PILOT’S CHECKLIST SR20WITH CIRRUS PERSPECTIVE+ AVIONICS

g. Bat 1 Master Switch ............................................................ ON h. Avionics Cooling Fan................................................. AUDIBLE i. Avionics Master Switch ....................................................... ON j. Fuel Quantity................................................................CHECK k. Fuel Selector ................................... SELECT FULLEST TANK l. Flaps ................................................100% CHECK LIGHT ON m. Lights...................................................... CHECK OPERATION n. Stall Warning System Inlet ......................... UNOBSTRUCTED (Continued on following page) 3 1 5 6 7 8 9 10 11 12 13 4 2 SR22_FM04_1454 March 2017 NORMAL PREFLIGHT P/N 11935-006 N - 4 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 0 o. Stall Warning................................................................... TEST p. Pitot Heat ............................................................................ ON (1) Verify probe is hot. q. Pitot Heat .......................................................................... OFF r. Avionics Master Switch ..................................................... OFF s. Bat 1 and 2 Master Switches ............................................ OFF t. Alternate Static Source ............................................. NORMAL u. Circuit Breakers.....................................................................IN v. Fire Extinguisher ....................... CHARGED AND AVAILABLE w. Emergency Egress Hammer ..................................AVAILABLE x. CAPS Handle ................................................. PIN REMOVED 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. Elevator and Tab .................... CONDITION AND MOVEMENT d. Rudder ........................................FREEDOM OF MOVEMENT e. Rudder Trim Tab....................... CONDITION AND SECURITY f. 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 (Continued on following page) March 2017 NORMAL PREFLIGHT N - 5 P/N 11935-006 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 0 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. Wing Tip Light and Lens .......... CONDITION AND SECURITY c. Fuel Vent (underside)................................. UNOBSTRUCTED 7. Right Wing Forward and Main Gear a. Leading Edge and Stall Strips.............................. CONDITION b. Fuel Cap........................... CHECK QUANTITY AND SECURE c. Fuel Drains (2 underside)...................... DRAIN AND SAMPLE d. Landing Light........................................................ CONDITION e. Wheel Fairings ..... SECURITY, ACCUMULATION OF DEBRIS f. Tire ............................. CONDITION, INFLATION, AND WEAR g. Wheel and Brakes ................... FLUID LEAKS, EVIDENCE OF OVERHEATING, GENERAL CONDITION, AND SECURITY h. Chocks and Tiedown Ropes ..................................... REMOVE 8. Nose, Right Side a. Engine Oil................................. CHECK 6-7 QUARTS, LEAKS b. Engine Oil Dipstick/Filler CAP & Door....................... SECURE c. Cowling .......................................... ATTACHMENTS SECURE d. Exhaust Pipe ....CONDITION, SECURITY, AND CLEARANCE 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........... CONDITION (INDENTATIONS, NICKS, ETC.) f. Spinner................ CONDITION, SECURITY, AND OIL LEAKS g. Air Inlets ..................................................... UNOBSTRUCTED (Continued on following page) March 2017 NORMAL PREFLIGHT P/N 11935-006 N - 6 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 0 10. Nose, Left Side a. Cowling .......................................... ATTACHMENTS SECURE b. Gascolator (underside)... DRAIN FOR 3 SECONDS, SAMPLE c. External Power ...............................................DOOR SECURE 11. Left Main Gear and Forward Wing 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. Fuel Cap........................... CHECK QUANTITY AND SECURE g. Leading Edge and Stall Strips.............................. CONDITION 12. Left Wing Tip a. Fuel Vent (underside)..................................UNOBSTRUCTED b. Pitot Mast (underside) ...... COVER REMOVED, TUBE CLEAR c. Wing Tip Light and Lens .......... CONDITION AND SECURITY d. 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 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 AND SECURE March 2017 NORMAL PREFLIGHT / BEFORE STARTING N - 7 P/N 11935-006 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 0 Starting Engine 1. External Power (If applicable) ........................................CONNECT 2. Brakes .................................................................................. HOLD 3. Bat Master Switches ......................................ON (CHECK VOLTS) 4. Strobe Lights ............................................................................. ON 5. Power Lever ............................................................ OPEN ¼ INCH 6. Mixture..............................................................................CUTOFF 7. Propeller Area..................................................................... CLEAR 8. Fuel Pump ................................................................................. ON 9. Mixture............................................................ADVANCE TO RICH UNTIL STABLE FUEL FLOW IS INDICATED (3 - 5 SECONDS) 10. Mixture..............................................................................CUTOFF 11. Ignition Switch .......START (RELEASE AFTER ENGINE STARTS) 12. Mixture....................................... SMOOTHLY ADVANCE TO RICH (AFTER ENGINE STARTS) 13. Power Lever ................................RETARD (MAINTAIN 1000 RPM) 14. Fuel Pump ............................................................................... OFF 15. Oil Pressure........................................................................CHECK 16. Alt Master Switches ................................................................... ON 17. Avionics Power Switch ............................................................... ON 18. Engine Parameters ........................................................ MONITOR 19. External Power (If applicable) ..................................DISCONNECT 20. Amp Meter/Indication..........................................................CHECK 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 March 2017 NORMAL STARTING / TAXI P/N 11935-006 N - 8 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 0 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. Flaps.......................................................... SET 50% AND CHECK 8. Transponder............................................................................. SET 9. Autopilot..............................................................................CHECK 10. Navigation Radios/GPS ..................................SET FOR TAKEOFF 11. Cabin Heat/Defrost .................................................AS REQUIRED 12. Brakes................................................................................... HOLD 13. Mixture..........................................................................FULL RICH 14. Power Lever................................................................... 2200 RPM 15. Alternator ............................................................................CHECK a. Pitot Heat ............................................................................ ON b. Navigation Lights................................................................. ON c. Landing Light....................................................................... ON d. Annunciator Lights .......................................................CHECK 16. Voltage................................................................................CHECK 17. Pitot Heat................................................................AS REQUIRED 18. Navigation Lights ....................................................AS REQUIRED 19. Landing Light ..........................................................AS REQUIRED 20. Magnetos............................................. CHECK LEFT AND RIGHT a. Ignition Switch ............................ R, NOTE RPM, THEN BOTH b. Ignition Switch ............................. L, NOTE RPM, THEN BOTH 21. Engine Parameters .............................................................CHECK 22. Power Lever................................................................... 1000 RPM 23. Fuel Pump ................................................................................. ON 24. Flight Instruments, HSI, and Altimeter............... CHECK AND SET 25. Flight Controls ........................................... FREE AND CORRECT 26. Trim......................................................................... SET TAKEOFF 27. Autopilot...................................................................DISCONNECT March 2017 NORMAL BEFORE TAKEOFF N - 9 P/N 11935-006 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 0 Normal Takeoff 1. Brakes.........................RELEASE (STEER WITH RUDDER ONLY) 2. Power Lever ........................................................ FULL FORWARD 3. Engine Parameters .............................................................CHECK 4. Elevator Control ...................ROTATE SMOOTHLY AT 71-75 KIAS 5. At 85 KIAS, Flaps ...................................................................... UP Short Field Takeoff 1. Flaps........................................................................................ 50% 2. Brakes .................................................................................. HOLD 3. Power Lever ........................................................ FULL FORWARD 4. Engine Parameters .............................................................CHECK 5. Brakes.........................RELEASE (STEER WITH RUDDER ONLY) 6. Elevator Control ........................ ROTATE SMOOTHLY AT 71 KIAS 7. Airspeed at Obstacle ......................................................... 81 KIAS When clear of obstacle: 8. Flaps.......................................................................................... UP Climb 1. Climb Power............................................................................. SET 2. Flaps............................................................................ VERIFY UP 3. Mixture...............................LEAN AS REQUIRED FOR ALTITUDE 4. Engine Parameters .............................................................CHECK 5. Fuel Pump ..............................................................AS REQUIRED Cruise 1. Fuel Pump ............................................................................... OFF • Note • The Fuel Pump must be set to ON during maneuvering flight (i.e. flight training maneuvers, chandelles, stalls, etc.). 2. Cruise Power ........................................................................... SET 3. Mixture......................................................... LEAN AS REQUIRED 4. Engine Parameters ........................................................ MONITOR 5. Fuel Flow and Balance .................................................. MONITOR March 2017 NORMAL TAKEOFF / CLIMB CRUISE P/N 11935-006 N - 10 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 0 Cruise Leaning 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 Before Landing 1. Seat Belt and Shoulder Harness ..................................... SECURE 2. Fuel Pump ................................................................................. ON 3. Mixture..........................................................................FULL RICH 4. Flaps.......................................................................AS REQUIRED 5. Autopilot..................................................................AS REQUIRED Normal Landing 1. Flaps...................................................................................... 100% 2. Airspeed ....................................................................... 81-83 KIAS If Icing Conditions Exist: a. Airspeed on Short Final .............................................. 88 KIAS 3. Power Lever............................................................AS REQUIRED After touchdown: 4. Brakes.....................................................................AS REQUIRED Mixture Description Exhaust Gas Temperature Best Power 100 °F Rich Of Peak EGT Best Economy Peak EGT March 2017 NORMAL CRUISE / DESCENT LANDING N - 11 P/N 11935-006 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 0 Short Field Landing 1. Flaps...................................................................................... 100% 2. Airspeed ............................................................................ 78 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 ................................ BEST ANGLE OF CLIMB (81 KIAS) After clear of obstacles: 5. Flaps ......................................................................................... UP 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 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 March 2017 NORMAL LANDING / SHUTDOWN P/N 11935-006 P - i Performance Table of Contents 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 0 Takeoff Distance: 3150 LB...............................................................P-1 Takeoff Distance: 2600 LB...............................................................P-2 Cruise Performance .........................................................................P-3 Cruise Performance .........................................................................P-4 Landing Distance Table - Flaps 100% .............................................P-5 Landing Distance Table - Flaps 50% ...............................................P-6 Landing Distance Table - Flaps 0% .................................................P-7 Wind Components ...........................................................................P-8 Weight and Balance .........................................................................P-9 Loading Calculations ...................................................................P-9 Loading Data .............................................................................P-10 Moment Limits ..........................................................................P-10 Temperature Conversion ...............................................................P-11 • Note • Aircraft with optional Air Conditioning System: Brake Horsepower is reduced by approximately 6 BHP. March 2017 NORMAL PERFORMANCE ABNORMAL EMERGENCY PERFORMANCE P - 1 P/N 11935-006 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 0 Takeoff Distance: 3150 LB WEIGHT = 3150 LB Approx. Speed at Liftoff = 75 KIAS Speed over 50 Ft. Obstacle = 81 KIAS Flaps 50%; Full Throttle, Mixture Set; Dry, Level, Paved Runway Headwind: Subtract 10% for each 12 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Refer to list of factors. Dry Grass: Add 15% of ground roll to