Sharp R-360ES Spezifikationen Seite 1

AIRPLANE INFORMATION MANUALfor theCIRRUS DESIGN SR20Aircraft Serials 1148 thru 1267 and Aircraft Serials 1005 thru 1147 after 3000 Pound Gross Weight

1-8 P/N 13999-002 Info ManualSection 1 Cirrus DesignGeneral SR20Symbols, Abbreviations and TerminologyGeneral Airspeed Terminology and SymbolsKCAS Kno

4-18 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20ClimbNormal climbs are performed flaps UP (0%) and full power at speeds 5to

P/N 13999-002 Info Manual 4-19Cirrus Design Section 4SR20 Normal ProceduresCruiseNormal cruising is performed between 55% and 75% power. Theengine pow

4-20 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Cruise LeaningThe engine is equipped with an altitude compensating fuel pum

P/N 13999-002 Info Manual 4-21Cirrus Design Section 4SR20 Normal ProceduresDescent1. Altimeter...

4-22 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Short Field LandingFor a short field landing in smooth air conditions, make

P/N 13999-002 Info Manual 4-23Cirrus Design Section 4SR20 Normal ProceduresAfter Landing1. Power Lever ...

4-24 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20StallsSR20 stall characteristics are conventional. Power-off stalls may bea

P/N 13999-002 Info Manual 4-25Cirrus Design Section 4SR20 Normal ProceduresEnvironmental ConsiderationsCold Weather OperationStartingIf the engine has

4-26 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Hot air must be applied directly to the oil sump and external oillines as w

P/N 13999-002 Info Manual 4-27Cirrus Design Section 4SR20 Normal Procedures(Continued on following page)11. Power Lever ...

P/N 13999-002 Info Manual 1-9Cirrus Design Section 1SR20 GeneralMeteorological TerminologyVSOStalling Speed is the minimum steady flight speed at whic

4-28 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Noise Characteristics/AbatementThe certificated noise levels for the Cirrus

P/N 13999-002 Info Manual 5-1Cirrus Design Section 5SR20 Performance DataSection 5Performance DataTable of ContentsIntroduction ...

5-2 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Range / Endurance Profile ...

P/N 13999-002 Info Manual 5-3Cirrus Design Section 5SR20 Performance DataIntroductionPerformance data in this section are presented for operationalpla

5-4 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Flight PlanningThe performance tables in this section present sufficient info

P/N 13999-002 Info Manual 5-5Cirrus Design Section 5SR20 Performance DataCruise Conditions:• Total distance ...

5-6 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20• Decrease in total distance (2734 feet x 0.092) ...252 feet• Corr

P/N 13999-002 Info Manual 5-7Cirrus Design Section 5SR20 Performance Dataclimb performance is to increase the time, fuel, and distance to climbby appr

5-8 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Fuel RequiredThe total fuel requirement for the flight may be estimated using

P/N 13999-002 Info Manual 5-9Cirrus Design Section 5SR20 Performance DataLandingA procedure similar to takeoff should be used for estimating thelandin

1-10 P/N 13999-002 Info ManualSection 1 Cirrus DesignGeneral SR20Engine Power TerminologyPerformance and Flight Planning Terminology• Pressure Altitud

5-10 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-1Airspeed Calibration Normal Static Source• Note •• Indicated airsp

P/N 13999-002 Info Manual 5-11Cirrus Design Section 5SR20 Performance DataAirspeed CalibrationAlternate Static Source• Note •• Indicated airspeed valu

5-12 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-3Altitude CorrectionNormal Static Source• Note •• Indicated airspee

P/N 13999-002 Info Manual 5-13Cirrus Design Section 5SR20 Performance DataAltitude CorrectionAlternate Static Source• Note •• Indicated airspeed value

5-14 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-5Temperature Conversion• Note •• To convert from Celsius (°C) to Fa

P/N 13999-002 Info Manual 5-15Cirrus Design Section 5SR20 Performance DataOutside Air TemperatureforISA ConditionExample:Pressure Altitude...

5-16 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-7Stall Speeds• Note •• Altitude loss during wings level stall may b

P/N 13999-002 Info Manual 5-17Cirrus Design Section 5SR20 Performance DataWind Components• Note •• The maximum demonstrated crosswind is 21 knots. Val

5-18 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Takeoff Distance Factors:The following factors are to be applied to the comp

P/N 13999-002 Info Manual 5-19Cirrus Design Section 5SR20 Performance DataTakeoff DistanceWEIGHT = 3000 LBSpeed at Liftoff = 68 KIASSpeed over 50 Ft.

P/N 13999-002 Info Manual 1-11Cirrus Design Section 1SR20 GeneralWeight and Balance TerminologyNMPGNautical Miles Per Gallon is the distance (in nauti

5-20 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-9Takeoff DistanceWEIGHT = 2500 LBSpeed at Liftoff = 65 KIASSpeed ov

P/N 13999-002 Info Manual 5-21Cirrus Design Section 5SR20 Performance DataTakeoff Climb Gradient• Note •• Climb Gradients shown are the gain in altitu

5-22 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-11Takeoff Rate of Climb• Note •• Rate-of-Climb values shown are cha

P/N 13999-002 Info Manual 5-23Cirrus Design Section 5SR20 Performance DataEnroute Climb Gradient• Note •• Climb Gradients shown are the gain in altitu

5-24 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-13Enroute Rate of Climb• Note •• Rate-of-Climb values shown are cha

P/N 13999-002 Info Manual 5-25Cirrus Design Section 5SR20 Performance DataEnroute Rate of Climb Vs Density AltitudeConditions:• Power ...

5-26 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-15Time, Fuel and Distance to ClimbFactors:• Taxi Fuel - Add 1 gallo

P/N 13999-002 Info Manual 5-27Cirrus Design Section 5SR20 Performance DataCruise PerformanceConditions: Example:• Mixture ...

5-28 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-16Cruise Performance8000 Feet Pressure AltitudeISA - 30° C (-31° C)

P/N 13999-002 Info Manual 5-29Cirrus Design Section 5SR20 Performance DataRange / Endurance Profile• Note •• Fuel Remaining For Cruise accounts for 10

1-12 P/N 13999-002 Info ManualSection 1 Cirrus DesignGeneral SR20• Station is a location along the airplane fuselage measuredin inches from the refere

5-30 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-17Range / Endurance Profile65% POWER Mixture = Best PowerPress AltF

P/N 13999-002 Info Manual 5-31Cirrus Design Section 5SR20 Performance DataBalked Landing Climb Gradient• Note •• Balked Landing Climb Gradients shown

5-32 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-19Balked Landing Rate of Climb• Note •• Balked Landing Rate of Clim

P/N 13999-002 Info Manual 5-33Cirrus Design Section 5SR20 Performance DataLanding DistanceFactors:The following factors are to be applied to the compu

5-34 P/N 13999-002 Info ManualSection 5 Cirrus DesignPerformance Data SR20Figure 5-20Landing DistanceWEIGHT = 2900 LBSpeed over 50 Ft Obstacle = 75 KI

P/N 13999-002 Info Manual 6-1Cirrus Design Section 6SR20 Weight and BalanceSection 6Weight and BalanceTable of ContentsIntroduction ...

