PILOT’S CHECKLIST SR22 WITH 3600 POUND TAKEOFF WEIGHT AND FLIGHT INTO KNOWN ICE SYSTEM

PILOT’S CHECKLIST SR22 WITH 3600 POUND TAKEOFF WEIGHT AND FLIGHT INTO KNOWN ICE SYSTEM The procedures in this publication are abbreviated and derived from procedures in the 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. COPYRIGHT © 2013 CIRRUS DESIGN CORPORATION DULUTH, MINNESOTA, USA ISSUED: February 2013 P/N 13728-010 Quick Reference Checklist for SR22 Aircraft Serials 3915 and Subsequent with 3600 Pound Takeoff Weight and Flight Into Known Ice System C I R R U S P I L O T ’ S C H E C K L I S T M O D E L S R 2 2 Normal Procedures Table of Contents P/N 13728-010 N - i Primary Flight Display ......................................................................N-1 Airspeeds for Normal Operation ......................................................N-2 Preflight Inspection ..........................................................................N-3 Before Starting Engine .....................................................................N-9 Starting Engine ................................................................................N-9 Cold Weather Operation: Starting ..................................................N-10 Before Taxiing ................................................................................N-10 Taxiing ...........................................................................................N-10 Before Takeoff ...............................................................................N-11 Normal Takeoff ..............................................................................N-13 Short Field Takeoff.........................................................................N-13 Climb ..............................................................................................N-13 Icing Conditions: In Flight...............................................................N-14 If Icing Conditions Exist: ............................................................N-14 Inadvertent Icing Encounter:......................................................N-14 Icing Conditions: In Flight...............................................................N-15 While in Icing Conditions: ..........................................................N-15 After Leaving Icing Conditions:..................................................N-15 Cruise.............................................................................................N-15 Descent ..........................................................................................N-16 If Icing Conditions Exist: ............................................................N-16 Before Landing...............................................................................N-17 Normal Landing..............................................................................N-17 Short Field Landing ........................................................................N-17 Balked Landing/Go-Around............................................................N-17 After Landing..................................................................................N-18 Shutdown .......................................................................................N-18 Oxygen Duration (Precise Flight System) ......................................N-19 February 2013 NORMAL PERFORMANCE ABNORMAL EMERGENCY NORMAL N - 1 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Primary Flight Display LEGEND 1. True Airspeed 2. Airspeed Indicator 3. Horizontal Situation Indicator (HSI) 4. Attitude Indicator 5. Slip/Skid Indicator 6. Vertical Deviation Indicator (VDI) 7. Selected Altitude Bug 8. Current Altitude 9. Altimeter 10. Selected Altitude 11. Vertical Speed Indicator (VSI) 12. Current Heading 13. Lubber Line 14. Selected Heading Bug 15. Flight Phase 16. Navigation Source 17. Aircraft Symbol 18. Course Deviation Scale 19. Rotating Compass Rose 20. Course Pointer N W S E 6 3 33 30 24 21 13 12 125° XTK 1.01NM 21. To/From Indicator 22. Course Deviation Indicator 23. Current Track Indicator 24. Turn Rate/Heading Trend Vector 25. Turn Rate Indicator SR22_FM07_2790 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 TERM GPS HSI DETAIL February 2013 NORMAL PFD LEGEND P/N 13728-010 N - 2 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Airspeeds for Normal Operation Takeoff Rotation: • Normal, Flaps 50%......................................................... 73 KIAS • Obstacle Clearance, Flaps 50% ..................................... 84 KIAS Enroute 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 KIAS Landing 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% (V REF) ..................................... 79 KIAS Go-Around, Flaps 50%: • Full Power....................................................................... 80 KIAS Maximum Recommended Turbulent Air Penetration: • 3600 lb.......................................................................... 140 KIAS • 2900 lb.......................................................................... 123 KIAS Maximum Demonstrated Crosswind Velocity: • Takeoff or Landing ......................................................... 21 Knots Anti-Ice System: • Minimum Airspeed For FIKI Conditions.........................95 KIAS* *Includes all phases of flight, including approach, except as required for takeoff and landing. • Max Airspeed Anti-Ice System Ops...... 177 KIAS and 204 KTAS • Recommended Holding Airspeed................................. 120 KIAS February 2013 NORMAL AIRSPEEDS N - 3 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Preflight Inspection 1. Cabin a. Required Documents ................................................ On Board b. Avionics Power Switch ...................................................... OFF c. Bat 2 Master Switch ........................................................... ON d. PFD ............................................................................Verify On e. Essential Bus Voltage ............................................ 23-25 Volts f. Flap Position Light ............................................................OUT g. Battery 1 Master Switch ...................................................... ON h. Avionics Cooling Fan.................................................... Audible i. Lights............................................................. Check Operation j. Stall Warning .....................................................................Test k. Fuel Quantity ................................................................. Check l. Fuel Selector .............................................. Select Fullest Tank m. Flaps ....................................................100%, Check Light ON n. Bat 1 and 2 Master Switch ................................................ OFF (Continued on following page) 3 1 5 6 7 8 9 10 11 12 13 4 2 SR22_FM04_1454 February 2013 NORMAL PREFLIGHT P/N 13728-010 N - 4 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 o. Alternate Static Source ............................................. NORMAL p. Circuit Breakers.....................................................................IN q. Avionics Master Switch ....................................................... ON r. Cabin Speaker .................................................................... ON s. Cabin Doors .................................................................... Close t. 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 ................ Check v. PUMP BKUP Switch ......................................................... OFF w. ICE PROTECT System Switch............................................ ON x. ICE PROTECT Mode Switch......................................... NORM (1) Metering Pump Duty Cycle.......... Verify 30s ON, 90s OFF (2) Deicing Fluid and Endurance Indications ................ Check y. ICE PROTECT Mode Switch........................................... HIGH (1) Metering Pump Duty Cycle........... Verify Continuously ON (2) Deicing Fluid and Endurance Indications ................ Check z. ICE Inspection Lights Switch............................................... ON (1) Verify LH and RH Operation. aa. PITOT HEAT Switch ....................... ON 45 seconds, then OFF ab. Fire Extinguisher ................................. Charged and Available ac. Emergency Egress Hammer ...................................... Available ad. CAPS Handle ..................................................... Pin Removed (Continued on following page) February 2013 NORMAL PREFLIGHT N - 5 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 2. Left Fuselage a. Door Lock ...................................................................... Unlock b. COM 1 Antenna (top) ...................... Condition and Attachment c. Transponder Antenna (underside)... Condition and Attachment d. Wing/Fuselage Fairing ................................................... Check e. COM 2 Antenna (underside) ........... Condition and Attachment f. Baggage Door ............................................Closed and Secure g. Static Button.............................................. Check for Blockage h. Parachute Cover ........................................Sealed and Secure 3. Empennage a. Tiedown Rope ............................................................. Remove b. Horizontal and Vertical Stabilizers............................. Condition c. Stabilizers Porous Panels.......................... Condition / Security (1) Verify Evidence of Deicing Fluid Along Length of Panels and Elevator Horns. d. Elevator and Tab .............................. Condition and Movement e. Rudder ................................................. Freedom of Movement f. Rudder Trim Tab................................... Condition and Security g. Attachment hinges, bolts and cotter pins ...................... Secure 4. Right Fuselage a. Static Button.............................................. Check for Blockage b. Wing/Fuselage Fairings.................................................. Check c. Door Lock ...................................................................... Unlock 5. Right Wing Trailing Edge a. Flap and Rub Strips (if installed) .......... Condition and Security b. Aileron and Tab ................................ Condition and Movement c. Aileron Gap Seal ......................................................... Security d. Hinges, actuation arm, bolts, and cotter pins ................ Secure 6. Right Wing Tip a. Tip .......................................................................... Attachment b. Strobe, Nav Light and Lens.................. Condition and Security c. Fuel Vent (underside) ..........................................Unobstructed (Continued on following page) February 2013 NORMAL PREFLIGHT P/N 13728-010 N - 6 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 7. Right Wing Forward and Main Gear a. Leading Edge and Stall Strips................................... Condition b. Fuel Cap....................................... Check Quantity and Secure c. Fluid Tank.............................................Verify Desired Quantity (1) Filler Cap ....................................... Condition and Security (2) Fluid Vent (underside)................................... Unobstructed d. Porous Panels ...................................... Condition and Security (1) Check Evidence of Deicing Fluid Along Length of Panels. e. Lift Transducer Faceplate ................................. Perceptibly Hot f. Lift Transducer Vane ...................................................Very Hot (1) Verify Stall Warning System audio annunciation within 4 seconds after lifting stall vane with wooden tooth pick or tongue depressor. g. Fuel Drains (2 underside).............................Drain and Sample h. Wheel Fairings ......................Security, Accumulation of Debris i. Tire ............................................ Condition, Inflation, and Wear j. Wheel and Brakes ........Fluid Leaks, Evidence of Overheating, General Condition, and Security. k. Chocks and Tiedown Ropes ....................................... Remove l. Cabin Air Vent ..................................................... Unobstructed 8. Nose, Right Side a. Vortex Generator....................................................... Condition b. Ice-Inspection Light ................................... Condition / Security c. Cowling .................................................... Attachments Secure d. Exhaust Pipe ..................... Condition, Security, and Clearance e. Gascolator (underside)................ Drain for 3 seconds, Sample 9. Nose Gear, Propeller, and Spinner a. Tow Bar ....................................................... Remove and Stow b. Strut .......................................................................... Condition c. Wheel Fairing ........................Security, Accumulation of Debris d. Wheel and Tire.......................... Condition, Inflation, and Wear e. Propeller........................... Check adequate Ground Clearance (Continued on following page) February 2013 NORMAL PREFLIGHT N - 7 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 f. Spinner............................... Condition, Security, and Oil Leaks g. Slinger Ring..................................... Evidence Of Deicing Fluid h. Air Inlets ..............................................................Unobstructed i. Alternator .................................................................. Condition 10. Nose, Left Side a. Landing Light............................................................. Condition b. Engine Oil......... Check 6-8 quarts, Leaks, Cap & Door Secure c. Cowling .................................................... Attachments Secure d. External Power ..................................................... Door Secure e. Vortex Generator ....................................................... Condition f. Ice-Inspection Light ................................... Condition / Security g. Windshield Spray Nozzles......................... Condition / Security h. Exhaust Pipe(s)................. Condition, Security, and Clearance 11. Left Wing Forward and Main Gear a. Wheel fairings .......................Security, Accumulation of Debris b. Tire ............................................ Condition, Inflation, and Wear c. Wheel and Brakes ........Fluid Leaks, Evidence of Overheating, General Condition, and Security. d. Chocks and Tiedown Ropes ....................................... Remove e. Fuel Drains (2 underside).............................Drain and Sample f. Cabin Air Vent ..................................................... Unobstructed g. Fuel Cap....................................... Check Quantity and Secure h. Fluid Tank.............................................Verify Desired Quantity (1) Filler Cap ....................................... Condition and Security (2) Fluid Vent (underside)................................... Unobstructed i. Leading Edge and Stall Strips................................... Condition j. Porous Panels ........................................... Condition / Security (1) Check Evidence of Deicing Fluid Along Length of Panels. 12. Left Wing Tip a. Fuel Vent (underside) ..........................................Unobstructed b. Pitot Mast (underside) ................. Cover Removed, Tube Clear c. Pitot Probe (underside) .......................................Unobstructed (Continued on following page) February 2013 NORMAL PREFLIGHT P/N 13728-010 N - 8 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 d. Pitot Probe ..................................................................Very Hot e. Strobe, Nav Light and Lens.................. Condition and Security f. Tip ......................................................................... Attachment 13. Left Wing Trailing Edge a. Flap And Rub Strips (If installed) ......... Condition and Security b. Aileron .................................................. Freedom of movement c. Aileron Gap Seal ......................................................... Security d. Hinges, actuation arm, bolts, and cotter pins ................ Secure 14. Cabin a. Fluid Quantity .................................... Verify 5 Gallon Minimum b. ICE PROTECT System Switch.......................................... OFF c. Flaps ................................................................................... 0% d. Battery 1 Master Switch .................................................... OFF e. Avionics Master Switch ..................................................... OFF f. Cabin Speaker .................................................................. OFF February 2013 NORMAL PREFLIGHT N - 9 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Before Starting Engine 1. Preflight Inspection ................................................... COMPLETED 2. Weight and Balance............................................ Verify within limits 3. Emergency Equipment ................................................ ON BOARD 4. Passengers......................................................................BRIEFED 5. Seats, Seat Belts, and Harnesses ................ ADJUST & SECURE Starting Engine 1. External Power (If applicable) ........................................CONNECT 2. Brakes .................................................................................. HOLD 3. Bat Master Switches ............................................ON (Check Volts) 4. Strobe Lights ............................................................................. ON 5. Mixture ..........................................................................FULL RICH 6. Power Lever ........................................................ FULL FORWARD 7. Fuel Pump ..........................................................................BOOST 8. Propeller Area..................................................................... CLEAR 9. Power Lever ........................................................... OPEN ¼ INCH 10. Ignition Switch .......................START (Release after engine starts) 11. Mixture ................................................................................... LEAN until RPM rises to a maximum value. Leave the mixture in this position during taxi and until run-up. 12. Power Lever .............................. RETARD (to maintain 1000 RPM) 13. Oil Pressure ........................................................................CHECK 14. Alt Master Switches ................................................................... ON 15. Avionics Power Switch ............................................................... ON 16. Engine Parameters ........................................................ MONITOR 17. External Power (If applicable) ..................................DISCONNECT 18. Amp Meter/Indication..........................................................CHECK February 2013 NORMAL STARTING ENGINE P/N 13728-010 N - 10 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Cold Weather Operation: Starting 1. Ignition Switch ......................................................................... OFF 2. Propeller ...........................................Hand TURN several rotations 3. External Power (If applicable) ........................................CONNECT 4. Brakes .................................................................................. HOLD 5. Bat Master Switches .........................................ON (check voltage) 6. Mixture..........................................................................FULL RICH 7. Power lever ......................................................... FULL FORWARD 8. Fuel Pump .............................HIGH BOOST/PRIME, then BOOST 9. Propeller Area..................................................................... CLEAR 10. Power Lever ............................................................ OPEN ¼ INCH 11. Ignition Switch .......................START (Release after engine starts) 12. Power Lever ............................... RETARD (to maintain 1000 RPM) 13. Oil Pressure........................................................................CHECK 14. Alt Master Switches ................................................................... ON 15. Avionics Power Switch............................................................... ON 16. Engine Parameters .........................................................MONITOR 17. External Power (If applicable) ..................................DISCONNECT 18. Amp Meter/Indication..........................................................CHECK 19. Strobe Lights ............................................................................. ON Before Taxiing 1. Flaps..................................................................................UP (0%) 2. Radios/Avionics ......................................................AS REQUIRED 3. Cabin Heat/Defrost ................................................ AS REQUIRED 4. Fuel Selector .......................................................... SWITCH TANK Taxiing 1. Parking Brake ............................................................ DISENGAGE 2. Brakes.................................................................................CHECK 3. HSI Orientation ...................................................................CHECK 4. Attitude Gyro.......................................................................CHECK 5. Turn Coordinator ................................................................CHECK February 2013 NORMAL STARTING/ TAXI N - 11 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Before Takeoff 1. Doors .............................................................................. LATCHED 2. CAPS Handle ................................................. Verify Pin Removed 3. Seat Belts and Shoulder Harness ................................... SECURE 4. Air Conditioner...........................................................AS DESIRED • Caution • Use of RECIRC mode prohibited in flight. 5. Fuel Quantity ..................................................................CONFIRM 6. Fuel Selector ........................................................ FULLEST TANK 7. Fuel Pump ..........................................................................BOOST 8. Mixture ....................................................................AS REQUIRED 9. Flaps ............................................................... SET 50% & CHECK 10. Transponder............................................................................. SET 11. Autopilot..............................................................................CHECK 12. Navigation Radios/GPS ..........................................SET for Takeoff 13. Cabin Heat/Defrost .................................................AS REQUIRED 14. Brakes................................................................................... HOLD 15. Power Lever ................................................................... 1700 RPM 16. Alternator ............................................................................CHECK a. Pitot Heat ............................................................................ ON b. Navigation Lights................................................................. ON c. Landing Light....................................................................... ON d. Annunciator Lights .......................................................CHECK Verify both ALT 1 and ALT 2 caution lights out and positive amps indication for each alternator. 