Cirrus SR20 Specifications

PILOT’S OPERATING HANDBOOKAND FAA APPROVEDAIRPLANE FLIGHT MANUALfor theCIRRUS DESIGN SR20Aircraft Serials 2016 and Subsequent with Cirrus Perspective

Front Matter-4 P/N 11934-004Section Front Matter Cirrus DesignForeword SR20 Revision ServiceRevision service for this Handbook is provided at no cost

3A-8 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Integrated Avionics SystemAvionics Switch OffAVIONICS OFF CautionThe AVIONICS maste

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-9MFD Cooling Fan FailureMFD FAN FAIL AdvisoryThe cooling fan for the MFD is inoperati

3A-10 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Pitot Static SystemPitot Static MalfunctionStatic Source BlockedIf erroneous readi

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-11Pitot Heat Required AnnunciationPITOT HEAT REQUIRED CautionDisplayed 20 seconds aft

3A-12 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Flight Control SystemElectric Trim/Autopilot FailureAny failure or malfunction of

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-13Landing Gear SystemBrake Failure During TaxiGround steering is accomplished by diff

3A-14 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Other ConditionsAborted TakeoffUse as much of the remaining runway as needed to sa

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-15Parking Brake Engaged AnnunciationPARK BRAKE CautionParking brake is set.1. Parking

3A-16 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Revision 1Intentionally Left Blank

P/N 11934-004 4-1Cirrus Design Section 4SR20 Normal ProceduresSection 4Normal ProceduresTable of ContentsIntroduction ...

Cirrus Design Section Front MatterSR20 ForewordP/N 11934-004 Front Matter-5Retention of DataIn the event a new title page is issued, the weight and ba

4-2 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Original IssueIntentionally Left Blank

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-3IntroductionThis section provides amplified procedures for normal operation.Normal proce

4-4 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Normal ProceduresPreflight InspectionBefore carrying out preflight inspections, ensure

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-51. Cabina. Required Documents...On Boardb.

4-6 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 3. Empennagea. Tiedown Rope ...

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-7e. Tire ...Condition, Inflation, and Wear• Caut

4-8 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 d. External Power ...Door Securee. Ex

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-9Before Starting Engine1. Preflight Inspection ...

4-10 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Starting EngineIf the engine is warm, no priming is required. For the first start of t

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-116. Power Lever ... FULL FORWARD7.

Front Matter-6 P/N 11934-004Section Front Matter Cirrus DesignForeword SR20 Original IssueIntentionally Left Blank

4-12 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Before Taxiing1. Flaps ...

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-13Before TakeoffDuring cold weather operations, the engine should be properlywarmed up be

4-14 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 16. Pitot Heat ... AS REQU

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-15Takeoff• Note •The engine is equipped with an altitude compensating fuelpump that autom

4-16 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Normal Takeoff1. Brakes...RELEASE (Steer with Rudder

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-17ClimbNormal climbs are performed flaps UP (0%) and full power at speeds 5to 10 knots hi

4-18 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 CruiseNormal cruising is performed between 55% and 85% power. Theengine power setting

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-19Cruise LeaningThe engine is equipped with an altitude compensating fuel pump thatautoma

4-20 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Descent1. Altimeter...

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-21Landing• Caution •Landings should be made with full flaps. Landings with lessthan full

P/N 11934-004 1-1Cirrus Design Section 1SR20 GeneralSection 1GeneralTable of ContentsIntroduction ...

4-22 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Balked Landing/Go-AroundIn a balked landing (go-around) climb, disengage autopilot, ap

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-23Shutdown1. Fuel Pump (if used) ...

4-24 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Environmental ConsiderationsCold Weather Operation• Caution •An engine that has been s

Cirrus Design Section 4SR20 Normal ProceduresP/N 11934-004 4-251. Ignition Switch...

4-26 P/N 11934-004Section 4 Cirrus DesignNormal Procedures SR20 Hot Weather OperationAvoid prolonged engine operation on the ground. Fuel BOOST mustbe

P/N 11934-004 5-1Cirrus Design Section 5SR20 Performance DataSection 5Performance DataTable of ContentsIntroduction ...