6-2 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight and Balance SR20Intentionally Left BlankSeptember 2011

P/N 13999-002 Info Manual 6-3Cirrus Design Section 6SR20 Weight & BalanceIntroductionThis section describes the procedure for establishing the bas

6-4 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20Figure 6-1FS350.2"BUTTOCK LINE (BL)20015010050BL 0.050100150200SR20_

P/N 13999-002 Info Manual 6-5Cirrus Design Section 6SR20 Weight & BalanceSR20_FM06_1021ASpirit LevelLONGITUDINAL LEVELINGLATERAL LEVELINGSpirit Le

P/N 13999-002 Info Manual 2-1Cirrus Design Section 2SR20 LimitationsSection 2LimitationsTable of ContentsIntroduction ...

6-6 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20Figure 6-3Airplane Weighing FormWeighing PointScale Reading- Tare = Net W

P/N 13999-002 Info Manual 6-7Cirrus Design Section 6SR20 Weight & BalanceAirplane Weighing ProceduresA basic empty weight and center of gravity we

6-8 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR204. Measuring (Figure 6-3):a. Obtain measurement ‘x’ by measuring horizont

P/N 13999-002 Info Manual 6-9Cirrus Design Section 6SR20 Weight & BalanceThe above procedure determines the airplane Basic Empty Weight,moment, an

6-10 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20Figure 6-4Weight & Balance RecordUse this form to maintain a continu

P/N 13999-002 Info Manual 6-11Cirrus Design Section 6SR20 Weight & BalanceLocation Length Width Height VolumeCabin 122” 49.3” 49.7 137 cu ftBaggag

6-12 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20Loading InstructionsIt is the responsibility of the pilot to ensure that

P/N 13999-002 Info Manual 6-13Cirrus Design Section 6SR20 Weight & Balance• The total moment/1000 must not be above the maximum orbelow the minimu

6-14 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20Figure 6-6Weight & Balance Loading FormSerial Num:_________________D

P/N 13999-002 Info Manual 6-15Cirrus Design Section 6SR20 Weight & BalanceLoading DataUse the following chart or table to determine the moment/100

2-2 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20September 2011Intentionally Left Blank

6-16 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20Figure 6-8Moment LimitsUse the following chart or table to determine if

P/N 13999-002 Info Manual 6-17Cirrus Design Section 6SR20 Weight & BalanceEquipment ListThis list will be determined after the final equipment has

6-18 P/N 13999-002 Info ManualSection 6 Cirrus DesignWeight & Balance SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 7-1Cirrus Design Section 7SR20 Airplane DescriptionSection 7Airplane and Systems DescriptionTable of ContentsIntroduction ..

7-2 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Baggage Compartment...

Reading Lights...7-56Overhead Dome Light...

7-4 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 7-5Cirrus Design Section 7SR20 Airplane DescriptionIntroductionThis section provides a basic description and operation of th

7-6 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20AirframeFuselageThe SR20 monocoque fuselage is constructed primarily of c

P/N 13999-002 Info Manual 7-7Cirrus Design Section 7SR20 Airplane DescriptionEmpennageThe empennage consists of a horizontal stabilizer, a two-pieceel

P/N 13999-002 Info Manual 2-3Cirrus Design Section 2SR20 LimitationsIntroduction• Note •Limitations associated with optional equipment are notdescribe

7-8 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Flight ControlsThe SR20 uses conventional flight controls for ailerons, e

P/N 13999-002 Info Manual 7-9Cirrus Design Section 7SR20 Airplane DescriptionSR20_FM07_1461Figure 7-1Elevator Control SystemSeptember 2011

7-10 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Aileron SystemThe ailerons provide airplane roll control. The ailerons a

P/N 13999-002 Info Manual 7-11Cirrus Design Section 7SR20 Airplane DescriptionSR20_FM07_1462Figure 7-2Aileron Control SystemSeptember 2011

7-12 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Rudder SystemThe rudder provides airplane directional (yaw) control. The

P/N 13999-002 Info Manual 7-13Cirrus Design Section 7SR20 Airplane DescriptionSR20_FM07_1463Figure 7-3Rudder Control SystemSeptember 2011

7-14 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Trim SystemsRoll and pitch trim are provided by adjusting the neutral po

P/N 13999-002 Info Manual 7-15Cirrus Design Section 7SR20 Airplane DescriptionYaw Trim SystemYaw trim is provided by spring cartridge attached to the

7-16 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Flight Deck ArrangementThe following paragraphs are a general descriptio

P/N 13999-002 Info Manual 7-17Cirrus Design Section 7SR20 Airplane Description123456781314151618192021179101112KNOTS1201301401501601201401601008060 11

2-4 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Figure 2-1Airspeed LimitationsThe indicated airspeeds in the following table are b

7-18 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Flight Instruments• Note •For additional information on instrument limit

P/N 13999-002 Info Manual 7-19Cirrus Design Section 7SR20 Airplane DescriptionVertical Speed IndicatorAirplane rate of climb or descent in feet per mi

7-20 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20indicated. Power for gyro operation is supplied through the 5-ampTURN CO

P/N 13999-002 Info Manual 7-21Cirrus Design Section 7SR20 Airplane DescriptionCourse Deviation IndicatorThe Course Deviation Indicator (CDI) displays

7-22 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20course and heading outputs provided to the autopilot to allow NAV/LOC/GP

P/N 13999-002 Info Manual 7-23Cirrus Design Section 7SR20 Airplane Descriptioncan be displayed and switched to any NAV receiver including GPS1,GPS2, N

7-24 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Wing FlapsThe electrically controlled, single-slotted flaps provide low-

P/N 13999-002 Info Manual 7-25Cirrus Design Section 7SR20 Airplane DescriptionSR20_FM07_1460Figure 7-5Flap Control SystemSeptember 2011

7-26 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Landing GearMain GearThe main landing gear are bolted to composite wing

P/N 13999-002 Info Manual 7-27Cirrus Design Section 7SR20 Airplane DescriptionAirplane Cabin Cabin Doors Two large forward hinged doors allow crew and

P/N 13999-002 Info Manual 2-5Cirrus Design Section 2SR20 LimitationsAirspeed Indicator MarkingsThe airspeed indicator markings are based upon Section

7-28 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Figure 7-6CABIN SPEAKEREGRESS HAMMER(IN ARMREST)OVERHEAD LIGHT AND SWITC

P/N 13999-002 Info Manual 7-29Cirrus Design Section 7SR20 Airplane DescriptionTo loosen tie-down straps:1. Lift buckle release and pull on buckle to l