17. Voltage................................................................................CHECK 18. Pitot Heat ................................................................AS REQUIRED 19. Navigation Lights ....................................................AS REQUIRED 20. Landing Light ..........................................................AS REQUIRED (Continued on following page) February 2013 NORMAL BEFORE TAKEOFF P/N 13728-010 N - 12 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 21. Magnetos.................................................... CHECK Left and Right RPM drop must not exceed 150 RPM for either magneto. RPM differential must not exceed 75 RPM between magnetos a. Ignition Switch .................................. R, note RPM, then BOTH b. Ignition Switch ...................................L, note RPM, then BOTH 22. Engine Parameters .............................................................CHECK 23. Power Lever ................................................................... 1000 RPM 24. Flight Instruments, HSI, and Altimeter.................... CHECK & SET 25. Flight Controls .................................................FREE & CORRECT 26. Trim..............................................................................SET Takeoff 27. Autopilot...................................................................DISCONNECT If Icing Conditions are Anticipated Immediately After Takeoff: 28. ICE PROTECT System Switch .................................................. ON 29. ICE PROTECT Mode Switch ................................... NORM / HIGH 30. PITOT HEAT Switch................................................................... ON 31. Cabin Heat............................................................................... HOT 32. Windshield Defrost .................................................................... ON 33. Ice-Inspection Lights...............................................AS REQUIRED 34. Verify airframe is free of contamination immediately before takeoff. 35. Flaps..............................................RETRACT as soon as practical February 2013 NORMAL BEFORE TAKEOFF N - 13 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Normal Takeoff 1. Brakes.................................... RELEASE (Steer with Rudder Only) 2. Power Lever ........................................................ FULL FORWARD 3. Engine Parameters .............................................................CHECK 4. Elevator Control ........................ ROTATE Smoothly at 73-76 KIAS 5. At 90 KIAS, Flaps ...................................................................... UP Short Field Takeoff 1. Flaps ........................................................................................ 50% 2. Brakes .................................................................................. HOLD 3. Power Lever ........................................................ FULL FORWARD 4. Mixture ..................................................................................... SET 5. Engine Parameters .............................................................CHECK 6. Brakes.................................... RELEASE (Steer with Rudder Only) 7. Elevator Control ..............................ROTATE Smoothly at 73 KIAS 8. Airspeed at Obstacle ......................................................... 84 KIAS Climb 1. Climb Power............................................................................. SET 2. Flaps ............................................................................... Verify UP 3. Mixture .............................................. LEAN as required for altitude 4. Engine Parameters .............................................................CHECK 5. Fuel Pump ..........................................................................BOOST February 2013 NORMAL TAKEOFF/ CLIMB P/N 13728-010 N - 14 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Icing Conditions: In Flight If Icing Conditions Exist: 1. PITOT HEAT Switch......................................................... Verify ON 2. ICE PROTECT System Switch .................................................. ON 3. ICE PROTECT Mode Switch ................................... NORM / HIGH 4. WIND SHLD Push-Button......................... PRESS AS REQUIRED 5. Monitor ice accumulation. If ice accumulation occurs: a. ICE PROTECT Mode ...................................................... HIGH If ice continues accumulating: b. ICE PROTECT Mode Push-Button ...................................MAX If ice accretions do not shed: c. PUMP BKUP Switch ........................................................... ON d. Perform Deicing System Failure checklist. Inadvertent Icing Encounter: 1. PITOT HEAT Switch......................................................... Verify ON 2. ICE PROTECT System Switch .................................................. ON a. ICE PROTECT Mode Push-Button ...................................MAX to initially dissipate ice accumulation, then b. ICE PROTECT Mode Switch............................. HIGH / NORM If excess ice accumulation occurs, then: c. ICE PROTECT Mode Push-Button ...................................MAX If ice does not shed perform Deicing System Failure checklist. 3. WIND SHLD Push-Button......................... PRESS AS REQUIRED 4. Airspeed ................................................... MAINTAIN 95-177 KIAS or less than 204 KTAS (Continued on following page) February 2013 NORMAL ICING N - 15 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Icing Conditions: In Flight While in Icing Conditions: 1. FLAPS ....................................................................................... UP 2. Ice-Inspection Lights...............................................AS REQUIRED 3. Cabin Heat...............................................................................HOT 4. Windshield Defrost .................................................................... ON 5. Deicing Fluid Quantity ................................................... MONITOR a. Ensure adequate quantity to complete flight. After Leaving Icing Conditions: 1. Deicing System........................................................................ OFF 2. Airspeed ......................................as flight CONDITIONS DICTATE 3. Ice-Inspection Lights...............................................AS REQUIRED 4. Cabin Heat..............................................................AS REQUIRED 5. Windshield Defrost .................................................AS REQUIRED 6. WIND SHLD Push-Button......................... PRESS AS REQUIRED Cruise 1. Oxygen .................................................................. AS REQUIRED 2. Cruise Altitude ........................................................ ESTABLISHED 3. Power Lever .................................... REDUCE to 30.5 in.Hg or less 4. Fuel Pump ..............................................................AS REQUIRED 5. Mixture .............................................................................. ADJUST 6. Engine Parameters ........................................................ MONITOR 7. Fuel Flow and Balance .................................................. MONITOR If any CHT’s exceed 420°F: 8. Mixture ........................................... LEAN 0.5 GPH and MONITOR If Icing Conditions are Encountered During Cruise: 9. Perform Checklist...................................Icing Conditions - In Flight 10. Engine Power....................... INCREASE to maintain cruise speed. 11. Autopilot.......................................................................As Required Disconnect every 30 minutes to detect any out-of-trim conditions. When disconnecting the autopilot with ice accretions on the airplane, the pilot should be alert for out-of-trim forces. February 2013 NORMAL ICING/ CRUISE P/N 13728-010 N - 16 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Descent 1. Altimeter .................................................................................. SET 2. Cabin Heat/Defrost .................................................AS REQUIRED 3. Landing Light ............................................................................. ON 4. Fuel System........................................................................CHECK 5. Mixture....................................................................AS REQUIRED 6. Brake Pressure ...................................................................CHECK If Icing Conditions Exist: 1. ICE PROTECT System Switch .................................................. ON 2. ICE PROTECT Mode Switch ................................................. HIGH 3. Monitor ice accumulation. If ice continues to accumulate: a. ICE PROTECT Mode Push-Button ...................................MAX If ice does not shed: b. PUMP BKUP Switch ........................................................... ON c. Perform Deicing System Failure checklist. 4. WIND SHLD Push-Button......................... PRESS AS REQUIRED 5. Ice-Inspection Lights...............................................AS REQUIRED 6. Flaps........................................................................................ 50% 7. Airspeed .........................................................Minimum of 95 KIAS 8. Airspeed on Short Final ..................................................... 88 KIAS February 2013 NORMAL DESCENT N - 17 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Before Landing 1. Seat Belt and Shoulder Harness ..................................... SECURE 2. Fuel Pump ..........................................................................BOOST 3. Mixture ....................................................................AS REQUIRED 4. Flaps .......................................................................AS REQUIRED 5. Autopilot..................................................................AS REQUIRED Normal Landing 1. Flaps ...................................................................................... 100% 2. Airspeed ....................................................................... 80-85 KIAS If Icing Conditions Exist: a. Airspeed on Short Final .............................................. 88 KIAS 3. Power Lever ............................................................AS REQUIRED After touchdown: 4. Brakes.....................................................................AS REQUIRED Short Field Landing 1. Flaps ...................................................................................... 100% 2. Airspeed ............................................................................ 79 KIAS 3. Power Lever ............................................................AS REQUIRED After clear of obstacles: 4. Power Lever ...................................................... REDUCE TO IDLE After touchdown: 5. Brakes............................................................................ MAXIMUM Balked Landing/Go-Around 1. Autopilot..................................................................... DISENGAGE 2. Power Lever ........................................................ FULL FORWARD 3. Flaps ........................................................................................ 50% 4. Airspeed ....................................................................... 80-85 KIAS After clear of obstacles: 5. Flaps ......................................................................................... UP February 2013 NORMAL LANDING P/N 13728-010 N - 18 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 After Landing 1. Power Lever ................................................................... 