5-2 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Original IssueIntentionally Left Blank

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-3IntroductionPerformance data in this section are presented for operationalplanning so tha

5-4 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Airspeed Calibration - Normal Static Source• Note •Indicated airspeed values assume zero

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-5Airspeed Calibration - Alternate Static Source• Note •Indicated airspeed values assume ze

1-2 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 Original IssueIntentionally Left Blank

5-6 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Altitude Correction - Normal Static Source• Note •Add correction to desired altitude to

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-7Altitude Correction - Alternate Static Source• Note •Add correction to desired altitude t

5-8 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Temperature ConversionTo convert from Celsius (°C) to Fahrenheit (°F), find, in the shad

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-9Outside Air Temperature for ISA ConditionPressAltFeetISA-40°C ISA-20°C ISA ISA+10°C ISA+

5-10 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Stall Speeds• Note •Altitude loss during wings level stall may be 250 feet or more.KIAS

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-11Wind Components• Note •The max demonstrated crosswind is 20 knots. Value not considered

5-12 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Takeoff Distance• Note •The following factors are to be applied to the computed takeoff

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-13Takeoff Distance - 3050 LBWEIGHT = 3050 LBSpeed at Liftoff = 71 KIASSpeed over 50 Ft. Ob

5-14 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Takeoff Distance - 2500 LBWEIGHT = 2500 LBSpeed at Liftoff = 68 KIASSpeed over 50 Ft Ob

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-15Takeoff Climb Gradient• Note •Climb Gradients shown are the gain in altitude for the hor

Cirrus Design Section 1SR20 GeneralP/N 11934-004 1-3IntroductionThis section contains information of general interest to pilots andowners. You will f

5-16 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Takeoff Rate of Climb• Note •Rate-of-Climb values shown are change in altitude for unit

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-17Enroute Climb Gradient• Note •Climb Gradients shown are the gain in altitude for the hor

5-18 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Enroute Rate of Climb• Note •Rate-of-Climb values shown are change in altitude in feet

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-19Enroute Rate of Climb Vs Density Altitude Conditions:• Power ...

5-20 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Time, Fuel and Distance to Climb• Note •Taxi Fuel - Add 1.5 gallon for start, taxi, and

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-21Cruise Performance• Note •Subtract 10 KTAS if nose wheel pant and fairing removed. Lower

5-22 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Cruise Performance (Continued)8000 Feet Pressure AltitudeISA - 30° C (-31° C) ISA (-1°

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-23Range / Endurance Profile• Note •Fuel Remaining For Cruise accounts for 10.1 gallons for

5-24 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Range / Endurance Profile (Continued)65% POWER Mixture = Best PowerPress AltFTClimbFuel

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-25Balked Landing Climb Gradient• Note •Balked Landing Climb Gradients shown are the gain i

1-4 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 Figure 1-1Airplane Three View74 inches 3-BLADE188 cm38.3 ft11.67 m9.1 ft2.8 m9 inches (minimum)23

5-26 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Balked Landing Rate of Climb• Note •Balked Landing Rate of Climb values shown are the f

Cirrus Design Section 5SR20 Performance DataP/N 11934-004 5-27Landing Distance• Note •The following factors are to be applied to the computed landing

5-28 P/N 11934-004Section 5 Cirrus DesignPerformance Data SR20 Landing DistanceWEIGHT = 3050 LBSpeed over 50 Ft Obstacle = 77 KIASFlaps - 100% · Idle

P/N 11934-004 6-1Cirrus Design Section 6SR20 Weight and Balance DataSection 6Weight and Balance DataTable of ContentsIntroduction ...

6-2 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 Original IssueIntentionally Left Blank

Cirrus Design Section 6SR20 Weight and Balance DataP/N 11934-004 6-3IntroductionThis section describes the procedure for establishing the basic empty

6-4 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 Airplane Weighing FormWeighing PointScale Reading- Tare = Net Weight X Arm = Mome

Cirrus Design Section 6SR20 Weight and Balance DataP/N 11934-004 6-5Airplane Weighing ProceduresA basic empty weight and center of gravity were estab

6-6 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 side of the firewall (FS 100). Add 100 to this measurement toobtain left and righ

Cirrus Design Section 6SR20 Weight and Balance DataP/N 11934-004 6-7Airplane LevelingFigure 6-2SR22_FM06_1440ASpirit LevelLONGITUDINAL LEVELINGLATERA

Cirrus Design Section 1SR20 GeneralP/N 11934-004 1-5Location Length Width Height VolumeCabin122” 49.3” 49.7 137 cu ftBaggage Compartment36” 39.8” 38.

6-8 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 Loading InstructionsIt is the responsibility of the pilot to ensure that the airp

Cirrus Design Section 6SR20 Weight and Balance DataP/N 11934-004 6-9Weight and Balance Loading Form• Note •For Center of Gravity Envelope, refer to S

6-10 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 Loading DataUse the following chart or table to determine the moment/1000 for fu

Cirrus Design Section 6SR20 Weight and Balance DataP/N 11934-004 6-11Moment LimitsUse the following chart or table to determine if the weight and mom

6-12 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 Weight & Balance RecordUse this form to maintain a continuous history of cha

Cirrus Design Section 6SR20 Weight and Balance DataP/N 11934-004 6-13Equipment ListThis list will be determined after the final equipment has been in

6-14 P/N 11934-004Section 6 Cirrus DesignWeight and Balance Data SR20 Original IssueIntentionally Left Blank

P/N 11934-004 7-1Cirrus Design Section 7SR20 Airplane and Systems DescriptionSection 7Airplane and Systems DescriptionTable of ContentsIntroduction .