dis- tances. Air Conditioner: Add 100 feet to ground roll and 150 feet to distance over 50' obstacle if Air Conditioner is ON during takeoff. PRESS ALT FT DISTANCE FT TEMPERATURE ~ °C 0 10 20 30 40 50 ISA SL Grnd Roll 1503 1623 1748 1877 2011 2150 1685 50 ft 2273 2443 2618 2799 2986 3179 2530 1000 Grnd Roll 1653 1784 1921 2063 2210 2363 1825 50 ft 2491 2675 2867 3065 3270 3482 2732 2000 Grnd Roll 1818 1962 2113 2269 2431 2599 1978 50 ft 2730 2932 3142 3359 3584 3817 2953 3000 Grnd Roll 2002 2161 2326 2498 2676 2862 2145 50 ft 2995 3217 3447 3686 3932 4187 3195 4000 Grnd Roll 2206 2381 2563 2753 2950 3154 2329 50 ft 3288 3532 3785 4048 4319 4599 3460 5000 Grnd Roll 2433 2626 2827 3037 3254 3479 2530 50 ft 3614 3883 4161 4449 4747 5055 3749 6000 Grnd Roll 2687 2900 3122 3353 3592 3841 2752 50 ft 3976 4272 4578 4895 5224 5563 4066 7000 Grnd Roll 2969 3205 3450 3705 3970 4245 2995 50 ft 4379 4705 5042 5392 5754 6127 4414 8000 Grnd Roll 3322 3586 3861 4146 4442 4750 3300 50 ft 4883 5246 5622 6013 6416 6833 4851 9000 Grnd Roll 3752 4050 4360 4682 5017 5364 3669 50 ft 5495 5904 6328 6767 7221 7691 5380 10000 Grnd Roll 4240 4577 4927 5291 5670 6062 4082 50 ft 6188 6649 7127 7621 8133 8663 5970 March 2017 PERFORMANCE TAKEOFF 3150 LB P/N 11935-006 P - 2 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 0 Takeoff Distance: 2600 LB WEIGHT = 2600 LB Approx. Speed at Liftoff = 69 KIAS Speed over 50 Ft Obstacle = 75 KIAS Flaps 50%; Full Throttle, Mixture Set; Dry, Level, Paved Runway Headwind: Subtract 10% for each 12 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Refer to list of factors. Dry Grass: Add 15% of ground roll to dis- tances. Air Conditioner: Add 100 feet to ground roll and 150 feet to distance over 50' obstacle if Air Conditioner is ON during takeoff. PRESS ALT FT DISTANCE FT TEMPERATURE ~ °C 0 10 20 30 40 50 ISA SL Grnd Roll 913 986 1061 1140 1221 1305 1023 50 ft 1408 1513 1621 1732 1848 1967 1566 1000 Grnd Roll 1004 1083 1166 1252 1342 1435 1108 50 ft 1542 1656 1775 1897 2024 2154 1692 2000 Grnd Roll 1104 1192 1283 1378 1476 1578 1201 50 ft 1690 1815 1945 2079 2218 2361 1828 3000 Grnd Roll 1215 1312 1412 1517 1625 1738 1303 50 ft 1854 1991 2133 2281 2433 2590 1978 4000 Grnd Roll 1339 1446 1556 1671 1791 1915 1414 50 ft 2036 2186 2342 2504 2672 2844 2141 5000 Grnd Roll 1477 1595 1717 1844 1975 2112 1536 50 ft 2237 2403 2574 2752 2936 3126 2320 6000 Grnd Roll 1631 1761 1896 2036 2181 2332 1671 50 ft 2461 2643 2832 3028 3230 3440 2516 7000 Grnd Roll 1803 1946 2095 2250 2411 2577 1818 50 ft 2710 2911 3119 3335 3558 3788 2731 8000 Grnd Roll 2017 2178 2344 2518 2697 2884 2004 50 ft 3021 3245 3477 3718 3967 4224 3001 9000 Grnd Roll 2278 2459 2647 2843 3046 3257 2228 50 ft 3399 3651 3913 4184 4464 4754 3328 10000 Grnd Roll 2575 2779 2992 3213 3442 3681 2478 50 ft 3827 4112 4406 4711 5027 5353 3693 March 2017 PERFORMANCE TAKEOFF 2600 LB P - 3 P/N 11935-006 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 0 Cruise Performance *For power settings greater than 75% power, Best Power. • Note • Subtract 10 KTAS if nose wheel pant and fairing removed. Lower KTAS by 10% if nose and main wheel pants and 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: • Mixture ......................................................................................... Target Fuel Flow* • Weight ........................................................................................................ 2600 LB • Winds ............................................................................................................... Zero • Shaded Cells: Cruise Pwr above 85% not recommended. Press Alt ISA - 30°C ISA ISA + 30°C RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 2000 2700 27.1 94% 151 16.5 90% 156 15.8 85% 158 15.2 2500 27.1 86% 148 14.9 82% 151 14.2 78% 153 13.7 2500 26.0 81% 145 14.2 77% 148 13.6 73% 150 11.5 2500 24.9 77% 142 13.5 73% 144 12.3 69% 146 10.9 2500 23.8 72% 139 13.3 68% 140 11.6 65% 142 10.3 2500 22.7 67% 135 12.5 64% 136 10.9 61% 138 9.7 2500 21.6 62% 130 11.7 59% 132 10.3 56% 132 9.1 2500 20.5 58% 126 11.0 55% 127 9.6 52% 127 8.5 2500 19.4 53% 121 10.2 50% 121 9.0 48% 121 8.0 4000 2700 25.2 88% 152 15.6 84% 155 14.9 80% 157 14.4 2500 25.2 80% 147 14.1 76% 150 13.4 73% 152 11.2 2500 24.1 76% 144 13.4 72% 146 12.0 68% 148 10.6 2500 23.0 71% 140 13.0 67% 142 11.3 64% 144 10.0 2500 21.9 66% 136 12.2 63% 138 10.6 60% 139 9.4 2500 20.8 61% 132 11.4 58% 133 9.9 55% 134 8.8 2500 19.7 57% 127 10.6 54% 128 9.3 51% 128 8.2 2500 18.6 52% 121 9.9 49% 122 8.6 47% 122 7.7 2500 17.5 47% 115 9.1 45% 115 8.0 42% 115 7.1 March 2017 PERFORMANCE CRUISE P/N 11935-006 P - 4 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 0 Cruise Performance Press Alt ISA - 30°C ISA ISA + 30°C RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 6000 2700 23.4 82% 151 14.7 78% 154 14.1 74% 156 11.4 2500 23.4 75% 146 13.5 71% 148 11.7 68% 150 10.4 2500 22.3 70% 142 12.7 66% 144 11.0 63% 145 9.7 2500 21.2 65% 138 11.9 62% 140 10.3 59% 141 9.1 2500 20.1 60% 133 11.1 57% 135 9.7 55% 136 8.6 2500 19.0 56% 128 10.3 53% 129 9.0 50% 129 8.0 2500 17.9 51% 123 9.6 48% 123 8.4 46% 123 7.4 2500 16.8 46% 116 8.8 44% 116 7.7 42% 115 6.9 8000 2700 21.6 76% 150 13.9 72% 152 11.9 69% 154 10.5 2500 21.6 70% 144 12.5 66% 146 10.8 63% 148 9.5 2500 20.5 65% 140 11.6 61% 142 10.1 58% 143 8.9 2500 19.4 60% 135 10.9 57% 137 9.4 54% 137 8.4 2500 18.3 55% 130 10.1 52% 131 8.8 50% 131 7.8 2500 17.2 50% 124 9.3 48% 124 8.1 45% 124 7.2 2500 16.1 45% 117 8.6 43% 117 7.5 41% 116 6.7 10000 2700 20.0 71% 148 12.7 67% 150 11.0 64% 151 9.7 2500 20.0 65% 142 11.5 61% 144 10.0 58% 145 8.8 2500 18.9 60% 138 10.7 56% 139 9.3 54% 139 8.2 2500 17.8 55% 132 9.9 52% 133 8.6 49% 133 7.6 2500 16.7 50% 126 9.1 47% 126 8.0 45% 126 7.1 2500 15.6 45% 119 8.4 43% 118 7.3 41% 117 6.5 12000 2700 18.5 66% 146 11.7 62% 147 10.1 59% 148 8.9 2500 18.5 60% 140 10.6 57% 141 9.2 54% 142 8.1 2500 17.4 55% 135 9.8 52% 135 8.5 49% 135 7.5 2500 16.3 50% 128 9.0 47% 128 7.9 45% 128 6.9 2500 15.2 45% 121 8.3 43% 120 7.2 40% 119 6.4 14000 2700 17.1 61% 143 10.8 57% 144 9.3 54% 145 8.2 2500 17.1 55% 137 9.8 52% 138 8.5 50% 138 7.5 2500 16.0 50% 131 9.0 48% 131 7.8 45% 130 6.9 2500 14.9 45% 123 8.2 43% 123 7.1 41% 121 6.3 March 2017 PERFORMANCE CRUISE P - 5 P/N 11935-006 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 0 Landing Distance Table - Flaps 100% WEIGHT: 3150 LB Speed over 50 Ft Obstacle: 78 KIAS Flaps: 100% Power: Idle Runway: Dry, Level Paved Surface Headwind: Subtract 10% per each 13 knots headwind. Tailwind: Add 10% for each 2 knots tail- wind up to 10 knots. Runway Slope: Ref. Factors. 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 809 838 868 897 927 957 853 Total 2557 2609 2663 2717 2773 2829 2636 1000 Grnd Roll 838 869 900 931 961 992 878 Total 2610 2665 2722 2779 2838 2898 2682 2000 Grnd Roll 870 901 933 965 997 1029 905 Total 2666 2725 2785 2846 2907 2970 2731 3000 Grnd Roll 902 935 968 1001 1034 1067 932 Total 2726 2788 2852 2916 2981 3048 2782 4000 Grnd Roll 936 971 1005 1039 1073 1108 960 Total 2790 2856 2923 2991 3060 3130 2837 5000 Grnd Roll 972 1007 1043 1079 1114 1150 990 Total 2858 2928 2999 3070 3143 3217 2894 6000 Grnd Roll 1009 1046 1083 1120 1157 1194 1021 Total 2931 3004 3079 3155 3232 3310 2954 7000 Grnd Roll 1048 1086 1125 1163 1201 1240 1052 Total 3008 3086 3165 3245 3326 3409 3017 8000 Grnd Roll 1089 1128 1168 1208 1248 1288 1085 Total 3091 3173 3256 3341 3427 3513 3084 9000 Grnd Roll 1131 1173 1214 1255 1297 1338 1119 Total 3179 3265 3353 3443 3533 3625 3154 10000 Grnd Roll 1176 1219 1262 1305 1348 1391 1155 Total 3272 3364 3457 3551 3646 3743 3228 March 2017 PERFORMANCE LANDING DISTANCE P/N 11935-006 P - 6 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 0 Landing Distance Table - Flaps 50% WEIGHT: 3150 LB Speed over 50 Ft Obstacle: 82 KIAS Flaps: 50% Power: Idle Runway: Dry, Level Paved Surface Headwind: Subtract 10% per each 13 knots headwind. Tailwind: Add 10% for each 2 knots tail- wind up to 10 knots. Runway Slope: Ref. Factors. 