SR22 Checklist

PILOT’S CHECKLIST
SR22
WITH 3600 POUND TAKEOFF WEIGHT AND FLIGHT INTO KNOWN ICE SYSTEM
Quick Reference Checklist
for
SR22 Aircraft Serials 3915 and Subsequent with 3600 Pound Takeoff
Weight and Flight Into Known Ice System
The procedures in this publication are abbreviated and derived from procedures in the
FAA Approved Airplane Flight Manual and Pilot’s Operating Handbook (POH) P/N
13772-004 Original Issue. These procedures do not supersede the procedures in the
basic POH. In the event of conflict, the basic POH shall take precedence.
COPYRIGHT © 2013 CIRRUS DESIGN CORPORATION DULUTH, MINNESOTA, USA

ISSUED: February 2013
P/N 13728-010
NORMAL PERFORMANCE ABNORMAL EMERGENCY
NORMAL
CIRRUS P ILOT’S CHEC KL IS T MODEL SR22
Normal Procedures
Table of Contents
Primary Flight Display ......................................................................N-1
Airspeeds for Normal Operation ......................................................N-2
Preflight Inspection ..........................................................................N-3
Before Starting Engine .....................................................................N-9
Starting Engine ................................................................................N-9
Cold Weather Operation: Starting ..................................................N-10
Before Taxiing ................................................................................N-10
Taxiing ...........................................................................................N-10
Before Takeoff ...............................................................................N-11
Normal Takeoff ..............................................................................N-13
Short Field Takeoff.........................................................................N-13
Climb ..............................................................................................N-13
Icing Conditions: In Flight...............................................................N-14
If Icing Conditions Exist: ............................................................N-14
Inadvertent Icing Encounter:......................................................N-14
Icing Conditions: In Flight...............................................................N-15
While in Icing Conditions: ..........................................................N-15
After Leaving Icing Conditions:..................................................N-15
Cruise.............................................................................................N-15
Descent ..........................................................................................N-16
If Icing Conditions Exist: ............................................................N-16
Before Landing...............................................................................N-17
Normal Landing..............................................................................N-17
Short Field Landing ........................................................................N-17
Balked Landing/Go-Around............................................................N-17
After Landing..................................................................................N-18
Shutdown .......................................................................................N-18
Oxygen Duration (Precise Flight System) ......................................N-19
P/N 13728-010 N-i

February 2013
NORMAL
LEGEND
CIRRUS P ILOT CHEC KL IS T MODEL SR22
PFD
Primary Flight Display
1 2 3 4 5 6 7 8 9 10 11
25 125° 12
24 13
12 13
23 E 14
LEGEND
S
1. True Airspeed
6
2. Airspeed Indicator 22 GPS TERM 15

21
3. Horizontal Situation Indicator (HSI)

4. Attitude Indicator
3
5. Slip/Skid Indicator 21 16
XTK 1.01NM
24
6. Vertical Deviation Indicator (VDI)

N
7. Selected Altitude Bug 20 17

8. Current Altitude
W
9. Altimeter 33 30
10. Selected Altitude 19 18
11. Vertical Speed Indicator (VSI)
12. Current Heading
13. Lubber Line HSI DETAIL
14. Selected Heading Bug
15. Flight Phase
16. Navigation Source 21. To/From Indicator
17. Aircraft Symbol 22. Course Deviation Indicator
18. Course Deviation Scale 23. Current Track Indicator
19. Rotating Compass Rose 24. Turn Rate/Heading Trend Vector SR22_FM07_2790
20. Course Pointer 25. Turn Rate Indicator
N-1 P/N 13728-010

February 2013
NORMAL
Airspeeds for Normal Operation
AIRSPEEDS
Takeoff Rotation:
• Normal, Flaps 50%......................................................... 73 KIAS
• Obstacle Clearance, Flaps 50% ..................................... 84 KIAS
Enroute Climb, Flaps Up:
• Normal .................................................................. 110-120 KIAS
• Best Rate of Climb, SL ................................................. 108 KIAS
• Best Rate of Climb, 10,000............................................. 99 KIAS
• Best Angle of Climb, SL.................................................. 88 KIAS
• Best Angle of Climb, 10,000 ........................................... 88 KIAS
Landing Approach:
• Normal Approach, Flaps Up ...................................... 90-95 KIAS
• Normal Approach, Flaps 50% ................................... 85-90 KIAS
• Normal Approach, Flaps 100% ................................. 80-85 KIAS
• Short Field, Flaps 100% (VREF) ..................................... 79 KIAS
Go-Around, Flaps 50%:
• Full Power....................................................................... 80 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3600 lb.......................................................................... 140 KIAS
• 2900 lb.......................................................................... 123 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing ......................................................... 21 Knots
Anti-Ice System:
• Minimum Airspeed For FIKI Conditions.........................95 KIAS*
*Includes all phases of flight, including approach, except as
required for takeoff and landing.
• Max Airspeed Anti-Ice System Ops...... 177 KIAS and 204 KTAS
• Recommended Holding Airspeed................................. 120 KIAS
P/N 13728-010 N-2

February 2013
NORMAL

PREFLIGHT
3
5 4
7 2
1
8
13
9 10
11
12
SR22_FM04_1454
Preflight Inspection
1. Cabin
a. Required Documents ................................................ On Board
b. Avionics Power Switch ...................................................... OFF
c. Bat 2 Master Switch ........................................................... ON
d. PFD ............................................................................Verify On
e. Essential Bus Voltage ............................................ 23-25 Volts
f. Flap Position Light ............................................................OUT
g. Battery 1 Master Switch ...................................................... ON
h. Avionics Cooling Fan.................................................... Audible
i. Lights............................................................. Check Operation
j. Stall Warning .....................................................................Test
k. Fuel Quantity ................................................................. Check
l. Fuel Selector .............................................. Select Fullest Tank
m. Flaps ....................................................100%, Check Light ON
n. Bat 1 and 2 Master Switch ................................................ OFF
(Continued on following page)
N-3 P/N 13728-010
February 2013
NORMAL
o. Alternate Static Source ............................................. NORMAL

p. Circuit Breakers.....................................................................IN
q. Avionics Master Switch ....................................................... ON
r. Cabin Speaker .................................................................... ON
s. Cabin Doors .................................................................... Close
PREFLIGHT
t. WIND SHLD Push-Button ............................................... Press
(1) Verify evidence of deicing fluid from spray nozzles.
u. PUMP BKUP Switch ........................................................... ON
(1) Metering Pump Duty Cycle........... Verify Continuously ON
(2) Deicing Fluid and Endurance Indications ................ Check
v. PUMP BKUP Switch ......................................................... OFF
w. ICE PROTECT System Switch............................................ ON
x. ICE PROTECT Mode Switch......................................... NORM
(1) Metering Pump Duty Cycle.......... Verify 30s ON, 90s OFF
y. ICE PROTECT Mode Switch........................................... HIGH
(1) Metering Pump Duty Cycle........... Verify Continuously ON
z. ICE Inspection Lights Switch............................................... ON
(1) Verify LH and RH Operation.
aa. PITOT HEAT Switch ....................... ON 45 seconds, then OFF
ab. Fire Extinguisher ................................. Charged and Available
ac. Emergency Egress Hammer ...................................... Available
ad. CAPS Handle ..................................................... Pin Removed
P/N 13728-010 N-4

February 2013
NORMAL
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
PREFLIGHT
e. COM 2 Antenna (underside) ........... Condition and Attachment

f. Baggage Door ............................................Closed and Secure
g. Static Button.............................................. Check for Blockage
h. Parachute Cover ........................................Sealed and Secure
3. Empennage
a. Tiedown Rope ............................................................. Remove
b. Horizontal and Vertical Stabilizers............................. Condition
c. Stabilizers Porous Panels.......................... Condition / Security
(1) Verify Evidence of Deicing Fluid Along Length of Panels
and Elevator Horns.
d. Elevator and Tab .............................. Condition and Movement
e. Rudder ................................................. Freedom of Movement
f. Rudder Trim Tab................................... Condition and Security
g. Attachment hinges, bolts and cotter pins ...................... Secure
4. Right Fuselage
a. Static Button.............................................. Check for Blockage
b. Wing/Fuselage Fairings.................................................. Check
c. Door Lock ...................................................................... Unlock
5. Right Wing Trailing Edge
a. Flap and Rub Strips (if installed) .......... Condition and Security
b. Aileron and Tab ................................ Condition and Movement
c. Aileron Gap Seal ......................................................... Security
d. Hinges, actuation arm, bolts, and cotter pins ................ Secure
6. Right Wing Tip
a. Tip .......................................................................... Attachment
b. Strobe, Nav Light and Lens.................. Condition and Security
c. Fuel Vent (underside) ..........................................Unobstructed
N-5 P/N 13728-010

February 2013
NORMAL
7. Right Wing Forward and Main Gear

a. Leading Edge and Stall Strips................................... Condition
b. Fuel Cap....................................... Check Quantity and Secure
c. Fluid Tank.............................................Verify Desired Quantity
(1) Filler Cap ....................................... Condition and Security
(2) Fluid Vent (underside)................................... Unobstructed
d. Porous Panels ...................................... Condition and Security
(1) Check Evidence of Deicing Fluid Along Length of Panels.
PREFLIGHT
e. Lift Transducer Faceplate ................................. Perceptibly Hot
f. Lift Transducer Vane ...................................................Very Hot
(1) Verify Stall Warning System audio annunciation within 4
seconds after lifting stall vane with wooden tooth pick or
tongue depressor.
g. Fuel Drains (2 underside).............................Drain and Sample
h. Wheel Fairings ......................Security, Accumulation of Debris
i. Tire ............................................ Condition, Inflation, and Wear
j. Wheel and Brakes ........Fluid Leaks, Evidence of Overheating,
General Condition, and Security.
k. Chocks and Tiedown Ropes ....................................... Remove
l. Cabin Air Vent ..................................................... Unobstructed
8. Nose, Right Side
a. Vortex Generator ....................................................... Condition
b. Ice-Inspection Light ................................... Condition / Security
c. Cowling .................................................... Attachments Secure
d. Exhaust Pipe ..................... Condition, Security, and Clearance
e. Gascolator (underside)................ Drain for 3 seconds, Sample
9. Nose Gear, Propeller, and Spinner
a. Tow Bar ....................................................... Remove and Stow
b. Strut .......................................................................... Condition
c. Wheel Fairing ........................Security, Accumulation of Debris
d. Wheel and Tire.......................... Condition, Inflation, and Wear
e. Propeller........................... Check adequate Ground Clearance
P/N 13728-010 N-6

