Quick Reference Checklist for SR20 Serials 2016 and Subsequent with Perspective Avionics

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. Oil Annunciator.....................................................................On o. Bat 1 and 2 Master Switches ............................................ OFF 3 1 5 6 7 8 9 10 11 12 13 4 2 SR22_FM04_1454 July 2011 NORMAL PREFLIGHT P/N 11935-005 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 0 p. Alternate Static Source ............................................. NORMAL q. Circuit Breakers.....................................................................IN r. Fire Extinguisher ................................. Charged and Available s. Emergency Egress Hammer ...................................... Available t. 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 5. Right Wing Trailing Edge a. Flap and Rub Strips (if installed) .......... Condition and Security b. Aileron and Tab .................................Condition and Movement c. Hinges, actuation arm, bolts, and cotter pins ................ Secure 6. Right Wing Tip a. Tip .......................................................................... Attachment b. Strobe, Nav Light and Lens.................. Condition and Security (Continued on following page) July 2011 NORMAL PREFLIGHT N - 5 P/N 11935-005 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 0 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. Wheel Fairings ......................Security, Accumulation of Debris e. Tire ............................................ Condition, Inflation, and Wear f. Wheel and Brakes ........Fluid Leaks, Evidence of Overheating, General Condition, and Security g. Chocks and Tiedown Ropes ....................................... Remove h. Cabin Air Vent .....................................................Unobstructed 8. Nose, Right Side a. Cowling .................................................... Attachments Secure b. Exhaust Pipe ..................... Condition, Security, and Clearance c. 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............................Condition (indentations, nicks, etc.) f. Spinner............................... Condition, Security, and Oil Leaks g. Air Inlets ..............................................................Unobstructed h. Alternator Belt .......................................Condition and Tension 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. Exhaust Pipe(s)................. Condition, Security, and Clearance 11. Left Main Gear and Forward Wing a. Wheel Fairings ......................Security, Accumulation of Debris b. Tire ............................................ Condition, Inflation, and Wear July 2011 NORMAL PREFLIGHT P/N 11935-005 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 0 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. Leading Edge and Stall Strips................................... Condition 12. Left Wing Tip a. Fuel Vent (underside).......................................... Unobstructed b. Pitot Mast (underside) ................. Cover Removed, Tube Clear c. Strobe, Nav 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. 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 & SECURE July 2011 NORMAL BEFORE STARTING N - 7 P/N 11935-005 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 0 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 .................................................... PRIME, then BOOST 8. Propeller Area..................................................................... CLEAR 9. Power Lever ........................................................... OPEN ¼ INCH 10. Ignition Switch .......................START (Release after engine starts) 11. Power Lever ............................... RETARD (to maintain 1000 RPM) 12. Oil Pressure........................................................................CHECK 13. Alt Master Switches ................................................................... ON 14. Avionics Power Switch ............................................................... ON 15. Engine Parameters ........................................................ MONITOR 16. External Power (If applicable) ..................................DISCONNECT 17. 