HOT AIR VALVE MIXING CHAMBER FRESH AIR VALVE DISTRIBUTION MANIFOLD CREW DEFOG VENTS VENTS RAM AIR PASSENGER HOT AIR...
Page 119 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NVIRONMENTAL ONTROL Figure 13-2: Air Conditioning System (If installed) EXHAUST HEAT RAM AIR RAM AIR EXCHANGER HOT AIR VALVE FRESH AIR VALVE MIXING CHAMBER RECIRCULATION CHECK VALVE COMPRESSOR EVAPORATOR DISTRIBUTION MANIFOLD CONDENSER CREW...
Page 120 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NVIRONMENTAL ONTROL Operation Distribution Ventilation and cooling is provided by ducting fresh air from a NACA inlet on the RH cowl to the mixing chamber located on the lower RH portion of the firewall. Depending on operating mode and temperature selection, the...
Page 121 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NVIRONMENTAL ONTROL In air conditioning mode (if installed), refrigerant enters the engine mounted compressor as a vapor and is pressurized until the heat-laden vapor reaches a point much hotter than the outside air. The compressor then pumps the vapor to the condenser where it cools, changes to a liquid, and passes to the receiver-drier.
Page 122 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 NVIRONMENTAL ONTROL Selecting Panel-Foot-Windshield button opens the windshield diffuser butterfly valve which permits shared airflow to the defrosting mechanism and cabin floor outlets. When the Windshield selector button is pushed, the cabin floor butterfly valve is closed providing maximum airflow to the windshield diffuser.
Page 123 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 NVIRONMENTAL ONTROL Power Source 28 VDC for environmental system control panel operation is provided through the 2-amp ECS CTRL circuit breaker on Main Bus 1. The optional blower fan is powered by 28 VDC provided through a 15-amp CABIN FAN circuit breaker on A/C Bus 2.
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Page 125 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 14: Air Data System Table of Contents Air Data System .................. 3 Pitot-Static ..................3 Overview ..................3 Operation..................3 Controls ................... 3 Power Source .................. 3 Alerts ....................3 Alternate Static Source..............
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Page 127 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 YSTEM Air Data System Pitot-Static Overview The pitot-static system consists of a single heated pitot tube mounted on the left wing and dual static ports mounted in the fuselage. Serials 9750 thru 10614: The pitot heat is pilot controlled through a panel-mounted switch.
Page 128 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 YSTEM Alternate Static Source Overview The alternate static pressure source valve is installed on the switch and control panel to the right of the pilot’s leg. Operation The alternate static pressure source valve supplies static pressure from inside the cabin instead of the external static ports.
Page 129 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 YSTEM Figure 14-1: Serials w/ Triple ADAHRS: Pitot-Static System (1 of 2) GSU 75 #1 GSU 75 #2 MD302 ALTERNATE STATIC AIR SOURCE PITOT STATIC WATER TRAPS STATIC PITOT PITOT PORTS TUBE HEAT...
Page 130 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 YSTEM Figure 14-1: Serials w/ Dual ADAHRS: Pitot-Static System (2 of 2) GSU 75 #1 GI 275 #2 ALTERNATE STATIC AIR SOURCE PITOT STATIC WATER TRAPS STATIC PITOT PORTS TUBE PITOT (HEATED) HEAT 7.5A...
Page 131 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 YSTEM Stall Warning System Overview The airplane is equipped with an aural stall warning system and stick shakers which provide visual, tactile, and oral cues of an imminent stall to the crew. The stick shaker generates a vibration into the side stick via a DC gear-motor, spinning a weight mounted to the forward side of the side stick.
Page 132 NFORMATION ANUAL HAPTER IRRUS SR22 YSTEM Ice protection for the lift transducer is provided by two faceplate heaters, one vane heater and one case heater using the PROBE HEAT switch, if installed. To prevent overheating during ground operations, a signal from the avionics is used to operate the heaters at 25% power during ground operation or 100% power while in the air.
Page 133 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 15: Automation Table of Contents Automation ..................3 Automatic Flight Control System ............3 Overview ..................3 Operation..................3 AFCS Mode Controller ..............6 Overview ..................6 Operation..................6 Power Source ..................
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Page 135 This airplane is equipped with a two-axis (three-axis optional), dual channel, fail passive Automatic Flight Control System (AFCS) which is fully integrated within the Cirrus Perspective Touch+ Avionics System architecture. Refer to Cirrus Perspective Touch+ Avionics System Pilot’s Guide for additional description and operating procedures.