7-2 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Ignition and Starter System...

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-5IntroductionThis section provides a basic description and operation of t

1-6 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 Figure 1-3Turning Radius9.1 ft. (2.77 m)0.5 ft. (0.15 m)24.3 ft. (7.41 m)7.0 ft. (2

7-6 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 AirframeFuselageThe aircraft’s monocoque fuselage is constructed primari

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-7EmpennageThe empennage consists of a horizontal stabilizer, a two-piecee

7-8 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Flight ControlsThe aircraft uses conventional flight controls for ailero

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-9Figure 7-1Elevator SystemSR20_FM07_1461Original Issue

7-10 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Aileron SystemThe ailerons provide airplane roll control. The ailerons

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-11Figure 7-2Aileron SystemSR20_FM07_1462Original Issue

7-12 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Rudder SystemThe rudder provides airplane directional (yaw) control. Th

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-13Figure 7-3Rudder SystemSR20_FM07_1463Original Issue

7-14 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Instrument PanelThe instrument panel is of all metal construction and i

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-15Figure 7-4Instrument Panel and Console151820213459111012141716136478619

Cirrus Design Section 1SR20 GeneralP/N 11934-004 1-7The AirplaneEngineNumber of Engines...

7-16 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Flight InstrumentsFlight instruments and annunciations are displayed on

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-17Figure 7-5Flight Instruments LEGEND 1. True Airspeed 2. Airspeed

7-18 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Attitude IndicatorThe primary attitude indicator is show on the upper c

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-19Airspeed IndicatorPrimary airspeed data is provided by the Air Data Com

7-20 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 AltimeterPrimary altitude data is provided by the Air Data Computer and

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-21The HSI presents heading, turn rate, course deviation, bearing, andnavi

7-22 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Wing FlapsThe electrically controlled, single-slotted flaps provide low

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-23Figure 7-6Wing FlapsSR20_FM07_1460Original Issue

7-24 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Landing GearMain GearThe main landing gear are bolted to composite wing

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-25each brake assembly which transmit signals via the Engine AirframeUnit

Copyright © 2008 - All Rights ReservedCirrus Design Corporation4515 Taylor CircleDuluth, MN 55811

1-8 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 FuelTotal Capacity ...58.5 U.S. Gallons (221.0 L)Total

7-26 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Baggage CompartmentThe baggage compartment door, located on the left si

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-27SeatsThe seating arrangement consists of two individually adjustable se

7-28 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Seat Belt and Shoulder HarnessIntegrated seat belt and shoulder harness

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-294. Restraint harnesses should fit snug against the shoulder with thelap

7-30 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 EngineThe aircraft is powered by a Teledyne Continental IO-360-ES, six-

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-31Mixture ControlThe mixture control lever, labeled RICH-MIXTURE-CUTOFF,

7-32 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Engine IndicatingEngine information is displayed as analog-style gages,

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-33Figure 7-7Engine Controls and IndicatingDensity Alt 8000 FtOat

7-34 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 TachometerEngine speed (RPM) is shown in the upper mid-left corner of t

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-35Oil TemperatureOil temperature is shown in the upper right corner of th

Cirrus Design Section 1SR20 GeneralP/N 11934-004 1-9Symbols, Abbreviations and TerminologyGeneral Airspeed Terminology and SymbolsKCAS Knots Calibrat

7-36 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Engine Lubrication SystemThe engine is provided with a wet-sump, high-p

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-37finally through the cylinder intake ports into the combustion chambers.

7-38 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 PropellerThe airplane is equipped with a constant-speed, aluminum-alloy

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-39Fuel SystemAn 56-gallon usable wet-wing fuel storage system provides fu

7-40 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 contamination and grade. The fuel must be sampled prior to eachflight.