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 July 2011 NORMAL START / TAXI P/N 11935-005 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 0 Before Takeoff 1. Doors .............................................................................. LATCHED 2. CAPS Handle ................................................. Verify Pin Removed 3. Seat Belts and Shoulder Harness ................................... SECURE 4. Air Conditioner...........................................................AS DESIRED 5. Fuel Quantity ..................................................................CONFIRM 6. Fuel Selector ........................................................ FULLEST TANK 7. Fuel Pump ................................................................................. ON 8. Flaps............................................................... SET 50% & CHECK 9. Transponder............................................................................. SET 10. Autopilot..............................................................................CHECK 11. Navigation Radios/GPS ..........................................SET for Takeoff 12. Cabin Heat/Defrost .................................................AS REQUIRED 13. Brakes................................................................................... HOLD 14. Power Lever ................................................................... 1700 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. RPM drop ≤150, difference between mags ≤75 RPM. 21. Engine Parameters .............................................................CHECK 22. Power Lever ................................................................... 1000 RPM 23. Flight Instruments, HSI, and Altimeter.................... CHECK & SET 24. Flight Controls .................................................FREE & CORRECT 25. Trim..............................................................................SET Takeoff 26. Autopilot...................................................................DISCONNECT July 2011 NORMAL BEFORE TAKEOFF N - 9 P/N 11935-005 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 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 65-70 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 65 KIAS 7. Airspeed at Obstacle ......................................................... 77 KIAS Climb 1. Climb Power............................................................................. SET 2. Flaps ................................................................................ Verify UP 3. Mixture ..........................................................................FULL RICH 4. Engine Parameters .............................................................CHECK 5. Fuel Pump ............................................................................... OFF July 2011 NORMAL TAKEOFF / CLIMB P/N 11935-005 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 0 Cruise 1. Fuel Pump ............................................................................... OFF 2. Cruise Power ........................................................................... SET 3. Mixture................................................................ LEAN as required 4. Engine Parameters .........................................................MONITOR 5. Fuel Flow and Balance ...................................................MONITOR 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 ..........................................................................BOOST 3. Mixture..........................................................................FULL RICH 4. Flaps.......................................................................AS REQUIRED 5. Autopilot..................................................................AS REQUIRED Balked Landing/Go-Around 1. Autopilot..................................................................... DISENGAGE 2. Power Lever ........................................................ FULL FORWARD 3. Flaps........................................................................................ 50% 4. Airspeed ........................ BEST ANGLE OF CLIMB (81 – 83 KIAS) After clear of obstacles: 5. Flaps ......................................................................................... UP Mixture Description Exhaust Gas Temperature Best Power 75° F Rich Of Peak EGT Best Economy 50° F Lean Of Peak EGT July 2011 NORMAL CRUISE / DESCENT N - 11 P/N 11935-005 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 0 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 - MAG GROUNDING CHECK 4. Mixture ..............................................................................CUTOFF 5. All Switches ............................................................................. OFF 6. Magnetos ................................................................................. OFF 7. ELT ...........................................................TRANSMIT LIGHT OUT 8. Chocks, Tie-downs, Pitot Covers ............................AS REQUIRED July 2011 NORMAL SHUTDOWN P/N 11935-005 N - 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: 2500 LB...............................................................P-1 Takeoff Distance: 3050 LB...............................................................P-2 Cruise Performance .........................................................................P-3 Cruise Performance .........................................................................P-4 Landing Distance .............................................................................P-5 Wind Components ...........................................................................P-6 Weight and Balance .........................................................................P-7 Loading Calculations ...................................................................P-7 Loading Data ...............................................................................P-8 Moment Limits .............................................................................P-8 Temperature Conversion .................................................................P-9 • Note • Aircraft with optional Air Conditioning System; Brake Horsepower is reduced by approximately 6 BHP. July 2011 NORMAL PERFORMANCE ABNORMAL EMERGENCY PERFORMANCE P - 1 P/N 11935-005 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 0 Takeoff Distance: 2500 LB WEIGHT = 2500 LB Speed at Liftoff = 68 KIAS Speed over 50 Ft Obstacle = 75 KIAS Flaps - 50% · Takeoff Pwr · Dry Paved Headwind: Subtract 10% for each 12 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Ref. Factors. Dry Grass: Add 20% to Ground Roll. Wet Grass: Add 30% to Ground Roll. Air Conditioner: Add 300 feet to ground roll and 400 feet to distance over 50' obstacle if A/C is ON during takeoff. PRESS ALT FT DISTANCE FT TEMPERATURE ~ °C 0 10 20 30 40 ISA SL Grnd Roll 787 850 915 983 1054 882 50 ft 1215 1306 1400 1497 1598 1353 1000 Grnd Roll 864 933 1005 1079 1157 954 50 ft 1329 1428 1531 1637 1748 1459 2000 Grnd Roll 949 1025 1104 1186 1271 1032 50 ft 1454 1563 1676 1792 1913 1574 3000 Grnd Roll 1043 1126 1213 1304 1398 1118 50 ft 1593 1712 1835 1963 2095 1700 4000 Grnd Roll 1147 1239 1335 1434 1537 1211 50 ft 1745 1876 2011 2151 2296 1836 5000 Grnd Roll 1263 1364 1469 1579 1693 1313 50 ft 1914 2057 2206 2359 2518 1985 6000 Grnd Roll 1392 1503 1619 1739 1865 1424 50 ft 2101 2258 2421 2589 2764 2147 7000 Grnd Roll 1534 1657 1785 1546 50 ft 2307 2479 2658 2324 8000 Grnd Roll 1692 1828 1969 1679 50 ft 2535 2725 2922 2516 9000 Grnd Roll 1868 2018 2174 1825 50 ft 2788 2997 3213 2727 10000 Grnd Roll 2064 2229 1984 50 ft 3068 3298 2956 July 2011 PERFORMANCE TAKEOFF 2500 LB P/N 11935-005 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 0 Takeoff Distance: 3050 LB WEIGHT = 3050 LB Speed at Liftoff = 71 KIAS Speed over 50 Ft. Obstacle = 77 KIAS Flaps - 50% · Takeoff Pwr · Dry Paved Headwind: Subtract 10% for each 12 knots headwind. Tailwind: Add 10% for each 2 knots tailwind up to 10 knots. Runway Slope: Ref. Factors. Dry Grass: Add 20% to Ground Roll. Wet Grass: Add 30% to Ground Roll. Air Conditioner: Add 300 feet to ground roll and 400 feet to distance over 50' obstacle if A/C is ON during takeoff. PRESS ALT FT DISTANCE FT TEMPERATURE ~ °C 0 10 20 30 40 ISA SL Grnd Roll 1319 1424 1534 1648 1767 1478 50 ft 1996 2145 2300 2460 2626 2221 1000 Grnd Roll 1448 1563 1684 1809 1940 1599 50 ft 2183 2346 2515 2691 2872 2396 2000 Grnd Roll 1590 1717 1850 1988 2131 1730 50 ft 2389 2568 2753 2945 3144 2586 3000 Grnd Roll 1748 1888 2034 2185 2343 1874 50 ft 2616 2812 3015 3226 3444 2792 4000 Grnd Roll 1923 2077 2237 2404 2577 2030 50 ft 2868 3082 3305 3536 3775 3017 5000 Grnd Roll 2117 2287 2463 2647 2837 2201 50 ft 3145 3381 3625 3879 4141 3262 6000 Grnd Roll 2333 2519 2714 2916 3126 2388 50 ft 3452 3711 3980 4258 4546 3529 7000 Grnd Roll 2572 2777 2992 2592 50 ft 3792 4076 4371 3820 8000 Grnd Roll 2837 3064 3300 2815 50 ft 4167 4480 4805 4137 9000 Grnd Roll 3132 3383 3644 3059 50 ft 4584 4928 5285 4483 10000 Grnd Roll 3460 3737 3326 50 ft 5045 5424 4860 July 2011 PERFORMANCE TAKEOFF 3050 LB P - 3 P/N 11935-005 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 0 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. Conditions: • Mixture ...................................................................................................Best