Page 136 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 UTOMATION • Auto-trim operation (pitch only) • Manual electric trim • Two axis airplane control (pitch and roll), including approaches • Level (LVL) mode engagement command of zero roll and zero vertical speed...
Page 137 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 UTOMATION Figure 15-1: Automatic Flight Control System Schematic AFCS MODE CONTROLLER INTEGRATED INTEGRATED AVIONICS AVIONICS UNIT 2 UNIT 1 PITCH TRIM ADAPTER PITCH TRIM MOTOR PITCH ROLL SERVO SERVO SERVO PITCH AXIS ROLL AXIS...
Page 138 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 UTOMATION AFCS Mode Controller Overview The AFCS mode controller, located in the lower section of the center console, provides primary control of autopilot modes. A pitch wheel is included for adjustment of pitch mode reference.
Page 139 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 UTOMATION Throttle and Mixture Servos (If Installed) Overview The throttle servo is located in the mid console forward of the control quadrant. The mixture servo is located in the mid console below the control quadrant.
Page 140 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 UTOMATION Electronic Stability and Protection Overview Electronic Stability and Protection (ESP) assists the pilot in maintaining the airplane in a safe flight condition. Through the use of the AFCS sensors, processors, and servos, ESP provides control force feedback, i.e., a “soft barrier”, to maintain the aircraft within the pitch, roll, and airspeed flight...
Page 141 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 UTOMATION Figure 15-2: Roll Protection Limits Always Protected Only Protected after cross- ing turn-on threshold 0° 15° 30° 45° 60° 75° 90° Bank Angle Engagement Limit: ..................45° Maximum Stick Force attained at ..............50°...
Page 142 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 UTOMATION Figure 15-4: Low Pitch Protection Limits Always Protected Only Protected after cross- ing turn-on threshold -0° -5° -10° -15° -20° -25° Nose Down Pitch Angle Engagement Limit:..................-15.5° Maximum Stick Force attained at:............-20.5°...
Page 143 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 UTOMATION Figure 15-5: High Airspeed Protection Limits - Below 17,500 ft PA Always Protected Only Protected after cross- ing turn-on threshold Indicated Airspeed (KIAS) Engagement Limit: ................200 KIAS Maximum Stick Force attained at: .............205 KIAS Disengagement Threshold (Zero Stick Force): ........190 KIAS...
Page 144 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 UTOMATION Low Speed Mode To protect against an impending stall, the low speed mode uses stick forces, similar to those used for the pitch and roll modes, to control the pitch atti- tude. These stick forces are triggered by the stall warning system. Upon stall warning system activation, the system commands the pitch servo to apply a nose-down supplemental force.
Page 145 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 UTOMATION Serials w/ Safe Return Autoland Activation Safe Return Autoland is activated after Automatic Level mode has been engaged for one minute. Once Safe Return Autoland is activated, the system enters a 10-second waiting period, and displays an EMER AUTOLAND ACTIVATING Warning with associated ‘Emergency Autoland activating’...
Page 146 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 UTOMATION Altitude-Critical Modes (ALT, GS, GP, GA, TO) Upon stall warning system activation, the AFCS will disregard its flight director and autopilot reference modes and sacrifice altitude for airspeed. The system will hold wings level and airspeed will progressively increase by 1 knot per second until stall warning becomes inactive.
Page 147 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 16: Ice Protection System Table of Contents Ice Protection System (If Installed)............3 Wing, Stabilizer, and Propeller Ice Protection System ...... 3 Overview ..................3 Controls ................... 6 Indications ..................7 Power Source ..................
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Page 149 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ROTECTION YSTEM NSTALLED Ice Protection System (If Installed) Wing, Stabilizer, and Propeller Ice Protection System Overview The Ice Protection System (IPS) can prevent and remove ice accumulation on the flight surfaces by distributing a thin film of ice protection fluid on the wing, horizontal stabilizer, vertical stabilizer, elevator tips, and propeller.
Page 150 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ROTECTION YSTEM NSTALLED ings of the outer surface. The leading edge of the panel serves as a reservoir as fluid entering the panel fills the cavity behind the porous membrane then overcomes this resistance to be distributed by the openings in the external surface.