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-41Figure 7-8Fuel System SchematicCHECKVALVECHECKVALVETHROTTLEMETERING V

7-42 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Fuel IndicatingFuel system information is displayed as analog-style gag

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-43Figure 7-9Fuel System Controls and Indicating7134568Fuel System Indicat

7-44 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Each indicator also provides an output signal to the Engine AirframeUni

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-45Fuel Totalizer and Calculated InformationFuel totalizer calculations ar

1-10 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 Meteorological TerminologyVSOStalling Speed is the minimum steady flight speed atwhich the aircr

7-46 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Electrical SystemThe airplane is equipped with a two-alternator, two-ba

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-47Figure 7-10Electrical System Schematic30ABAT 2SWITCHBAT 2AVIONICSSWITCH

7-48 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Power DistributionPower is supplied to the airplane circuits through th

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-49Main Distribution Bus 2The output from ALT 2 is connected to the Main D

7-50 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Main Distribution Bus 1 or Main Distribution Bus 2 in the MCU. In theca

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-51Electrical System ControlThe rocker type electrical system MASTER switc

7-52 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 AVIONICS Master SwitchA rocker switch, labeled AVIONICS, controls elect

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-53Electrical IndicatingElectrical system information is displayed as bar

7-54 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Figure 7-11Electrical / Lighting Controls and Indicating LEGEND 1

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-55Lighting SystemsExterior LightingThe airplane is equipped with wing tip

Cirrus Design Section 1SR20 GeneralP/N 11934-004 1-11Engine Power TerminologyPerformance and Flight Planning Terminology• Pressure Altitude is the al

7-56 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Interior LightingInterior lighting for the airplane consists of separat

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-57Environmental SystemStandard cabin heating and ventilation is accomplis

7-58 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Figure 7-12Environmental SystemFLOOR AIRFLOWAIR FLOW VALVEHOT AIRVALVES

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-59DistributionFrom the mixing chamber, the air is distributed by either r

7-60 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Pressing the Panel-Foot selector button opens the cabin floor butterfly

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-61Stall Warning SystemThe airplane is equipped with an electro-pneumatic

7-62 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Pitot-Static SystemThe Pitot-Static system consists of a single heated

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-63Figure 7-13Pitot-Static System STATICBUTTONSPITOT HEATPFD Air DataSR20

7-64 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 AvionicsPerspective Integrated Avionics SystemThe Perspective Integrate

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-65Figure 7-14Perspective Integrated Avionics System SchematicTRANSPONDERE

1-12 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 Weight and Balance TerminologyNMPG Nautical Miles Per Gallon is the distance (in nautical miles)

7-66 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 GDU Primary Flight DisplayThe Primary Flight Display, located directly

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-67MAIN BUS 3 and the 5-amp MFD PWR 2 circuit breaker on MAIN BUS1. Either

7-68 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Figure 7-15Perspective Integrated Avionics System (Sheet 1 of 2)111

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-69Figure 7-15Perspective Integrated Avionics System (Sheet 2 of 2)Flight

7-70 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 GIA 63W Integrated Avionics UnitsThe Integrated Avionics Units, located

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-71GMA 347 Audio Panel with Integrated Marker Beacon ReceiverThe Audio Pan

7-72 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Optional AvionicsGFC 700 3-Axis Autopilot and GMC 705 Autopilot Control

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-73information is displayed on the MFD and indicates the relative range,be

7-74 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 information. 28 VDC for ADF System operation is supplied through the3-a

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-75• Flight path marker,• Terrain warning system,• Field of view depiction

Cirrus Design Section 1SR20 GeneralP/N 11934-004 1-13• Station is a location along the airplane fuselage measuredin inches from the reference datum a

7-76 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Figure 7-16Equipment Locations15171665428SR20_FM07_3011 LEGEND 1.

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-77Avionics Support EquipmentAntennasTwo rod-type COM antennas are mounted

7-78 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Headset and Microphone InstallationThe airplane is equipped with provis

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-79Cabin FeaturesEmergency Locator TransmitterThe airplane is equipped wit

7-80 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 b. Disconnect fixed antenna lead from front of unit.c. Disconnect lead

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-81Hour MetersThe airplane is equipped with two hour meters located inside

7-82 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Cirrus Airplane Parachute SystemThe aircraft is equipped with a Cirrus

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-83rate at which the parachute inflates. As the slider moves down thesuspe

7-84 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Pulling the activation T-handle straight down generates thegreatest for

Cirrus Design Section 7SR20 Airplane and Systems DescriptionP/N 11934-004 7-85Deployment CharacteristicsWhen the rocket launches, the parachute assem

1-14 P/N 11934-004Section 1 Cirrus DesignGeneral SR20 Original IssueIntentionally Left Blank

7-86 P/N 11934-004Section 7 Cirrus DesignAirplane and Systems Description SR20 Original IssueIntentionally Left Blank

P/N 11934-004 8-1Cirrus Design Section 8SR20 Handling, Servicing, & MaintenanceSection 8Handling, Servicing, & MaintenanceTable of ContentsIn

8-2 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, & Maintenance SR20 Original IssueIntentionally Left Blank

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-3IntroductionThis section provides general guidelines for handling, s

8-4 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 • Service Advisory Notices – are used to notify you of optionalServi

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-5Airplane Records and CertificatesThe Federal Aviation Administration

8-6 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Airworthiness DirectivesThe Federal Aviation Administration (FAA) pu

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-7only be performed by a licensed Airframe and Powerplant (A&P)mec

8-8 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Pilot Performed Preventative MaintenanceThe holder of a Pilot Certif

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-9• Replace any hose connection, except hydraulic connections,with rep

P/N 11934-004 2-1Cirrus Design Section 2SR20 LimitationsSection 2LimitationsTable of ContentsIntroduction ...