1000 RPM 2. Fuel Pump ............................................................................... OFF 3. Flaps.......................................................................................... UP 4. Transponder........................................................................... STBY 5. Lights ......................................................................AS REQUIRED 6. Pitot Heat................................................................................. OFF 7. ICE PROTECT System Switch ................................................ OFF 8. PUMP BKUP Switch ................................................................ OFF 9. Ice-Inspection Lights................................................................ OFF Shutdown 1. Fuel Pump (if used) ................................................................ OFF 2. Throttle ................................................................................... IDLE 3. Ignition Switch .................................................................... CYCLE 4. Mixture.............................................................................. CUTOFF 5. All Switches ............................................................................. OFF 6. Magnetos................................................................................. OFF 7. ELT ...........................................................TRANSMIT LIGHT OUT 8. Chocks, Tie-downs, Pitot Covers ............................AS REQUIRED February 2013 NORMAL AFTER LANDING SHUTDOWN N - 19 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Oxygen Duration (Precise Flight System) ABOVE 18,000FT MASK ONLY Masks or Cannulas Below 18,000FT Masks required if user has Nasal Blockage or Congestion. 1 PERSON - STD 2 PERSONS - STD 3 PERSONS - STD 4 PERSONS - STD 1 PERSON - OXY 2 PERSONS - OXY 3 PERSONS - OXY 4 PERSONS - OXY 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 0 5 10 15 20 25 30 35 40 45 50 55 60 65 ABOVE 18,000FT MASK ONLY Usage Altitude (Ft * 1,000) Hours of Available O2 1 PERSON - STD 2 PERSONS - STD 3 PERSONS - STD 4 PERSONS - STD 1 PERSON - OXY 2 PERSONS - OXY 3 PERSONS - OXY 4 PERSONS - OXY 70 75 80 85 Oxygen System Usage Duration - A5 Flowmeter (STD) Standard Cannula/Mask - (OXY) Oxymiser Cannual Tested Values at Altitude for flow rates STPD (77 Cu. Ft. Serviced to 1,800 PSIG -5%), Flow Rates are For Reference Only 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 0 5 10 15 20 25 30 35 40 45 50 55 60 65 Masks or Cannulas Below 18,000FT Masks required if user has Nasal Blockage or Congestion. Oxygen System Usage Duration - A4 Flowmeter (STD) Standard Cannula/Mask - (OXY) Oxymiser Cannual Tested Values at Altitude for flow rates STPD (77 Cu. Ft. Serviced to 1,800 PSIG -5%), Flow Rates are For Reference Only SR22_FM09_3295 Usage Altitude (Ft * 1,000) Hours of Available O2 February 2013 NORMAL O2 DURATION C I R R U S P I L O T ’ S C H E C K L I S T M O D E L S R 2 2 Performance Table of Contents P/N 13728-010 P - i Takeoff Distance: 3600 LB...............................................................P-1 Takeoff Distance: 2900 LB...............................................................P-2 Cruise Performance .........................................................................P-3 Landing Distance .............................................................................P-5 Stall Speeds with Ice Accumulation .................................................P-6 Cruise Performance with Ice Accumulation .....................................P-7 Cruise Performance with Ice Accumulation .................................P-8 Landing Distance with Ice Accumulation .........................................P-9 Wind Components .........................................................................P-10 Weight and Balance .......................................................................P-11 Loading Calculations .................................................................P-11 Loading Data .............................................................................P-12 Moment Limits ...........................................................................P-12 Temperature Conversion ...............................................................P-13 • Note • Aircraft with optional Air Conditioning System; Brake Horsepower is reduced by approximately 6 BHP. February 2013 NORMAL PERFORMANCE ABNORMAL EMERGENCY PERF P - 1 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Takeoff Distance: 3600 LB Weight: 3600 LB Speed at Liftoff: 76 KIAS Speed over 50 Ft. Obstacle: 84 KIAS Flaps: 50% Power: Takeoff Runway: Dry, Paved, Level Headwind: Subtract 10% for each 12 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Reference Notes. Dry Grass: Add 20% to Ground Roll. Wet Grass: Add 30% to Ground Roll. Air Conditioner: Add 100' to ground roll and 150' to distance over 50' obstacle if Air Conditioner if ON during takeoff. PRESS ALT FT DISTANCE FT TEMPERATURE ~°C 0 10 20 30 40 50 ISA SL Grnd Roll 965 1042 1123 1207 1294 1384 1082 50 ft 1680 1804 1933 2066 2203 2345 1868 1000 Grnd Roll 1063 1148 1237 1330 1426 1526 1175 50 ft 1844 1980 2121 2267 2418 2573 2022 2000 Grnd Roll 1172 1267 1365 1467 1573 1683 1277 50 ft 2025 2174 2329 2490 2656 2827 2190 3000 Grnd Roll 1295 1399 1507 1620 1737 1858 1389 50 ft 2226 2391 2561 2738 2920 3109 2375 4000 Grnd Roll 1431 1546 1666 1791 1920 2054 1512 50 ft 2451 2632 2820 3014 3215 3422 2578 5000 Grnd Roll 1584 1711 1844 1982 2125 2273 1648 50 ft 2701 2900 3107 3322 3543 3772 2801 6000 Grnd Roll 1755 1896 2043 2195 2354 2519 1798 50 ft 2979 3200 3428 3665 3910 4162 3047 7000 Grnd Roll 1946 2103 2266 2435 2611 2794 1963 50 ft 3291 3535 3787 4049 4319 4598 3317 8000 Grnd Roll 2161 2335 2516 2704 2900 3102 2146 50 ft 3640 3909 4189 4478 4777 5086 3616 9000 Grnd Roll 2403 2596 2798 3007 3224 3449 2349 50 ft 4030 4329 4639 4959 5291 5633 3946 10000 Grnd Roll 2675 2890 3114 3347 3589 3840 2574 50 ft 4469 4800 5144 5499 5867 6247 4312 February 2013 PERFORMANCE TAKEOFF P/N 13728-010 P - 2 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Takeoff Distance: 2900 LB Weight: 2900 LB Speed at Liftoff: 70 KIAS Speed over 50 Ft. Obstacle: 74 KIAS Flaps: 50% Power: Takeoff Runway: Dry, Paved, Level Headwind: Subtract 10% for each 12 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Reference Notes. Dry Grass: Add 20% to Ground Roll. Wet Grass: Add 30% to Ground Roll. Air Conditioner: Add 100' to ground roll and 150' to distance over 50' obstacle if Air Conditioner if ON during takeoff. PRESS ALT FT DISTANCE FT TEMPERATURE ~°C 0 10 20 30 40 50 ISA SL Grnd Roll 610 659 710 763 818 875 684 50 ft 971 1043 1118 1195 1275 1358 1080 1000 Grnd Roll 673 727 783 841 902 965 743 50 ft 1066 1146 1228 1313 1401 1492 1170 2000 Grnd Roll 743 802 864 929 995 1064 809 50 ft 1173 1260 1351 1444 1541 1641 1269 3000 Grnd Roll 821 887 955 1026 1100 1177 880 50 ft 1292 1388 1487 1590 1697 1807 1378 4000 Grnd Roll 908 981 1057 1135 1217 1302 959 50 ft 1424 1530 1639 1753 1871 1992 1498 5000 Grnd Roll 1006 1086 1170 1257 1348 1442 1046 50 ft 1571 1688 1809 1935 2065 2199 1630 6000 Grnd Roll 1116 1205 1298 1394 1494 1598 1143 50 ft 1736 1865 1999 2138 2281 2429 1775 7000 Grnd Roll 1238 1337 1440 1547 1659 1774 1249 50 ft 1920 2063 2211 2365 2523 2687 1936 8000 Grnd Roll 1376 1486 1601 1720 1843 1971 1367 50 ft 2127 2285 2449 2619 2795 2977 2113 9000 Grnd Roll 1532 1654 1781 1914 2051 2194 1498 50 ft 2359 2534 2716 2904 3099 3300 2309 10000 Grnd Roll 1707 1843 1985 2132 2285 2444 1643 50 ft 2619 2814 3016 3225 3441 3665 2527 February 2013 TAKEOFF PERFORMANCE P - 3 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Cruise Performance • Note • Subtract 10 KTAS if nose wheel pant and fairing removed. Lower KTAS by 10% if nose and main wheel pants & fairings are removed. Aircraft with optional Air Conditioning System - Cruise performance is reduced by 2 knots. For maximum performance, turn air-conditioner off. Aircraft with optional Enhanced Vision System; Cruise performance is reduced by up to 1 knot. Conditions: • Weight ........................................................................................................ 3400 LB • Winds ............................................................................................................... Zero Press Alt ISA - 30°C ISA ISA + 30°C RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2000 2700 27.4 103% 186 24.6 98% 186 23.3 93% 181 22.0 2600 27.4 99% 183 23.5 94% 183 22.2 89% 178 21.5 2500 27.4 93% 179 22.1 88% 179 20.9 84% 174 20.8 2500 26.4 89% 176 21.1 84% 176 19.9 80% 171 20.2 2500 25.4 84% 173 20.0 80% 173 19.0 76% 168 19.5 2500 24.4 80% 170 19.0 76% 170 18.0 72% 165 18.8 2500 23.4 76% 167 18.0 72% 167 17.0 68% 162 18.1 4000 2700 25.4 96% 185 22.9 91% 185 21.6 87% 180 20.8 2600 25.4 92% 182 21.9 87% 182 20.7 83% 177 20.6 2500 25.4 87% 178 20.6 82% 178 19.5 78% 173 19.9 2500 24.4 82% 175 19.5 78% 175 18.5 74% 170 19.2 2500 23.4 78% 172 18.5 74% 172 17.5 70% 167 18.5 2500 22.4 73% 169 17.4 69% 169 16.5 66% 163 17.7 2500 21.4 69% 165 16.4 65% 165 15.5 62% 159 16.9 6000 2700 23.5 89% 184 21.2 85% 184 20.1 81% 179 19.6 2600 23.5 85% 181 20.3 81% 181 19.2 77% 176 19.1 2500 23.5 80% 177 19.1 76% 177 18.1 72% 172 18.3 2500 22.5 76% 174 18.1 72% 174 17.1 68% 169 17.6 2500 21.5 72% 170 17.0 68% 170 16.1 64% 165 16.9 2500 20.5 67% 166 15.9 64% 166 15.1 60% 161 16.1 2500 19.5 63% 162 14.9 59% 162 14.1 56% 157 15.3 February 2013 PERFORMANCE CRUISE P/N 13728-010 P - 4 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 8000 2700 21.7 83% 183 19.7 78% 183 18.6 75% 178 17.7 2600 21.7 79% 180 18.8 75% 180 17.8 71% 175 17.0 2500 21.7 75% 176 17.7 71% 176 16.8 67% 171 16.0 2500 20.7 70% 172 16.7 66% 172 15.8 63% 167 15.0 2500 19.7 66% 168 15.6 62% 168 14.8 59% 163 14.0 2500 18.7 61% 163 14.5 58% 163 13.8 55% 158 13.1 2500 17.7 57% 159 13.5 54% 159 12.8 51% 153 12.1 10000 2700 20.0 77% 182 18.2 73% 182 17.3 69% 176 16.4 2600 20.0 71% 177 17.0 68% 177 16.1 64% 172 15.3 2500 20.0 67% 173 16.0 64% 173 15.1 61% 167 14.4 2500 19.0 63% 168 14.9 59% 168 14.1 56% 163 13.4 2500 18.0 58% 163 13.8 55% 163 13.1 52% 158 12.5 2500 17.0 54% 158 12.8 51% 158 12.1 48% 153 11.5 12000 2700 18.5 71% 180 16.9 67% 180 16.0 64% 175 15.2 2600 18.5 68% 177 16.2 64% 177 15.3 61% 172 14.5 2500 18.5 64% 173 15.2 60% 173 14.4 58% 167 13.7 2500 17.5 59% 168 14.1 56% 168 13.4 53% 162 12.7 2500 16.5 55% 162 13.0 52% 162 12.3 49% 157 11.7 2500 15.5 50% 156 12.0 48% 156 11.3 45% 151 10.8 14000 2700 17.1 66% 178 15.6 62% 178 14.8 59% 173 14.1 2600 17.1 63% 175 14.9 60% 175 14.1 57% 170 13.5 2500 17.1 59% 171 14.1 56% 171 13.3 53% 165 12.7 2500 16.1 55% 165 13.0 52% 165 12.3 49% 159 11.7 2500 15.1 50% 159 11.9 47% 159 11.2 45% 153 10.7 16000 2700 15.8 61% 176 14.5 58% 176 13.7 55% 171 13.0 2600 15.8 58% 173 13.8 55% 173 13.1 52% 167 12.5 2500 15.8 55% 168 13.0 52% 168 12.3 49% 163 11.7 2500 14.8 50% 162 11.9 47% 162 11.3 45% 156 10.7 17000 2700 15.2 59% 175 13.9 55% 175 13.2 53% 169 12.5 2600 15.2 56% 171 13.3 53% 171 12.6 50% 166 12.0 2500 15.2 53% 167 12.5 50% 167 11.9 47% 162 11.3 2500 14.2 48% 160 11.4 45% 160 10.8 43% 155 10.3 Press Alt ISA - 30°C ISA ISA + 30°C RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH February 2013 CRUISE PERFORMANCE P - 5 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Landing Distance WEIGHT: 3600 LB Speed over 50 Ft Obstacle: 79 KIAS Flaps: 100% Power: Idle Runway: Dry, Paved, Level Headwind: Subtract 10% for each 13 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Reference Notes Dry Grass: Add 20% to Ground Roll Wet Grass: Add 60% to Ground Roll PRESS ALT FT DISTANCE FT TEMPERATURE ~°C 0 10 20 30 40 50 ISA SL Grnd Roll 1117 1158 1198 1239 1280 1321 1178 Total 2447 2505 2565 2625 2685 2747 2535 1000 Grnd Roll 1158 1200 1243 1285 1327 1370 1213 Total 2506 2567 2630 2693 2757 2821 2585 2000 Grnd Roll 1201 1245 1289 1333 1377 1421 1250 Total 2568 2633 2699 2765 2832 2900 2636 3000 Grnd Roll 1246 1292 1337 1383 1428 1474 1287 Total 2635 2702 2771 2841 2911 2983 2691 4000 Grnd Roll 1293 1340 1388 1435 1482 1530 1326 Total 2705 2776 2848 2922 2996 3070 2748 5000 Grnd Roll 1342 1391 1440 1489 1539 1588 1367 Total 2779 2854 2930 3007 3085 3163 2808 6000 Grnd Roll 1393 1444 1495 1546 1598 1649 1409 Total 2857 2936 3016 3097 3179 3261 2871 7000 Grnd Roll 1447 1500 1553 1606 1659 1712 1453 Total 2941 3024 3108 3193 3279 3365 2937 8000 Grnd Roll 1503 1558 1613 1668 1724 1779 1499 Total 3029 3116 3205 3294 3384 3475 3006 9000 Grnd Roll 1562 1619 1677 1734 1791 1848 1546 Total 3122 3214 3307 3401 3496 3592 3079 10000 Grnd Roll 1624 1683 1743 1802 1862 1921 1595 Total 3221 3318 3416 3515 3614 3715 3155 February 2013 PERFORMANCE LANDING P/N 13728-010 P - 6 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Stall Speeds with Ice Accumulation • Note • Altitude loss during wings level stall may be 600 feet or more. KIAS values may not be accurate at stall. Conditions: • Weight ........................................................................................................ 