Page 151 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ROTECTION YSTEM NSTALLED Figure 16-1: System Schematic SLINGER RING WI NDS HIELD NOZZLES LH WING INBD PANEL RH WING INBD PANEL RH WING OUTBD PANEL LH WING OUTBD PANEL RH FILLER LH FILLER...
Page 152 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ROTECTION YSTEM NSTALLED Controls System operation is controlled by the bolster switch panel and the touch- screen controllers: • Bolster Switch Panel: Metering pump operation and mode control (flow rate) are controlled by the ON/OFF, HIGH/NORM, and MAX switches.
Page 153 MFD. Numerically digital value is used to indicate LH and RH tank fluid quantity in 0.1-gallon increments. Refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide for additional information on system annunciation and control. Power Source The system operates on 28 VDC provided through the 7.5-amp ICE...
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Page 155 HAPTER SR22 ABLE OF ONTENTS Chapter 17: Avionics Table of Contents Avionics ....................5 Cirrus Perspective Touch+ Avionics System........5 Overview ..................5 Operation..................6 Power Source .................. 6 GDU 1450W/1250W Primary Flight Display........10 Overview ..................10 Operation..................10 Power Source ................
Page 156 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ABLE OF ONTENTS Power Source ................16 GTX 335 Mode S Transponder (If Installed)........16 Overview..................16 Operation ..................16 Power Source ................16 GMA 36B Audio Panel..............17 Overview..................17 Operation ..................17 Power Source ................
Page 157 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Gateway Module (If Installed)............22 Overview ..................22 Operation..................22 Power Source ................22 GRA 55 Radar Altimeter (If Installed)..........23 Overview ..................23 Operation..................23 Power Source ................23 GDL 60 LTE/Wi-Fi Datalink (If Installed) .........
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Page 159 GDL 60 LTE/Wi-Fi Datalink (if installed) • Flight Stream 510 Wireless Avionics Interface (if installed) Refer to Cirrus Perspective Touch+ Avionics System Pilot’s Guide (P/N 190-02955-XX) for a detailed description of the system and its oper- ating modes. P/N 44766-001...
Page 160 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS Operation For specific avionics component operation details, refer to the applicable system. Power Source For specific avionics component circuit protection details, refer to the applicable system. 17-6 P/N 44766-001 Revision 1...
Page 161 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 VIONICS Figure 17-1: Perspective Touch+ Schematic - Serials 9750 thru 10614 (1 of 3) XM SATELLITE DATA LINK RECEIVER (optional) TOUCH TOUCH SCREEN #1 SCREEN #2 MAG #1 MAG #2 AUTOPILOT MODE CONTROLLER...
Page 162 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS Figure 17-1: Perspective Touch+ Schematic - Serials 10615 & subs w/ Dual ADAHRS (2 of 3) XM SATELLITE DATALINK RECEIVER (optional) TOUCH SCREEN #2 TOUCH SCREEN #1 AUTOPILOT MODE CONTROLLER MAG #1...
Page 163 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 VIONICS Figure 17-1: Perspective Touch+ Schematic - Serials 10615 & subs w/ Triple ADAHRS (3 of 3) XM SATELLITE DATALINK RECEIVER (optional) TOUCH SCREEN #2 TOUCH SCREEN #1 MAG #1 AUTOPILOT MODE CONTROLLER...
Page 164 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS GDU 1450W/1250W Primary Flight Display Overview The Primary Flight Display (PFD), located directly in front of the pilot, is the primary display of flight parameter information (attitude, airspeed, heading, and altitude) during normal operations. The PFD also displays communication and navigation frequencies and displays warning/status annunciations on airplane systems.
Page 165 IRRUS ILOT NFORMATION ANUAL HAPTER SR22 VIONICS Operation The MFD accepts data from a variety of sources through a high-speed data bus connection. During reversionary operation (PFD failure), or when the DISPLAY BACKUP push button is selected, a PFW is available on the MFD to display information typically available on the PFD.
Page 166 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS Figure 17-2: Cirrus Perspective Touch+ Avionics System Schematic (1 of 2) DISPLAY BACKUP BARO PUSH STD GARMIN GARMIN LEGEND 1. Softkeys 2. PFD 3. Baro Knob 4. Display Backup Push Button 5. MFD 6.