8-10 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Ground HandlingApplication of External PowerA ground service recept

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-11TowingThe airplane may be moved on the ground by the use of the nos

8-12 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 TaxiingBefore attempting to taxi the airplane, ground personnel sho

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-13ParkingThe airplane should be parked to protect the airplane from w

8-14 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 TiedownThe airplane should be moored for immovability, security and

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-15Raise Airplane• Caution •Do not jack the aircraft outside or in ope

8-16 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 ServicingLanding Gear ServicingThe main landing gear wheel assembli

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-17• Leaking brake fluid at the caliper. This can be observed bychecki

8-18 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Tire InflationFor maximum service from the tires, keep them inflate

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-19sooner under unfavorable operating conditions. The following grades

2-2 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Placards ...

8-20 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Product SupplierAeroshell (R) W Shell AustraliaAeroshell Oil WAeros

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-21Fuel System ServicingFuel Filtration Screen/Element After the first

8-22 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 • Note •Do not permit fuel nozzle to come in contact with bottom of

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-23The gascolator incorporates a filter bypass that activates a red, p

8-24 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Battery ServiceThe aircraft is delivered with a maintenance free, r

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-25Cleaning and CareCleaning Exterior Surfaces• Note •Prior to cleanin

8-26 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Cleaning Product Cleaning Application SupplierPure Carnauba Wax Fus

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-27Windscreen and WindowsBefore cleaning an acrylic window, rinse away

8-28 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Do not use abrasive cleansers or cleaning pads on thegermanium wind

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-293. Allow the solvent to remain on the gear from five to ten minutes

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-3IntroductionThe limitations included in this Section of the Pilot’s OperatingHandbook (POH) ar

8-30 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Cleaning Product Cleaning Application SupplierPrist Interior Windsc

Cirrus Design Section 8SR20 Handling, Servicing, and MaintenanceP/N 11934-004 8-31Instrument Panel and Electronic Display ScreensThe instrument panel

8-32 P/N 11934-004Section 8 Cirrus DesignHandling, Servicing, and Maintenance SR20 Leather Upholstery and SeatsFor routine maintenance, occasionally w

Cirrus Design Section 9SR20 SupplementsP/N 11934-004 9-1Section 9SupplementsThis section of the handbook contains FAA Approved Supplementsnecessary to

9-2 P/N 11934-004Section 9 Cirrus DesignSupplements SR20 Original IssueIntentionally Left Blank

P/N 11934-004 9-3Cirrus Design Section 9SR20 Log of SupplementsSection 9Log of SupplementsPart Number Title Date___ 11934-S17 SR20 Airplanes Register

9-4 P/N 11934-004Section 9 Cirrus DesignLog of Supplements SR20 Revision 1FAA Approved POH Supplements must be in the airplane for flight operations w

P/N 11934-S36 1 of 8Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforArtex ME406 4

2 of 8 P/N 11934-S36Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThe 406 MHz emergency locator transmitter (ELT) is a radio-frequencytran

P/N 11934-S36 3 of 8Cirrus Design Section 9SR20 SupplementsSection 2 - LimitationsNo Change.Section 3 - Emergency ProceduresForced LandingBefore perfo

P/N 11934-004 ACirrus Design Pilot’s Operating HandbookSR20 List of Effective PagesList of Effective PagesUse this page to determine the current effec

2-4 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Airspeed LimitationsThe indicated airspeeds in the following table are based upon Section5 Ai

4 of 8 P/N 11934-S36Section 9 Cirrus DesignSupplements SR20Portable Use of ELTThe ELT transmitter can be removed from the airplane and used as aperson

P/N 11934-S36 5 of 8Cirrus Design Section 9SR20 SupplementsSection 7 - Systems DescriptionThis airplane is equipped with a self-contained Artex ME406

6 of 8 P/N 11934-S36Section 9 Cirrus DesignSupplements SR20Section 8 - Handling, Servicing & MaintenanceELT and RCPI batteries must be inspected i

P/N 11934-S36 7 of 8Cirrus Design Section 9SR20 Supplementssystem or provide the same level of confidence as does anAM radio.1. Tune aircraft receiver