Power • 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 27.8 101% 160 16.0 95% 160 15.0 91% 157 14.2 2500 27.8 90% 154 14.1 85% 154 13.4 81% 151 12.9 2500 26.6 85% 151 13.4 80% 151 12.8 76% 148 11.7 2500 25.4 80% 147 12.7 75% 147 11.6 72% 144 11.3 2500 24.1 74% 143 11.5 70% 143 11.1 67% 140 10.7 2500 22.9 69% 139 11.0 65% 139 10.6 62% 136 10.2 2500 22.0 65% 136 10.5 62% 136 10.2 59% 133 9.9 2500 19.7 55% 127 9.5 52% 127 9.20 50% 124 8.9 4000 2700 25.8 94% 159 14.8 89% 159 14.4 84% 157 13.4 2500 25.8 84% 153 13.3 79% 153 12.7 75% 150 11.7 2500 24.8 80% 150 12.7 75% 150 11.6 72% 147 11.2 2500 23.6 75% 146 11.5 70% 146 11.1 67% 143 10.8 2500 22.3 69% 141 10.9 65% 141 10.5 62% 138 10.2 2500 21.0 63% 136 10.3 60% 136 10.0 57% 133 9.7 2500 19.8 58% 131 9.8 55% 131 9.4 52% 129 9.2 6000 2700 24.0 88% 159 13.8 83% 159 13.1 79% 156 12.6 2500 24.0 79% 152 12.0 74% 152 11.5 71% 149 11.1 2500 23.0 74% 148 11.5 70% 148 11.1 67% 145 10.7 2500 21.8 69% 144 11.0 65% 144 10.6 62% 141 10.2 2500 20.8 65% 140 10.4 61% 140 10.0 58% 137 9.7 2500 19.4 59% 134 9.8 55% 134 9.5 53% 131 9.2 July 2011 PERFORMANCE CRUISE P/N 11935-005 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 0 Cruise Performance Press Alt ISA - 30°C ISA ISA + 30°C RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 8000 2700 22.2 82% 157 12.9 77% 157 11.6 73% 154 11.4 2500 22.2 73% 150 11.4 69% 150 11.0 65% 147 10.6 2500 21.2 69% 146 10.9 65% 146 10.5 62% 143 10.2 2500 20.1 64% 142 10.4 60% 142 10.0 57% 139 9.7 2500 18.9 59% 136 9.8 55% 136 9.5 52% 134 9.2 2500 17.7 53% 131 9.2 50% 131 8.9 48% 128 8.7 10000 2700 20.6 76% 155 11.7 72% 155 11.2 68% 152 10.9 2500 20.6 68% 148 10.8 64% 148 10.5 61% 145 10.1 2500 19.6 64% 144 10.4 60% 144 10.0 57% 141 9.7 2500 18.5 59% 139 9.8 55% 139 9.5 53% 136 9.2 2500 17.3 54% 134 9.3 50% 134 9.0 48% 131 8.7 12000 2700 19.0 70% 153 11.1 66% 153 10.7 63% 150 10.3 2500 19.0 63% 146 10.3 59% 146 9.9 56% 143 9.6 2500 18.0 59% 141 9.8 55% 141 9.5 52% 138 9.2 2500 16.8 53% 136 9.2 50% 136 8.9 47% 133 8.6 14000 2700 17.6 66% 151 10.5 62% 151 10.2 58% 148 9.8 2500 17.6 59% 144 9.8 55% 144 9.5 52% 141 9.2 2500 16.5 54% 142 9.3 50% 142 9.0 48% 139 8.7 July 2011 PERFORMANCE CRUISE P - 5 P/N 11935-005 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 0 Landing Distance WEIGHT = 3050 LB Speed over 50 Ft Obstacle = 78 KIAS Flaps - 100% · Idle · Dry, Level Paved Surface Headwind: Subtract 10% per each 13 knots headwind. Tailwind: Add 10% for each 2 knots tailwind 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 ISA SL Grnd Roll 809 838 868 897 927 853 Total 2557 2609 2663 2717 2773 2636 1000 Grnd Roll 838 869 900 931 961 878 Total 2610 2665 2722 2779 2838 2682 2000 Grnd Roll 870 901 933 965 997 905 Total 2666 2725 2785 2846 2907 2731 3000 Grnd Roll 902 935 968 1001 1034 932 Total 2726 2788 2852 2916 2981 2782 4000 Grnd Roll 936 971 1005 1039 1073 960 Total 2790 2856 2923 2991 3060 2837 5000 Grnd Roll 972 1007 1043 1079 1114 990 Total 2858 2928 2999 3070 3143 2894 6000 Grnd Roll 1009 1046 1083 1120 1157 1021 Total 2931 3004 3079 3155 3232 2954 7000 Grnd Roll 1048 1086 1125 1163 1201 1052 Total 3008 3086 3165 3245 3326 3017 8000 Grnd Roll 1089 1128 1168 1208 1248 1085 Total 3091 3173 3256 3341 3427 3084 9000 Grnd Roll 1131 1173 1214 1255 1297 1119 Total 3179 3265 3353 3443 3533 3154 10000 Grnd Roll 1176 1219 1262 1305 1348 1155 Total 3272 3364 3457 3551 3646 3228 July 2011 PERFORMANCE LANDING DISTANCE P/N 11935-005 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 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 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 July 2011 PERFORMANCE WIND COMPONENTS P - 7 P/N 11935-005 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 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 6 pounds at an average moment\1000 of 0.922. 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 3000 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 6. Fuel Load 56 Gallon @6.0 lb/gal. maximum 7. Ramp Weight Subtotal items 5 and 6 8. Fuel for start, taxi, and runup Normally 6 lb at avg. mmnt of 922.8 - - 9. Takeoff Weight Subtract Item 8 from item 7 July 2011 PERFORMANCE WEIGHT AND BALANCE P/N 11935-005 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 0 Loading Data Use this table to determine the Moment/1000. * 130 lb Maximum **56 U.S Gallons Usable 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 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 2700 375 398 2650 369 390 July 2011 PERFORMANCE WEIGHT AND BALANCE P - 9 P/N 11935-005 