Page 167 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 VIONICS Figure 17-2: Cirrus Perspective Touch+ Avionics System Schematic (2 of 2) GARMIN LEGEND 1. Small Upper Knob 2. Large Upper Knob 3. Softkeys 4. Lower Knob SR22_PM17_1099 P/N 44766-001 17-13 Revision 1...
Page 168 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS GSU 75 Air Data, Attitude & Heading Reference System Overview The Air Data, Attitude, and Heading Reference System (ADAHRS) unit(s), mounted behind the PFD, includes the Attitude and Heading Reference System (AHRS) and the Air Data Computer (ADC).
Page 169 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 VIONICS GIA 64W Integrated Avionics Units Overview The integrated avionics units, located forward of the MFD and PFD, func- tion as the main integration hub, linking all integrated avionics system components with the flight displays.
Page 170 Power Source 28 VDC for Mode S transponder operation is provided through the 2-amp XPDR circuit breaker on Main Bus 1. Refer to the Cirrus Perspective Touch+ Avionics System Guide for a complete description of the system, its operating modes, and additional detailed operating procedures.
Page 171 Operation The satellite weather system is controlled by GTC or the Flight Stream 510 Wireless Avionics Interface. Refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide for a complete description of the system, its operating modes, and additional detailed operating procedures.
Page 172 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS GSR 56 Iridium Satellite Network Transceiver (If Installed) Overview The Iridium satellite network transceiver, mounted in the empennage avionics compartment, communicates with the primary integrated avionics unit and audio panel to provide near real-time weather, voice, and data services to the cabin audio system and integrated displays.
Page 173 Power Source 28 VDC for TAS operation is provided through the 5-amp TRAFFIC circuit breaker on Main Bus 1. Refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide for a general description of the system and its operating modes.
Page 174 MFW every two seconds via the secondary integrated avionics unit. Refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide for a general description of the system and its operating modes.
Page 175 AM broadcast band. The ADF antenna is located on the fuselage belly. Operation Refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide for a general description of the system and its operating modes. Power Source 28 VDC for ADF operation is provided through the 3-amp DME/ADF circuit breaker on Main Bus 1.
Page 176 The gateway module provides a cellular connection while on the ground for automatic transmission of aircraft data. This data can then be accessed by the pilot via a mobile application provided by Cirrus. The gateway module also provides access to the current status of aircraft consumables when the aircraft is unattended by remotely powering select systems on the aircraft when requested via the mobile application Cirrus IQ.
Page 177 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 VIONICS GRA 55 Radar Altimeter (If Installed) Overview The GRA 55 Radar Altimeter is composed of a transceiver that is mounted under the RH passenger seat and two radar altimeter antennas. Operation The GRA 55 Radar Altimeter measures AGL altitudes from 0 to 2,500 feet.
Page 178 5-amp GTC 1B/MFD B circuit breaker on Main Bus 1. For a complete description of the Flight Stream 510 system, its operating modes, and additional detailed operating procedures, refer to the Cirrus Perspective Touch+ Avionics System Pilot’s Guide. Hour Meters Overview Total and flight hours are calculated by the avionics.
Page 179 28 VDC for headset power is provided through the 1-amp headset power fuse located behind the circuit breaker panel. Avionics Cooling Fans Overview Three electric fans provide forced ambient-air cooling for the Cirrus Perspective Touch+ Avionics System. P/N 44766-001 17-25...
Page 180 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 VIONICS Operation A fan located forward of the instrument panel provides ambient air cooling directly to the integrated avionics units. Two additional fans blow air directly onto the heat sinks located on the forward sides of the PFD and MFD.
Page 181 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 18: Cabin Features Table of Contents Cabin Features..................3 Emergency Locator Transmitter (ELT) ..........3 Overview ..................3 Operation..................3 Fire Extinguisher ................6 Overview ..................6 Operation..................6 USB Ports..................
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Page 183 The transmitter is automatically activated upon sensing a change of velocity along its longitudinal axis exceeding 4 to 5 feet per second, or upon sensing deployment of the Cirrus Airframe Parachute System (CAPS). Once activated, the ELT transmits VHF band audio sweeps at 121.5 MHz until battery power is gone.
Page 184 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ABIN EATURES To Use ELT Portably The ELT transmitter can be removed from the airplane and used as a personal locating device if it is necessary to leave the airplane after an acci- dent.