8 of 8 P/N 11934-S36Section 9 Cirrus DesignSupplements SR20Revision 01: 12-18-08Intentionally Left Blank

P/N 11934-S41 1 of 16Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforGarmin GFC 7

2 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThe aircraft is equipped with a Garmin GFC 700 digital AutomaticFlight

P/N 11934-S41 3 of 16Cirrus Design Section 9SR20 Supplements7. The autopilot and flight director will not command pitch or rollbeyond the Command Limi

4 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Section 3A - Abnormal ProceduresAutopilot MiscompareAP MISCOMP CautionAutopilot miscompare

P/N 11934-S41 5 of 16Cirrus Design Section 9SR20 SupplementsAltitude Selection DeviationALTITUDE SEL AdvisoryThe pilot has programmed the autopilot to

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-5Airspeed Indicator MarkingsThe airspeed indicator markings are based upon Section 5 AirspeedCa

6 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Before Taxiing1. Manual Electric Trim...

P/N 11934-S41 7 of 16Cirrus Design Section 9SR20 SupplementsSection 7 - System DescriptionThis airplane is equipped with a GFC 700 - a two axis, fully

8 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Figure - 1GFC 705MODE CONTROLLERPITCH TRIMCARTRIDGEINTEGRATEDAVIONICS UNIT 2INTEGRATEDAVIO

P/N 11934-S41 9 of 16Cirrus Design Section 9SR20 SupplementsGFC 705 AFCS Mode ControllerThe GFC 705 AFCS Mode Controller, located in the upper section

10 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20view, will deactivate the Flight Director and remove the command barsunless the autopilot

P/N 11934-S41 11 of 16Cirrus Design Section 9SR20 SupplementsFlight Management System KeyboardThe Flight Management System Keyboard, found in the cent

12 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Figure - 2347812 13116914 15HDG NAVAP LVL IAS ALTAPRFD VSVNVUPDNFlight Management System

P/N 11934-S41 13 of 16Cirrus Design Section 9SR20 SupplementsRoll and Pitch ServoThe Roll Servo, located below the passenger seat, and the PitchServo,

14 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Autopilot Disconnect SwitchThe yoke mounted Autopilot Disconnect Switch disengages theaut

P/N 11934-S41 15 of 16Cirrus Design Section 9SR20 SupplementsAnnunciation System• Note •Refer to the Cirrus Perspective Pilot’s Guide for a detailedde

2-6 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Powerplant LimitationsEngineTeledyne Continental ...

16 of 16 P/N 11934-S41Section 9 Cirrus DesignSupplements SR20Section 8 – Handling, Service, & MaintenanceNo Change.Section 10 – Safety Information

P/N 11934-S42 1 of 6Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight Manual Supplementfor the Garmin

2 of 6 P/N 11934-S42Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThe airplane is equipped with the Garmin Terrain Awareness/WarningSystem

P/N 11934-S42 3 of 6Cirrus Design Section 9SR20 SupplementsSection 3 - Emergency ProceduresTo prevent unwanted aural alerting during ditching or other

4 of 6 P/N 11934-S42Section 9 Cirrus DesignSupplements SR20Section 4 - Normal ProceduresNormal operating procedures are outlined in the Cirrus Perspec

P/N 11934-S42 5 of 6Cirrus Design Section 9SR20 SupplementsSystem ConstraintsSystem test at startup: Aural tone lasting approximately one secondindica

6 of 6 P/N 11934-S42Section 9 Cirrus DesignSupplements SR20Original Issue: 12-18-08Intentionally Left Blank

P/N 11934-004 10-1Cirrus Design Section 10SR20 Safety InformationSection 10Safety InformationTable of ContentsIntroduction ...

10-2 P/N 11934-004Section 10 Cirrus DesignSafety Information SR20 Original IssueIntentionally Left Blank

Cirrus Design Section 10SR20 Safety InformationP/N 11934-004 10-3IntroductionThis aircraft is designed to operate safely and efficiently in a flighten

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-7Propeller• Note •Two-blade propellers are not EASA approved for use on thisairplane. Airplanes

10-4 P/N 11934-004Section 10 Cirrus DesignSafety Information SR20 Cirrus Airframe Parachute System (CAPS)The Cirrus Airframe Parachute System (CAPS) i

Cirrus Design Section 10SR20 Safety InformationP/N 11934-004 10-5Loss of ControlLoss of control may result from many situations, such as: a controlsys

10-6 P/N 11934-004Section 10 Cirrus DesignSafety Information SR20 General Deployment InformationDeployment SpeedThe maximum speed at which deployment