3600 LB • CG ..................................................................................................................Noted • Power..................................................................................................................Idle • Bank Angle .....................................................................................................Noted Weight LB Bank Angle Deg STALL SPEEDS Flaps 0% Full Up Flaps 50% KIAS KCAS KIAS KCAS 3600 Most FWD CG 0 77 76 72 69 15 79 77 73 70 30 83 82 75 74 45 91 90 82 82 60 107 107 95 98 3600 Most AFT CG 0 77 76 72 69 15 79 77 73 70 30 83 82 75 74 45 91 90 82 82 60 107 107 95 98 February 2013 ICE PERF STALL PERFORMANCE P - 7 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Cruise Performance with Ice Accumulation • Note • Aircraft with optional Air Conditioning System - Cruise performance is reduced by 2 knots. For maximum performance, the air-conditioner should be off. Conditions: • Cruise Weight ............................................................................................ 3400 LB • Winds ............................................................................................................... Zero 2000 Feet Pressure Altitude ISA -30°C (-19°C) ISA (11°C) ISA + 30°C (41°C) RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2700 27.4 103% 160 24.6 2600 27.4 99% 157 23.5 2500 27.4 93% 153 22.1 2500 26.4 89% 150 21.1 2500 25.4 84% 146 20.0 2500 24.4 80% 142 19.0 2500 23.4 76% 137 18.0 4000 Feet Pressure Altitude ISA -30°C (-23°C) ISA (7°C) ISA + 30°C (37°C) RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2700 25.4 96% 158 22.9 2600 25.4 92% 155 21.9 2500 25.4 87% 150 20.6 2500 24.4 82% 146 19.5 2500 23.4 78% 141 18.5 2500 22.4 73% 136 17.4 2500 21.4 69% 130 16.4 6000 Feet Pressure Altitude ISA -30°C (-27°C) ISA (3°C) ISA + 30°C (33°C) RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2700 23.5 89% 155 21.2 85% 155 20.1 2600 23.5 85% 151 20.3 81% 151 19.2 2500 23.5 80% 146 19.1 76% 146 18.1 2500 22.5 76% 140 18.1 72% 140 17.1 2500 21.5 72% 134 17.0 68% 134 16.1 2500 20.5 67% 128 15.9 64% 128 15.1 2500 19.5 63% 120 14.9 59% 120 14.1 February 2013 PERFORMANCE ICE PERF CRUISE P/N 13728-010 P - 8 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Cruise Performance with Ice Accumulation 8000 Feet Pressure Altitude ISA -30°C (-31°C) ISA (-1°C) ISA + 30°C (29°C) RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2700 21.7 83% 150 19.7 78% 150 18.6 2600 21.7 79% 146 18.8 75% 146 17.8 2500 21.7 75% 140 17.7 71% 140 16.8 2500 20.7 70% 133 16.7 66% 133 15.8 2500 19.7 66% 126 15.6 62% 126 14.8 2500 18.7 61% 117 14.5 58% 117 13.8 2500 17.7 57% 108 13.5 54% 108 12.8 10,000 Feet Pressure Altitude ISA -30°C (-35°C) ISA (-5°C) ISA + 30°C (25°C) RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2700 20.0 77% 144 18.2 73% 144 17.3 2600 20.0 71% 136 17.0 68% 136 16.1 2500 20.0 67% 129 16.0 64% 129 15.1 2500 19.0 63% 120 14.9 59% 120 14.1 2500 18.0 58% 111 13.8 55% 111 13.1 2500 17.0 54% 100 12.8 51% 100 12.1 February 2013 ICE PERF CRUISE PERFORMANCE P - 9 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Landing Distance with Ice Accumulation • Note • Sloped Runway - Increase distances by 27% of ground roll distance for each 1% downslope. Decrease distances by 9% of ground roll distance for each 1% upslope. Associated balked landing climb gradient less than 3.3% shown in heavier table borders. WEIGHT: 3600 LB Speed over 50 Ft Obstacle: 88 KIAS Flaps: 50% Power: Smooth power reduction from obstacle to idle at touchdown. Runway: Dry, Paved, Level Headwind: Subtract 10% for each 13 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Reference Notes Dry Grass: Add 20% to Ground Roll Wet Grass: Add 60% to Ground Roll PRESS ALT FT DISTANCE FT TEMPERATURE ~°C -20 -10 0 5 ISA SL Grnd Roll 1356 1409 1463 1489 Total 2833 2908 2984 3022 1000 Grnd Roll 1406 1461 1517 1544 Total 2903 2981 3061 3101 2000 Grnd Roll 1458 1516 1573 1602 Total 2977 3059 3143 3185 3000 Grnd Roll 1513 1572 1632 1662 Total 3055 3142 3229 3274 4000 Grnd Roll 1570 1632 1694 1725 Total 3138 3229 3321 3367 5000 Grnd Roll 1629 1694 1758 1790 Total 3225 3321 3418 3466 6000 Grnd Roll 1692 1758 1825 1859 Total 3318 3418 3520 3571 7000 Grnd Roll 1757 1826 1896 1930 Total 3416 3522 3628 3682 8000 Grnd Roll 1825 1897 1969 2005 1963 Total 3520 3631 3743 3800 3583 9000 Grnd Roll 1896 1971 2046 2084 2025 Total 3630 3746 3864 3924 3656 10000 Grnd Roll 1971 2049 2127 2166 2089 Total 3746 3869 3993 4055 3733 February 2013 PERFORMANCE ICE PERF LANDING P/N 13728-010 P - 10 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Wind Components • Note • The maximum demonstrated crosswind is 21 knots. Value not considered limiting. Conditions: Example: (See Chart ) • Runway Heading .......................... 10° Wind/Flight Path Angle ................. 50° • Wind Direction .............................. 60° Crosswind Component......... 12 Knots • Wind Velocity ........................15 Knots Headwind Component ......... 10 Knots 10 10 Headwind Tailwind WIND COMPONENTS - KNOTS 0 ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH SR2_FM05_1014 40 30 20 10 0 -10 -20 20 30 40 50 60 70 80 90 100 110 120 30 40 10 20 130 140 150 160 170 180 20 30 40 50 CROSSWIND COMPONENT ~ KNOTS VELOCITY ~ KNOTS WIND February 2013 WIND CMPNNTS PERFORMANCE P - 11 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Weight and Balance Loading Calculations For Moment/1000, refer to Loading Data table on following page. Calculation Instructions 1. Enter the current basic empty weight and moment from the aircraft’s Weight and Balance Record. 2. Enter the total weight and moment/1000 for the front seat occupants from the adjacent Loading Data Table. 3. Enter the total weight and moment/1000 for the rear seat occupants from the adjacent Loading Data Table. 4. Enter the total weight and moment/1000 for the baggage from the adjacent Loading Data Table. 5. If desired, subtotal the weight and moment/1000 entries from steps 1 - 4. 6. Enter the weight and moment/1000 of usable fuel loaded on the airplane. 7. Subtotal the weight and moment/1000. 8. Enter values for typical start, taxi, and run-up operations of 9 pounds at an average moment\1000 of 1.394. 9. Subtract step 8 weight and moment/1000 from the Ramp Weight to determine the Takeoff Weight and moment/1000. a. Verify Takeoff Weight does not exceed the 3600 pounds. b. Verify Moment/1000 does falls between the interpolated minimum and maximum values listed on the adjacent Moment Limits Table. Description Weight Moment/1000 1. Empty Weight Includes unusable fuel and full oil 2. Front Seats Occupants Pilot and Passenger 3. Rear Seats Occupants 4. Baggage 130 lb maximum 5. Zero Fuel Condition Subtotal items 1 thru 4 3400 lb maximum 6. Fuel Load 92 Gallon @6.0 lb/gal. maximum 7. Ramp Weight Subtotal items 5 and 6 8. Fuel for start, taxi, and runup Normally 9 lb at avg. mmnt of 1394.1 - - 9. Takeoff Weight Subtract Item 8 from item 7 February 2013 PERFORMANCE W&B P/N 13728-010 P - 12 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Loading Data Use this table to determine the Moment/1000. Moment Limits Use this table to determine if Loading Calculations are within limits. Weight LB Fwd Pass FS 143.5 Aft Pass FS 180.0 Baggage FS 208.0 Fuel FS 154.9 Weight LB Fwd Pass FS 143.5 Aft Pass FS 180.0 Fuel FS 154.9 20 2.9 3.6 4.2 3.1 300 43.1 54.0 46.5 40 5.7 7.2 8.3 6.2 320 45.9 57.6 49.6 60 8.6 10.8 12.5 9.3 340 48.8 61.2 52.7 80 11.5 14.4 16.6 12.4 360 51.7 64.8 55.8 100 14.4 18.0 20.8 15.5 380 54.5 68.4 58.9 120 17.2 21.6 25.0 18.6 400 57.4 72.0 62.0 140 20.1 25.2 27.04* 21.7 420 60.3 75.6 65.1 160 23.0 28.8 24.8 440 63.1 79.2 68.2 180 25.8 32.4 27.9 460 82.8 71.3 200 28.7 36.0 31.0 480 86.4 74.4 220 31.6 39.6 34.1 500 90.0 77.5 240 34.4 43.2 37.2 520 80.5 260 37.3 46.8 40.3 552** 85.5 280 40.2 50.4 43.4 *130 lb Maximum **92 U.S. Gallons Usable Weight LB Moment/1000 Weight LB Moment/1000 Minimum Maximum Minimum Maximum 2200 304 326 2950 414 437 2250 311 333 3000 422 444 2300 318 341 3050 430 452 2350 326 348 3100 438 459 2400 333 355 3150 445 467 2450 340 363 3200 453 474 2500 347 370 3250 461 481 2550 354 378 3300 469 489 2600 362 385 3350 477 496 2650 369 392 *3400 484 504 2700 375 400 3450 494 511 2750 383 407 3500 501 519 2800 390 415 3550 508 526 2850 398 422 3600 515 533 2900 406 430 *NOTE: Maximum zero fuel weight. February 2013 PERFORMANCE W&B P - 13 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Temperature Conversion To convert from Celsius (°C) to Fahrenheit (°F), find, in the shaded columns, the number representing the temperature value (°C) to be converted. The equivalent Fahrenheit temperature is read to the right.  EXAMPLE: 38°C = 100°F. To convert from Fahrenheit (°F) to Celsius (°C), find in the shaded columns area, the number representing the temperature value (°F) to be converted. The equivalent Celsius temperature is read to the left.  