7-30 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20To fold seat back forward:1. From the baggage access, lift the carpet pa

P/N 13999-002 Info Manual 7-31Cirrus Design Section 7SR20 Airplane Description• Caution •No slack may exist between the occupant’s shoulder andrestrai

7-32 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR201. Loosen retaining clamp and remove the extinguisher from itsmounting b

P/N 13999-002 Info Manual 7-33Cirrus Design Section 7SR20 Airplane DescriptionEngineThe SR20 is powered by a Teledyne Continental IO-360-ES, six-cylin

7-34 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20the engine compartment through two vents in the aft portion of thecowlin

P/N 13999-002 Info Manual 7-35Cirrus Design Section 7SR20 Airplane DescriptionEngine ExhaustEngine exhaust gases are routed through a dual tuned exhau

7-36 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Start/Ignition SwitchA rotary-type key switch, located on the left bolst

P/N 13999-002 Info Manual 7-37Cirrus Design Section 7SR20 Airplane DescriptionEngine Instruments7,895,64Serials 1005 thru 1581.GITFERLFUEL Controls

Copyright © 2011 - All Rights ReservedCirrus Design Corporation4515 Taylor CircleDuluth, MN 55811

2-6 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Power Plant LimitationsEngineTeledyne Continental ...

7-38 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20TachometerA 2¼” tachometer is mounted on the right instrument panel adja

P/N 13999-002 Info Manual 7-39Cirrus Design Section 7SR20 Airplane DescriptionPressure indicator receives a pressure signal from an oil pressuresensor

7-40 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20PropellerThe airplane is equipped with a constant-speed, aluminum-alloyp

P/N 13999-002 Info Manual 7-41Cirrus Design Section 7SR20 Airplane DescriptionFuel SystemA 56-gallon usable wet-wing fuel storage system provides fuel

7-42 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Figure 7-8SR20_FM07_1016ESerials 1005 thru 1227 before SB 20-73-02.Seria

P/N 13999-002 Info Manual 7-43Cirrus Design Section 7SR20 Airplane DescriptionThe airplane may be serviced to a reduced capacity to permit heaviercabi

7-44 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20When the fuel tanks are 1/4 full or less, prolongeduncoordinated flight

P/N 13999-002 Info Manual 7-45Cirrus Design Section 7SR20 Airplane Descriptionmode to deliver a continuous 4-6 psi boost to the fuel flow for vaporsup

7-46 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Brake SystemThe main wheels have hydraulically operated, single-disc typ

P/N 13999-002 Info Manual 7-47Cirrus Design Section 7SR20 Airplane DescriptionCALIPERASSEMBLYCALIPERASSEMBLYRUDDERPEDAL(4)SR20_FM07_1015PARKING BRAKEV

P/N 13999-002 Info Manual 2-7Cirrus Design Section 2SR20 LimitationsPropeller• Note •Two-blade propellers are not EASA approved for use on thisairplan

7-48 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Parking Brake• Caution •Do not pull the PARK BRAKE knob in flight. If a

P/N 13999-002 Info Manual 7-49Cirrus Design Section 7SR20 Airplane DescriptionElectrical SystemThe standard airplane is equipped with 28-volt direct c

7-50 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Figure 7-10ALT.CNTL.UNIT25A(MCU)MASTER CNTL. UNITMASTER1ALTERNATORALT.RE

P/N 13999-002 Info Manual 7-51Cirrus Design Section 7SR20 Airplane DescriptionPower DistributionPower distribution for the SR20 consists of the electr

7-52 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Avionics Power SwitchA rocker switch, labeled AVIONICS POWER, controls e

P/N 13999-002 Info Manual 7-53Cirrus Design Section 7SR20 Airplane DescriptionLow Volts Warning LightThe airplane is equipped with a red LOW VOLTS war

7-54 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Circuit Breakers and FusesIndividual electrical circuits connected to th

P/N 13999-002 Info Manual 7-55Cirrus Design Section 7SR20 Airplane DescriptionExterior LightingThe airplane is equipped with standard wing tip and tai

7-56 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Interior LightingInterior lighting for the airplane consists of separate

P/N 13999-002 Info Manual 7-57Cirrus Design Section 7SR20 Airplane DescriptionEnvironmental SystemCabin heating and ventilation is accomplished by sup

2-8 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Figure 2-3Instrument MarkingsInstrument(Range)Red Line Green Arc Yellow Arc Red Li

7-58 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Figure 7-11AIR INLETFOOT-WARMERDIFFUSERAIR GASPERFRESH AIRCONDITIONEDAIR

P/N 13999-002 Info Manual 7-59Cirrus Design Section 7SR20 Airplane DescriptionCabin Heat ControlThe amount of heated air allowed into the air mixing p

7-60 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Figure 7-12AIRSPEEDINDICATORPRIMARY FLIGHT DISPLAYSerials 1005 thru 1

P/N 13999-002 Info Manual 7-61Cirrus Design Section 7SR20 Airplane DescriptionPitot-Static SystemThe Pitot-Static system consists of a single heated P

7-62 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20static pressure source is selected, refer to Section 5 airspeedcalibrati

P/N 13999-002 Info Manual 7-63Cirrus Design Section 7SR20 Airplane DescriptionINSTRUMENT AIR FILTER (PAPER)FOAMFILTERVACUUMREGULATORVACUUMENGINE-DRIV

7-64 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Suction GaugeThe suction gauge, located on the far right side of the ins

P/N 13999-002 Info Manual 7-65Cirrus Design Section 7SR20 Airplane DescriptionStall Warning SystemThe airplane is equipped with an electro-pneumatic s

7-66 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Standard AvionicsThe following paragraphs and equipment descriptions des

P/N 13999-002 Info Manual 7-67Cirrus Design Section 7SR20 Airplane Description• Mode C Transponder with altitude encoder (Garmin GTX 320 orGTX 327) -

P/N 13999-002 Info Manual 2-9Cirrus Design Section 2SR20 LimitationsCenter of Gravity LimitsReference Datum ...100 in

7-68 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Multi-Function DisplayThis airplane is equipped with an Avidyne FlightMa

P/N 13999-002 Info Manual 7-69Cirrus Design Section 7SR20 Airplane DescriptionPower for the MCU is 28 VDC supplied through the 5-amp MFD circuitbreake

7-70 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20AutopilotThe airplane may be equipped with the standard S-TEC SystemTwen

P/N 13999-002 Info Manual 7-71Cirrus Design Section 7SR20 Airplane Descriptioncontrol switches on the control yoke handles. The control knobprovides m

7-72 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20GPS NavigationThe airplane is equipped with two GPS navigators. The Garm

P/N 13999-002 Info Manual 7-73Cirrus Design Section 7SR20 Airplane DescriptionCommunication (COM) TransceiversTwo VHF communications (COM) transceiver

7-74 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Navigation (Nav) ReceiverThe Garmin GNS 430 provides an integrated Navig