February 2013
NORMAL
f. Spinner............................... Condition, Security, and Oil Leaks

g. Slinger Ring..................................... Evidence Of Deicing Fluid
h. Air Inlets ..............................................................Unobstructed
i. Alternator .................................................................. Condition
10. Nose, Left Side
a. Landing Light............................................................. Condition
b. Engine Oil......... Check 6-8 quarts, Leaks, Cap & Door Secure
c. Cowling .................................................... Attachments Secure
PREFLIGHT
d. External Power ..................................................... Door Secure

e. Vortex Generator ....................................................... Condition
f. Ice-Inspection Light ................................... Condition / Security
g. Windshield Spray Nozzles......................... Condition / Security
h. Exhaust Pipe(s)................. Condition, Security, and Clearance
11. Left Wing Forward and Main Gear
a. Wheel fairings .......................Security, Accumulation of Debris
b. Tire ............................................ Condition, Inflation, and Wear
c. Wheel and Brakes ........Fluid Leaks, Evidence of Overheating,
General Condition, and Security.
d. Chocks and Tiedown Ropes ....................................... Remove
e. Fuel Drains (2 underside).............................Drain and Sample
f. Cabin Air Vent ..................................................... Unobstructed
g. Fuel Cap....................................... Check Quantity and Secure
h. Fluid Tank.............................................Verify Desired Quantity
(1) Filler Cap ....................................... Condition and Security
(2) Fluid Vent (underside)................................... Unobstructed
i. Leading Edge and Stall Strips................................... Condition
j. Porous Panels ........................................... Condition / Security
(1) Check Evidence of Deicing Fluid Along Length of Panels.
12. Left Wing Tip
a. Fuel Vent (underside) ..........................................Unobstructed
b. Pitot Mast (underside) ................. Cover Removed, Tube Clear
c. Pitot Probe (underside) .......................................Unobstructed
N-7 P/N 13728-010

February 2013
NORMAL
d. Pitot Probe ..................................................................Very Hot

e. Strobe, Nav Light and Lens.................. Condition and Security
f. Tip ......................................................................... Attachment
13. Left Wing Trailing Edge
a. Flap And Rub Strips (If installed) ......... Condition and Security
b. Aileron .................................................. Freedom of movement
c. Aileron Gap Seal ......................................................... Security
d. Hinges, actuation arm, bolts, and cotter pins ................ Secure
14. Cabin
a. Fluid Quantity .................................... Verify 5 Gallon Minimum
b. ICE PROTECT System Switch.......................................... OFF
PREFLIGHT
c. Flaps ................................................................................... 0%
d. Battery 1 Master Switch .................................................... OFF
e. Avionics Master Switch ..................................................... OFF
f. Cabin Speaker .................................................................. OFF
P/N 13728-010 N-8

February 2013
NORMAL
Before Starting Engine

1. Preflight Inspection ................................................... COMPLETED
2. Weight and Balance............................................ Verify within limits
3. Emergency Equipment ................................................ ON BOARD
4. Passengers......................................................................BRIEFED
5. Seats, Seat Belts, and Harnesses ................ ADJUST & SECURE
Starting Engine
1. External Power (If applicable) ........................................CONNECT
2. Brakes .................................................................................. HOLD
3. Bat Master Switches ............................................ON (Check Volts)
STARTING
ENGINE
4. Strobe Lights ............................................................................. ON

5. Mixture ..........................................................................FULL RICH
6. Power Lever ........................................................ FULL FORWARD
7. Fuel Pump ..........................................................................BOOST
8. Propeller Area..................................................................... CLEAR
9. Power Lever ........................................................... OPEN ¼ INCH
10. Ignition Switch .......................START (Release after engine starts)
11. Mixture ................................................................................... LEAN
until RPM rises to a maximum value. Leave the mixture in this
position during taxi and until run-up.
12. Power Lever .............................. RETARD (to maintain 1000 RPM)
13. Oil Pressure ........................................................................CHECK
14. Alt Master Switches ................................................................... ON
15. Avionics Power Switch ............................................................... ON
16. Engine Parameters ........................................................ MONITOR
17. External Power (If applicable) ..................................DISCONNECT
18. Amp Meter/Indication..........................................................CHECK
N-9 P/N 13728-010

February 2013
NORMAL
Cold Weather Operation: Starting

1. Ignition Switch ......................................................................... OFF
2. Propeller ...........................................Hand TURN several rotations
3. External Power (If applicable) ........................................CONNECT
4. Brakes .................................................................................. HOLD
5. Bat Master Switches .........................................ON (check voltage)
6. Mixture..........................................................................FULL RICH
7. Power lever ......................................................... FULL FORWARD
8. Fuel Pump .............................HIGH BOOST/PRIME, then BOOST
9. Propeller Area..................................................................... CLEAR
10. Power Lever ............................................................ OPEN ¼ INCH
11. Ignition Switch .......................START (Release after engine starts)
12. Power Lever ............................... RETARD (to maintain 1000 RPM)
13. Oil Pressure........................................................................CHECK
STARTING/
TAXI
15. Avionics Power Switch............................................................... ON
16. Engine Parameters .........................................................MONITOR
17. External Power (If applicable) ..................................DISCONNECT
18. Amp Meter/Indication..........................................................CHECK
19. Strobe Lights ............................................................................. ON
Before Taxiing
1. Flaps..................................................................................UP (0%)
2. Radios/Avionics ......................................................AS REQUIRED
3. Cabin Heat/Defrost ................................................ AS REQUIRED
4. Fuel Selector .......................................................... SWITCH TANK
Taxiing
1. Parking Brake ............................................................ DISENGAGE
2. Brakes.................................................................................CHECK
3. HSI Orientation ...................................................................CHECK
4. Attitude Gyro.......................................................................CHECK
5. Turn Coordinator ................................................................CHECK
P/N 13728-010 N - 10
February 2013
NORMAL
Before Takeoff
1. Doors .............................................................................. LATCHED
2. CAPS Handle ................................................. Verify Pin Removed
3. Seat Belts and Shoulder Harness ................................... SECURE
4. Air Conditioner ...........................................................AS DESIRED
• Caution •
Use of RECIRC mode prohibited in flight.
5. Fuel Quantity ..................................................................CONFIRM
6. Fuel Selector ........................................................ FULLEST TANK
7. Fuel Pump ..........................................................................BOOST
8. Mixture ....................................................................AS REQUIRED
9. Flaps ............................................................... SET 50% & CHECK
10. Transponder............................................................................. SET
11. Autopilot..............................................................................CHECK
TAKEOFF
BEFORE
12. Navigation Radios/GPS ..........................................SET for Takeoff

13. Cabin Heat/Defrost .................................................AS REQUIRED
14. Brakes................................................................................... HOLD
15. Power Lever ................................................................... 1700 RPM
16. Alternator ............................................................................CHECK
a. Pitot Heat ............................................................................ ON
b. Navigation Lights................................................................. ON
c. Landing Light....................................................................... ON
d. Annunciator Lights .......................................................CHECK
Verify both ALT 1 and ALT 2 caution lights out and positive
amps indication for each alternator.
17. Voltage................................................................................CHECK
18. Pitot Heat ................................................................AS REQUIRED
19. Navigation Lights ....................................................AS REQUIRED
20. Landing Light ..........................................................AS REQUIRED
N - 11 P/N 13728-010
February 2013
NORMAL
21. Magnetos.................................................... CHECK Left and Right

RPM drop must not exceed 150 RPM for either magneto. RPM
differential must not exceed 75 RPM between magnetos
a. Ignition Switch .................................. R, note RPM, then BOTH
b. Ignition Switch ...................................L, note RPM, then BOTH
22. Engine Parameters .............................................................CHECK
23. Power Lever ................................................................... 1000 RPM
24. Flight Instruments, HSI, and Altimeter .................... CHECK & SET
25. Flight Controls .................................................FREE & CORRECT
26. Trim..............................................................................SET Takeoff
27. Autopilot...................................................................DISCONNECT
If Icing Conditions are Anticipated Immediately After Takeoff:
28. ICE PROTECT System Switch .................................................. ON
29. ICE PROTECT Mode Switch ................................... NORM / HIGH
30. PITOT HEAT Switch................................................................... ON
31. Cabin Heat............................................................................... HOT
32. Windshield Defrost .................................................................... ON
33. Ice-Inspection Lights...............................................AS REQUIRED
TAKEOFF
BEFORE
34. Verify airframe is free of contamination immediately before takeoff.
35. Flaps..............................................RETRACT as soon as practical
P/N 13728-010 N - 12
February 2013
NORMAL
Normal Takeoff
1. Brakes.................................... RELEASE (Steer with Rudder Only)
4. Elevator Control ........................ ROTATE Smoothly at 73-76 KIAS
5. At 90 KIAS, Flaps ...................................................................... UP
Short Field Takeoff

1. Flaps ........................................................................................ 50%
2. Brakes .................................................................................. HOLD
4. Mixture ..................................................................................... SET
6. Brakes.................................... RELEASE (Steer with Rudder Only)
7. Elevator Control ..............................ROTATE Smoothly at 73 KIAS
8. Airspeed at Obstacle ......................................................... 84 KIAS
Climb
TAKEOFF/
CLIMB
1. Climb Power............................................................................. SET

2. Flaps ............................................................................... Verify UP
3. Mixture .............................................. LEAN as required for altitude
5. Fuel Pump ..........................................................................BOOST
N - 13 P/N 13728-010
February 2013
NORMAL
Icing Conditions: In Flight

If Icing Conditions Exist:
1. PITOT HEAT Switch......................................................... Verify ON
3. ICE PROTECT Mode Switch ................................... NORM / HIGH
4. WIND SHLD Push-Button......................... PRESS AS REQUIRED
5. Monitor ice accumulation.
If ice accumulation occurs:
a. ICE PROTECT Mode ...................................................... HIGH
If ice continues accumulating:
b. ICE PROTECT Mode Push-Button ...................................MAX
If ice accretions do not shed:
c. PUMP BKUP Switch ........................................................... ON
d. Perform Deicing System Failure checklist.
Inadvertent Icing Encounter:
1. PITOT HEAT Switch......................................................... Verify ON
a. ICE PROTECT Mode Push-Button ...................................MAX
to initially dissipate ice accumulation, then
b. ICE PROTECT Mode Switch............................. HIGH / NORM
ICING
If excess ice accumulation occurs, then:
c. ICE PROTECT Mode Push-Button ...................................MAX
If ice does not shed perform Deicing System Failure checklist.
4. Airspeed ................................................... MAINTAIN 95-177 KIAS
or less than 204 KTAS
P/N 13728-010 N - 14
February 2013
NORMAL
Icing Conditions: In Flight