EXAMPLE: 38°F = 3°C. Temp to Convert °C or °F Temp to Convert °C or °F Temp to Convert °C or °F °C  °F °C  °F °C  °F -50 -58 -72 -17 2 36 17 62 144 -49 -56 -69 -16 4 39 18 64 147 -48 -54 -65 -14 6 43 19 66 151 -47 -52 -62 -13 8 46 20 68 154 -46 -50 -58 -12 10 50 21 70 158 -44 -48 -54 -11 12 54 22 72 162 -43 -46 -51 -10 14 57 23 74 165 -42 -44 -47 -9 16 61 24 76 169 -41 -42 -44 -8 18 64 26 78 172 -40 -40 -40 -7 20 68 27 80 176 -39 -38 -36 -6 22 72 28 82 180 -38 -36 -33 -4 24 75 29 84 183 -37 -34 -29 -3 26 79 30 86 187 -36 -32 -26 -2 28 82 31 88 190 -34 -30 -22 -1 30 86 32 90 194 -33 -28 -18 0 32 90 33 92 198 -32 -26 -15 1 34 93 34 94 201 -31 -24 -11 2 36 97 36 96 205 -30 -22 -8 3 38 100 37 98 208 -29 -20 -4 4 40 104 38 100 212 -28 -18 0 6 42 108 39 102 216 -27 -16 3 7 44 111 40 104 219 -26 -14 7 8 46 115 41 106 223 -24 -12 10 9 48 118 42 108 226 -23 -10 14 10 50 122 43 110 230 -22 -8 18 11 52 126 44 112 234 -21 -6 21 12 54 129 46 114 237 -20 -4 25 13 56 133 47 116 241 -19 -2 28 14 58 136 48 118 244 -18 0 32 16 60 140 49 120 248 February 2013 PERFORMANCE TEMP CONVERT C I R R U S P I L O T ’ S C H E C K L I S T M O D E L S R 2 2 Abnormal Procedures Table of Contents P/N 13728-010 A - i Flight Environment ...........................................................................A-1 Inadvertent Icing Encounter.........................................................A-1 Inadvertent IMC Encounter..........................................................A-1 Door Open In Flight .....................................................................A-1 Abnormal Landings ..........................................................................A-2 Landing With Failed Brakes.........................................................A-2 Landing With Flat Tire .................................................................A-2 Engine System .................................................................................A-3 Low Idle Oil Pressure ..................................................................A-3 Manifold Pressure High ...............................................................A-3 Starter Engaged ..........................................................................A-3 Fuel System .....................................................................................A-4 Low Fuel Quantity........................................................................A-4 Left OR Right Fuel Tank Quantity ...............................................A-4 Fuel Imbalance ............................................................................A-4 Electrical System .............................................................................A-5 Low Voltage on Main Bus 1.........................................................A-5 Low Voltage on Main Bus 2.........................................................A-5 Perspective Crew Alerting System (CAS) Index CAS Message Page CAS Message Page OIL PRESS A-3 MFD FAN FAIL A-7 MAN PRESSURE A-3 PITOT HEAT FAIL A-8 START ENGAGE A-3 PITOT HEAT REQD A-8 FUEL QTY A-4 FLAPS A-9 L FUEL QTY A-4 BRAKE TEMP A-9 R FUEL QTY A-4 ANTI ICE QTY A-10 FUEL IMBALANCE A-4 AOA OVERHEAT A-10 M BUS 1 A-5 ANTI ICE PSI A-11 M BUS 2 A-5 ANTI ICE PSI A-11 BATT 1 A-5 ANTI ICE SPD A-11 ALT 1 A-6 ANTI ICE LVL A-12 ALT 2 A-6 ANTI ICE HTR A-12 AVIONICS OFF A-7 PARK BRAKE A-13 PFD FAN FAIL A-7 February 2013 NORMAL PERFORMANCE ABNORMAL EMERGENCY ABNORMAL C I R R U S P I L O T ’ S C H E C K L I S T M O D E L S R 2 2 Abnormal Procedures Table of Contents A - ii P/N 13728-010 Battery 1 Current Sensor.............................................................A-5 Low Alternator 1 Output ..............................................................A-6 Low Alternator 2 Output...............................................................A-6 Integrated Avionics System..............................................................A-7 Avionics Switch Off......................................................................A-7 PFD Cooling Fan Failure .............................................................A-7 MFD Cooling Fan Failure ............................................................A-7 Flight Displays Too Dim...............................................................A-7 Pitot Static System ...........................................................................A-8 Pitot Static Malfunction ................................................................A-8 Pitot Heat Current Sensor Annunciation......................................A-8 Pitot Heat Required Annunciation ...............................................A-8 Flight Control System.......................................................................A-9 Electric Trim/Autopilot Failure......................................................A-9 Flap System Exceedance............................................................A-9 Landing Gear System ......................................................................A-9 Brake Failure During Taxi ............................................................A-9 Left/Right Brake Over-Temperature ............................................A-9 Anti-Ice System ..............................................................................A-10 Windshield De-Ice System Malfunction .....................................A-10 Heated Lift Transducer Malfunction...........................................A-10 Low Fluid Quantity Caution .......................................................A-10 Lift Transducer Overheat Caution .............................................A-10 Persistent Low Pressure Caution ..............................................A-11 High Pressure Caution ..............................................................A-11 Speed Caution...........................................................................A-11 Left/Right Anti-Ice Fluid Level Caution ......................................A-12 Stall Warning / AOA Heater Failure Caution .............................A-12 Other Conditions ............................................................................A-13 Aborted Takeoff .........................................................................A-13 Parking Brake Engaged Annunciation.......................................A-13 Communications Failure............................................................A-13 Electrical System Schematic..........................................................A-14 February 2013 NORMAL PERFORMANCE ABNORMAL EMERGENCY ABNORMAL P/N 13728-010 A - 1 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Flight Environment Inadvertent Icing Encounter 1. Pitot Heat................................................................................... ON 2. Exit icing conditions. Turn back or change altitude. 3. Cabin Heat..................................................................... MAXIMUM 4. Windshield Defrost ..................................................... FULL OPEN 5. Alternate Induction Air ............................................................... ON Inadvertent IMC Encounter 1. Airplane Control...................... ESTABLISH straight and level flight 2. Autopilot.............................. ENGAGE to hold heading and altitude 3. Heading ............................................... RESET to initiate 180° turn Door Open In Flight 1. Airplane Control..............................................................MAINTAIN February 2013 ABNORMAL IN FLIGHT A - 2 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Abnormal Landings Landing With Failed Brakes One brake inoperative 1. Land on the side of runway corresponding to the inoperative brake. 2. Maintain directional control using rudder and working brake. Both brakes inoperative 1. Divert to the longest, widest runway with the most direct headwind. 2. Land on downwind side of the runway. 3. Use the rudder for obstacle avoidance. 4. Perform Emergency Engine Shutdown on Ground checklist. Landing With Flat Tire Main Gear 1. Land on the side of the runway corresponding to the good tire. 2. Maintain directional control with the brakes and rudder. 3. Do not taxi. Stop the airplane and perform a normal engine shutdown. Nose Gear 1. Land in the center of the runway. 2. Hold the nosewheel off the ground as long as possible. 3. Do not taxi. Stop the airplane and perform a normal engine shutdown. February 2013 ABNORMAL LANDING P/N 13728-010 A - 3 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Engine System Low Idle Oil Pressure 1. If In-Flight.................................. LAND AS SOON AS PRACTICAL Manifold Pressure High 1. Power Lever .........................................REDUCE to less than 36.5" 2. Flight.............................................................................CONTINUE If noticeable surging is present: 3. Complete Overboost / Pressure Relief Valve Emergency Checklist Starter Engaged On-Ground 1. Ignition Switch ...........................DISENGAGE prior to 20 Seconds 2. Battery Switches........... Wait 20 seconds before next start attempt If starter does not disengage (relay or solenoid failure): 3. BAT 1 Switch ........................................................................... OFF 4. Engine ....................................................................... SHUTDOWN 5. STARTER Circuit breaker ...................................................... PULL In-Flight 1. Ignition Switch ......................................Ensure not stuck in START 2. STARTER Circuit breaker ...................................................... PULL 3. Flight.............................................................................CONTINUE Engine start will not be available at destination. OIL PRESS MAN PRESSURE START ENGAGE February 2013 ABNORMAL ENGINE A - 4 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Fuel System Low Fuel Quantity 1. Fuel Quantity Gages...........................................................CHECK If fuel quantity indicates less than or equal to 14 gallons: a. Land as soon as practical. If fuel quantity indicates more than 14 gallons: a. Flight ...................................................CONTINUE, MONITOR Left OR Right Fuel Tank Quantity Conduct the following procedure if either of the annunciations listed below are displayed on the MFD. 1. Indicated (L or R) Fuel Quantity Gage................................CHECK If fuel quantity indicates less than or equal to 14 gallons: a. If On-Ground .............................. REFUEL PRIOR TO FLIGHT b. If In-Flight ............................................CONTINUE, MONITOR If fuel quantity indicates more than 14 gallons: a. If On-Ground .......................... CORRECT PRIOR TO FLIGHT b. If In-Flight ............................................CONTINUE, MONITOR Fuel Imbalance 1. Fuel Quantity Gages...........................................................CHECK 2. Fuel Pump ..........................................................................BOOST If HIGH BOOST already in use for vapor suppression, pump should be left in this position for tank switch. 3. Fuel Selector ......................................... SELECT FULLEST TANK 4. Fuel Pump ..............................................................AS REQUIRED After switching tanks, message will remain until sensed imbalance is less than 10 gallons. FUEL QTY L FUEL QTY R FUEL QTY FUEL IMBALANCE February 2013 ABNORMAL FUEL P/N 13728-010 A - 5 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Electrical System Low Voltage on Main Bus 1 1. Perform Alt 1 Caution (Failure) Checklist. Low Voltage on Main Bus 2 1. Perform Alt 1 and Alt 2 Caution (Failure) checklists. Battery 1 Current Sensor 1. Main Bus 1, 2 and Non-Essential Bus Loads .................. REDUCE 2. Main Bus 1, 2 and Essential Bus Voltages .....................MONITOR 3. Land as soon as practical. M BUS 1 M BUS 2 BATT 1 February 2013 ABNORMAL ELECTRIC A - 6 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Low Alternator 1 Output 1. ALT 1 Circuit Breaker.............................................. CHECK & SET 2. ALT 1 Master Switch ........................................................... CYCLE If alternator does not reset (low A1 Current and M1 voltage): 3. ALT 1 Master Switch ................................................................ OFF 4. Non-Essential Bus Loads ................................................ REDUCE a. If flight conditions permit, consider shedding the following to preserve Battery 1: (1) Air Conditioning, (2) Landing Light, (3) Yaw Servo, (4) Convenience Power (aux items plugged into armrest jack) 5. Continue Flight, avoiding IMC or night flight as able. Low Alternator 2 Output 1. ALT 2 Circuit Breaker.............................................. CHECK & SET 2. ALT 2 Master Switch ........................................................... CYCLE If alternator does not reset (low A2 Current and M2 voltage less than M1 voltage): 3. ALT 2 Master Switch ................................................................ OFF 4. Continue Flight, avoiding IMC or night flight as able (reduced power redundancy). ALT 1 ALT 2 February 2013 ABNORMAL ELECTRIC P/N 13728-010 A - 7 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Integrated Avionics System Avionics Switch Off 1. AVIONICS Switch ........................................... ON, AS REQUIRED PFD Cooling Fan Failure 1. AVIONICS FAN 2 Circuit Breaker ....................................... CYCLE If annunciation does not extinguish: a. Hot cabin temperatures...... LAND AS SOON AS PRACTICAL b. Cool cabin temperatures .....................CONTINUE, MONITOR MFD Cooling Fan Failure 1. AVIONICS FAN 1 Circuit Breaker ....................................... CYCLE If annunciation does not extinguish: a. High cabin temperatures .... LAND AS SOON AS PRACTICAL b. Low cabin temperatures......................CONTINUE, MONITOR Flight Displays Too Dim 1. INSTRUMENT dimmer knob ..............OFF (full counter-clockwise) If flight displays do not provide sufficient brightness: 2. Revert to standby instruments. AVIONICS OFF PFD FAN FAIL MFD FAN FAIL February 2013 ABNORMAL AVIONICS A - 8 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Pitot Static System Pitot Static Malfunction Static Source Blocked 1. Pitot Heat ................................................................................... ON 2. Alternate Static Source......................................................... OPEN Pitot Tube Blocked 1. Pitot Heat ................................................................................... ON Pitot Heat Current Sensor Annunciation 1. Pitot Circuit Breaker............................................................ CYCLE 2. Pitot Heat ............................................................. CYCLE OFF, ON If inadvertent icing encountered, perform Inadvertent Icing Encounter Emergency Checklist and: a. Airspeed ....................... EXPECT NO RELIABLE INDICATION b. Exit icing conditions using attitude, altitude, and power instruments. Pitot Heat Required Annunciation 1. Pitot Heat ................................................................................... ON PITOT HEAT FAIL PITOT HEAT REQD February 2013 ABNORMAL PITOT- STATIC P/N 13728-010 A - 9 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Flight Control System Electric Trim/Autopilot Failure 1. Airplane Control.......................................... MAINTAIN MANUALLY 2. Autopilot (if engaged)................................................. DISENGAGE If Problem Is Not Corrected: 3. Circuit Breakers ............................................PULL AS REQUIRED • PITCH TRIM • ROLL TRIM • YAW SERVO • AP SERVOS 4. Power Lever ............................................................AS REQUIRED 5. Control Yoke .................................MANUALLY HOLD PRESSURE 6. Land as soon as practical. Flap System Exceedance 1. Airspeed .......................................................................... REDUCE or 1. Flaps.............................................................................. RETRACT Landing Gear System Brake Failure During Taxi 1. Engine Power .........................................................AS REQUIRED 2. Directional Control ............................... MAINTAIN WITH RUDDER 3. Brake Pedal(s) ...................................................................... PUMP If directional control can not be maintained: 4. Ignition Switch ......................................................................... OFF Left/Right Brake Over-Temperature 1. Stop aircraft and allow the brakes to cool. FLAPS BRAKE TEMP February 2013 ABNORMAL FLT CNTRLS LANDING GEAR A - 10 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Anti-Ice System Windshield De-Ice System Malfunction 1. ICE PROTECT A Circuit Breaker........................................ CYCLE 2. Fluid Quantity .................................. SWITCH TO FULLEST TANK 3. WIND SHLD Push-Button......................... PRESS AS REQUIRED If the forward field of view is overly restricted during landing approach and taxiing: a. Cabin Heat ........................................................................HOT b. Windshield Defrost .............................................................. ON c. Execute a forward slip as required for visibility. d. Avoid taxiing without adequate forward visibility. Heated Lift Transducer Malfunction If ice forms on lift transducer: 1. STALL VANE HEAT Circuit Breaker.................................... CYCLE 2. PITOT HEAT Switch............................................. CYCLE OFF, ON If ice remains on lift transducer: 1. Stall Warning System ......... EXPECT NO RELIABLE INDICATION This includes: • Impending stall warning. • Stall speed indication. 2. Airspeed ............................................. MONITOR, DO NOT STALL 3. Fly published V REF speeds......... Minimum 88 KIAS with 50% Flap Low Fluid Quantity Caution 1. Icing Conditions .........................................................AVOID / EXIT Lift Transducer Overheat Caution 1. PITOT HEAT Switch................................................................. OFF 2. Icing Conditions .........................................................AVOID / EXIT ANTI ICE QTY AOA OVERHEAT February 2013 ABNORMAL ANTI-ICE P/N 13728-010 A - 11 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Persistent Low Pressure Caution 1. ICE PROTECT A and B Circuit Breakers ................................ SET 2. Anti-Ice - TKS Quantity.................... SWITCH TO FULLEST TANK 3. WIND SHLD Push-Button................................................... PRESS a. Repeat operation of windshield pump to verify system is primed properly as evidenced by anti-ice fluid exiting windshield nozzles. 4. ICE PROTECT Mode Switch ................................................. HIGH If caution annunciation extinguishes: a. Anti-Ice System ........................................................MONITOR If caution annunciation does not extinguishes or intermittent: a. PUMP BKUP Switch ........................................................... ON b. Icing Conditions...................................................AVOID / EXIT High Pressure Caution 1. Evidence of Anti-Ice Flow ...............................MONITOR / VERIFY 2. Icing Conditions .........................................................AVOID / EXIT Speed Caution 1. Airspeed ................................................... MAINTAIN 95-177 KIAS or less than 204 KTAS ANTI ICE PSI ANTI ICE PSI ANTI ICE SPD February 2013 ABNORMAL ANTI-ICE A - 12 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Left/Right Anti-Ice Fluid Level Caution 1. Revert to manual control of the fluid source to control the fluid level quantity. If ANTI ICE FLO or ANTI ICE PSI annunciates: a. Switch to opposite tank. b. WIND SHLD Push-Button ............................................ PRESS (1) Repeat operation of windshield pump to verify system is primed properly as evidenced by anti-ice fluid exiting windshield nozzles. Stall Warning / AOA Heater Failure Caution 1. STALL VANE HEAT Circuit Breaker.................................... CYCLE 2. PITOT HEAT Circuit Breaker .............................................. CYCLE 3. Icing Conditions .........................................................AVOID / EXIT 4. Fly aircraft normally using airframe buffet as the stall warning. Ice accumulations on the stall warning vane may result in unreliable stall warning system operation. ANTI ICE LVL ANTI ICE HTR February 2013 ABNORMAL ANTI-ICE P/N 13728-010 A - 13 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Other Conditions Aborted Takeoff 1. Power Lever ............................................................................ IDLE 2. Brakes.....................................................................AS REQUIRED Parking Brake Engaged Annunciation 1. Parking Brake .................................................................RELEASE 2. Monitor CAS for BRAKE TEMP Caution. Stop aircraft and allow the brakes to cool if necessary. Communications Failure 1. Switches, Controls ..............................................................CHECK 2. Frequency........................................................................ CHANGE 3. Circuit Breakers ....................................................................... SET 4. Headset ........................................................................... CHANGE 5. Hand Held Microphone..................................................CONNECT PARK BRAKE February 2013 ABNORMAL OTHER A - 14 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Electrical System Schematic STALL VANE HEAT CABIN AIR CONTROL 30A BAT 2 SWITCH BAT 2 AVIONICS SWITCH 20A 8A 8A 20A VOLT REG BAT 1 SWITCH EXTERNAL POWER MAIN DIST BUS 2 50A 50A 80A BAT 1 RELAY 30A 30A 30A STARTER SWITCH AVIONICS NON-ESSENTIAL RELAY 30A 30A STARTER 125A EXTERNAL POWER RELAY STARTER RELAY LANDING LIGHT LANDING LIGHT SWITCH 7.5A BAT 1 ALT 1 RELAY MAIN DIST BUS 1 30A ALT 1 F B 100A VOLT REG MASTER CONTROL UNIT ALT 1 SWITCH DME / ADF AVIONICS BUS AUDIO PANEL WEATHER / DATA LINK TRAFFIC XPONDER STDBY ATTD #2 MFD #2 MAIN BUS 1 CABIN LIGHTS / OXYGEN FUEL QTY KEYPADS / AP CTRL AP SERVOS AVIONICS ICE PROTECTION ESSENTIAL BUS 2 ENGINE INSTR STALL WARNING PITCH TRIM ROLL TRIM GPS NAV GIA 1 COM 1 ESSENTIAL BUS 1 ADC 1 AHRS 1 PFD #1 STDBY ATTD #1 ESSENTIAL POWER BAT 2 A/C BUS 1 A/C COND ALT 1 MFD #1 MAIN BUS 3 12V DC OUTLET YAW SERVO GPS NAV GIA 2 COM 2 MAIN BUS 2 AHRS 2/ (ADC 2) PFD #2 FUEL PUMP AVIONICS FAN 2 ALT 2 A/C BUS 2 CABIN FAN A/C COMPR NAV LIGHTS STROBE LIGHTS NON-ESSENTIAL BUS PITOT HEAT FLAPS STARTER AVIONICS FAN 1 RECOG LIGHTS ALT 2 SWITCH CIRCUIT BREAKER PANEL SR22_FM07_2806B ESSENTIAL DIST BUS 30A 30A ALT 2 F B 80A 50A EVS CAMERA February 2013 ABNORMAL ELEC SYS SCHEMATIC C I R R U S P I L O T ’ S C H E C K L I S T M O D E L S R 2 2 Emergency Procedures Table of Contents P/N 13728-010 E - i Airspeeds for Emergency Operations ..............................................E-1 Maximum Glide............................................................................E-1 Memory Items..............................................................................E-1 Engine Failures ................................................................................E-2 Engine Failure On Takeoff (Low Altitude)....................................E-2 Engine Failure In Flight................................................................E-2 Airstart..............................................................................................E-3 Engine Airstart .............................................................................E-3 Smoke and Fire................................................................................E-4 Cabin Fire In Flight ......................................................................E-4 Engine Fire In Flight ....................................................................E-4 Wing Fire In Flight .......................................................................E-5 Engine Fire During Start ..............................................................E-5 Smoke and Fume Elimination......................................................E-5 Emergency Descent.........................................................................E-6 Emergency Descent ....................................................................E-6 Forced Landing ................................................................................E-6 Emergency Landing Without Engine Power ................................E-6 Ditching........................................................................................E-6 Landing Without Elevator Control................................................E-6 Engine System .................................................................................E-7 Engine Partial Power Loss ..........................................................E-7 Oil Pressure Out of Range ..........................................................E-7 Oil Temperature High ..................................................................E-7 High Cylinder Head Temperature................................................E-8 Fuel System Emergencies ...............................................................E-9 Low Fuel Quantity........................................................................E-9 Fuel Imbalance ............................................................................E-9 Perspective Crew Alerting System (CAS) Index CAS Message Page CAS Message Page OIL PRESS E-7 ESS BUS E-12 OIL TEMP E-7 CO LVL HIGH E-13 CHT E-8 ANTI ICE FLO E-15 FUEL QTY E-9 ANTI ICE CTL E-15 FUEL IMBALANCE E-9 ANTI ICE QTY E-15 RPM E-10 AOA OVERHEAT E-15 M BUS 1 E-11 BRAKE TEMP E-18 M BUS 2 E-11 START ENGAGE E-18 February 2013 NORMAL PERFORMANCE ABNORMAL EMERGENCY EMRGNCY C I R R U S P I L O T ’ S C H E C K L I S T M O D E L S R 2 2 Emergency Procedures Table of Contents E - ii P/N 13728-010 Propeller System Emergencies......................................................E-10 Engine Speed High....................................................................E-10 Propeller Governor Failure .......................................................E-10 Electrical System Emergencies......................................................E-11 High Voltage on Main Bus 1 ......................................................E-11 High Voltage on Main Bus 2 ......................................................E-11 High or Low Voltage on Essential Bus ......................................E-12 Environmental System Emergencies .............................................E-13 Carbon Monoxide Level High ....................................................E-13 Anti-Ice System ..............................................................................E-14 Anti-Ice System Failure / Excessive Ice Accumulation ..............E-14 Low Flow Rate Warning ............................................................E-15 Tank Control Failure Warning....................................................E-15 Low Fluid Quantity Warning ......................................................E-15 AOA Probe Overheat Warning ..................................................E-15 Integrated Avionics System Emergencies......................................E-16 Attitude & Heading Reference System (AHRS) Failure.............E-16 Air Data Computer (ADC) Failure ..............................................E-16 PFD Display Failure...................................................................E-16 Unusual Attitude Emergencies.......................................................E-17 Inadvertent Spin Entry ...............................................................E-17 Inadvertent Spiral Dive During IMC Flight .................................E-17 Other Emergencies ........................................................................E-17 Power Lever Linkage Failure.....................................................E-17 Emergency Engine Shutdown On Ground ................................E-17 Left/Right Brake Over-Temperature ..........................................E-18 Starter Engaged ........................................................................E-18 Emergency Ground Egress .......................................................E-18 CAPS Deployment .........................................................................E-19 Circuit Breaker Panel .....................................................................E-20 February 2013 NORMAL PERFORMANCE ABNORMAL EMERGENCY EMRGNCY P/N 13728-010 E - 1 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Airspeeds for Emergency Operations Maneuvering Speed: 3600 lb ................................................................................... 140 KIAS Best Glide: All Weights ............................................................................... 92 KIAS Emergency Landing (Engine-out): Flaps Up................................................................................... 90 KIAS Flaps 50% ................................................................................ 85 KIAS Flaps 100% .............................................................................. 80 KIAS Maximum Glide Best Glide Speed .................................................... 92 KIAS at 3600 lb Maximum Glide Ratio ~ 8.8 : 1 • Note • Maximum Glide Ratio with Ice Accumulation ~ 6.4: 1 Memory Items Checklist steps emphasized by underlining such as the example below, should be memorized for accomplishment without reference to the procedure. 1. Best Glide Speed........................................................ ESTABLISH 14000 12000 10000 8000 6000 2000 4000 0 6 8 10 12 14 16 18 4 2 20 0 GROUND DISTANCE - NAUTICAL MILES HEIGHT ABOVE GROUND - FEET SR22_FM03_3563 February 2013 EMERGENCY AIRSPEEDS E - 2 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Engine Failures Engine Failure On Takeoff (Low Altitude) 1. Best Glide or Landing Speed (as appropriate) ........... ESTABLISH 2. Mixture ..............................................................................CUTOFF 3. Fuel Selector ........................................................................... OFF 4. Ignition Switch ......................................................................... OFF 5. Flaps .......................................................................AS REQUIRED If time permits: 6. Power Lever ............................................................................ IDLE 7. Fuel Pump ............................................................................... OFF 8. Bat-Alt Master Switches .......................................................... OFF 9. Seat Belts ......................................................ENSURE SECURED Engine Failure In Flight 1. Best Glide Speed........................................................ ESTABLISH 2. Mixture ....................................................................AS REQUIRED 3. Fuel Selector ........................................................SWITCH TANKS 4. Fuel Pump ......................................................................... BOOST 5. Alternate Induction Air .............................................................. ON 6. Air Conditioner (if installed) .................................................... OFF 7. Ignition Switch ........................................................ CHECK, BOTH 8. Power Lever ...................................................................... ½ OPEN If engine does not start: 9. Perform Engine Airstart or Forced Landing checklist, as required. February 2013 EMERGENCY ENGINE FAILURE P/N 13728-010 E - 3 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Airstart Engine Airstart 1. Bat Master Switches .................................................................. ON 2. Power Lever ............................................................ OPEN ½ INCH 3. Mixture.................................................................RICH, AS REQ’D 4. Fuel Selector ........................................................SWITCH TANKS 5. Ignition Switch .......................................................................BOTH 6. Fuel Pump ..........................................................................BOOST 7. Alternate Induction Air .............................................................. ON 8. Alt Master Switches ................................................................. OFF 9. Starter (Propeller not Windmilling) .................................. ENGAGE 10. Power Lever ....................................................... slowly INCREASE 11. Alt Master Switches ................................................................... ON 12. If engine will not start, perform Forced Landing checklist. February 2013 EMERGENCY AIRSTART E - 4 P/N 13728-010 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Smoke and Fire Cabin Fire In Flight 1. Bat-Alt Master Switches ........................................OFF, AS REQ’D 2. Fire Extinguisher.............................................................ACTIVATE If airflow is not sufficient to clear smoke or fumes from cabin: 3. Cabin Doors.......................................................PARTIALLY OPEN 4. Avionics Power Switch ............................................................. OFF 5. All other switches..................................................................... OFF 6. Land as soon as possible. If setting master switches off eliminated source of fire or fumes and airplane is in night, weather, or IFR conditions: 7. Airflow Selector........................................................................ OFF 8. Bat-Alt Master Switches ............................................................ ON 9. Avionics Power Switch ............................................................... ON 10. Required Systems ....................................ACTIVATE one at a time 11. Temperature Selector ........................................................... COLD 12. Vent Selector ........................ FEET/PANEL/DEFROST POSITION 13. Airflow Selector...............................SET AIRFLOW TO MAXIMUM 14. Panel Eyeball Outlets ........................................................... OPEN 15. Land as soon as possible. Engine Fire In Flight 1. Mixture ..............................................................................CUTOFF 2. Fuel Pump ............................................................................... OFF 3. Fuel Selector ........................................................................... OFF 4. Airflow Selector........................................................................ OFF 5. Power Lever ........................................................................... IDLE 6. Ignition Switch ......................................................................... OFF 7. Cabin Doors.......................................................PARTIALLY OPEN 8. Land as soon as possible. February 2013 EMERGENCY SMOKE AND FIRE P/N 13728-010 E - 5 C I R R U S P I L O T C H E C K L I S T M O D E L S R 2 2 Wing Fire In Flight 1. Pitot Heat Switch ..................................................................... OFF 2. Navigation Light Switch ........................................................... OFF 3. Landing Light ........................................................................... OFF 4. Strobe Light Switch.................................................................. OFF 5. If possible, side slip to keep flames away from fuel tank and cabin. 6. Land as soon as possible. Engine Fire During Start 1. Mixture.............................................................................. CUTOFF 2. Fuel Pump ............................................................................... OFF 3. Fuel Selector ........................................................................... OFF 4. Power Lever .................................................................. FORWARD 5. Starter.................................................................................CRANK 6. If flames persist, perform Emergency Engine Shutdown on Ground and Emergency Ground Egress checklists. Smoke and Fume Elimination 1. Oxygen Masks or Cannulas ................................................... DON 2. Oxygen System ......................................................................... ON 3. Oxygen Flow Rate ......................................................... MAXIMUM 4. Air Conditioner (if installed) .................................................... OFF 5. Temperature Selector ........................................................... COLD 6. Vent Selector ........................ FEET/PANEL/DEFROST POSITION 7. Airflow Selector............................... SET