Page 185 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABIN EATURES Figure 18-1: Artex ELT 1000 System CENTER CONSOLE (REF) STARTER DISABLE ARM/ TEST TO TEST: PRESS TEST FOR 1 SECOND THEN RELEASE ELT SHELF (REF) LEGEND 1. Remote Switch 2. LED Annunciator 3.
Page 186 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ABIN EATURES Fire Extinguisher Overview A liquefied-gas-type fire extinguisher, containing Halon 1211, is mounted on the forward inboard side of the copilot footwell. The extinguisher is approved for use on class B (liquid, grease) and class C (electrical equip- ment) fires.
Page 187 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABIN EATURES USB Ports Overview Four Universal Serial Bus (USB) charging ports are installed throughout the aircraft. Two ports are located in the forward center console storage cubby, and one port is located in the left and one in the right aft storage pocket.
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Page 189 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 19: Recovery System Table of Contents Recovery System ................3 Cirrus Airframe Parachute System ............ 3 Overview ..................3 Operation..................4 Controls ................... 5 P/N 44766-001 19-1 Original Issue...
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Page 191 Recovery System Cirrus Airframe Parachute System The airplane is equipped with a Cirrus Airframe Parachute System (CAPS) designed to bring the airplane and its occupants to the ground in the event of a life-threatening emergency. The system is intended to save the lives of the occupants but will most likely destroy the airplane and may, in adverse circumstances, cause serious injury or death to the occupants.
Page 192 ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ECOVERY YSTEM A three-point harness connects the airplane fuselage structure to the para- chute. The aft harness strap is stowed in the parachute canister and attached to the structure at the aft baggage compartment bulkhead. The forward harness straps are routed from the canister to firewall attach points just under the surface of the fuselage skin.
Page 193 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ECOVERY YSTEM Controls Activation Handle CAPS is initiated by pulling the CAPS activation T-handle installed in the cabin ceiling on the airplane centerline just above the pilot’s right shoulder. Pulling the activation T-handle will activate the rocket and initiate the CAPS deployment sequence.
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Page 195 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE ONTENTS Chapter 20: Safe Return Autoland System Table of Contents Recovery System ................3 Safe Return Autoland (If Installed) ............ 3 Overview ..................3 Operation..................3 Controls ................... 5 Indications ..................5 Power Source ..................
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Page 197 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ECOVERY YSTEM Recovery System Safe Return Autoland (If Installed) Overview The Safe Return Autoland system is designed to safely land the aircraft and its passengers on autopilot in the event the pilot becomes incapacitated.
Page 198 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ECOVERY YSTEM Initial State When Safe Return Autoland is in the initial state, the following occurs: • The displays (PDF, MFD, and GTCs) switch to Safe Return Autoland mode. • The system begins transmitting automated text-to-speech voice messages over automatically tuned COM frequencies, including the 121.5 MHz emergency frequency.
Page 199 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ECOVERY YSTEM Secure Airplane After the airplane has stopped, Safe Return Autoland will automatically shut down the engine by removing power to the electric fuel pump and moving the mixture to the cutoff position. Instructions will then be provided on the displays and audio on how to safely exit the aircraft.
Page 200 ’ ILOT NFORMATION ANUAL HAPTER IRRUS SR22 ECOVERY YSTEM 28 VDC for Safe Return Autoland operation is provided through 1-amp EMER AUTOLAND circuit breaker on Main Bus 1. ELATED ABLE IGURE Refer to “Figure 20-1: Safe Return Autoland”. 20-6 P/N 44766-001...
Page 201 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ECOVERY YSTEM Figure 20-1: Safe Return Autoland SAFE RETURN AUTOLAND EMERGENCY USE ONLY PRESS TO ACTIVATE LEGEND 1. Safe Return Autoland NOTE Activated Indicator 2. Safe Return Autoland Illuminated green when Safe Return Push Button Autoland is activated.
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Page 203 ’ IRRUS ILOT NFORMATION ANUAL HAPTER SR22 ABLE OF ONTENTS Chapter 21: Log of Supplements Table of Contents As Required Log of Supplements P/N 44766-001 21-1 Revision 1...
Page 204 ONTENTS Applicable PIM Supplements should be inserted in this chapter. This Log of Supplements shows all Cirrus Aircraft Supple- ments available for the aircraft at the corresponding date of the revision level shown in the lower left corner. A check mark in the Part Number column indicates that the supple- ment is applicable to the PIM.

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