While in Icing Conditions:
1. FLAPS ....................................................................................... UP
3. Cabin Heat...............................................................................HOT
4. Windshield Defrost .................................................................... ON
5. Deicing Fluid Quantity ................................................... MONITOR
a. Ensure adequate quantity to complete flight.
After Leaving Icing Conditions:
1. Deicing System........................................................................ OFF
2. Airspeed ......................................as flight CONDITIONS DICTATE
4. Cabin Heat..............................................................AS REQUIRED
5. Windshield Defrost .................................................AS REQUIRED
Cruise
1. Oxygen .................................................................. AS REQUIRED
2. Cruise Altitude ........................................................ ESTABLISHED
3. Power Lever .................................... REDUCE to 30.5 in.Hg or less
CRUISE
ICING/
4. Fuel Pump ..............................................................AS REQUIRED

5. Mixture .............................................................................. ADJUST
6. Engine Parameters ........................................................ MONITOR
7. Fuel Flow and Balance .................................................. MONITOR
If any CHT’s exceed 420°F:
8. Mixture ........................................... LEAN 0.5 GPH and MONITOR
If Icing Conditions are Encountered During Cruise:
9. Perform Checklist...................................Icing Conditions - In Flight
10. Engine Power....................... INCREASE to maintain cruise speed.
11. Autopilot.......................................................................As Required
Disconnect every 30 minutes to detect any out-of-trim conditions.
When disconnecting the autopilot with ice accretions on the
airplane, the pilot should be alert for out-of-trim forces.
N - 15 P/N 13728-010
February 2013
NORMAL
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
2. ICE PROTECT Mode Switch ................................................. HIGH
3. Monitor ice accumulation.
If ice continues to accumulate:
a. ICE PROTECT Mode Push-Button ...................................MAX
If ice does not shed:
b. PUMP BKUP Switch ........................................................... ON
c. Perform Deicing System Failure checklist.
6. Flaps........................................................................................ 50%
7. Airspeed .........................................................Minimum of 95 KIAS
8. Airspeed on Short Final ..................................................... 88 KIAS
DESCENT
P/N 13728-010 N - 16
February 2013
NORMAL
Before Landing
1. Seat Belt and Shoulder Harness ..................................... SECURE
2. Fuel Pump ..........................................................................BOOST
4. Flaps .......................................................................AS REQUIRED
5. Autopilot..................................................................AS REQUIRED
Normal Landing
1. Flaps ...................................................................................... 100%
2. Airspeed ....................................................................... 80-85 KIAS
a. Airspeed on Short Final .............................................. 88 KIAS
3. Power Lever ............................................................AS REQUIRED
After touchdown:
4. Brakes.....................................................................AS REQUIRED
Short Field Landing

1. Flaps ...................................................................................... 100%
2. Airspeed ............................................................................ 79 KIAS
After clear of obstacles:
4. Power Lever ...................................................... REDUCE TO IDLE
After touchdown:
5. Brakes............................................................................ MAXIMUM
LANDING
Balked Landing/Go-Around
1. Autopilot..................................................................... DISENGAGE
3. Flaps ........................................................................................ 50%
4. Airspeed ....................................................................... 80-85 KIAS
After clear of obstacles:
5. Flaps ......................................................................................... UP
N - 17 P/N 13728-010
February 2013
NORMAL
After Landing
1. Power Lever ................................................................... 1000 RPM
2. Fuel Pump ............................................................................... OFF
3. Flaps.......................................................................................... UP
4. Transponder........................................................................... STBY
5. Lights ......................................................................AS REQUIRED
6. Pitot Heat................................................................................. OFF
7. ICE PROTECT System Switch ................................................ OFF
8. PUMP BKUP Switch ................................................................ OFF
9. Ice-Inspection Lights................................................................ OFF
Shutdown
1. Fuel Pump (if used) ................................................................ OFF
2. Throttle ................................................................................... IDLE
3. Ignition Switch .................................................................... CYCLE
4. Mixture.............................................................................. CUTOFF
5. All Switches ............................................................................. OFF
6. Magnetos................................................................................. OFF
7. ELT ...........................................................TRANSMIT LIGHT OUT
8. Chocks, Tie-downs, Pitot Covers ............................AS REQUIRED
SHUTDOWN
LANDING
AFTER
P/N 13728-010 N - 18
February 2013
NORMAL
Oxygen Duration (Precise Flight System)

Oxygen System Usage Duration - A4 Flowmeter
(STD) Standard Cannula/Mask - (OXY) Oxymiser Cannual
Tested Values at Altitude for flow rates STPD
(77 Cu. Ft. Serviced to 1,800 PSIG -5%), Flow Rates are For Reference Only
25
24
ABOVE 18,000FT
23
MASK ONLY
22
21
Usage Altitude (Ft * 1,000)
20
19
18
17 Masks or Cannulas Below 18,000FT
16 Masks required if user has Nasal
15 Blockage or Congestion.
14
13
12
11
10
9
8
0 5 10 15 20 25 30 35 40 45 50 55 60 65
Hours of Available O2
1 PERSON - STD 2 PERSONS - STD 3 PERSONS - STD 4 PERSONS - STD
1 PERSON - OXY 2 PERSONS - OXY 3 PERSONS - OXY 4 PERSONS - OXY
Oxygen System Usage Duration - A5 Flowmeter

(STD) Standard Cannula/Mask - (OXY) Oxymiser Cannual
Tested Values at Altitude for flow rates STPD
(77 Cu. Ft. Serviced to 1,800 PSIG -5%), Flow Rates are For Reference Only
25
24
ABOVE 18,000FT
23
MASK ONLY
22
21
20
Usage Altitude (Ft * 1,000)
19
18
17
16 Masks or Cannulas Below 18,000FT
Masks required if user has Nasal
15 Blockage or Congestion.
14
DURATION
13
12
O2
11
10
9
8
0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85
Hours of Available O2
1 PERSON - STD 2 PERSONS - STD 3 PERSONS - STD 4 PERSONS - STD
1 PERSON - OXY 2 PERSONS - OXY 3 PERSONS - OXY 4 PERSONS - OXY
SR22_FM09_3295
N - 19 P/N 13728-010
February 2013
CIRRUS
PERF
P ILOT’S CHEC KL IS T MODEL SR22
Performance
Table of Contents
Takeoff Distance: 3600 LB...............................................................P-1
Takeoff Distance: 2900 LB...............................................................P-2
Cruise Performance .........................................................................P-3
Landing Distance .............................................................................P-5
Stall Speeds with Ice Accumulation .................................................P-6
Cruise Performance with Ice Accumulation .....................................P-7
Cruise Performance with Ice Accumulation .................................P-8
Landing Distance with Ice Accumulation .........................................P-9
Wind Components .........................................................................P-10
Weight and Balance .......................................................................P-11
Loading Calculations .................................................................P-11
Loading Data .............................................................................P-12
Moment Limits ...........................................................................P-12
Temperature Conversion ...............................................................P-13
• Note •
Aircraft with optional Air Conditioning System; Brake
Horsepower is reduced by approximately 6 BHP.
P/N 13728-010 P-i

February 2013
PERFORMANCE
TAKEOFF
Takeoff Distance: 3600 LB

Weight: 3600 LB Headwind: Subtract 10% for each 12 knots
Speed at Liftoff: 76 KIAS headwind.
Speed over 50 Ft. Obstacle: 84 KIAS Tailwind: Add 10% for each 2 knots tailwind up
Flaps: 50% to 10 knots.
Power: Takeoff Runway Slope: Reference Notes.
Runway: Dry, Paved, Level Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
Air Conditioner: Add 100' to ground roll and
150' to distance over 50' obstacle if Air
Conditioner if ON during takeoff.
PRESS DISTANCE TEMPERATURE ~°C
ALT
FT FT 0 10 20 30 40 50 ISA
SL Grnd Roll 965 1042 1123 1207 1294 1384 1082
50 ft 1680 1804 1933 2066 2203 2345 1868
1000 Grnd Roll 1063 1148 1237 1330 1426 1526 1175
50 ft 1844 1980 2121 2267 2418 2573 2022
2000 Grnd Roll 1172 1267 1365 1467 1573 1683 1277
50 ft 2025 2174 2329 2490 2656 2827 2190
3000 Grnd Roll 1295 1399 1507 1620 1737 1858 1389
50 ft 2226 2391 2561 2738 2920 3109 2375
4000 Grnd Roll 1431 1546 1666 1791 1920 2054 1512
50 ft 2451 2632 2820 3014 3215 3422 2578
5000 Grnd Roll 1584 1711 1844 1982 2125 2273 1648
50 ft 2701 2900 3107 3322 3543 3772 2801
6000 Grnd Roll 1755 1896 2043 2195 2354 2519 1798
50 ft 2979 3200 3428 3665 3910 4162 3047
7000 Grnd Roll 1946 2103 2266 2435 2611 2794 1963
50 ft 3291 3535 3787 4049 4319 4598 3317
8000 Grnd Roll 2161 2335 2516 2704 2900 3102 2146
50 ft 3640 3909 4189 4478 4777 5086 3616
9000 Grnd Roll 2403 2596 2798 3007 3224 3449 2349
50 ft 4030 4329 4639 4959 5291 5633 3946
10000 Grnd Roll 2675 2890 3114 3347 3589 3840 2574
50 ft 4469 4800 5144 5499 5867 6247 4312
P-1 P/N 13728-010

February 2013
PERFORMANCE
Takeoff Distance: 2900 LB
TAKEOFF
Weight: 2900 LB Headwind: Subtract 10% for each 12 knots
Speed at Liftoff: 70 KIAS headwind.
Speed over 50 Ft. Obstacle: 74 KIAS Tailwind: Add 10% for each 2 knots tailwind up
Flaps: 50% to 10 knots.
Power: Takeoff Runway Slope: Reference Notes.
Runway: Dry, Paved, Level Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
Air Conditioner: Add 100' to ground roll and
150' to distance over 50' obstacle if Air
Conditioner if ON during takeoff.
ALT
FT FT 0 10 20 30 40 50 ISA
SL Grnd Roll 610 659 710 763 818 875 684
50 ft 971 1043 1118 1195 1275 1358 1080
1000 Grnd Roll 673 727 783 841 902 965 743
50 ft 1066 1146 1228 1313 1401 1492 1170
2000 Grnd Roll 743 802 864 929 995 1064 809
50 ft 1173 1260 1351 1444 1541 1641 1269
3000 Grnd Roll 821 887 955 1026 1100 1177 880
50 ft 1292 1388 1487 1590 1697 1807 1378
4000 Grnd Roll 908 981 1057 1135 1217 1302 959
50 ft 1424 1530 1639 1753 1871 1992 1498
5000 Grnd Roll 1006 1086 1170 1257 1348 1442 1046
50 ft 1571 1688 1809 1935 2065 2199 1630
6000 Grnd Roll 1116 1205 1298 1394 1494 1598 1143
50 ft 1736 1865 1999 2138 2281 2429 1775
7000 Grnd Roll 1238 1337 1440 1547 1659 1774 1249
50 ft 1920 2063 2211 2365 2523 2687 1936
8000 Grnd Roll 1376 1486 1601 1720 1843 1971 1367
50 ft 2127 2285 2449 2619 2795 2977 2113
9000 Grnd Roll 1532 1654 1781 1914 2051 2194 1498
50 ft 2359 2534 2716 2904 3099 3300 2309
10000 Grnd Roll 1707 1843 1985 2132 2285 2444 1643
50 ft 2619 2814 3016 3225 3441 3665 2527
P/N 13728-010 P-2