P/N 13999-002 Info Manual 7-75Cirrus Design Section 7SR20 Airplane DescriptionAudio System The Garmin GMA 340 audio control unit, located in the cente

7-76 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Emergency Locator TransmitterThe airplane is equipped with a self-contai

P/N 13999-002 Info Manual 7-77Cirrus Design Section 7SR20 Airplane DescriptionPortable use of ELT:3. Remove access at lower aft center of baggage comp

2-10 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Maneuver LimitsAerobatic maneuvers, including spins, are prohibited.• Note •Becau

7-78 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Digital ClockThe airplane is equipped with a 2¼” Davtron M803 digital cl

P/N 13999-002 Info Manual 7-79Cirrus Design Section 7SR20 Airplane Description2. Press Control to activate count-up timer. Elapsed time counts upto 59

7-80 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Cirrus Airplane Parachute SystemThe SR20 is equipped with a Cirrus Airpl

P/N 13999-002 Info Manual 7-81Cirrus Design Section 7SR20 Airplane Descriptionsequence the slider limits the initial diameter of the parachute and the

7-82 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20Attempting to activate the rocket by pushing the activation T-handle for

P/N 13999-002 Info Manual 7-83Cirrus Design Section 7SR20 Airplane Descriptionequal to the velocity of the surface wind. In addition, surface windsmay

7-84 P/N 13999-002 Info ManualSection 7 Cirrus DesignAirplane Description SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 8-1Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceSection 8Handling, Servicing, MaintenanceTable of ContentsInt

8-2 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 8-3Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceIntroductionThis section provides general guidelines for hand

P/N 13999-002 Info Manual 2-11Cirrus Design Section 2SR20 LimitationsKinds of Operation The SR20 is equipped and approved for the following type opera

8-4 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20• Service Bulletins – -are of special importance. When yourec

P/N 13999-002 Info Manual 8-5Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceAirplane Records and CertificatesThe Federal Aviation Adminis

8-6 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Airworthiness DirectivesThe Federal Aviation Administration (

P/N 13999-002 Info Manual 8-7Cirrus Design Section 8SR20 Handling, Servicing, Maintenanceinspection is listed, in detail, in Chapter 5 of the Aircraft

8-8 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Pilot Performed Preventative MaintenanceThe holder of a Pilot

P/N 13999-002 Info Manual 8-9Cirrus Design Section 8SR20 Handling, Servicing, Maintenance12. Replace any hose connection, except hydraulic connections

8-10 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Ground HandlingApplication of External PowerA ground service

P/N 13999-002 Info Manual 8-11Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceTowingThe airplane may be moved on the ground by the use of

8-12 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20TaxiingBefore attempting to taxi the airplane, ground person

P/N 13999-002 Info Manual 8-13Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceParkingThe airplane should be parked to protect the airplane

2-12 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Emergency Locator Transmitter1111Restraint System A/R A/R A/R A/R One Seat Belt f

8-14 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20TiedownThe airplane should be moored for immovability, secur

P/N 13999-002 Info Manual 8-15Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceJackingTwo jacking points are provided: one at each wing tie

8-16 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20ServicingLanding Gear ServicingThe main landing gear wheel a

P/N 13999-002 Info Manual 8-17Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceBrake InspectionThe brake assemblies and linings should be c

8-18 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Tire InflationFor maximum service from the tires, keep them

P/N 13999-002 Info Manual 8-19Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceOil ServicingThe oil capacity of the Teledyne Continental IO

8-20 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Approved Oils For the first 25 hours of operation (on a new

P/N 13999-002 Info Manual 8-21Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceProduct SupplierAeroshell (R) W Shell AustraliaAeroshell Oil

8-22 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Fuel System ServicingAfter the first 25 hours of operation,

P/N 13999-002 Info Manual 8-23Cirrus Design Section 8SR20 Handling, Servicing, Maintenance2. Connect ground wire from refuel nozzle to airplane exhaus

P/N 13999-002 Info Manual 2-13Cirrus Design Section 2SR20 LimitationsWheel Pants — — — — May be removed.LightsAnticollision Lights 2 2 2 2Instrument L

8-24 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Fuel Contamination and SamplingTypically, fuel contamination

P/N 13999-002 Info Manual 8-25Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceBattery ServiceAccess to the 24 volt battery is gained by re

8-26 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Cleaning and CareCleaning Exterior Surfaces• Note •Prior to

P/N 13999-002 Info Manual 8-27Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceCleaning Product Cleaning Application SupplierMild Dishwashe

8-28 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Windscreen and WindowsBefore cleaning an acrylic window, rin

P/N 13999-002 Info Manual 8-29Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceEngine CompartmentBefore cleaning the engine compartment, pl

8-30 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Cleaning Interior SurfacesSeats, carpet, upholstery panels,

P/N 13999-002 Info Manual 8-31Cirrus Design Section 8SR20 Handling, Servicing, MaintenanceCleaning Product Cleaning Application SupplierPristInterior

8-32 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20Instrument Panel and Electronic Display ScreensThe instrumen

P/N 13999-002 Info Manual 8-33Cirrus Design Section 8SR20 Handling, Servicing, Maintenance2. Soiled upholstery, may be cleaned with a good upholstery

2-14 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20IcingFlight into known icing conditions is prohibited.Runway SurfaceThis airplane

8-34 P/N 13999-002 Info ManualSection 8 Cirrus DesignHandling, Servicing, Maintenance SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 9-1Cirrus Design Section 9SR20 SupplementsSection 9SupplementsThis section of the handbook contains FAA Approved Supplements

9-2 P/N 13999-002 Info ManualSection 9 Cirrus DesignSupplements SR20Intentionally Left BlankSeptember 2011

P/N 13999-002 Info Manual 9-3Cirrus Design Section 9SR20 SupplementsSection 9Log of SupplementsPart Number Title Date___ 11934-S01 R2 Garmin GMA 340 A

9-4 P/N 13999-002 Info ManualSection 9 Cirrus DesignSupplements SR20___11934-S51 SR20 Airplanes Registered in Colombia 12-07-10September 2011FAA Appro

P/N 11934-S01 1 of 10Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforGarmin GMA 3

2 of 10 P/N 11934-S01Section 9 Cirrus DesignSupplements SR20Figure - 1Section 1 - GeneralThis supplement provides detailed operating instructions for

P/N 11934-S01 3 of 10Cirrus Design Section 9SR20 SupplementsSection 2 - LimitationsUse of auxiliary AUDIO IN entertainment input and the optionallyins

4 of 10 P/N 11934-S01Section 9 Cirrus DesignSupplements SR20A fail-safe circuit connects the pilot’s headset directly to the COM1transceiver in the ev

P/N 11934-S01 5 of 10Cirrus Design Section 9SR20 Supplementsthe copilot mic/audio source. The pilot has receive and transmitcapabilities on COM1 and t