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 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 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 July 2011 PERFORMANCE TEMP CONVERSION P/N 11935-005 N - 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 Perspective Crew Alerting System (CAS) Index CAS Message Page OIL PRESS A-3 START ENGAGE A-3 FUEL QTY A-4 L FUEL QTY A-4 R FUEL QTY A-4 FUEL FILTER A-4 M BUS 1 A-5 M BUS 2 A-5 BATT 1 A-5 ALT 1 A-6 ALT 2 A-6 AVIONICS OFF A-7 PFD 1 FAN FAIL A-7 MFD FAN FAIL A-7 PITOT HEAT FAIL A-8 PITOT HT REQD A-8 FLAPS A-9 BRAKE TEMP A-10 PARK BRAKE A-10 July 2011 NORMAL PERFORMANCE ABNORMAL EMERGENCY ABNORMAL N - ii P/N 11935-005 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 Left OR Right Fuel Tank Quantity ...............................................A-4 Fuel Filter in Bypass Mode ..........................................................A-4 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 Flight Displays Too Dim...............................................................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-10 Brake Failure During Taxi..........................................................A-10 Left/Right Brake Over-Temperature ..........................................A-10 Other Conditions ............................................................................A-10 Aborted Takeoff .........................................................................A-10 Parking Brake Engaged Annunciation.......................................A-10 July 2011 NORMAL PERFORMANCE ABNORMAL EMERGENCY P/N 11935-005 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 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 July 2011 ABNORMAL IN FLIGHT A - 2 P/N 11935-005 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 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. July 2011 ABNORMAL LANDING P/N 11935-005 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 0 Engine System Low Idle Oil Pressure 1. If In-Flight.................................. LAND AS SOON AS PRACTICAL Starter Engaged Annunciation 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 START ENGAGE July 2011 ABNORMAL ENGINE A - 4 P/N 11935-005 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 0 Fuel System Low Fuel Quantity FUEL QTY Caution 1. Fuel Quantity Gages...........................................................CHECK If fuel quantity indicates less than or equal to 8 gallons: a. Land as soon as practical. If fuel quantity indicates more than 8 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 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 Filter in Bypass Mode 1. If In-Flight.................................. LAND AS SOON AS PRACTICAL 2. Replace fuel filter element prior to next flight. FUEL QTY L FUEL QTY R FUEL QTY FUEL FILTER July 2011 ABNORMAL FUEL P/N 11935-005 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 0 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 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 practical. M BUS 1 M BUS 2 BATT 1 July 2011 ABNORMAL ELECTRICAL A - 6 P/N 11935-005 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 0 Low Alternator 1 Output ALT 1 Caution (Failure) 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: Air Conditioning, Landing Light, Yaw Servo, Convenience Power. 5. Continue Flight, avoiding IMC or night flight as able. Low Alternator 2 Output ALT 2 Caution (Failure) 1. ALT 2 Circuit Breaker.............................................. CHECK & SET 2. ALT 2 Master Switch........................................................... CYCLE If alternator does not reset: 3. ALT 2 Master Switch................................................................ OFF 4. Continue Flight, avoiding IMC or night flight as able. ALT 1 ALT 2 July 2011 ABNORMAL ELECTRICAL P/N 11935-005 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 0 Integrated Avionics System Avionics Switch Off 1. AVIONICS Switch ........................................... ON, AS REQUIRED Flight Displays Too Dim 1. INSTRUMENT dimmer knob ................................................... OFF If Flight Displays are not controllable with INSTRUMENT dimmer knob: a. CABIN LIGHTS Circuit Breaker ...................................... PULL b. Revert to standby instruments with flashlight for illumination. 