February 2013
PERFORMANCE
Cruise Performance
Conditions:
CRUISE
• Weight ........................................................................................................ 3400 LB

• Winds ............................................................................................................... Zero
• Note •
Subtract 10 KTAS if nose wheel pant and fairing removed. Lower KTAS by
10% if nose and main wheel pants & fairings are removed.
Aircraft with optional Air Conditioning System - Cruise performance is
reduced by 2 knots. For maximum performance, turn air-conditioner off.
Aircraft with optional Enhanced Vision System; Cruise performance is
reduced by up to 1 knot.
Press ISA - 30°C ISA ISA + 30°C

Alt RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2000 2700 27.4 103% 186 24.6 98% 186 23.3 93% 181 22.0
2600 27.4 99% 183 23.5 94% 183 22.2 89% 178 21.5
2500 27.4 93% 179 22.1 88% 179 20.9 84% 174 20.8
2500 26.4 89% 176 21.1 84% 176 19.9 80% 171 20.2
2500 25.4 84% 173 20.0 80% 173 19.0 76% 168 19.5
2500 24.4 80% 170 19.0 76% 170 18.0 72% 165 18.8
2500 23.4 76% 167 18.0 72% 167 17.0 68% 162 18.1
4000 2700 25.4 96% 185 22.9 91% 185 21.6 87% 180 20.8
2600 25.4 92% 182 21.9 87% 182 20.7 83% 177 20.6
2500 25.4 87% 178 20.6 82% 178 19.5 78% 173 19.9
2500 24.4 82% 175 19.5 78% 175 18.5 74% 170 19.2
2500 23.4 78% 172 18.5 74% 172 17.5 70% 167 18.5
2500 22.4 73% 169 17.4 69% 169 16.5 66% 163 17.7
2500 21.4 69% 165 16.4 65% 165 15.5 62% 159 16.9
6000 2700 23.5 89% 184 21.2 85% 184 20.1 81% 179 19.6
2600 23.5 85% 181 20.3 81% 181 19.2 77% 176 19.1
2500 23.5 80% 177 19.1 76% 177 18.1 72% 172 18.3
2500 22.5 76% 174 18.1 72% 174 17.1 68% 169 17.6
2500 21.5 72% 170 17.0 68% 170 16.1 64% 165 16.9
2500 20.5 67% 166 15.9 64% 166 15.1 60% 161 16.1
2500 19.5 63% 162 14.9 59% 162 14.1 56% 157 15.3
P-3 P/N 13728-010

February 2013
PERFORMANCE
Press ISA - 30°C ISA ISA + 30°C

Alt RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
8000 2700 21.7 83% 183 19.7 78% 183 18.6 75% 178 17.7
2600 21.7 79% 180 18.8 75% 180 17.8 71% 175 17.0
2500 21.7 75% 176 17.7 71% 176 16.8 67% 171 16.0
CRUISE
2500 20.7 70% 172 16.7 66% 172 15.8 63% 167 15.0
2500 19.7 66% 168 15.6 62% 168 14.8 59% 163 14.0
2500 18.7 61% 163 14.5 58% 163 13.8 55% 158 13.1
2500 17.7 57% 159 13.5 54% 159 12.8 51% 153 12.1
10000 2700 20.0 77% 182 18.2 73% 182 17.3 69% 176 16.4
2600 20.0 71% 177 17.0 68% 177 16.1 64% 172 15.3
2500 20.0 67% 173 16.0 64% 173 15.1 61% 167 14.4
2500 19.0 63% 168 14.9 59% 168 14.1 56% 163 13.4
2500 18.0 58% 163 13.8 55% 163 13.1 52% 158 12.5
2500 17.0 54% 158 12.8 51% 158 12.1 48% 153 11.5
12000 2700 18.5 71% 180 16.9 67% 180 16.0 64% 175 15.2
2600 18.5 68% 177 16.2 64% 177 15.3 61% 172 14.5
2500 18.5 64% 173 15.2 60% 173 14.4 58% 167 13.7
2500 17.5 59% 168 14.1 56% 168 13.4 53% 162 12.7
2500 16.5 55% 162 13.0 52% 162 12.3 49% 157 11.7
2500 15.5 50% 156 12.0 48% 156 11.3 45% 151 10.8
14000 2700 17.1 66% 178 15.6 62% 178 14.8 59% 173 14.1
2600 17.1 63% 175 14.9 60% 175 14.1 57% 170 13.5
2500 17.1 59% 171 14.1 56% 171 13.3 53% 165 12.7
2500 16.1 55% 165 13.0 52% 165 12.3 49% 159 11.7
2500 15.1 50% 159 11.9 47% 159 11.2 45% 153 10.7
16000 2700 15.8 61% 176 14.5 58% 176 13.7 55% 171 13.0
2600 15.8 58% 173 13.8 55% 173 13.1 52% 167 12.5
2500 15.8 55% 168 13.0 52% 168 12.3 49% 163 11.7
2500 14.8 50% 162 11.9 47% 162 11.3 45% 156 10.7
17000 2700 15.2 59% 175 13.9 55% 175 13.2 53% 169 12.5
2600 15.2 56% 171 13.3 53% 171 12.6 50% 166 12.0
2500 15.2 53% 167 12.5 50% 167 11.9 47% 162 11.3
2500 14.2 48% 160 11.4 45% 160 10.8 43% 155 10.3
P/N 13728-010 P-4

February 2013
PERFORMANCE
Landing Distance
WEIGHT: 3600 LB Headwind: Subtract 10% for each 13
Speed over 50 Ft Obstacle: 79 KIAS knots headwind.
Flaps: 100% Tailwind: Add 10% for each 2 knots
Power: Idle tailwind up to 10 knots.
Runway: Dry, Paved, Level Runway Slope: Reference Notes
LANDING
Dry Grass: Add 20% to Ground Roll

Wet Grass: Add 60% to Ground Roll

ALT
FT FT 0 10 20 30 40 50 ISA
SL Grnd Roll 1117 1158 1198 1239 1280 1321 1178
Total 2447 2505 2565 2625 2685 2747 2535
1000 Grnd Roll 1158 1200 1243 1285 1327 1370 1213
Total 2506 2567 2630 2693 2757 2821 2585
2000 Grnd Roll 1201 1245 1289 1333 1377 1421 1250
Total 2568 2633 2699 2765 2832 2900 2636
3000 Grnd Roll 1246 1292 1337 1383 1428 1474 1287
Total 2635 2702 2771 2841 2911 2983 2691
4000 Grnd Roll 1293 1340 1388 1435 1482 1530 1326
Total 2705 2776 2848 2922 2996 3070 2748
5000 Grnd Roll 1342 1391 1440 1489 1539 1588 1367
Total 2779 2854 2930 3007 3085 3163 2808
6000 Grnd Roll 1393 1444 1495 1546 1598 1649 1409
Total 2857 2936 3016 3097 3179 3261 2871
7000 Grnd Roll 1447 1500 1553 1606 1659 1712 1453
Total 2941 3024 3108 3193 3279 3365 2937
8000 Grnd Roll 1503 1558 1613 1668 1724 1779 1499
Total 3029 3116 3205 3294 3384 3475 3006
9000 Grnd Roll 1562 1619 1677 1734 1791 1848 1546
Total 3122 3214 3307 3401 3496 3592 3079
10000 Grnd Roll 1624 1683 1743 1802 1862 1921 1595
Total 3221 3318 3416 3515 3614 3715 3155
P-5 P/N 13728-010

February 2013
PERFORMANCE
Stall Speeds with Ice Accumulation

Conditions:
• Weight ........................................................................................................ 3600 LB
• CG ..................................................................................................................Noted
• Power..................................................................................................................Idle
• Bank Angle .....................................................................................................Noted
• Note •
Altitude loss during wings level stall may be 600 feet or more.
ICE PERF
KIAS values may not be accurate at stall.
STALL
Weight Bank STALL SPEEDS
Angle Flaps 0%
Full Up Flaps 50%
LB Deg KIAS KCAS KIAS KCAS

0 77 76 72 69
3600
15 79 77 73 70
30 83 82 75 74
Most FWD
45 91 90 82 82
CG
60 107 107 95 98
3600 0 77 76 72 69
15 79 77 73 70
Most 30 83 82 75 74
AFT 45 91 90 82 82
CG 60 107 107 95 98
P/N 13728-010 P-6

February 2013
PERFORMANCE
Cruise Performance with Ice Accumulation

Conditions:
• Cruise Weight ............................................................................................ 3400 LB
• Winds ............................................................................................................... Zero
• Note •
Aircraft with optional Air Conditioning System - Cruise performance is
reduced by 2 knots. For maximum performance, the air-conditioner should be
off.
2000 Feet Pressure Altitude

ICE PERF
CRUISE
ISA -30°C (-19°C) ISA (11°C) ISA + 30°C (41°C)

RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 27.4 103% 160 24.6
2600 27.4 99% 157 23.5
2500 27.4 93% 153 22.1
2500 26.4 89% 150 21.1
2500 25.4 84% 146 20.0
2500 24.4 80% 142 19.0
2500 23.4 76% 137 18.0

ISA -30°C (-23°C) ISA (7°C) ISA + 30°C (37°C)
2700 25.4 96% 158 22.9
2600 25.4 92% 155 21.9
2500 25.4 87% 150 20.6
2500 24.4 82% 146 19.5
2500 23.4 78% 141 18.5
2500 22.4 73% 136 17.4
2500 21.4 69% 130 16.4

ISA -30°C (-27°C) ISA (3°C) ISA + 30°C (33°C)
2700 23.5 89% 155 21.2 85% 155 20.1
2600 23.5 85% 151 20.3 81% 151 19.2
2500 23.5 80% 146 19.1 76% 146 18.1
2500 22.5 76% 140 18.1 72% 140 17.1
2500 21.5 72% 134 17.0 68% 134 16.1
2500 20.5 67% 128 15.9 64% 128 15.1
2500 19.5 63% 120 14.9 59% 120 14.1
P-7 P/N 13728-010