P/N 13999-002 Info Manual 2-15Cirrus Design Section 2SR20 LimitationsTaxi PowerMaximum continuous engine speed for taxiing is 1000 RPM on flat,smooth,

6 of 10 P/N 11934-S01Section 9 Cirrus DesignSupplements SR20The Audio Control Panel has provisions for up to two separatepersonal entertainment input

P/N 11934-S01 7 of 10Cirrus Design Section 9SR20 Supplements• Right Outer Knob – Copilot and passenger mic VOX level. CWrotation increases the amount

8 of 10 P/N 11934-S01Section 9 Cirrus DesignSupplements SR20button. ALL mode is active when neither PILOT or CREW have beenselected. The following tab

P/N 11934-S01 9 of 10Cirrus Design Section 9SR20 SupplementsMarker beacon audio is selected by pressing the MKR push-button. Ifno marker beacon signal

10 of 10 P/N 11934-S01Section 9 Cirrus DesignSupplements SR20XM Radio System (Optional Installation)• Note •For a detailed operating instructions, ref

P/N 11934-S10 1 of 10Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforDual Alterna

2 of 10 P/N 11934-S10Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThis airplane is equipped with a Dual Alternator System. Refer toSectio

P/N 11934-S10 3 of 10Cirrus Design Section 9SR20 SupplementsSection 3 - Emergency ProceduresAlternator FailureAbnormal ammeter indications and illumin

4 of 10 P/N 11934-S10Section 9 Cirrus DesignSupplements SR201. Affected ALT Master Switch ...OFF2. A

P/N 11934-S10 5 of 10Cirrus Design Section 9SR20 Supplements• Note •Switch equipment ‘Off’ or pull circuit breakers for non-essential equipment until

P/N 13999-002 Info Manual 1-1Cirrus Design Section 1SR20 GeneralSection 1GeneralTable of ContentsIntroduction ...

2-16 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Systems and Equipment LimitsCirrus Airframe Parachute System (CAPS)VPD Maximum De

6 of 10 P/N 11934-S10Section 9 Cirrus DesignSupplements SR20Section 7 - Systems DescriptionElectrical SystemThe airplane is equipped with 28-volt dire

P/N 11934-S10 7 of 10Cirrus Design Section 9SR20 SupplementsShould both alternators fail, the battery will supply system current anda discharge rate w

8 of 10 P/N 11934-S10Section 9 Cirrus DesignSupplements SR20avionics power switch must also be turned on. Positioning either ALTswitch to the off posi

P/N 11934-S10 9 of 10Cirrus Design Section 9SR20 Supplements• Note •Illumination of ALT FAIL caution light may occur during lowRPM conditions with an

10 of 10 P/N 11934-S10Section 9 Cirrus DesignSupplements SR20ESSENTIAL 1 and ESSENTIAL 2 circuit breakers. Avionics loads onthe Non-essential Avionics

P/N 11934-S11 1 of 4Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforL-3 Avionics

2 of 4 P/N 11934-S11Section 9 Cirrus DesignSupplements SR20Section 1 GeneralThis airplane is equipped with a L-3 Avionics Systems WX500Stormscope Sens

P/N 11934-S11 3 of 4Cirrus Design Section 9SR20 SupplementsSTRK or CELL – STRK will be displayed if the Strike mode isselected. In this mode, individu

4 of 4 P/N 11934-S11Section 9 Cirrus DesignSupplements SR20Revision 01: 07-18-05Intentionally Left Blank

P/N 11934-S12 1 of 8Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforGarmin GTX 32

P/N 13999-002 Info Manual 2-17Cirrus Design Section 2SR20 Limitationsdated May 1998 or later revision, must be available to the pilotduring all flight

2 of 8 P/N 11934-S12Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThe airplane is equipped with a single Garmin GTX 327 ATC Mode A/C (iden

P/N 11934-S12 3 of 8Cirrus Design Section 9SR20 SupplementsSection 2 - LimitationsNo Change Section 3 - Emergency ProceduresNo ChangeSection 4 - Norma

4 of 8 P/N 11934-S12Section 9 Cirrus DesignSupplements SR20Section 5 - PerformanceNo ChangeSection 6 - Weight & BalanceNo ChangeSection 7 - System

P/N 11934-S12 5 of 8Cirrus Design Section 9SR20 SupplementsMode Selector KeysThe mode selector keys are located in a circular arrangementimmediately t

6 of 8 P/N 11934-S12Section 9 Cirrus DesignSupplements SR20Code Selector KeysCode selection is accomplished by depressing the eight selector keys(numb

P/N 11934-S12 7 of 8Cirrus Design Section 9SR20 SupplementsReply LightThe reply light is the small reverse video “R” immediately below themode annunci

8 of 8 P/N 11934-S12Section 9 Cirrus DesignSupplements SR20COUNT DOWN TIMER - The count down timer is controlled by theSTART / STOP key. The CRSR and

P/N 11934-S13 1 of 16Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook and FAA Approved Airplane Flight ManualSupplementforS-Tec Syste

2 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThis airplane is equipped with an S-TEC System 55X Autopilot. TheSystem

P/N 11934-S13 3 of 16Cirrus Design Section 9SR20 SupplementsRoll and pitch information are displayed on attitude indicator.Autopilot Flight Director i

2-18 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Other LimitationsSmokingSmoking is prohibited in this airplane.September 2011

4 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20g. The ILS is flown at normal approach speeds, and within anySTC or TC speed constraints a

P/N 11934-S13 5 of 16Cirrus Design Section 9SR20 SupplementsSR20_FM09_1509SPSGIALFSWCYDR+VSGSALTREV TRIMAPRNAVHDGFIFTY FIVE XS-TECVSALTAPRREVHDGNAVFig

6 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20Section 3 - Emergency ProceduresAutopilot MalfunctionRefer to Electric Trim/Autopilot Fail

P/N 11934-S13 7 of 16Cirrus Design Section 9SR20 SupplementsSystem Failure and Caution AnnunciationsIf any of the following failure annunciations occu

8 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20Section 4 - Normal ProceduresRefer to Section 7 – Systems Description for a description of

P/N 11934-S13 9 of 16Cirrus Design Section 9SR20 Supplements6. Overpower Test:a. Grasp control yoke and input left aileron, right aileron, noseup, and

10 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20Altitude Hold Mode1. Manually fly the airplane to the desired altitude and level off.• No

P/N 11934-S13 11 of 16Cirrus Design Section 9SR20 Supplementsautopilot will synchronize to and hold the vertical speed at the timethe mode was engaged

12 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20Turns while in GPSS mode can exceed the standard rate by20% to 30%.In NAV mode while trac

P/N 11934-S13 13 of 16Cirrus Design Section 9SR20 SupplementsGlideslope Intercept and Tracking1. Begin with a reliable ILS signal selected on the NAV

P/N 13999-002 Info Manual 2-19Cirrus Design Section 2SR20 LimitationsPlacardsREFER TO AFM FOR APPROVED OILSENGINE OIL GRADEBELOW 40° F SAE 30 OR 10W3

14 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20steering is accomplished by autopilot steering commands to theaileron trim motor and spri

P/N 11934-S13 15 of 16Cirrus Design Section 9SR20 Supplementsautopilot automatically initiates a tracking gain program to reduce turnrate to 45% stand

16 of 16 P/N 11934-S13Section 9 Cirrus DesignSupplements SR20(-) value indicates descent. Vertical speed can be adjusted by rotatingthe VS knob on the

P/N 11934-S15 1 of 6Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforL-3 Avionics

2 of 6 P/N 11934-S15Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThis airplane is equipped with a L-3 Avionics Systems SkyWatchSKY497 Tra

P/N 11934-S15 3 of 6Cirrus Design Section 9SR20 SupplementsSection 4 - Normal ProceduresAfter Engine Start1. Avionics Power Switch ...

