SR22T Abbreviated Checklist, W/ FIKI
PILOT’S CHECKLISTSR22WITH 3600 POUND TAKEOFF WEIGHT AND FLIGHT INTO KNOWN ICE SYSTEM
Quick Reference ChecklistforSR22 Aircraft Serials 3915 and Subsequent with 3600 Pound TakeoffWeight and Flight Into Known Ice SystemThe procedures in this publication are abbreviated and derived from procedures in theFAA Approved Airplane Flight Manual and Pilot’s Operating Handbook (POH) P/N13772-004 Original Issue. These procedures do not supersede the procedures in thebasic POH. In the event of conflict, the basic POH shall take precedence.COPYRIGHT 2013 CIRRUS DESIGN CORPORATION DULUTH, MINNESOTA, USAISSUED: February 2013P/N 13728-010
PERFORMANCECIRRUSABNORMALP ILOT’S CHEC KL IS TEMERGENCYMODEL SR22Normal ProceduresTable of ContentsPrimary Flight Display .N-1Airspeeds for Normal Operation .N-2Preflight Inspection .N-3Before Starting Engine .N-9Starting Engine .N-9Cold Weather Operation: Starting .N-10Before Taxiing .N-10Taxiing .N-10Before Takeoff .N-11Normal Takeoff .N-13Short Field Takeoff.N-13Climb .N-13Icing Conditions: In Flight.N-14If Icing Conditions Exist: .N-14Inadvertent Icing Encounter:.N-14Icing Conditions: In Flight.N-15While in Icing Conditions: .N-15After Leaving Icing Conditions:.N-15Cruise.N-15Descent .N-16If Icing Conditions Exist: .N-16Before Landing.N-17Normal Landing.N-17Short Field Landing .N-17Balked Landing/Go-Around.N-17After Landing.N-18Shutdown .N-18Oxygen Duration (Precise Flight System) .N-19P/N 13728-010February 2013N-iNORMALNORMAL
CIRRUSP ILOT CHEC KL IS TMODEL SR22Primary Flight 6N2420TERM3321GPS21N-110125 24LEGEND1. True Airspeed2. Airspeed Indicator3. Horizontal Situation Indicator (HSI)4. Attitude Indicator5. Slip/Skid Indicator6. Vertical Deviation Indicator (VDI)7. Selected Altitude Bug8. Current Altitude9. Altimeter10. Selected Altitude11. Vertical Speed Indicator (VSI)12. Current Heading13. Lubber Line14. Selected Heading Bug15. Flight Phase16. Navigation Source17. Aircraft Symbol18. Course Deviation Scale19. Rotating Compass Rose20. Course Pointer9301WPFDLEGENDNORMAL1718HSI DETAIL21. To/From Indicator22. Course Deviation Indicator23. Current Track Indicator24. Turn Rate/Heading Trend Vector25. Turn Rate IndicatorSR22 FM07 2790P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Takeoff Rotation: Normal, Flaps 50%. 73 KIAS Obstacle Clearance, Flaps 50% . 84 KIASEnroute Climb, Flaps Up: Normal . 110-120 KIAS Best Rate of Climb, SL . 108 KIAS Best Rate of Climb, 10,000. 99 KIAS Best Angle of Climb, SL. 88 KIAS Best Angle of Climb, 10,000 . 88 KIASLanding Approach: Normal Approach, Flaps Up . 90-95 KIAS Normal Approach, Flaps 50% . 85-90 KIAS Normal Approach, Flaps 100% . 80-85 KIAS Short Field, Flaps 100% (VREF) . 79 KIASGo-Around, Flaps 50%: Full Power. 80 KIASMaximum Recommended Turbulent Air Penetration: 3600 lb. 140 KIAS 2900 lb. 123 KIASMaximum Demonstrated Crosswind Velocity: Takeoff or Landing . 21 KnotsAnti-Ice System: Minimum Airspeed For FIKI Conditions.95 KIAS**Includes all phases of flight, including approach, except asrequired for takeoff and landing. Max Airspeed Anti-Ice System Ops. 177 KIAS and 204 KTAS Recommended Holding Airspeed. 120 KIASP/N 13728-010February 2013N-2AIRSPEEDSAirspeeds for Normal Operation
NORMALPREFLIGHTCIRRUSP ILOT CHEC KL IS TMODEL SR2263542718131091112SR22 FM04 1454Preflight Inspection1. Cabina. Required Documents . On Boardb.Avionics Power Switch . OFFc.Bat 2 Master Switch . ONd. PFD .Verify One. Essential Bus Voltage . 