Cirrus Design Section 10SR20 Safety InformationP/N 11934-004 10-7Landing ConsiderationsAfter a CAPS deployment, the airplane will descend at less than

10-8 P/N 11934-004Section 10 Cirrus DesignSafety Information SR20 • If a door is open prior to touchdown in a CAPS landing, the doorwill most likely b

Cirrus Design Section 10SR20 Safety InformationP/N 11934-004 10-9Post Impact FireIf there is no fire prior to touchdown and the pilot is able to shut

10-10 P/N 11934-004Section 10 Cirrus DesignSafety Information SR20 Taxiing, Steering, and Braking PracticesCirrus aircraft use a castering nose wheel

Cirrus Design Section 10SR20 Safety InformationP/N 11934-004 10-11• Use only as much power (throttle) as is necessary to achieveforward movement. Keep

10-12 P/N 11934-004Section 10 Cirrus DesignSafety Information SR20 Original IssueIntentionally Left Blank

2-8 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Engine Instrument Markings & AnnunciationsThe following describes the engine instrument m

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-9FuelElectrical*20 seconds delay. **30 second delay.Instrument(Range & Units)RedArc/BarYell

2-10 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Center of Gravity LimitsReference Datum ...100 inches forwa

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-11Maneuver LimitsAerobatic maneuvers are prohibited.Spins are prohibited.This airplane is certi

2-12 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Kinds of Operation The aircraft is equipped and approved for the following typeoperations:•

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-13ALT 1 Annunciator 1 1 1 1ALT 2 Annunciator — — 1 1Circuit Breakers A/R A/R A/R A/R As require

B P/N 11934-004Cirrus Design Pilot’s Operating HandbookSR20 List of Effective PagesList of Effective Pages (Cont.)Page Status Page Status Page Status4

2-14 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Ice & Rain ProtectionAlternate Engine Air Induc-tion System1111Alternate Static Air Sour

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-15Altimeter 1 1 1 1Magnetic Compass 1 1 1 1Pitot System 1 1 1 1Static System, Normal 1 1 1 1Att

2-16 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 IcingFlight into known icing conditions is prohibited.Runway SurfaceThis airplane may be ope

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-17Taxi PowerMaximum continuous engine speed for taxiing is 1000 RPM on flat,smooth, hard surfac

2-18 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Systems and Equipment LimitsCirrus Perspective Integrated Avionics System1. The Cirrus Persp

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-19f. RNAV approaches must be conducted utilizing the GPSsensor.g. When conducting missed approa

2-20 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 10. The SYNTHETIC VISION SYSTEM (SVS) cannot be used forflight guidance, navigation, traffic

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-21L-3 Stormscope Weather Information System1. Use of the Stormscope is not intended for hazardo

2-22 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 PlacardsFigure 2-2Placards (Sheet 1 of 6)Upper fuselage, either side of CAPS rocket cover:WA

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-23Figure 2-3Placards (Sheet 2 of 6)NO PUSHElevator and Rudder, both sides:EXTERNAL POWER28 V DC

P/N 11934-004 CCirrus Design Pilot’s Operating HandbookSR20 List of Effective PagesList of Effective Pages (Cont.)Page Status Page Status Page Status8

2-24 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Figure 2-4(Sheet 3 of 6)MAXMIXTUREIDLEFRICTIONBOOSTPRIMEFUELPUMPCUTOFFOFFLIFT BUTTON FOR OFF

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-25Figure 2-5(Sheet 4 of 6)NO STEPRESCUE: FRACTURE AND REMOVE WINDOW OPERATE PER AIRPLANE FLIGHT

2-26 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Figure 2-6(Sheet 5 of 6)Instrument Panel, center:DISPLAYBACKUPGRAB HEREBolster Panel, both s

Cirrus Design Section 2SR20 LimitationsP/N 11934-004 2-27Figure 2-7(Sheet 6 of 6)6. RESTRAINT SYSTEM...SECURE5. MASTER SWITCH...

2-28 P/N 11934-004Section 2 Cirrus DesignLimitations SR20 Original IssueIntentionally Left Blank

P/N 11934-004 3-1Cirrus Design Section 3SR20 Emergency ProceduresSection 3Emergency ProceduresTable of ContentsIntroduction ...

3-2 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Low Fuel Quantity ...

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-3IntroductionThis section provides procedures for handling emergencies andcritical fli

3-4 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Emergency Procedures GuidanceAlthough this section provides procedures for handling

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-5Take Appropriate Action — In most situations, the procedures listedin this section wi

D P/N 11934-004Cirrus Design Pilot’s Operating HandbookSR20 List of Effective PagesList of Effective Pages (Cont.)Page Status Page Status Page StatusR

3-6 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Airspeeds for Emergency OperationsManeuvering Speed:3050 lb ...