4 of 6 P/N 11934-S15Section 9 Cirrus DesignSupplements SR20Switch to Normal from the Standby ScreenSkyWatch must be switched out of STBY to display tr

P/N 11934-S15 5 of 6Cirrus Design Section 9SR20 SupplementsDo not maneuver solely on traffic information shown on thedisplay. Information shown on the

6 of 6 P/N 11934-S15Section 9 Cirrus DesignSupplements SR20SkyWatch may be pilot controlled through the GNS 430 controller.STBY (standby), OPER (opera

P/N 11934-S22 1 of 10Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementForGarmin GNS 4

2-20 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Figure 2-5Upper fuselage, either side of CAPS rocket cover:WARNING!STAY CLEAR WHE

2 of 10 P/N 11934-S22Section 9 Cirrus DesignSupplements SR20Figure - 1Section 1 - GeneralThe airplane is equipped with a Garmin GNS 430 GPS Navigator

P/N 11934-S22 3 of 10Cirrus Design Section 9SR20 SupplementsSection 2 – LimitationsProvided the GPS Navigator is receiving adequate usable signals, it

4 of 10 P/N 11934-S22Section 9 Cirrus DesignSupplements SR206. The aircraft must have other approved navigation equipmentinstalled and operating appro

P/N 11934-S22 5 of 10Cirrus Design Section 9SR20 SupplementsThe Navigator will display a welcome page while the self-test is inprogress. When the self

6 of 10 P/N 11934-S22Section 9 Cirrus DesignSupplements SR202. Single GARMIN GNS 430 (GPS 1) interfaced with the HSI andMFD and a single GARMIN GNC 42

P/N 11934-S22 7 of 10Cirrus Design Section 9SR20 Supplementsb. GPS 2 in this configuration is a GARMIN GNS 430 GPSNavigator with VHF Com interfaced wi

8 of 10 P/N 11934-S22Section 9 Cirrus DesignSupplements SR20VHF NAV is powered by 28 VDC through the Avionics MasterSwitch and the 5-amp GPS2 circuit

P/N 11934-S22 9 of 10Cirrus Design Section 9SR20 SupplementsJeppesen NavData card slot in each panel. The GNS 430 navigator ispowered by 28 VDC throug

10 of 10 P/N 11934-S22Section 9 Cirrus DesignSupplements SR20side of the GNS 430 front panel. Frequency tuning is accomplished byrotating the large an

P/N 11934-S23 1 of 8Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementForGarmin GNC 42

P/N 13999-002 Info Manual 2-21Cirrus Design Section 2SR20 LimitationsAirplane serials 1005 thru 1019without SB 20-11-01.100 KIAS100%120 KIAS50%UPAirpl

2 of 8 P/N 11934-S23Section 9 Cirrus DesignSupplements SR20Figure - 1Section 1 - GeneralThe airplane is equipped with a GARMIN GNC 420 GPS Navigatorwi

P/N 11934-S23 3 of 8Cirrus Design Section 9SR20 SupplementsSection 2 - Limitations1. The GARMIN GNC 420 Pilot's Guide and Reference, P/N 190-0014

4 of 8 P/N 11934-S23Section 9 Cirrus DesignSupplements SR20Section 3 - Emergency Procedures1. If GPS Navigator information is not available or is inva

P/N 11934-S23 5 of 8Cirrus Design Section 9SR20 SupplementsGPS Course Remote Display GNC 420 GPS course information is displayed on the airplane CDI.

6 of 8 P/N 11934-S23Section 9 Cirrus DesignSupplements SR20GPS NavigatorThe GARMIN GNC 420 GPS navigator is the secondary system (GPS2), is IFR certif

P/N 11934-S23 7 of 8Cirrus Design Section 9SR20 Supplementschannels). The tuning controls are located at the left side of the GNC420 front panel. Freq

8 of 8 P/N 11934-S23Section 9 Cirrus DesignSupplements SR20Revision 02: 08-15-07Intentionally Left Blank

P/N 11934-S30 1 of 12Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforHoneywell KG

2 of 12 P/N 11934-S30Section 9 Cirrus DesignSupplements SR20Section 1 - GeneralThe airplane is equipped with an Honeywell KGP 560 TerrainAwareness and

P/N 11934-S30 3 of 12Cirrus Design Section 9SR20 SupplementsSection 2 - Limitations1. Do not use the Terrain Awareness Display for navigation of theai

2-22 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Figure 2-5Engine control panel (cont):SR20_FM02_1520BOFF OFF100 KIAS100%120 KIAS5

4 of 12 P/N 11934-S30Section 9 Cirrus DesignSupplements SR20Activate TAWS• Note •If the aircraft horizontal position derived from the GarminNavigator

P/N 11934-S30 5 of 12Cirrus Design Section 9SR20 SupplementsResponse To Awareness Alerts Aural “TERRAIN AHEAD” AlertAural “OBSTACLE AHEAD” AlertAmber

6 of 12 P/N 11934-S30Section 9 Cirrus DesignSupplements SR20Section 7 - Systems DescriptionThe Honeywell KGP 560 Terrain Awareness and Warning Systemc

P/N 11934-S30 7 of 12Cirrus Design Section 9SR20 Supplements GNS-430GPSAvidyne PFDTransponderTAWS5AVIONICSNON-ESSENTIALBUSConfigurationModuleGMA 340Au

8 of 12 P/N 11934-S30Section 9 Cirrus DesignSupplements SR20TAWS Annunciator Panel TAWS terrain annunciations and control functions are incorporatedin

P/N 11934-S30 9 of 12Cirrus Design Section 9SR20 SupplementsAnnunciator Color FunctionSELF TEST N/A Provides test function for TAWSTERR INHIBIT AMBER

10 of 12 P/N 11934-S30Section 9 Cirrus DesignSupplements SR20MFD Terrain Awareness Display • WARNING •Do not use the Terrain Awareness Display for nav