23-25 Voltsf.Flap Position Light .OUTg. Battery 1 Master Switch . ONh. Avionics Cooling Fan. Audiblei.Lights. Check Operationj.Stall Warning .Testk.Fuel Quantity . Checkl.Fuel Selector . Select Fullest Tankm. Flaps .100%, Check Light ONn. Bat 1 and 2 Master Switch . OFF(Continued on following page)N-3P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22o.Alternate Static Source . NORMALp.Circuit Breakers.INr.Cabin Speaker . ONs.Cabin Doors . Closet.WIND SHLD Push-Button . Press(1) Verify evidence of deicing fluid from spray nozzles.u. PUMP BKUP Switch . ON(1) Metering Pump Duty Cycle. Verify Continuously ON(2) Deicing Fluid and Endurance Indications . Checkv.PUMP BKUP Switch . OFFw. ICE PROTECT System Switch. ONx.ICE PROTECT Mode Switch. NORM(1) Metering Pump Duty Cycle. Verify 30s ON, 90s OFF(2) Deicing Fluid and Endurance Indications . Checky.ICE PROTECT Mode Switch. HIGH(1) Metering Pump Duty Cycle. Verify Continuously ON(2) Deicing Fluid and Endurance Indications . Checkz.ICE Inspection Lights Switch. ON(1) Verify LH and RH Operation.aa. PITOT HEAT Switch . ON 45 seconds, then OFFab. Fire Extinguisher . Charged and Availableac. Emergency Egress Hammer . Availablead. CAPS Handle . Pin Removed(Continued on following page)P/N 13728-010February 2013N-4PREFLIGHTq. Avionics Master Switch . ON
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR222. Left Fuselagea. Door Lock . Unlockb.COM 1 Antenna (top) . Condition and Attachmentc.Transponder Antenna (underside). Condition and AttachmentPREFLIGHTd. Wing/Fuselage Fairing . Checke. COM 2 Antenna (underside) . Condition and Attachmentf.Baggage Door .Closed and Secureg. Static Button. Check for Blockageh. Parachute Cover .Sealed and Secure3. Empennagea. Tiedown Rope . Removeb.Horizontal and Vertical Stabilizers. Conditionc.Stabilizers Porous Panels. Condition / Security(1) Verify Evidence of Deicing Fluid Along Length of Panelsand Elevator Horns.d. Elevator and Tab . Condition and Movemente. Rudder . Freedom of Movementf.Rudder Trim Tab. Condition and Securityg. Attachment hinges, bolts and cotter pins . Secure4. Right Fuselagea. Static Button. Check for Blockageb.Wing/Fuselage Fairings. Checkc.Door Lock . Unlock5. Right Wing Trailing Edgea. Flap and Rub Strips (if installed) . Condition and Securityb.Aileron and Tab . Condition and Movementc.Aileron Gap Seal . Securityd. Hinges, actuation arm, bolts, and cotter pins . Secure6. Right Wing Tipa. Tip . Attachmentb.Strobe, Nav Light and Lens. Condition and Securityc.Fuel Vent (underside) .Unobstructed(Continued on following page)N-5P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR227. Right Wing Forward and Main Geara. Leading Edge and Stall Strips. Conditionb.Fuel Cap. Check Quantity and Securec.Fluid Tank.Verify Desired Quantity(1) Filler Cap . Condition and Security(2) Fluid Vent (underside). Unobstructed(1) Check Evidence of Deicing Fluid Along Length of Panels.e. Lift Transducer Faceplate . Perceptibly Hotf.Lift Transducer Vane .Very Hot(1) Verify Stall Warning System audio annunciation within 4seconds after lifting stall vane with wooden tooth pick ortongue depressor.g. Fuel Drains (2 underside).Drain and Sampleh. Wheel Fairings .Security, Accumulation of Debrisi.Tire . Condition, Inflation, and Wearj.Wheel and Brakes .Fluid Leaks, Evidence of Overheating,General Condition, and Security.k.Chocks and Tiedown Ropes . Removel.Cabin Air Vent . Unobstructed8. Nose, Right Sidea. Vortex Generator . Conditionb.Ice-Inspection Light . Condition / Securityc.Cowling . Attachments Secured. Exhaust Pipe . Condition, Security, and Clearancee. Gascolator (underside). Drain for 3 seconds, Sample9. Nose Gear, Propeller, and Spinnera. Tow Bar . Remove and Stowb.Strut . Conditionc.Wheel Fairing .Security, Accumulation of Debrisd. Wheel and Tire. Condition, Inflation, and Weare. Propeller. Check adequate Ground Clearance(Continued on following page)P/N 13728-010February 2013N-6PREFLIGHTd. Porous Panels . Condition and Security