February 2013
PERFORMANCE
Cruise Performance with Ice Accumulation

ISA -30°C (-31°C) ISA (-1°C) ISA + 30°C (29°C)
2700 21.7 83% 150 19.7 78% 150 18.6
2600 21.7 79% 146 18.8 75% 146 17.8
2500 21.7 75% 140 17.7 71% 140 16.8
2500 20.7 70% 133 16.7 66% 133 15.8
2500 19.7 66% 126 15.6 62% 126 14.8
2500 18.7 61% 117 14.5 58% 117 13.8
2500 17.7 57% 108 13.5 54% 108 12.8
10,000 Feet Pressure Altitude
ICE PERF
ISA -30°C (-35°C) ISA (-5°C) ISA + 30°C (25°C)
CRUISE
2700 20.0 77% 144 18.2 73% 144 17.3
2600 20.0 71% 136 17.0 68% 136 16.1
2500 20.0 67% 129 16.0 64% 129 15.1
2500 19.0 63% 120 14.9 59% 120 14.1
2500 18.0 58% 111 13.8 55% 111 13.1
2500 17.0 54% 100 12.8 51% 100 12.1
P/N 13728-010 P-8

February 2013
PERFORMANCE
Landing Distance with Ice Accumulation

• Note •
Sloped Runway - Increase distances by 27% of ground roll distance for each
1% downslope. Decrease distances by 9% of ground roll distance for each 1%
upslope.
Associated balked landing climb gradient less than 3.3% shown in heavier
table borders.
WEIGHT: 3600 LB Headwind: Subtract 10% for each 13

Speed over 50 Ft Obstacle: 88 KIAS knots headwind.
Flaps: 50% Tailwind: Add 10% for each 2 knots
Power: Smooth power reduction from obstacle to tailwind up to 10 knots.
idle at touchdown. Runway Slope: Reference Notes
Runway: Dry, Paved, Level Dry Grass: Add 20% to Ground Roll
Wet Grass: Add 60% to Ground Roll
ALT
ICE PERF
LANDING
FT FT -20 -10 0 5 ISA

SL Grnd Roll 1356 1409 1463 1489
Total 2833 2908 2984 3022
1000 Grnd Roll 1406 1461 1517 1544
Total 2903 2981 3061 3101
2000 Grnd Roll 1458 1516 1573 1602
Total 2977 3059 3143 3185
3000 Grnd Roll 1513 1572 1632 1662
Total 3055 3142 3229 3274
4000 Grnd Roll 1570 1632 1694 1725
Total 3138 3229 3321 3367
5000 Grnd Roll 1629 1694 1758 1790
Total 3225 3321 3418 3466
6000 Grnd Roll 1692 1758 1825 1859
Total 3318 3418 3520 3571
7000 Grnd Roll 1757 1826 1896 1930
Total 3416 3522 3628 3682
8000 Grnd Roll 1825 1897 1969 2005 1963
Total 3520 3631 3743 3800 3583
9000 Grnd Roll 1896 1971 2046 2084 2025
Total 3630 3746 3864 3924 3656
10000 Grnd Roll 1971 2049 2127 2166 2089
Total 3746 3869 3993 4055 3733
P-9 P/N 13728-010

February 2013
PERFORMANCE
Wind Components
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
• Note •
The maximum demonstrated crosswind is 21 knots. Value not considered
limiting.
40
0
10 50
20 W
IN
D
30 30
VE
TH
LO
PA
CI
40
TY
HT
40
~
IG
KN
FL
OT
D
CMPNNTS
AN
S
50
WIND
ON
30
I
CT
20
RE
DI
D
60
IN
W
N
EE
20
TW
BE
70
E
GL
10
AN
WIND COMPONENTS - KNOTS
Headwind
10
80
0 90
Tailwind
100
-10
110
SR2_FM05_1014
170 150
140 130
180 160 120
-20
10 20 30 40
CROSSWIND COMPONENT ~ KNOTS
P/N 13728-010 P - 10
February 2013
PERFORMANCE
Weight and Balance

Loading Calculations
For Moment/1000, refer to Loading Data table on following page.
Description Weight Moment/1000
1. Empty Weight
Includes unusable fuel and full oil
2. Front Seats Occupants
Pilot and Passenger
3. Rear Seats Occupants
4. Baggage
130 lb maximum
5. Zero Fuel Condition
Subtotal items 1 thru 4
3400 lb maximum
6. Fuel Load
92 Gallon @6.0 lb/gal. maximum
7. Ramp Weight
Subtotal items 5 and 6
W&B
8. Fuel for start, taxi, and runup - -

Normally 9 lb at avg. mmnt of 1394.1
9. Takeoff Weight
Subtract Item 8 from item 7
Calculation Instructions
1. Enter the current basic empty weight and moment from the aircraft’s
Weight and Balance Record.
2. Enter the total weight and moment/1000 for the front seat occupants from
the adjacent Loading Data Table.
3. Enter the total weight and moment/1000 for the rear seat occupants from
the adjacent Loading Data Table.
4. Enter the total weight and moment/1000 for the baggage from the
adjacent Loading Data Table.
5. If desired, subtotal the weight and moment/1000 entries from steps 1 - 4.
6. Enter the weight and moment/1000 of usable fuel loaded on the airplane.
7. Subtotal the weight and moment/1000.
8. Enter values for typical start, taxi, and run-up operations of 9 pounds at an
average moment\1000 of 1.394.
9. Subtract step 8 weight and moment/1000 from the Ramp Weight to
determine the Takeoff Weight and moment/1000.
a. Verify Takeoff Weight does not exceed the 3600 pounds.
b. Verify Moment/1000 does falls between the interpolated minimum
and maximum values listed on the adjacent Moment Limits Table.
P - 11 P/N 13728-010
February 2013
PERFORMANCE
Loading Data
Use this table to determine the Moment/1000.
Weight Fwd Aft Baggage Fuel Weight Fwd Aft Fuel
Pass Pass Pass Pass
LB FS 143.5 FS 180.0 FS 208.0 FS 154.9 LB FS 143.5 FS 180.0 FS 154.9
20 2.9 3.6 4.2 3.1 300 43.1 54.0 46.5
40 5.7 7.2 8.3 6.2 320 45.9 57.6 49.6
60 8.6 10.8 12.5 9.3 340 48.8 61.2 52.7
80 11.5 14.4 16.6 12.4 360 51.7 64.8 55.8
100 14.4 18.0 20.8 15.5 380 54.5 68.4 58.9
120 17.2 21.6 25.0 18.6 400 57.4 72.0 62.0
140 20.1 25.2 27.04* 21.7 420 60.3 75.6 65.1
160 23.0 28.8 24.8 440 63.1 79.2 68.2
180 25.8 32.4 27.9 460 82.8 71.3
200 28.7 36.0 31.0 480 86.4 74.4
220 31.6 39.6 34.1 500 90.0 77.5
240 34.4 43.2 37.2 520 80.5
260 37.3 46.8 40.3 552** 85.5
280 40.2 50.4 43.4
*130 lb Maximum **92 U.S. Gallons Usable
Moment Limits
Use this table to determine if Loading Calculations are within limits.
W&B
Weight Moment/1000 Weight Moment/1000
LB Minimum Maximum LB Minimum Maximum
2200 304 326 2950 414 437

2250 311 333 3000 422 444
2300 318 341 3050 430 452
2350 326 348 3100 438 459
2400 333 355 3150 445 467
2450 340 363 3200 453 474
2500 347 370 3250 461 481
2550 354 378 3300 469 489
2600 362 385 3350 477 496
2650 369 392 *3400 484 504
2700 375 400 3450 494 511
2750 383 407 3500 501 519
2800 390 415 3550 508 526
2850 398 422 3600 515 533
2900 406 430
*NOTE: Maximum zero fuel weight.
P/N 13728-010 P - 12
February 2013
PERFORMANCE
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 Temp to Convert Temp to Convert

°C or °F °C or °F °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
CONVERT
-39 -38 -36 -6 22 72 28 82 180

TEMP
-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
P - 13 P/N 13728-010
February 2013
ABNORMAL
Abnormal Procedures
Table of Contents
Perspective Crew Alerting System (CAS) Index
CAS Message Page CAS Message Page

OIL PRESS A-3 MFD FAN FAIL A-7
MAN PRESSURE A-3 PITOT HEAT FAIL A-8
START ENGAGE A-3 PITOT HEAT REQD A-8
FUEL QTY A-4 FLAPS A-9
L FUEL QTY A-4 BRAKE TEMP A-9
R FUEL QTY A-4 ANTI ICE QTY A-10
FUEL IMBALANCE A-4 AOA OVERHEAT A-10
M BUS 1 A-5 ANTI ICE PSI A-11
M BUS 2 A-5 ANTI ICE PSI A-11
BATT 1 A-5 ANTI ICE SPD A-11
ALT 1 A-6 ANTI ICE LVL A-12
ALT 2 A-6 ANTI ICE HTR A-12
AVIONICS OFF A-7 PARK BRAKE A-13
PFD FAN FAIL A-7
Flight Environment ...........................................................................A-1

Inadvertent Icing Encounter.........................................................A-1
Inadvertent IMC Encounter..........................................................A-1
Door Open In Flight .....................................................................A-1
Abnormal Landings ..........................................................................A-2
Landing With Failed Brakes.........................................................A-2
Landing With Flat Tire .................................................................A-2
Engine System .................................................................................A-3
Low Idle Oil Pressure ..................................................................A-3
Manifold Pressure High ...............................................................A-3
Starter Engaged ..........................................................................A-3
Fuel System .....................................................................................A-4
Low Fuel Quantity........................................................................A-4
Left OR Right Fuel Tank Quantity ...............................................A-4
Fuel Imbalance ............................................................................A-4
Electrical System .............................................................................A-5
Low Voltage on Main Bus 1.........................................................A-5
Low Voltage on Main Bus 2.........................................................A-5
P/N 13728-010 A-i