P/N 11934-S30 11 of 12Cirrus Design Section 9SR20 SupplementsGeometric Altitude versus Measured Sea LevelAn indication of MSL-G or Geometric Altitude

12 of 12 P/N 11934-S30Section 9 Cirrus DesignSupplements SR20Self Test Proper operation of the TAWS can be verified when the aircraft is onthe ground

P/N 11934-S31 1 of 4Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforAvidyne EMax™

P/N 13999-002 Info Manual 2-23Cirrus Design Section 2SR20 LimitationsSerials 1337 & subs with SRV option.DAY - NIGHT - VFRBolster Switch Panel, le

2 of 4 P/N 11934-S31Section 9 Cirrus DesignSupplements SR20Figure - 1Section 1 - GeneralEMax™ Engine Instrumentation provides the pilot with enginepar

P/N 11934-S31 3 of 4Cirrus Design Section 9SR20 SupplementsSection 2 - LimitationsNo Change.Section 3 - Emergency ProceduresNo Change.Section 4 - Norm

4 of 4 P/N 11934-S31Section 9 Cirrus DesignSupplements SR20providing full-time recording of critical engine performanceparameters.The Engine Instrumen

P/N 11934-S32 1 of 4Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforAvidyne CMax™

2 of 4 P/N 11934-S32Section 9 Cirrus DesignSupplements SR20Figure - 1Section 1 - GeneralAvidyne CMax™ Electronic Approach Charts allows the pilot to v

P/N 11934-S32 3 of 4Cirrus Design Section 9SR20 SupplementsSection 2 - Limitations1. Do not use the CMax Approach Charts function for navigation ofthe

4 of 4 P/N 11934-S32Section 9 Cirrus DesignSupplements SR20Refer to Avidyne FlightMax EX5000C Pilot’s Guide, for a morecomplete description of CMax Ap

P/N 11934-S33 1 of 4Cirrus Design Section 9SR20 SupplementsPilot’s Operating Handbook andFAA Approved Airplane Flight ManualSupplementforXM Satellite

2 of 4 P/N 11934-S33Section 9 Cirrus DesignSupplements SR20Figure - 1Section 1 - GeneralThe XM Satellite Weather System enhances situational awareness

P/N 11934-S33 3 of 4Cirrus Design Section 9SR20 SupplementsSection 2 - Limitations1. Do not use the XM Satellite Weather System for navigation of thea

2-24 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Figure 2-5FASTEN SEAT BELT • NO SMOKINGFIRE EXTINGUISHER FORWARD LEFT OF PILOT SE

4 of 4 P/N 11934-S33Section 9 Cirrus DesignSupplements SR20•METARs•SIGMETs•AIRMETs•TFRs• Lightning StrikesThe XM Satellite Weather System is powered b

P/N 13999-002 Info Manual 10-1Cirrus Design Section 10SR20 Safety InformationSection 10Safety InformationTable of ContentsIntroduction ...

10-2 P/N 13999-002 Info ManualSection 10 Cirrus DesignSafety Information SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 10-3Cirrus Design Section 10SR20 Safety InformationIntroductionThe Cirrus Design SR20 is a modern, advanced technology airpl

10-4 P/N 13999-002 Info ManualSection 10 Cirrus DesignSafety Information SR20Cirrus Airframe Parachute System (CAPS)DeploymentThe Cirrus Airframe Para

P/N 13999-002 Info Manual 10-5Cirrus Design Section 10SR20 Safety Informationcontinued safe flight and landing. If it is not, CAPS activation should b

10-6 P/N 13999-002 Info ManualSection 10 Cirrus DesignSafety Information SR20if time and altitude are critical, and/or ground impact is imminent, theC

P/N 13999-002 Info Manual 10-7Cirrus Design Section 10SR20 Safety InformationLanding ConsiderationsAfter a CAPS deployment, the airplane will descend

10-8 P/N 13999-002 Info ManualSection 10 Cirrus DesignSafety Information SR20If the pilot elects to touchdown with a door opened, there are severaladd

P/N 13999-002 Info Manual 10-9Cirrus Design Section 10SR20 Safety Informationconsider unlatching a door prior to assuming the emergency landingbody po

P/N 13999-002 Info Manual 2-25Cirrus Design Section 2SR20 LimitationsSR20_FM02_122412378-001 REV ABaggage Compartment Door, inside:Baggage Compartment

10-10 P/N 13999-002 Info ManualSection 10 Cirrus DesignSafety Information SR20Taxiing, Steering, and Braking PracticesCirrus aircraft use a castering

P/N 13999-002 Info Manual 10-11Cirrus Design Section 10SR20 Safety Information• Do not “ride the brakes”. Pilots should consciously removepressure fro

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1-2 P/N 13999-002 Info ManualSection 1 Cirrus DesignGeneral SR20Intentionally Left BlankSeptember 2011

2-26 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20Figure 2-5C.A.P.S. PARACHUTE RECOVERY SYSTEM THIS AIRCRAFT IS EQUIPPED WITH A 1

P/N 13999-002 Info Manual 2-27Cirrus Design Section 2SR20 Limitations6. RESTRAINT SYSTEM...SECURE 5. MASTER SWITCH...O

2-28 P/N 13999-002 Info ManualSection 2 Cirrus DesignLimitations SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 3-1Cirrus Design Section 3SR20 Emergency ProceduresSection 3Emergency ProceduresTable of ContentsIntroduction ...

3-2 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Vacuum System Failure...

P/N 13999-002 Info Manual 3-3Cirrus Design Section 3SR20 Emergency ProceduresIntroductionThis section provides procedures for handling emergencies and

3-4 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Airspeeds for Emergency OperationsManeuvering Speed:3000 lb ...

P/N 13999-002 Info Manual 3-5Cirrus Design Section 3SR20 Emergency ProceduresEmergency Procedures GuidanceAlthough this section provides procedures fo

3-6 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Take Appropriate Action — In most situations, the procedures listedin thi

P/N 13999-002 Info Manual 3-7Cirrus Design Section 3SR20 Emergency ProceduresGround EmergenciesEngine Fire During StartA fire during engine start may

P/N 13999-002 Info Manual 1-3Cirrus Design Section 1SR20 GeneralIntroductionThis section contains information of general interest to pilots andowners.