NORMALCIRRUSf.P ILOT CHEC KL IS TMODEL SR22Spinner. Condition, Security, and Oil Leaksg. Slinger Ring. Evidence Of Deicing Fluidh. Air Inlets .Unobstructedi.Alternator . Condition10. Nose, Left SidePREFLIGHTa. Landing Light. Conditionb.Engine Oil. Check 6-8 quarts, Leaks, Cap & Door Securec.Cowling . Attachments Secured. External Power . Door Securee. Vortex Generator . Conditionf.Ice-Inspection Light . Condition / Securityg. Windshield Spray Nozzles. Condition / Securityh. Exhaust Pipe(s). Condition, Security, and Clearance11. Left Wing Forward and Main Geara. Wheel fairings .Security, Accumulation of Debrisb.Tire . Condition, Inflation, and Wearc.Wheel and Brakes .Fluid Leaks, Evidence of Overheating,General Condition, and Security.d. Chocks and Tiedown Ropes . Removee. Fuel Drains (2 underside).Drain and Samplef.Cabin Air Vent . Unobstructedg. Fuel Cap. Check Quantity and Secureh. Fluid Tank.Verify Desired Quantity(1) Filler Cap . Condition and Security(2) Fluid Vent (underside). Unobstructedi.Leading Edge and Stall Strips. Conditionj.Porous Panels . Condition / Security(1) Check Evidence of Deicing Fluid Along Length of Panels.12. Left Wing Tipa. Fuel Vent (underside) .Unobstructedb.Pitot Mast (underside) . Cover Removed, Tube Clearc.Pitot Probe (underside) .Unobstructed(Continued on following page)N-7P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22d. Pitot Probe .Very Hote. Strobe, Nav Light and Lens. Condition and Securityf.Tip . Attachment13. Left Wing Trailing Edgea. Flap And Rub Strips (If installed) . Condition and Securityb.Aileron . Freedom of movementc.Aileron Gap Seal . Securityd. Hinges, actuation arm, bolts, and cotter pins . Secure14. Cabinb.ICE PROTECT System Switch. OFFc.Flaps . 0%d. Battery 1 Master Switch . OFFe. Avionics Master Switch . OFFf.Cabin Speaker . OFFP/N 13728-010February 2013N-8PREFLIGHTa. Fluid Quantity . Verify 5 Gallon Minimum
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Before Starting Engine1. Preflight Inspection . COMPLETED2. Weight and Balance. Verify within limits3. Emergency Equipment . ON BOARD4. Passengers.BRIEFED5. Seats, Seat Belts, and Harnesses . ADJUST & SECUREStarting Engine1. External Power (If applicable) .CONNECTSTARTINGENGINE2. Brakes . HOLD3. Bat Master Switches .ON (Check Volts)4. Strobe Lights . ON5. Mixture .FULL RICH6. Power Lever . FULL FORWARD7. Fuel Pump .BOOST8. Propeller Area. CLEAR9. Power Lever . OPEN ¼ INCH10. Ignition Switch .START (Release after engine starts)11. Mixture . LEANuntil RPM rises to a maximum value. Leave the mixture in thisposition during taxi and until run-up.12. Power Lever . RETARD (to maintain 1000 RPM)13. Oil Pressure .CHECK14. Alt Master Switches . ON15. Avionics Power Switch . ON16. Engine Parameters . MONITOR17. External Power (If applicable) .DISCONNECT18. Amp Meter/Indication.CHECKN-9P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Cold Weather Operation: Starting1. Ignition Switch . OFF2. Propeller .Hand TURN several rotations3. External Power (If applicable) .CONNECT4. Brakes . HOLD5. Bat Master Switches .ON (check voltage)6. Mixture.FULL RICH7. Power lever . FULL FORWARD8. Fuel Pump .HIGH BOOST/PRIME, then BOOST9. Propeller Area. CLEAR10. Power Lever . OPEN ¼ INCH11. Ignition Switch .START (Release after engine starts)13. Oil Pressure.CHECK14. Alt Master Switches . ON15. Avionics Power Switch. ON16. Engine Parameters .MONITOR17. External Power (If applicable) .DISCONNECT18. Amp Meter/Indication.CHECK19. Strobe Lights . ONBefore Taxiing1. Flaps.UP (0%)2. Radios/Avionics .AS REQUIRED3. Cabin Heat/Defrost . AS REQUIRED4. Fuel Selector . SWITCH TANKTaxiing1. Parking Brake . DISENGAGE2. Brakes.CHECK3. HSI Orientation .CHECK4. Attitude Gyro.CHECK5. Turn Coordinator .CHECKP/N 13728-010February 2013N - 10STARTING/TAXI12. Power Lever . RETARD (to maintain 1000 RPM)