February 2013
EMERGENCY ABNORMAL PERFORMANCE NORMAL
ABNORMAL
Abnormal Procedures
Table of Contents
Battery 1 Current Sensor .............................................................A-5
Low Alternator 1 Output ..............................................................A-6
Low Alternator 2 Output...............................................................A-6
Integrated Avionics System..............................................................A-7
Avionics Switch Off......................................................................A-7
PFD Cooling Fan Failure .............................................................A-7
MFD Cooling Fan Failure ............................................................A-7
Flight Displays Too Dim...............................................................A-7
Pitot Static System ...........................................................................A-8
Pitot Static Malfunction ................................................................A-8
Pitot Heat Current Sensor Annunciation......................................A-8
Pitot Heat Required Annunciation ...............................................A-8
Flight Control System.......................................................................A-9
Electric Trim/Autopilot Failure......................................................A-9
Flap System Exceedance............................................................A-9
Landing Gear System ......................................................................A-9
Brake Failure During Taxi ............................................................A-9
Left/Right Brake Over-Temperature ............................................A-9
Anti-Ice System ..............................................................................A-10
Windshield De-Ice System Malfunction .....................................A-10
Heated Lift Transducer Malfunction...........................................A-10
Low Fluid Quantity Caution .......................................................A-10
Lift Transducer Overheat Caution .............................................A-10
Persistent Low Pressure Caution ..............................................A-11
High Pressure Caution ..............................................................A-11
Speed Caution...........................................................................A-11
Left/Right Anti-Ice Fluid Level Caution ......................................A-12
Stall Warning / AOA Heater Failure Caution .............................A-12
Other Conditions ............................................................................A-13
Aborted Takeoff .........................................................................A-13
Parking Brake Engaged Annunciation.......................................A-13
Communications Failure............................................................A-13
Electrical System Schematic..........................................................A-14
A - ii P/N 13728-010
February 2013
ABNORMAL
Flight Environment
IN FLIGHT
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
P/N 13728-010 A-1

February 2013
ABNORMAL
Abnormal Landings
LANDING
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.
A-2 P/N 13728-010

February 2013
ABNORMAL
Engine System
Low Idle Oil Pressure
OIL PRESS
ENGINE
1. If In-Flight.................................. LAND AS SOON AS PRACTICAL
Manifold Pressure High
MAN PRESSURE
1. Power Lever .........................................REDUCE to less than 36.5"

2. Flight.............................................................................CONTINUE
If noticeable surging is present:
3. Complete Overboost / Pressure Relief Valve Emergency Checklist
Starter Engaged
START ENGAGE
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
3. Flight.............................................................................CONTINUE
Engine start will not be available at destination.
P/N 13728-010 A-3

February 2013
ABNORMAL
Fuel System
Low Fuel Quantity
FUEL QTY
FUEL
1. Fuel Quantity Gages...........................................................CHECK

If fuel quantity indicates less than or equal to 14 gallons:
a. Land as soon as practical.
If fuel quantity indicates more than 14 gallons:
a. Flight ...................................................CONTINUE, MONITOR
Left OR Right Fuel Tank Quantity
Conduct the following procedure if either of the annunciations listed
below are displayed on the MFD.
L FUEL QTY R FUEL QTY
1. Indicated (L or R) Fuel Quantity Gage................................CHECK

a. If On-Ground .............................. REFUEL PRIOR TO FLIGHT
b. If In-Flight ............................................CONTINUE, MONITOR
a. If On-Ground .......................... CORRECT PRIOR TO FLIGHT
Fuel Imbalance
FUEL IMBALANCE

2. Fuel Pump ..........................................................................BOOST
If HIGH BOOST already in use for vapor suppression, pump
should be left in this position for tank switch.
3. Fuel Selector ......................................... SELECT FULLEST TANK
After switching tanks, message will remain until sensed
imbalance is less than 10 gallons.
A-4 P/N 13728-010
February 2013
ABNORMAL
Electrical System
Low Voltage on Main Bus 1
M BUS 1
1. Perform Alt 1 Caution (Failure) Checklist.

Low Voltage on Main Bus 2
ELECTRIC
M BUS 2
1. Perform Alt 1 and Alt 2 Caution (Failure) checklists.

Battery 1 Current Sensor
BATT 1
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.
P/N 13728-010 A-5

February 2013
ABNORMAL
Low Alternator 1 Output
ALT 1
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
ELECTRIC
4. Non-Essential Bus Loads ................................................ REDUCE

a. If flight conditions permit, consider shedding the following to
preserve Battery 1:
(1) Air Conditioning,
(2) Landing Light,
(3) Yaw Servo,
(4) Convenience Power (aux items plugged into armrest jack)
5. Continue Flight, avoiding IMC or night flight as able.
Low Alternator 2 Output
ALT 2
1. ALT 2 Circuit Breaker.............................................. CHECK & SET

2. ALT 2 Master Switch ........................................................... CYCLE
If alternator does not reset (low A2 Current and M2 voltage less
than M1 voltage):
3. ALT 2 Master Switch ................................................................ OFF
4. Continue Flight, avoiding IMC or night flight as able (reduced
power redundancy).
A-6 P/N 13728-010

February 2013
ABNORMAL
Integrated Avionics System

Avionics Switch Off
AVIONICS OFF
1. AVIONICS Switch ........................................... ON, AS REQUIRED

PFD Cooling Fan Failure
PFD FAN FAIL
1. AVIONICS FAN 2 Circuit Breaker ....................................... CYCLE
AVIONICS
If annunciation does not extinguish:
a. Hot cabin temperatures...... LAND AS SOON AS PRACTICAL
b. Cool cabin temperatures .....................CONTINUE, MONITOR
MFD Cooling Fan Failure
MFD FAN FAIL
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.
P/N 13728-010 A-7

February 2013
ABNORMAL
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

STATIC
PITOT-
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
PITOT HEAT REQD
1. Pitot Heat ................................................................................... ON
A-8 P/N 13728-010

February 2013
ABNORMAL
Flight Control System

Electric Trim/Autopilot Failure
1. Airplane Control.......................................... MAINTAIN MANUALLY
2. Autopilot (if engaged)................................................. DISENGAGE
If Problem Is Not Corrected:
3. Circuit Breakers ............................................PULL AS REQUIRED
• PITCH TRIM
• ROLL TRIM
• YAW SERVO
• AP SERVOS
5. Control Yoke .................................MANUALLY HOLD PRESSURE
FLT CNTRLS
LANDING
Flap System Exceedance
GEAR
FLAPS
1. Airspeed .......................................................................... REDUCE

or
1. Flaps.............................................................................. RETRACT
Landing Gear System

Brake Failure During Taxi
1. Engine Power .........................................................AS REQUIRED
2. Directional Control ............................... MAINTAIN WITH RUDDER
3. Brake Pedal(s) ...................................................................... PUMP
If directional control can not be maintained:
Left/Right Brake Over-Temperature
BRAKE TEMP
1. Stop aircraft and allow the brakes to cool.

P/N 13728-010 A-9
February 2013
ABNORMAL
Anti-Ice System
Windshield De-Ice System Malfunction
1. ICE PROTECT A Circuit Breaker........................................ CYCLE
2. Fluid Quantity .................................. SWITCH TO FULLEST TANK
If the forward field of view is overly restricted during landing
approach and taxiing:
a. Cabin Heat ........................................................................HOT
b. Windshield Defrost .............................................................. ON
c. Execute a forward slip as required for visibility.
d. Avoid taxiing without adequate forward visibility.
Heated Lift Transducer Malfunction
If ice forms on lift transducer:
1. STALL VANE HEAT Circuit Breaker.................................... CYCLE
ANTI-ICE
2. PITOT HEAT Switch............................................. CYCLE OFF, ON

If ice remains on lift transducer:
1. Stall Warning System ......... EXPECT NO RELIABLE INDICATION
This includes:
• Impending stall warning.
• Stall speed indication.
2. Airspeed ............................................. MONITOR, DO NOT STALL
3. Fly published VREF speeds......... Minimum 88 KIAS with 50% Flap
Low Fluid Quantity Caution
ANTI ICE QTY
1. Icing Conditions .........................................................AVOID / EXIT

Lift Transducer Overheat Caution
AOA OVERHEAT
1. PITOT HEAT Switch................................................................. OFF

A - 10 P/N 13728-010
February 2013
ABNORMAL
Persistent Low Pressure Caution
ANTI ICE PSI
1. ICE PROTECT A and B Circuit Breakers ................................ SET

2. Anti-Ice - TKS Quantity.................... SWITCH TO FULLEST TANK
3. WIND SHLD Push-Button................................................... PRESS
a. Repeat operation of windshield pump to verify system is
primed properly as evidenced by anti-ice fluid exiting
windshield nozzles.
If caution annunciation extinguishes:
a. Anti-Ice System ........................................................MONITOR
If caution annunciation does not extinguishes or intermittent:
a. PUMP BKUP Switch ........................................................... ON
b. Icing Conditions...................................................AVOID / EXIT
High Pressure Caution
ANTI-ICE
ANTI ICE PSI
1. Evidence of Anti-Ice Flow ...............................MONITOR / VERIFY

Speed Caution
ANTI ICE SPD
1. Airspeed ................................................... MAINTAIN 95-177 KIAS

or less than 204 KTAS
P/N 13728-010 A - 11
February 2013
ABNORMAL
Left/Right Anti-Ice Fluid Level Caution
ANTI ICE LVL
1. Revert to manual control of the fluid source to control the fluid level
quantity.
If ANTI ICE FLO or ANTI ICE PSI annunciates:
a. Switch to opposite tank.
b. WIND SHLD Push-Button ............................................ PRESS
(1) Repeat operation of windshield pump to verify system is
primed properly as evidenced by anti-ice fluid exiting
windshield nozzles.
Stall Warning / AOA Heater Failure Caution
ANTI ICE HTR
1. STALL VANE HEAT Circuit Breaker.................................... CYCLE

2. PITOT HEAT Circuit Breaker .............................................. CYCLE
ANTI-ICE
4. Fly aircraft normally using airframe buffet as the stall warning. Ice
accumulations on the stall warning vane may result in unreliable
stall warning system operation.
A - 12 P/N 13728-010
February 2013
ABNORMAL
Other Conditions
Aborted Takeoff
1. Power Lever ............................................................................ IDLE
2. Brakes.....................................................................AS REQUIRED
Parking Brake Engaged Annunciation
PARK BRAKE
1. Parking Brake .................................................................RELEASE

2. Monitor CAS for BRAKE TEMP Caution. Stop aircraft and allow
the brakes to cool if necessary.
Communications Failure
1. Switches, Controls ..............................................................CHECK
2. Frequency........................................................................ CHANGE
3. Circuit Breakers ....................................................................... SET
4. Headset ........................................................................... CHANGE
5. Hand Held Microphone..................................................CONNECT
OTHER
P/N 13728-010 A - 13
February 2013
ABNORMAL
Electrical System Schematic
100A LANDING
F ALT 1 B LIGHT
ALT 1 VOLT REG 7.5A

RELAY
MAIN DIST BUS 1

LANDING LIGHT
EXTERNAL SWITCH
ALT 1 30A
POWER RELAY
SWITCH
EXTERNAL 30A
POWER
30A
125A 50A
ESSENTIAL DIST BUS

30A
BAT 1 BAT 1
80A 50A
BAT 1 SWITCH RELAY
STARTER 30A
50A
STARTER
MAIN DIST BUS 2

RELAY
30A
STARTER
SWITCH
30A
80A
F ALT 2 B
30A
VOLT REG
MASTER CONTROL UNIT
ALT 2
SWITCH
A/C BUS 1
ESSENTIAL BUS 2
A/C COND ALT 2 AVIONICS