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 1029 1066 1104 1141 1179 1217 1085 Total 2704 2768 2833 2899 2966 3033 2800 1000 Grnd Roll 1067 1106 1145 1184 1223 1262 1117 Total 2768 2836 2904 2974 3044 3115 2856 2000 Grnd Roll 1106 1147 1187 1228 1268 1309 1151 Total 2837 2908 2980 3053 3127 3202 2915 3000 Grnd Roll 1148 1190 1232 1274 1316 1358 1186 Total 2909 2984 3060 3137 3216 3295 2977 4000 Grnd Roll 1191 1234 1278 1322 1365 1409 1222 Total 2987 3066 3146 3227 3309 3392 3042 5000 Grnd Roll 1236 1281 1327 1372 1417 1462 1259 Total 3069 3152 3236 3322 3408 3496 3111 6000 Grnd Roll 1283 1330 1377 1424 1471 1518 1298 Total 3156 3243 3332 3422 3513 3605 3183 7000 Grnd Roll 1333 1382 1431 1479 1528 1577 1338 Total 3248 3340 3434 3529 3624 3721 3258 8000 Grnd Roll 1385 1435 1486 1537 1587 1638 1380 Total 3346 3443 3542 3642 3742 3844 3338 9000 Grnd Roll 1439 1492 1544 1597 1650 1702 1424 Total 3450 3553 3656 3761 3867 3974 3421 10000 Grnd Roll 1496 1550 1605 1660 1715 1769 1469 Total 3560 3668 3778 3888 4000 4112 3509 March 2017 PERFORMANCE LANDING DISTANCE P - 7 P/N 11935-006 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 0 Landing Distance Table - Flaps 0% WEIGHT: 3150 LB Speed over 50 Ft Obstacle: 87 KIAS Flaps: 0% Power: Idle Runway: Dry, Level Paved Surface Headwind: Subtract 10% per each 13 knots headwind. Tailwind: Add 10% for each 2 knots tail- wind up to 10 knots. Runway Slope: Ref. Factors. 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 1185 1228 1272 1315 1358 1402 1250 Total 2971 3037 3105 3174 3243 3314 3071 1000 Grnd Roll 1229 1274 1319 1364 1409 1454 1287 Total 3038 3108 3179 3252 3325 3399 3130 2000 Grnd Roll 1274 1321 1368 1414 1461 1508 1326 Total 3109 3183 3258 3335 3412 3490 3191 3000 Grnd Roll 1322 1371 1419 1467 1516 1564 1366 Total 3185 3263 3342 3422 3504 3586 3256 4000 Grnd Roll 1372 1422 1472 1523 1573 1623 1408 Total 3265 3348 3431 3515 3601 3688 3323 5000 Grnd Roll 1424 1476 1528 1581 1633 1685 1451 Total 3351 3437 3525 3614 3704 3795 3395 6000 Grnd Roll 1479 1533 1587 1641 1695 1749 1495 Total 3441 3533 3625 3719 3814 3910 3470 7000 Grnd Roll 1536 1592 1648 1704 1760 1817 1542 Total 3537 3634 3731 3830 3930 4031 3548 8000 Grnd Roll 1595 1654 1712 1770 1829 1887 1590 Total 3640 3741 3844 3948 4053 4159 3631 9000 Grnd Roll 1658 1718 1779 1840 1900 1961 1641 Total 3748 3855 3963 4073 4183 4295 3718 10000 Grnd Roll 1723 1786 1849 1912 1975 2038 1693 Total 3863 3976 4090 4205 4322 4439 3809 March 2017 PERFORMANCE LANDING DISTANCE P/N 11935-006 P - 8 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 0 Wind Components • Note • The maximum demonstrated crosswind is 20 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° Headwind Tailwind 0° ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH 20° 30° 40° 50° 60° 70° 80° 90° 100° 110° 120° 130° 140° 150° 160° 170° 180° VELOCITY ~ KNOTS WIND 40 40 30 20 10 WIND COMPONENTS ~ KNOTS CROSSWIND COMPONENT ~ KNOTS -20 -10 0 10 20 40 30 SR20_FM05_5335 10 20 30 50 March 2017 PERFORMANCE WIND COMPONENTS P - 9 P/N 11935-006 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 0 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 Condition Weight to determine the Takeoff Condition Weight and moment/1000. a. Verify Takeoff Weight does not exceed the 3150 pounds. b. Verify Moment/1000 falls between the interpolated minimum and maximum values listed on the adjacent Moment Limits Table. Description Weight Moment/1000 1. Basic Empty Weight Includes unusable fuel and full oil 2. Front Seats Occupants Pilot and Passenger (total) 3. Rear Seats Occupants 4. Baggage Area 130 lb maximum 5. Zero Fuel Condition Weight Sub total items 1 thru 4 6. Fuel Loading 56 Gallon @6.0 lb/gal. maximum 7. Ramp Condition Weight Sub total items 5 and 6 8. Fuel for start, taxi, and run-up Normally 9 lb at average moment of 922.8 - - 9. Takeoff Condition Weight Subtract Item 8 from item 7 March 2017 PERFORMANCE WEIGHT AND BALANCE P/N 11935-006 P - 10 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 0 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 153.8 Weight LB Fwd Pass FS 143.5 Aft Pass FS 180.0 Fuel FS 153.8 20 2.87 3.60 4.16 3.10 220 31.57 39.60 34.08 40 5.74 7.20 8.32 6.20 240 34.44 43.20 37.18 60 8.61 10.80 12.48 9.29 260 37.31 46.80 40.27 80 11.48 14.40 16.64 12.39 280 40.18 50.40 43.37 100 14.35 18.00 20.80 15.49 300 43.05 54.00 46.47 120 17.22 21.60 24.96 18.59 320 45.92 57.60 49.57 140 20.09 25.20 27.04* 21.69 336** 48.79 61.20 52.05 160 22.96 28.80 24.78 360 51.66 64.80 180 25.83 32.40 27.88 380 54.53 68.40 200 28.70 36.00 30.98 400 57.40 72.00 * 130 lb Maximum ** 56 U.S Gallons Usable Weight LB Moment/1000 Weight LB Moment/1000 Minimum Maximum Minimum Maximum 2200 304 326 2700 375 398 2250 311 333 2750 383 406 2300 318 341 2800 390 414 2350 326 348 2850 398 421 2400 333 354 2900 406 429 2450 340 362 2950 414 437 2500 347 369 3000 421 444 2550 354 375 3050 429 452 2600 362 383 3100 438 459 2650 369 390 3150 445 467 March 2017 PERFORMANCE WEIGHT AND BALANCE P - 11 P/N 11935-006 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 0 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 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 March 2017 PERFORMANCE TEMP CONVERSION P/N 11935-006 A - i Abnormal Procedures Table of Contents 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 0 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 Starter Engaged Annunciation.....................................................A-3 Fuel System .....................................................................................A-4 Low Fuel Quantity........................................................................A-4 Left OR Right Fuel Tank Quantity ...............................................A-4 Fuel Imbalance ............................................................................A-5 Electrical System .............................................................................A-5 Low Voltage on Main Bus 1.........................................................A-5 Low Voltage on Main Bus 2.........................................................A-5 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 AVIONICS OFF Caution..............................................................A-7 PFD Cooling Fan Failure .............................................................A-7 Perspective + Crew Alerting System (CAS) Index CAS Message Page CAS Message Page OIL PRESS A-3 ALT 2 A-6 START ENGAGE A-3 AVIONICS OFF A-7 FUEL QTY A-4 PFD 1 FAN FAIL A-7 L FUEL QTY A-4 MFD FAN FAIL A-7 R FUEL QTY A-4 PITOT HEAT FAIL A-8 FUEL IMBALANCE A-5 PITOT HEAT REQD A-8 M BUS 1 A-5 FLAPS A-9 M BUS 2 A-5 BRAKE TEMP A-10 BATT 1 A-5 PARK BRAKE A-10 ALT 1 A-6 March 2017 NORMAL PERFORMANCE ABNORMAL EMERGENCY ABNORMAL A - ii P/N 11935-006 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 0 Abnormal Procedures Table of Contents PFD FAN FAIL Advisory .............................................................A-7 MFD Cooling Fan Failure ............................................................A-7 MFD FAN FAIL Advisory ............................................................