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Before Takeoff1. Doors . LATCHED2. CAPS Handle . Verify Pin Removed3. Seat Belts and Shoulder Harness . SECURE4. Air Conditioner .AS DESIRED Caution Use of RECIRC mode prohibited in flight.5. Fuel Quantity .CONFIRM6. Fuel Selector . FULLEST TANK7. Fuel Pump .BOOST8. Mixture .AS REQUIRED9. Flaps . SET 50% & CHECKBEFORETAKEOFF10. Transponder. SET11. Autopilot.CHECK12. Navigation Radios/GPS .SET for Takeoff13. Cabin Heat/Defrost .AS REQUIRED14. Brakes. HOLD15. Power Lever . 1700 RPM16. Alternator .CHECKa. Pitot Heat . ONb.Navigation Lights. ONc.Landing Light. ONd. Annunciator Lights .CHECKVerify both ALT 1 and ALT 2 caution lights out and positiveamps indication for each alternator.17. Voltage.CHECK18. Pitot Heat .AS REQUIRED19. Navigation Lights .AS REQUIRED20. Landing Light .AS REQUIRED(Continued on following page)N - 11P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR2221. Magnetos. CHECK Left and RightRPM drop must not exceed 150 RPM for either magneto. RPMdifferential must not exceed 75 RPM between magnetosa. Ignition Switch . R, note RPM, then BOTHb.Ignition Switch .L, note RPM, then BOTH22. Engine Parameters .CHECK23. Power Lever . 1000 RPM24. Flight Instruments, HSI, and Altimeter . CHECK & SET25. Flight Controls .FREE & CORRECT26. Trim.SET Takeoff27. Autopilot.DISCONNECTIf Icing Conditions are Anticipated Immediately After Takeoff:28. ICE PROTECT System Switch . ON29. ICE PROTECT Mode Switch . NORM / HIGH30. PITOT HEAT Switch. ON31. Cabin Heat. HOT33. Ice-Inspection Lights.AS REQUIRED34. Verify airframe is free of contamination immediately before takeoff.35. Flaps.RETRACT as soon as practicalP/N 13728-010February 2013N - 12BEFORETAKEOFF32. Windshield Defrost . ON
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Normal Takeoff1. Brakes. RELEASE (Steer with Rudder Only)2. Power Lever . FULL FORWARD3. Engine Parameters .CHECK4. Elevator Control . ROTATE Smoothly at 73-76 KIAS5. At 90 KIAS, Flaps . UPShort Field Takeoff1. Flaps . 50%2. Brakes . HOLD3. Power Lever . FULL FORWARD4. Mixture . SET5. Engine Parameters .CHECK6. Brakes. RELEASE (Steer with Rudder Only)7. Elevator Control .ROTATE Smoothly at 73 KIASTAKEOFF/CLIMB8. Airspeed at Obstacle . 84 KIASClimb1. Climb Power. SET2. Flaps . Verify UP3. Mixture . LEAN as required for altitude4. Engine Parameters .CHECK5. Fuel Pump .BOOSTN - 13P/N 13728-010February 2013
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Icing Conditions: In FlightIf Icing Conditions Exist:1. PITOT HEAT Switch. Verify ON2. ICE PROTECT System Switch . ON3. ICE PROTECT Mode Switch . NORM / HIGH4. WIND SHLD Push-Button. PRESS AS REQUIRED5. Monitor ice accumulation.If ice accumulation occurs:a. ICE PROTECT Mode . HIGHIf ice continues accumulating:b.ICE PROTECT Mode Push-Button .MAXIf ice accretions do not shed:c.PUMP BKUP Switch . ONd. Perform Deicing System Failure checklist.Inadvertent Icing Encounter:1. PITOT HEAT Switch. Verify ON2. ICE PROTECT System Switch . ONb.ICE PROTECT Mode Switch. HIGH / NORMIf excess ice accumulation occurs, then:c.ICE PROTECT Mode Push-Button .MAXIf ice does not shed perform Deicing System Failure checklist.3. WIND SHLD Push-Button. PRESS AS REQUIRED4. Airspeed . MAINTAIN 95-177 KIASor less than 204 KTAS(Continued on following page)P/N 13728-010February 2013N - 14ICINGa. ICE PROTECT Mode Push-Button .MAXto initially dissipate ice accumulation, then
NORMALCIRRUSP ILOT CHEC KL IS TMODEL SR22Icing Conditions: In FlightWhile in Icing Conditions:1. FLAPS . UP2. Ice-Inspection Lights.AS REQUIRED3. Cabin Heat.HOT4. Windshield Defrost .
FAA Approved Airplane Flight Manual and Pilot’s Operating Handbook (POH) P/N 13772-004 Original Issue. These procedures do not supersede the procedures in the basic POH. In the event of conflict, the basic POH shall take precedence. . CIRRUS PILOT’S CHECKLIST MODEL SR22 Normal Procedures Table of Contents P/N 13728-010 N - i
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