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 1 FAN FAIL MFD FAN FAIL July 2011 ABNORMAL AVIONICS A - 8 P/N 11935-005 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 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 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 HT REQD July 2011 ABNORMAL PITOT STATIC P/N 11935-005 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 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 • AUTOPILOT 4. Power Lever ............................................................AS REQUIRED 5. Control Yoke .................................MANUALLY HOLD PRESSURE 6. Land as soon as practical. Flap System Exceedance Flaps at 100%, airspeed greater than 109 KIAS for 5 seconds or more, OR Flaps at 50%, airspeed greater than 124 KIAS for 5 seconds or more. 1. Airspeed .......................................................................... REDUCE or 1. Flaps.............................................................................. RETRACT FLAPS ABNORMAL FLIGHT CONTROLS A - 10 P/N 11935-005 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 0 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: a. Ignition Switch ................................................................... OFF Left/Right Brake Over-Temperature 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 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 ..................................................................CHECK 4. Headset ........................................................................... CHANGE 5. Hand Held Microphone..................................................CONNECT BRAKE TEMP PARK BRAKE ABNORMAL LANDING GEAR P/N 11935-005 N - 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 Temperature High ..................................................................E-7 Engine Speed High......................................................................E-8 Perspective Crew Alerting System (CAS) Index CAS Message Page OIL PRESS E-7 OIL TEMP E-7 RPM E-8 CHT E-8 FUEL FLOW E-9 FUEL QTY E-9 M BUS 1 E-10 M BUS 2 E-10 ESS BUS E-11 CO LVL HIGH E-12 July 2011 NORMAL PERFORMANCE ABNORMAL EMERGENCY EMERGENCY N - ii P/N 11935-005 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 High Cylinder Head Temperature................................................E-8 Engine Partial Power Loss ..........................................................E-9 Fuel System .....................................................................................E-9 High Fuel Flow.............................................................................E-9 Low Fuel Quantity........................................................................E-9 Electrical System............................................................................E-10 High Voltage on Main Bus 1 ......................................................E-10 High Voltage on Main Bus 2 ......................................................E-10 High or Low Voltage on Essential Bus ......................................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 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 July 2011 NORMAL PERFORMANCE ABNORMAL EMERGENCY EMERGENCY P/N 11935-005 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 0 Airspeeds For Emergency Operations Maneuvering Speed: • 3050 lb.......................................................................... 130 KIAS • 2600 lb.......................................................................... 120 KIAS • 2200 lb.......................................................................... 110 KIAS Best Glide: • 3050 lb............................................................................ 99 KIAS • 2500 lb............................................................................ 95 KIAS Emergency Landing (Engine-Out): • Flaps Up ......................................................................... 87 KIAS • Flaps 50% ...................................................................... 82 KIAS • Flaps 100% .................................................................... 76 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 July 2011 EMERGENCY AIRSPEEDS E - 2 P/N 11935-005 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 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 ..........................................................................BOOST 5. Alternate Induction Air ............................................................... ON 6. Air Conditioner (if installed) ..................................................... OFF 7. Ignition Switch ........................................................ CHECK, BOTH 8. If no start, perform Engine Airstart or Forced Landing checklist. July 2011 EMERGENCY ENGINE FAILURE