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 FAIL Caution ........................................................A-8 Pitot Heat Required Annunciation ...............................................A-8 PITOT HEAT REQD Caution ......................................................A-8 Flight Control System.......................................................................A-9 Electric Trim/Autopilot Failure......................................................A-9 Flap System Exceedance............................................................A-9 FLAPS Caution ...........................................................................A-9 Landing Gear System ....................................................................A-10 Brake Failure During Taxi..........................................................A-10 Left/Right Brake Over-Temperature ..........................................A-10 BRAKE TEMP Caution .............................................................A-10 Other Conditions ............................................................................A-10 Aborted Takeoff .........................................................................A-10 Parking Brake Engaged Annunciation.......................................A-10 PARK BRAKE Caution .............................................................A-10 Communications Failure............................................................A-10 March 2017 NORMAL PERFORMANCE ABNORMAL EMERGENCY ABNORMAL P/N 11935-006 A - 1 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 0 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 March 2017 ABNORMAL IN FLIGHT A - 2 P/N 11935-006 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 0 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. March 2017 ABNORMAL LANDING P/N 11935-006 A - 3 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 0 Engine System Low Idle Oil Pressure OIL PRESS Caution 1. If In-Flight..............................LAND AS SOON AS PRACTICABLE Starter Engaged Annunciation START ENGAGE Caution On-Ground 1. Ignition Switch ................. DISENGAGE PRIOR TO 10 SECONDS 2. Wait 30 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 START ENGAGE March 2017 ABNORMAL ENGINE A - 4 P/N 11935-006 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 0 Fuel System Low Fuel Quantity FUEL QTY Caution 1. Fuel Quantity Gages...........................................................CHECK If left & right fuel quantities indicate less than or equal to 8 gallons per side: a. Land as soon as practicable. If left & right fuel quantities indicate more than 8 gallons per side: 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. L FUEL QTY or R FUEL QTY Advisory 1. Indicated (L or R) Fuel Quantity Gage................................CHECK If fuel quantity indicates less than or equal to 8 gallons: a. If On-Ground .............................. REFUEL PRIOR TO FLIGHT b. If In-Flight ............................................CONTINUE, MONITOR If fuel quantity indicates more than 8 gallons: a. If On-Ground .......................... CORRECT PRIOR TO FLIGHT b. If In-Flight ............................................CONTINUE, MONITOR FUEL QTY L FUEL QTY R FUEL QTY March 2017 ABNORMAL FUEL P/N 11935-006 A - 5 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 0 Fuel Imbalance FUEL IMBALANCE Caution 1. Fuel Quantity Gages...........................................................CHECK 2. Fuel Pump ................................................................................. ON If Fuel Pump is already ON 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 7.5 gallons. Electrical System Low Voltage on Main Bus 1 M BUS 1 Caution 1. Perform Alt 1 Caution (Failure) Checklist. Low Voltage on Main Bus 2 M BUS 2 Caution 1. Perform Alt 1 Caution (Failure) and Alt 2 Caution (Failure) Checklists. Battery 1 Current Sensor BATT 1 Caution 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 practicable. FUEL IMBALANCE M BUS 1 M BUS 2 BATT 1 March 2017 ABNORMAL FUEL / ELECTRICAL A - 6 P/N 11935-006 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 0 Low Alternator 1 Output ALT 1 Caution (Failure) 1. ALT 1 Circuit Breaker......................................... CHECK AND 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) Convenience Power (aux items plugged into armrest jack) 5. Continue Flight, avoiding IMC or night flight as able (reduced power redundancy). Low Alternator 2 Output ALT 2 Caution (Failure) 1. ALT 2 Circuit Breaker......................................... CHECK AND 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 March 2017 ABNORMAL ELECTRICAL P/N 11935-006 A - 7 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 0 Integrated Avionics System Avionics Switch Off AVIONICS OFF Caution 1. AVIONICS Switch ........................................... ON, AS REQUIRED PFD Cooling Fan Failure PFD FAN FAIL Advisory 1. AVIONICS FAN 2 Circuit Breaker ....................................... CYCLE If annunciation does not extinguish: a. Hot cabin temps .............LAND AS SOON AS PRACTICABLE b. Cool cabin temperatures .....................CONTINUE, MONITOR MFD Cooling Fan Failure MFD FAN FAIL Advisory 1. AVIONICS FAN 1 Circuit Breaker ....................................... CYCLE If annunciation does not extinguish: a. High cabin temps ...........LAND AS SOON AS PRACTICABLE 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 1 FAN FAIL MFD FAN FAIL March 2017 ABNORMAL AVIONICS A - 8 P/N 11935-006 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 0 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 PITOT HEAT FAIL Caution 1. Pitot Heat Circuit Breaker ................................................... CYCLE 2. Pitot Heat............................................................. CYCLE OFF, ON If inadvertent icing encountered, perform Inadvertent Icing Encounter Checklist and: a. Airspeed ....................... EXPECT NO RELIABLE INDICATION b. Exit icing conditions using attitude, altitude, and power instruments. Pitot Heat Required Annunciation PITOT HEAT REQD Caution 1. Pitot Heat................................................................................... ON PITOT HEAT FAIL PITOT HEAT REQD March 2017 ABNORMAL PITOT STATIC P/N 11935-006 A - 9 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 0 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 • AP SERVOS 4. Power Lever............................................................AS REQUIRED 5. Control Yoke .................................MANUALLY HOLD PRESSURE 6. Land as soon as practicable. Flap System Exceedance FLAPS Caution 1. Airspeed .......................................................................... REDUCE or 1. Flaps.............................................................................. RETRACT FLAPS March 2017 ABNORMAL FLIGHT CONTROLS A - 10 P/N 11935-006 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 0 Landing Gear System Brake Failure During Taxi 1. Engine Power..........................................................AS REQUIRED • To stop airplane - REDUCE • If necessary for steering - INCREASE 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 BRAKE TEMP Caution 1. Stop aircraft and allow the brakes to cool. Other Conditions Aborted Takeoff 1. Power Lever ............................................................................ IDLE 2. Brakes.....................................................................AS REQUIRED Parking Brake Engaged Annunciation PARK BRAKE Caution 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. Handheld Microphone ...................................................CONNECT BRAKE TEMP PARK BRAKE March 2017 ABNORMAL LANDING GEAR / OTHER P/N 11935-006 E - i Emergency Procedures Table of Contents 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 0 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 Engine Fire In Flight ....................................................................E-4 Cabin Fire In Flight ......................................................................E-4 Wing Fire In Flight .......................................................................E-5 Engine Fire During Start ..............................................................E-5 Smoke and Fume Elimination......................................................E-5 Forced Landings ..............................................................................E-6 Emergency Landing Without Engine Power ................................E-6 Emergency Descent ....................................................................E-6 Ditching........................................................................................E-6 Landing Without Elevator Control................................................E-6 Engine System .................................................................................E-7 Oil Pressure Out of Range ..........................................................E-7 OIL PRESS Warning ...................................................................E-7 Oil Temperature High ..................................................................E-7 OIL TEMP Warning ....................................................................E-7 Engine Speed High......................................................................E-7 RPM Warning: Engine Speed High .............................................E-7 High Cylinder Head Temperature................................................E-8 CHT Caution and Warning .........................................................E-8 Engine Partial Power Loss ..........................................................E-8 Fuel System .....................................................................................E-9 Low Fuel Quantity........................................................................E-9 Perspective + Crew Alerting System (CAS) Index CAS Message Page CAS Message Page OIL PRESS E-7 FUEL IMBALANCE E-9 OIL TEMP E-7 M BUS 1 E-10 RPM E-7 M BUS 2 E-10 CHT E-8 ESS BUS E-11 FUEL QTY E-9 CO LVL HIGH E-12 March 2017 NORMAL PERFORMANCE ABNORMAL EMERGENCY EMERGENCY E - ii P/N 11935-006 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 0 Table of Contents Emergency Procedures FUEL QTY Warning ....................................................................E-9 Fuel Imbalance ............................................................................E-9 Electrical System............................................................................E-10 High Voltage on Main Bus 1 ......................................................E-10 M BUS 1 Warning .....................................................................E-10 High Voltage on Main Bus 2 ......................................................E-10 M BUS 2 Warning .....................................................................E-10 High or Low Voltage on Essential Bus ......................................E-11 ESS BUS Warning ....................................................................E-11 Integrated Avionics System............................................................E-11 Attitude & Heading Reference System (AHRS) Failure.............E-11 Air Data Computer (ADC) Failure..............................................E-11 PFD Display Failure...................................................................E-11 Unusual Attitude.............................................................................E-12 Inadvertent Spin Entry ...............................................................E-12 Inadvertent Spiral Dive During IMC Flight .................................E-12 Environmental System Emergencies .............................................E-12 Carbon Monoxide Level High ....................................................E-12 CO LVL HIGH Warning ............................................................E-12 CAPS Deployment .........................................................................E-13 Other Emergencies ........................................................................E-13 Power Lever Linkage Failure.....................................................E-13 Emergency Engine Shutdown On Ground ................................E-13 Circuit Breaker Panel .....................................................................E-14 March 2017 NORMAL PERFORMANCE ABNORMAL EMERGENCY EMERGENCY P/N 11935-006 E - 1 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 0 Airspeeds For Emergency Operations Maneuvering Speed: • 3150 lb.......................................................................... 133 KIAS • 2700 lb.......................................................................... 123 KIAS • 2300 lb.......................................................................... 114 KIAS Best Glide: • 3150 lb.......................................................................... 100 KIAS • 2600 lb............................................................................ 92 KIAS Emergency Landing (Engine-Out): • Flaps Up ......................................................................... 89 KIAS • Flaps 50% ...................................................................... 83 KIAS • Flaps 100% .................................................................... 78 KIAS Maximum Glide Glide Ratio ~ 9 : 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 SR20_FM09_2765 March 2017 EMERGENCY AIRSPEEDS E - 2 P/N 11935-006 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 0 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 ................................................................................. ON 5. Alternate Induction Air ............................................................... ON 6. Air Conditioner (if installed) ..................................................... OFF 7. Ignition Switch ........................................................ CHECK, BOTH If engine does not start: 8. Perform Engine Airstart or Emergency Landing Without Engine Power checklist, as required. March 2017 EMERGENCY ENGINE FAILURE P/N 11935-006 E - 3 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 0 Airstart Engine Airstart 1. Bat Master Switches.................................................................. ON 2. Power Lever..................................................................... ½” OPEN 3. Mixture.................................................................RICH, AS REQ’D 4. Fuel Selector ........................................................SWITCH TANKS 5. Ignition Switch .......................................................................BOTH 6. Fuel Pump ................................................................................. ON 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 Landings checklist. March 2017 EMERGENCY AIRSTART E - 4 P/N 11935-006 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 0 Smoke and Fire 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. 