3-8 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Emergency Ground Egress• WARNING •While exiting the airplane, make sure e

P/N 13999-002 Info Manual 3-9Cirrus Design Section 3SR20 Emergency ProceduresIn-Flight EmergenciesEngine Failure On Takeoff (Low Altitude)If the engin

3-10 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Maximum GlideBest Glide Speed3000 lb 96 KIAS2500 lb 87 KIASMaximum Glide

P/N 13999-002 Info Manual 3-11Cirrus Design Section 3SR20 Emergency ProceduresEngine Failure In FlightIf the engine fails at altitude, pitch as necess

3-12 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Engine AirstartThe following procedures address the most common causes f

P/N 13999-002 Info Manual 3-13Cirrus Design Section 3SR20 Emergency ProceduresEngine Partial Power LossIndications of a partial power loss include flu

3-14 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20The following procedure provides guidance to isolate and correctsome of

P/N 13999-002 Info Manual 3-15Cirrus Design Section 3SR20 Emergency ProceduresLow Oil PressureIf low oil pressure is accompanied by a rise in oil temp

3-16 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Smoke and Fume EliminationIf smoke and/or fumes are detected in the cabi

P/N 13999-002 Info Manual 3-17Cirrus Design Section 3SR20 Emergency ProceduresCabin Fire In FlightIf the cause of the fire is readily apparent and acc

1-4 P/N 13999-002 Info ManualSection 1 Cirrus DesignGeneral SR20Figure 1-176" 2-BLADE74" 3-BLADE35.5'11.0'9.2'7"26.0&apo

3-18 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20switches OFF. Do not attempt to isolate the source of the fireby checkin

P/N 13999-002 Info Manual 3-19Cirrus Design Section 3SR20 Emergency ProceduresSpinsThe SR20 is not approved for spins, and has not been tested orcerti

3-20 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20CAPS DeploymentThe Cirrus Airframe Parachute System (CAPS) should be act

P/N 13999-002 Info Manual 3-21Cirrus Design Section 3SR20 Emergency ProceduresThe maximum demonstrated deployment speed is 135 KIAS.Reducing airspeed

3-22 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20All occupants must have seat belts and shoulder harness securelyfastened

P/N 13999-002 Info Manual 3-23Cirrus Design Section 3SR20 Emergency ProceduresLanding EmergenciesIf all attempts to restart the engine fail and a forc

3-24 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20Ditching1. Radio... Transmit (

P/N 13999-002 Info Manual 3-25Cirrus Design Section 3SR20 Emergency ProceduresLanding Without Elevator ControlThe pitch trim spring cartridge is attac

3-26 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20System MalfunctionsPower Lever Linkage FailureIf the Power Lever linkage

P/N 13999-002 Info Manual 3-27Cirrus Design Section 3SR20 Emergency ProceduresVacuum System FailureFailure of the engine driven vacuum pump is indicat

P/N 13999-002 Info Manual 1-5Cirrus Design Section 1SR20 General11"23'11"9'SR20_FM01_1002GROUND TURNING CLEARANCETURNING RADII ARE

3-28 P/N 13999-002 Info ManualSection 3 Cirrus DesignEmergency Procedures SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 3A-1Cirrus Design Section 3ASR20 Abnormal ProceduresSection 3AAbnormal ProceduresTable of ContentsIntroduction ...

3A-2 P/N 13999-002 Info ManualSection 3A Cirrus DesignAbnormal Procedures SR20September 2011Intentionally Left Blank

P/N 13999-002 Info Manual 3A-3Cirrus Design Section 3ASR20 Abnormal ProceduresIntroductionThis section provides procedures for handling abnormal syste

3A-4 P/N 13999-002 Info ManualSection 3A Cirrus DesignAbnormal Procedures SR20Abnormal Procedures GuidanceAlthough this section provides procedures fo

P/N 13999-002 Info Manual 3A-5Cirrus Design Section 3ASR20 Abnormal ProceduresGround ProceduresBrake Failure During TaxiGround steering is accomplishe

3A-6 P/N 13999-002 Info ManualSection 3A Cirrus DesignAbnormal Procedures SR20In-Flight ProceduresInadvertent Icing EncounterFlight into known icing c

P/N 13999-002 Info Manual 3A-7Cirrus Design Section 3ASR20 Abnormal ProceduresLanding ProceduresLanding With Failed BrakesOne brake inoperative1. Land

3A-8 P/N 13999-002 Info ManualSection 3A Cirrus DesignAbnormal Procedures SR20System MalfunctionsAlternator FailureAbnormal ammeter indications and il

P/N 13999-002 Info Manual 3A-9Cirrus Design Section 3ASR20 Abnormal Proceduresshould be completed. Battery power must be conserved for lateroperation

1-6 P/N 13999-002 Info ManualSection 1 Cirrus DesignGeneral SR20The AirplaneEngineNumber of Engines...

3A-10 P/N 13999-002 Info ManualSection 3A Cirrus DesignAbnormal Procedures SR20Communications FailureCommunications failure can occur for a variety of

P/N 13999-002 Info Manual 3A-11Cirrus Design Section 3ASR20 Abnormal ProceduresPitot Static MalfunctionStatic Source BlockedIf erroneous readings of t

3A-12 P/N 13999-002 Info ManualSection 3A Cirrus DesignAbnormal Procedures SR20Electric Trim/Autopilot FailureAny failure or malfunction of the electr

P/N 13999-002 Info Manual 4-1Cirrus Design Section 4SR20 Normal ProceduresSection 4Normal ProceduresTable of ContentsIntroduction ...

4-2 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Intentionally Left BlankSeptember 2011

P/N 13999-002 Info Manual 4-3Cirrus Design Section 4SR20 Normal ProceduresIntroductionThis section provides amplified procedures for normal operation.

4-4 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Airspeeds for Normal OperationUnless otherwise noted, the following speeds a

P/N 13999-002 Info Manual 4-5Cirrus Design Section 4SR20 Normal ProceduresNormal ProceduresPreflight InspectionBefore carrying out preflight inspectio

4-6 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Preflight Walk-Around1. Cabina. Required Documents...

P/N 13999-002 Info Manual 4-7Cirrus Design Section 4SR20 Normal Procedurese. Baggage Door ... Closed and Secur

P/N 13999-002 Info Manual 1-7Cirrus Design Section 1SR20 GeneralFuelTotal Capacity...60.5 U.S. Gallons (229.

4-8 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20c. Fuel Drains (2 underside) ... Drain and Sampled.

P/N 13999-002 Info Manual 4-9Cirrus Design Section 4SR20 Normal Procedures10. Nose, Left Sidea. Landing Light...

4-10 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Before Starting Engine1. Preflight Inspection ...

P/N 13999-002 Info Manual 4-11Cirrus Design Section 4SR20 Normal ProceduresStarting EngineIf the engine is warm, no priming is required. For the first

4-12 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR203. Bat Master Switch ... ON (Ch

P/N 13999-002 Info Manual 4-13Cirrus Design Section 4SR20 Normal Procedures15. Alt Master Switches ...

4-14 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Before TakeoffDuring cold weather operations, the engine should be properly

P/N 13999-002 Info Manual 4-15Cirrus Design Section 4SR20 Normal Procedures16. Pitot Heat ...

4-16 P/N 13999-002 Info ManualSection 4 Cirrus DesignNormal Procedures SR20Takeoff• Note •The engine is equipped with an altitude compensating fuelpum

P/N 13999-002 Info Manual 4-17Cirrus Design Section 4SR20 Normal ProceduresNormal Takeoff1. Brakes.........RELEASE (Steer w