ENGINE ICE
ALT 1 INSTR PROTECTION
STALL STDBY
MAIN BUS 1
8A
SCHEMATIC
WARNING ATTD #2
ELEC SYS
YAW
MAIN BUS 3
A/C BUS 2
SERVO ROLL MFD #2

A/C COMPR EVS TRIM
PITCH CABIN LIGHTS
CAMERA / OXYGEN
CABIN TRIM
FAN 12V DC
OUTLET FUEL QTY
MFD #1 AP SERVOS
ESSENTIAL KEYPADS
POWER / AP CTRL
ESSENTIAL BUS 1
STARTER
NON-ESSENTIAL BUS
BAT 2 CABIN AIR

AVIONICS AVIONICS CONTROL
FAN 1 FAN 2 GPS NAV
RECOG GPS NAV GIA 1
MAIN BUS 2
LIGHTS GIA 2 COM 1

AVIONICS BUS
NAV 8A DME / ADF

20A COM 2
LIGHTS ADC 1 AUDIO
STROBE AHRS 2/ PANEL
20A
LIGHTS (ADC 2) AHRS 1 WEATHER
PITOT FUEL / DATA LINK
HEAT PUMP STDBY
ATTD #1 XPONDER
FLAPS PFD #2
STALL PFD #1 TRAFFIC
VANE HEAT
CIRCUIT BREAKER PANEL

30A AVIONICS
SWITCH
BAT 2
BAT 2 AVIONICS
SWITCH NON-ESSENTIAL
RELAY SR22_FM07_2806B
A - 14 P/N 13728-010
February 2013
EMRGNCY
Emergency Procedures
Table of Contents
Perspective Crew Alerting System (CAS) Index
CAS Message Page CAS Message Page
OIL PRESS E-7 ESS BUS E-12
OIL TEMP E-7 CO LVL HIGH E-13
CHT E-8 ANTI ICE FLO E-15
FUEL QTY E-9 ANTI ICE CTL E-15
FUEL IMBALANCE E-9 ANTI ICE QTY E-15
RPM E-10 AOA OVERHEAT E-15
M BUS 1 E-11 BRAKE TEMP E-18
M BUS 2 E-11 START ENGAGE E-18
Airspeeds for Emergency Operations ..............................................E-1
Maximum Glide............................................................................E-1
Memory Items..............................................................................E-1
Engine Failures ................................................................................E-2
Engine Failure On Takeoff (Low Altitude)....................................E-2
Engine Failure In Flight................................................................E-2
Airstart..............................................................................................E-3
Engine Airstart .............................................................................E-3
Smoke and Fire................................................................................E-4
Cabin Fire In Flight ......................................................................E-4
Engine Fire In Flight ....................................................................E-4
Wing Fire In Flight .......................................................................E-5
Engine Fire During Start ..............................................................E-5
Smoke and Fume Elimination......................................................E-5
Emergency Descent.........................................................................E-6
Emergency Descent ....................................................................E-6
Forced Landing ................................................................................E-6
Emergency Landing Without Engine Power ................................E-6
Ditching........................................................................................E-6
Landing Without Elevator Control................................................E-6
Engine System .................................................................................E-7
Engine Partial Power Loss ..........................................................E-7
Oil Pressure Out of Range ..........................................................E-7
Oil Temperature High ..................................................................E-7
High Cylinder Head Temperature................................................E-8
Fuel System Emergencies ...............................................................E-9
Low Fuel Quantity........................................................................E-9
Fuel Imbalance ............................................................................E-9
P/N 13728-010 E-i

February 2013
EMERGENCY ABNORMAL PERFORMANCE NORMAL
EMRGNCY
Emergency Procedures
Table of Contents
Propeller System Emergencies......................................................E-10
Engine Speed High....................................................................E-10
Propeller Governor Failure .......................................................E-10
Electrical System Emergencies......................................................E-11
High Voltage on Main Bus 1 ......................................................E-11
High Voltage on Main Bus 2 ......................................................E-11
High or Low Voltage on Essential Bus ......................................E-12
Environmental System Emergencies .............................................E-13
Carbon Monoxide Level High ....................................................E-13
Anti-Ice System ..............................................................................E-14
Anti-Ice System Failure / Excessive Ice Accumulation ..............E-14
Low Flow Rate Warning ............................................................E-15
Tank Control Failure Warning....................................................E-15
Low Fluid Quantity Warning ......................................................E-15
AOA Probe Overheat Warning ..................................................E-15
Integrated Avionics System Emergencies......................................E-16
Attitude & Heading Reference System (AHRS) Failure.............E-16
Air Data Computer (ADC) Failure ..............................................E-16
PFD Display Failure...................................................................E-16
Unusual Attitude Emergencies.......................................................E-17
Inadvertent Spin Entry ...............................................................E-17
Inadvertent Spiral Dive During IMC Flight .................................E-17
Other Emergencies ........................................................................E-17
Power Lever Linkage Failure.....................................................E-17
Emergency Engine Shutdown On Ground ................................E-17
Left/Right Brake Over-Temperature ..........................................E-18
Starter Engaged ........................................................................E-18
Emergency Ground Egress .......................................................E-18
CAPS Deployment .........................................................................E-19
Circuit Breaker Panel .....................................................................E-20
E - ii P/N 13728-010
February 2013
EMERGENCY
Airspeeds for Emergency Operations
AIRSPEEDS
Maneuvering Speed:
3600 lb ................................................................................... 140 KIAS
Best Glide:
All Weights ............................................................................... 92 KIAS
Emergency Landing (Engine-out):
Flaps Up................................................................................... 90 KIAS
Flaps 50% ................................................................................ 85 KIAS
Flaps 100% .............................................................................. 80 KIAS
Maximum Glide
Best Glide Speed .................................................... 92 KIAS at 3600 lb
Maximum Glide Ratio ~ 8.8 : 1
14000
HEIGHT ABOVE GROUND - FEET
12000
10000
8000
6000
4000
2000
0
0 2 4 6 8 10 12 14 16 18 20
GROUND DISTANCE - NAUTICAL MILES
SR22_FM03_3563
• Note •
Maximum Glide Ratio with Ice Accumulation ~ 6.4: 1
Memory Items
Checklist steps emphasized by underlining such as the example
below, should be memorized for accomplishment without reference to
the procedure.
1. Best Glide Speed........................................................ ESTABLISH
P/N 13728-010 E-1

February 2013
EMERGENCY
Engine Failures
FAILURE
Engine Failure On Takeoff (Low Altitude)

ENGINE
1. Best Glide or Landing Speed (as appropriate) ........... ESTABLISH

2. Mixture ..............................................................................CUTOFF
3. Fuel Selector ........................................................................... 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
3. Fuel Selector ........................................................SWITCH TANKS
4. Fuel Pump ......................................................................... BOOST
5. Alternate Induction Air .............................................................. ON
6. Air Conditioner (if installed) .................................................... OFF
7. Ignition Switch ........................................................ CHECK, BOTH
8. Power Lever ...................................................................... ½ OPEN
If engine does not start:
9. Perform Engine Airstart or Forced Landing checklist, as required.
E-2 P/N 13728-010

February 2013
EMERGENCY
Airstart
Engine Airstart
1. Bat Master Switches .................................................................. ON
2. Power Lever ............................................................ OPEN ½ INCH
AIRSTART
3. Mixture.................................................................RICH, AS REQ’D
5. Ignition Switch .......................................................................BOTH
6. Fuel Pump ..........................................................................BOOST
7. Alternate Induction Air .............................................................. ON
8. Alt Master Switches ................................................................. OFF
9. Starter (Propeller not Windmilling) .................................. ENGAGE
10. Power Lever ....................................................... slowly INCREASE
12. If engine will not start, perform Forced Landing checklist.
P/N 13728-010 E-3

February 2013
EMERGENCY
Smoke and Fire

Cabin Fire In Flight
1. Bat-Alt Master Switches ........................................OFF, AS REQ’D
2. Fire Extinguisher.............................................................ACTIVATE
AND FIRE
SMOKE
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
Engine Fire In Flight
1. Mixture ..............................................................................CUTOFF
2. Fuel Pump ............................................................................... OFF
4. Airflow Selector........................................................................ OFF
5. Power Lever ........................................................................... IDLE
7. Cabin Doors.......................................................PARTIALLY OPEN
E-4 P/N 13728-010

February 2013
EMERGENCY
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.
Engine Fire During Start
AND FIRE
SMOKE
1. Mixture.............................................................................. CUTOFF
2. Fuel Pump ............................................................................... OFF
4. Power Lever .................................................................. FORWARD
5. Starter.................................................................................CRANK
6. If flames persist, perform Emergency Engine Shutdown on
Ground and Emergency Ground Egress checklists.
Smoke and Fume Elimination
1. Oxygen Masks or Cannulas ................................................... DON
2. Oxygen System ......................................................................... ON
3. Oxygen Flow Rate ......................................................... MAXIMUM
4. Air Conditioner (if installed) .................................................... OFF
7. Airflow Selector............................... SET AIRFLOW TO MAXIMUM
If source of smoke and fume is firewall forward:
a. Airflow Selector ................................................................. OFF
9. Prepare to land as soon as possible.
P/N 13728-010 E-5

February 2013
EMERGENCY
Emergency Descent
Emergency Descent
1. Power Lever ............................................................................ IDLE
3. Airspeed ................................................................ VNE (205 KIAS)
Forced Landing
Emergency Landing Without Engine Power
DESCENT
LANDING
FORCED

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
9. Fuel Pump ............................................................................... OFF
10. Flaps (when landing is assured) ............................................ 100%
11. Master Switches ...................................................................... OFF
12. Seat Belt(s) ....................................................................SECURED
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
E-6 P/N 13728-010
February 2013
EMERGENCY
Engine System
Engine Partial Power Loss
1. Fuel Pump ..........................................................................BOOST
3. Mixture..............................CHECK appropriate for flight conditions
4. Power Lever ....................................................................... SWEEP
5. Ignition Switch ...................................................... BOTH, L, then R
Oil Pressure Out of Range
OIL PRESS
ENGINE
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
1. Power............................................................................... REDUCE
2. Airspeed ....................................................................... INCREASE
3. Mixture.................................. ADJUST fuel flow to top of green arc
4. Oil Temperature Gage ....................................................MONITOR
If temperature remains high:
P/N 13728-010 E-7

February 2013
EMERGENCY
High Cylinder Head Temperature
CHT
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
ENGINE
2. Airspeed ...................................................................... INCREASE

3. Annunciations and Engine Temperatures ...................... MONITOR
If Caution or Warning annunciation is still illuminated:
4. Power Lever ............................................... MINIMUM REQUIRED
5. Engine Instruments ....................................................... MONITOR
If Caution annunciation only remains illuminated:
a. Land as soon as practical.
If Warning annunciation remains illuminated:
a. Land as soon as possible.
E-8 P/N 13728-010