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-7Engine FailuresEngine Failure On Takeoff (Low Altitude)If the engine fails immediatel

3-8 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Engine Failure In FlightIf the engine fails at altitude, pitch as necessary to estab

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-9AirstartEngine AirstartThe following procedures address the most common causes foreng

3-10 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Smoke and FireEngine Fire In FlightIf an engine fire occurs during flight, do not a

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-112. Fire Extinguisher... ACT

3-12 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Wing Fire In Flight1. Pitot Heat Switch...

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-13Smoke and Fume EliminationIf smoke and/or fumes are detected in the cabin, check the

3-14 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Emergency DescentEmergency Descent1. Power Lever ...

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-15Forced LandingsIf all attempts to restart the engine fail and a forced landing isimm

Cirrus Design Section Front MatterSR20 ForewordP/N 11934-004 Front Matter-1ForewordThis Pilot’s Operating Handbook (POH or Handbook) has beenprepared

3-16 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Ditching1. Radio... Transmit (121.5 MHz)

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-17Engine System EmergenciesOil Pressure Out of RangeOIL PRESS WarningOil pressure belo

3-18 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Oil Temperature HighOIL TEMP WarningOil temperature is greater than 240°F.1. Oil Te

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-19High Cylinder Head TemperatureCHT Caution and WarningCHT Warning: Temperature of one

3-20 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Engine Partial Power LossIndications of a partial power loss include fluctuating RP

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-211. Fuel Pump ...

3-22 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Propeller System EmergenciesPropeller Governor FailureIf the RPM does not respond t

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-23Fuel System Emergencies High Fuel FlowFUEL FLOW WarningFuel flow greater than 20 GPH

3-24 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Electrical System EmergenciesAlternator FailureThe most likely the cause of the alt

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-25Low Voltage on Essential BusESS BUS WarningIllumination of ESS BUS Warning indicates

Front Matter-2 P/N 11934-004Section Front Matter Cirrus DesignForeword SR20 The HandbookThis Pilot’s Operating Handbook has been prepared using GAMASp

3-26 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Low Alternator 1 Output ALT 1 CautionIllumination of ALT 1 indicates that the amper

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-27Integrated Avionics System Emergencies• Note •A “Red X” through any electronic displ

3-28 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Emergency ExitEmergency Ground Egress• WARNING •While exiting the airplane, make su

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-29Unusual Attitude EmergenciesSpinsThe aircraft is not approved for spins, and has not

3-30 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Inadvertent Spiral Dive During IMC FlightIn all cases, if the aircraft enters an un

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-31Other EmergenciesPower Lever Linkage FailureIf the Power Lever linkage fails in flig

3-32 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Left/Right Brake Over-Temperature AnnunciationBRAKE TEMP WarningBrake temperature i

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-33CAPS DeploymentThe Cirrus Airframe Parachute System (CAPS) should be activated inthe

3-34 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 2. Mixture (If time and altitude permit) ... CUTOFFGe

Cirrus Design Section 3SR20 Emergency ProceduresP/N 11934-004 3-3513. Assume emergency landing body position.The emergency landing body position is as

Cirrus Design Section Front MatterSR20 ForewordP/N 11934-004 Front Matter-3Revising the HandbookTwo types of revisions may be issued for this Handbook

3-36 P/N 11934-004Section 3 Cirrus DesignEmergency Procedures SR20 Original IssueIntentionally Left Blank

P/N 11934-004 3A-1Cirrus Design Section 3ASR20 Abnormal ProceduresSection 3AAbnormal ProceduresTable of ContentsIntroduction ...

3A-2 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Other Conditions ...

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-1IntroductionThis section provides procedures for handling abnormal system and/orflig

3A-2 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Flight EnvironmentInadvertent Icing EncounterFlight into known icing conditions is

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-3Abnormal LandingsLanding With Failed BrakesOne brake inoperative1. Land on the side

3A-4 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Engine SystemLow Idle Oil PressureOIL PRESS CautionOil pressure between 10 psi and

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-5Fuel SystemLeft Fuel Tank QuantityL FUEL QTY AdvisoryLeft fuel quantity is less than

3A-6 P/N 11934-004Section 3A Cirrus DesignAbnormal Procedures SR20 Fuel System (Cont)Fuel Filter in Bypass ModeFUEL FILTER AdvisoryThe fuel filter is

Cirrus Design Section 3ASR20 Abnormal ProceduresP/N 11934-004 3A-7Figure 3A-1Circuit Breaker PanelEVSCAMERACABINFANSTARTERAVIONICSFAN 1RECOGLIGHTSNAVL