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. March 2017 EMERGENCY SMOKE AND FIRE P/N 11935-006 E - 5 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 0 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. Air Conditioner (if installed) ..................................................... OFF 2. Temperature Selector ........................................................... COLD 3. Vent Selector ........................ FEET/PANEL/DEFROST POSITION 4. Airflow Selector...............................SET AIRFLOW TO MAXIMUM If source of smoke and fume is firewall forward: a. Airflow Selector ................................................................. OFF 5. Panel Eyeball Outlets ........................................................... OPEN 6. Prepare to land as soon as possible. March 2017 EMERGENCY SMOKE AND FIRE E - 6 P/N 11935-006 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 0 Forced Landings Emergency Landing Without Engine Power 1. Best Glide Speed........................................................ ESTABLISH 2. Radio ....................................... TRANSMIT (121.5 MHZ) MAYDAY GIVING LOCATION AND INTENTIONS 3. Transponder............................................................SQUAWK 7700 4. If off airport, ELT ............................................................ACTIVATE 5. Power Lever ............................................................................ IDLE 6. Mixture.............................................................................. CUTOFF 7. Fuel Selector ........................................................................... OFF 8. Ignition Switch ......................................................................... OFF 9. Fuel Pump ............................................................................... OFF 10. Flaps (when landing is assured)............................................ 100% 11. Master Switches ...................................................................... OFF 12. Seat Belt(s)....................................................................SECURED Emergency Descent 1. Power Lever ............................................................................ IDLE 2. Mixture....................................................................AS REQUIRED 3. Airspeed ................................................................ V NE (201 KIAS) Ditching 1. Radio ....................................... TRANSMIT (121.5 MHZ) MAYDAY GIVING LOCATION AND INTENTIONS 2. Transponder............................................................SQUAWK 7700 3. CAPS ..............................................................................ACTIVATE 4. Airplane ........................................................................ EVACUATE 5. Flotation Devices ............ INFLATE WHEN CLEAR OF AIRPLANE Landing Without Elevator Control 1. Flaps................................................................................ SET 50% 2. Trim............................................................................ SET 80 KIAS 3. Power.................................... AS REQUIRED FOR GLIDE ANGLE March 2017 EMERGENCY FORCED LANDING P/N 11935-006 E - 7 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 0 Engine System Oil Pressure Out of Range OIL PRESS Warning 1. Oil Pressure Gage ..............................................................CHECK If pressure low/high: a. Power ......REDUCE TO MINIMUM FOR SUSTAINED FLIGHT b. Land as soon as possible. (1) Prepare for potential engine failure. Oil Temperature High OIL TEMP Warning 1. Power............................................................................... REDUCE 2. Airspeed ....................................................................... INCREASE 3. Mixture..........................................................................FULL RICH 4. Oil Temperature Gage ....................................................MONITOR If temperature remains high: 5. Land as soon as possible. Engine Speed High RPM Warning: Engine Speed High 1. Tachometer.........................................................................CHECK If engine speed normal: a. If On-Ground ...........................CORRECT PRIOR TO FLIGHT b. If In-Flight ............................................CONTINUE, MONITOR If engine speed high: a. Perform Propeller Governor Failure checklist. 2. Oil Pressure Gage ..............................................................CHECK OIL PRESS OIL TEMP RPM March 2017 EMERGENCY ENGINE E - 8 P/N 11935-006 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 0 High Cylinder Head Temperature CHT Caution and Warning On-Ground 1. Power Lever ..................................................................... REDUCE 2. Annunciations and Engine Temperatures ...................... MONITOR If Caution or Warning annunciation is still illuminated: 3. Power Lever ................................................ MINIMUM REQUIRED 4. Flight......................................................................... PROHIBITED In-Flight 1. Power Lever ..................................................................... REDUCE 2. Airspeed ...................................................................... INCREASE 3. Mixture .........................................................................FULL RICH 4. Annunciations and Engine Temperatures ...................... MONITOR If Caution or Warning annunciation is still illuminated: 5. Power Lever ............................................... MINIMUM REQUIRED 6. Engine Instruments ....................................................... MONITOR If Caution annunciation only remains illuminated: a. Land as soon as practicable. If Warning annunciation remains illuminated: a. Land as soon as possible. Engine Partial Power Loss 1. Air Conditioner (if installed) ..................................................... OFF 2. Fuel Pump ................................................................................. ON 3. Fuel Selector ........................................................SWITCH TANKS 4. Mixture........CHECK APPROPRIATE FOR FLIGHT CONDITIONS 5. Power Lever ....................................................................... SWEEP 6. Alternate Induction Air ............................................................... ON 7. Ignition Switch ................................................... BOTH, L, THEN R 8. Land as soon as practicable. CHT March 2017 EMERGENCY ENGINE P/N 11935-006 E - 9 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 0 Fuel System Low Fuel Quantity FUEL QTY Warning 1. Fuel Quantity Gages...........................................................CHECK If fuel quantity indicates less than or equal to 7 gallons: a. If On-Ground .............................. REFUEL PRIOR TO FLIGHT b. If In-Flight .......................LAND AS SOON AS PRACTICABLE If fuel quantity indicates more than 7 gallons: a. If On-Ground ...........................CORRECT PRIOR TO FLIGHT b. If In-Flight ............................................CONTINUE, MONITOR Fuel Imbalance FUEL IMBALANCE Warning 1. Fuel Quantity Gages...........................................................CHECK 2. Fuel Pump ................................................................................. ON If the Boost Pump is 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 9.5 gallons. FUEL QTY FUEL IMBALANCE March 2017 EMERGENCY FUEL E - 10 P/N 11935-006 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 0 Electrical System High Voltage on Main Bus 1 M BUS 1 Warning 1. ALT 1 Master Switch........................................................... CYCLE 2. M Bus 1 Voltage (M1) .........................................................CHECK If M Bus 1 Voltage is greater than 32 Volts: 3. ALT 1 Master Switch................................................................ OFF 4. Perform Alt 1 Caution (Failure) checklist (do not reset alternator). High Voltage on Main Bus 2 M BUS 2 Warning 1. Main Bus 1 Voltage (M1) ....................................................CHECK If M Bus 1 Voltage is greater than 32 Volts: 2. Perform M Bus 1 Warning Checklist. 3. Main Bus 2 Voltage (M2) ....................................................CHECK If M Bus 2 Voltage is greater than 32 Volts: 4. ALT 2 Master Switch........................................................... CYCLE 5. Main Bus 2 Voltage (M2) ....................................................CHECK If M Bus 2 Voltage remains greater than 32 Volts: 6. ALT 2 Master Switch................................................................ OFF 7. Perform Alt 2 Caution (Failure) checklist (do not reset alternator). M BUS 1 M BUS 2 March 2017 EMERGENCY ELECTRICAL P/N 11935-006 E - 11 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 0 High or Low Voltage on Essential Bus ESS BUS Warning 1. Essential Bus Voltage (ESS) ..............................................CHECK If Essential Bus Voltage is greater than 32 volts: 2. Main Bus 1 and Main Bus 2 Voltages (M1 and M2)............CHECK 3. Perform appropriate M Bus 1 or M Bus 2 Warning checklists. If Essential Bus Voltage is less than 24.5 volts: 4. Perform Alt 1 Caution (Failure) and Alt 2 Caution (Failure) checklists. If unable to restore at least one alternator: 5. Non-Essential Loads ....................................................... REDUCE a. If flight conditions permit, consider shedding: Air Conditioning, Landing Light, Pitot Heat, Cabin Fan, Nav Lights, Strobe Lights, Audio Panel, COM 2 6. Land as soon as practicable (Battery reserve only). Integrated Avionics System Attitude & Heading Reference System (AHRS) Failure 1. Verify Avionics System has switched to functioning AHRS If not, manually switch to functioning AHRS: 2. Failed ADAHRS Circuit Breaker .............................................. SET If open, reset breaker. If circuit breaker opens again, do not reset. 3. Be prepared to revert to Standby Instruments (Altitude, Heading) Air Data Computer (ADC) Failure 1. Failed ADAHRS Circuit Breaker .............................................. SET If open, reset (close) circuit breaker. If circuit breaker opens again, do not reset. 2. Revert to Standby Instruments (Altitude, Airspeed). 3. Land as soon as practicable. PFD Display Failure 1. Display Backup ...............................................................ACTIVATE 2. Land as soon as practicable. ESS BUS March 2017 EMERGENCY ELEC / AVIONICS E - 12 P/N 11935-006 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 0 Unusual Attitude Inadvertent Spin Entry 1. CAPS ..............................................................................ACTIVATE Inadvertent Spiral Dive During IMC Flight 1. Power Lever ............................................................................ IDLE 2. Stop the spiral dive by using coordinated aileron and rudder control while referring to the attitude indicator and turn coordinator to level the wings. 3. Cautiously apply elevator back pressure to bring airplane to level flight attitude. 4. Trim for level flight. 5. Set power as required. 6. Use autopilot if functional otherwise keep hands off control yoke, use rudder to hold constant heading. 7. Exit IMC conditions as soon as possible. Environmental System Emergencies Carbon Monoxide Level High CO LVL HIGH Warning 1. Air Conditioner (if installed) ......................NOT IN RECIRC MODE 2. Temperature Selector ........................................................... COLD 3. Vent Selector ........................ FEET/PANEL/DEFROST POSITION 4. Airflow Selector...............................SET AIRFLOW TO MAXIMUM 5. Panel Eyeball Outlets ........................................................... OPEN If CO LVL HIGH does not extinguish: 6. Supplemental Oxygen (if available) a. Oxygen Masks or Cannulas ............................................. DON b. Oxygen System................................................................... ON c. Oxygen Flow Rate................................................... MAXIMUM 7. Land as soon as possible. CO LVL HIGH March 2017 EMERGENCY SPINS / ECS P/N 11935-006 E - 13 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 0 CAPS Deployment • WARNING • The maximum demonstrated deployment speed is 133 KIAS. 1. Activation Handle Cover .................................................. REMOVE 2. Activation Handle (Both Hands) ............. PULL STRAIGHT DOWN After deployment, as time permits: 3. Mixture.............................................................................. CUTOFF 4. Fuel Selector ........................................................................... OFF 5. Fuel Pump ............................................................................... OFF 6. Bat-Alt Master Switches .......................................................... OFF Turn the Bat-Alt Master Switches off after completing any necessary radio communications. 7. Ignition Switch ......................................................................... OFF 8. ELT ............................................................................................ ON 9. Seat Belts and Harnesses ...............................................TIGHTEN 10. Loose Items ..................................................................... SECURE 11. Assume emergency landing body position. 12. After the airplane comes to a complete stop, evacuate quickly and move upwind. Other Emergencies Power Lever Linkage Failure 1. Power Lever Movement ..................................................... VERIFY 2. Power......................................................................... SET IF ABLE 3. Flaps.................................................................... SET IF NEEDED 4. Mixture....................... AS REQUIRED (FULL RICH TO CUT-OFF) 5. Land as soon as possible. Emergency Engine Shutdown On Ground 1. Power Lever............................................................................ IDLE 2. Fuel Pump (if used) ................................................................. OFF 3. Mixture.............................................................................. CUTOFF 4. Fuel Selector ........................................................................... OFF 5. Ignition Switch ......................................................................... OFF 6. Bat-Alt Master Switches .......................................................... OFF March 2017 EMERGENCY CAPS / OTHER E - 14 P/N 11935-006 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 0 Circuit Breaker Panel 12V & USB POWER A/C COND EVS CAMERA YAW SERVO ALT 1 CONV LIGHTS CABIN AIR CONTROL CABIN FAN STARTER AVIONICS FAN 1 NAV LIGHTS STROBE LIGHTS PITOT HEAT FLAPS AVIONICS FAN 2 GPS NAV GIA 2 COM 2 ADAHRS 2 FUEL PUMP PFD B MFD A LANDING LIGHTS A/C COMPR SR20_FM07_5370 BAT 2 GPS NAV GIA 1 COM 1 ADAHRS 1 STDBY ATTD A PFD A PITCH TRIM ROLL TRIM ENGINE INSTR ALT2 STALL WARNING ESSENTIAL POWER DME / ADF AUDIO PANEL DATA LINK/ WEATHER TRAFFIC AP SERVOS FUEL QTY MFD B STDBY ATTD B CABIN LIGHTS KEYPADS/ AP CTRL XPONDER ICE LIGHTS AVIONICS March 2017 EMERGENCY CRCT BREAKER PANEL