February 2013
EMERGENCY
Fuel System Emergencies

Low Fuel Quantity
FUEL QTY

a. If On-Ground .............................. REFUEL PRIOR TO FLIGHT
b. If In-Flight ........................... LAND AS SOON AS PRACTICAL
a. If On-Ground ...........................CORRECT PRIOR TO FLIGHT
Fuel Imbalance
FUEL IMBALANCE
FUEL
2. Fuel Pump ..........................................................................BOOST
If HIGH BOOST already in use for vapor suppression, pump
should be left in this position for tank switch.
3. Fuel Selector ......................................... SELECT FULLEST TANK
After switching tanks, message will remain until sensed
imbalance is less than 12 gallons.
P/N 13728-010 E-9

February 2013
EMERGENCY
Propeller System Emergencies

Engine Speed High
RPM
1. Power Lever ...................... REDUCE by 2 in.Hg Manifold Pressure

If governor is not in control (RPM reduces and remains lower after
power adjustment):
2. Perform Propeller Governor Failure checklist
If governor is in control (RPM remains high, but stable after power
reduction):
below 34 in.Hg for climb, below 30.5in.Hg for cruise
If governed engine speed exceeds 2600 RPM:
PROP
If governed engine speed is 2600 RPM or less:

5. Flight .............................................................................CONTINUE
Propeller Governor Failure

1. Power Lever .....Reduce to minimum necessary for sustained flight
2. Airspeed ......................................................Reduce to 85-90 KIAS
3. Oil Pressure ................................................................... MONITOR
4. Land as soon as able
E - 10 P/N 13728-010
February 2013
EMERGENCY
Electrical System Emergencies

High Voltage on Main Bus 1
M BUS 1
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
1. Main Bus 1 Voltage (M1) ....................................................CHECK

2. Perform M Bus 1 Warning Checklist
ELEC SYS
4. ALT 2 Master Switch........................................................... CYCLE
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)
P/N 13728-010 E - 11
February 2013
EMERGENCY
High or Low Voltage on Essential Bus
ESS BUS
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 Main Bus 1 or Main Bus 2 Warning checklists
If Essential Bus Voltage is less than 24.5 Volts:
4. Perform Alt 1 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 practical (Battery reserve only)
ELEC SYS
E - 12 P/N 13728-010
February 2013
EMERGENCY
Environmental System Emergencies

Carbon Monoxide Level High
CO LVL HIGH
1. Air Conditioner (if installed) ......................NOT IN RECIRC MODE

4. Airflow Selector............................... SET AIRFLOW TO MAXIMUM
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
ENVIRO
P/N 13728-010 E - 13
February 2013
EMERGENCY
Anti-Ice System
Anti-Ice System Failure / Excessive Ice Accumulation
a. Repeat operation of windshield pump to verify metering
pumps are primed properly as evidenced by deicing fluid
exiting windshield nozzles.
4. ICE PROTECT Mode Switch ................................... VERIFY HIGH
5. PUMP BKUP Switch .................................................................. ON
If determined windshield pump is not priming:
6. Exit Icing Conditions Immediately.
7. Airspeed ....................................................95 KIAS OR GREATER
Maintain a minimum airspeed of 95 KIAS or higher to stay above
pre-stall buffet. If unable to maintain this airspeed, allow altitude to
decrease in order to maintain 95 KIAS.
8. Minimum Approach Speed w/ Residual Ice (Flaps 50%)... 88 KIAS
In severe icing conditions, it may not be possible to maintain
altitude or proper glide path on approach; in this case, it is
imperative that a safe airspeed be maintained, the stall warning
system may not function and there may be little or no pre-stall
buffet with heavy ice loads on the wing.
ICING
9. FLAPS ........................................................ MINIMUM REQUIRED

When landing is assured, select the minimum flap setting
required, not to exceed 50%, and maintain extra airspeed
consistent with available field length. Do not retract the flaps once
they have been extended unless required for go-around.
E - 14 P/N 13728-010
February 2013
EMERGENCY
Low Flow Rate Warning
ANTI ICE FLO

a. Repeat operation of windshield pump to verify metering
pumps are primed properly as evidenced by deicing fluid
exiting windshield nozzles.
If warning annunciation extinguishes:
a. Anti-Ice System ........................................................MONITOR
If warning annunciation does not extinguishes or intermittent:
a. PUMP BKUP Switch ........................................................... ON
b. Icing Conditions...................................................AVOID / EXIT
Tank Control Failure Warning
ANTI ICE CTL

Low Fluid Quantity Warning
ANTI ICE QTY

ICING

AOA Probe Overheat Warning
AOA OVERHEAT
1. PITOT HEAT Switch................................................................. OFF

P/N 13728-010 E - 15
February 2013
EMERGENCY
Integrated Avionics System Emergencies

Attitude & Heading Reference System (AHRS) Failure
1. Verify Avionics System has switched to functioning AHRS
If not, manually switch to functioning AHRS and attempt to bring
failed AHRS back on-line:
2. Failed AHRS Circuit Breaker ................................................... SET
If open, reset (close) circuit 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. ADC Circuit Breaker ................................................................ SET
If open, reset (close) circuit breaker. If circuit breaker opens again,
do not reset.
2. Revert to Standby Instruments (Altitude, Airspeed).
PFD Display Failure
1. Display Backup ...............................................................ACTIVATE
AVIONICS
E - 16 P/N 13728-010
February 2013
EMERGENCY
Unusual Attitude Emergencies

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 maintain a constant heading
through the coordinated aileron and rudder inputs.
7. Exit IMC conditions as soon as possible.
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)
Emergency Engine Shutdown On Ground
1. Power Lever ............................................................................ IDLE
2. Fuel Pump (if used) ................................................................. OFF
SPINS AND
3. Mixture.............................................................................. CUTOFF
OTHER

P/N 13728-010 E - 17
February 2013
EMERGENCY
Left/Right Brake Over-Temperature
BRAKE TEMP
1. Stop aircraft and allow the brakes to cool.

Starter Engaged
START ENGAGE
On-Ground
1. Ignition Switch ........................................................... DISENGAGE
2. Battery Switches................Wait 1 minute before next start attempt
If starter does not disengage (relay or solenoid failure):
3. BAT 1 Switch ........................................................................... OFF
4. Engine ....................................................................... SHUTDOWN
In-Flight
1. Ignition Switch ......................................Ensure not stuck in START
3. Flight .............................................................................CONTINUE
Engine start will not be available at destination.
Emergency Ground Egress
1. Engine ....................................................................... SHUTDOWN
2. Seat belts........................................................................RELEASE
3. Airplane .................................................................................. EXIT
OTHER
E - 18 P/N 13728-010
February 2013
CAPS Deployment
• WARNING •
The maximum demonstrated deployment speed is 140 KIAS.
1. Activation Handle Cover .................................................. REMOVE
2. Activation Handle (Both Hands) ............. PULL STRAIGHT DOWN
After Deployment as time permits:
3. Mixture.............................................................................. CUTOFF
5. Fuel Pump ............................................................................... OFF
Turn the Bat-Alt Master Switches off after completing any
necessary radio communications.
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.
CAPS
P/N 13728-010 E - 19
February 2013
Circuit Breaker Panel
AVIONICS
ICE
A/C COND
PROTECTION
STDBY
ALT1 ALT2
ATTD #2
YAW ENGINE
MFD #2
SERVO INSTR
EVS STALL CABIN LIGHTS

CAMERA WARNING / OXYGEN
12V DC ROLL
FUEL QTY
OUTLET TRIM
PITCH
A/C COMPR MFD #1 AP SERVOS
TRIM
CABIN ESSENTIAL KEYPADS

FAN POWER / AP CTRL
AVIONICS CABIN AIR

STARTER BAT 2
FAN 2 CONTROL
AVIONICS GPS NAV GPS NAV

DME / ADF
FAN 1 GIA 2 GIA 1
RECOG AUDIO
COM 2 COM 1
LIGHTS PANEL
NAV AHRS 2/ WEATHER

ADC 1
LIGHTS (ADC 2) / DATA LINK
STROBE
AHRS 1 XPONDER
LIGHTS
PITOT FUEL STDBY

TRAFFIC
HEAT PUMP ATTD #1
FLAPS PFD #2 PFD #1
STALL
VANE HEAT
CB PANEL
SR22_FM07_2949B
E - 20 P/N 13728-010
February 2013

SR22 Checklist

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PILOT’S CHECKLIST

COPYRIGHT © 2013 CIRRUS DESIGN CORPORATION DULUTH, MINNESOTA, USA

P/N 13728-010 N-i

Primary Flight Display

2. Airspeed Indicator 22 GPS TERM 15

3. Horizontal Situation Indicator (HSI)

6. Vertical Deviation Indicator (VDI)

7. Selected Altitude Bug 20 17

N-1 P/N 13728-010

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Airspeeds for Normal Operation

P/N 13728-010 N-2

CIRRUS P ILOT CHEC KL IS T MODEL SR22

CIRRUS P ILOT CHEC KL IS T MODEL SR22

o. Alternate Static Source ............................................. NORMAL

P/N 13728-010 N-4

CIRRUS P ILOT CHEC KL IS T MODEL SR22

e. COM 2 Antenna (underside) ........... Condition and Attachment

N-5 P/N 13728-010

CIRRUS P ILOT CHEC KL IS T MODEL SR22

7. Right Wing Forward and Main Gear

P/N 13728-010 N-6

CIRRUS P ILOT CHEC KL IS T MODEL SR22

f. Spinner............................... Condition, Security, and Oil Leaks

d. External Power ..................................................... Door Secure

N-7 P/N 13728-010

CIRRUS P ILOT CHEC KL IS T MODEL SR22

d. Pitot Probe ..................................................................Very Hot

P/N 13728-010 N-8

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Before Starting Engine

4. Strobe Lights ............................................................................. ON

N-9 P/N 13728-010

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Cold Weather Operation: Starting

CIRRUS P ILOT CHEC KL IS T MODEL SR22

12. Navigation Radios/GPS ..........................................SET for Takeoff

CIRRUS P ILOT CHEC KL IS T MODEL SR22

21. Magnetos.................................................... CHECK Left and Right

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Short Field Takeoff

1. Climb Power............................................................................. SET

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Icing Conditions: In Flight

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Icing Conditions: In Flight

4. Fuel Pump ..............................................................AS REQUIRED

CIRRUS P ILOT CHEC KL IS T MODEL SR22

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Short Field Landing

CIRRUS P ILOT CHEC KL IS T MODEL SR22

CIRRUS P ILOT CHEC KL IS T MODEL SR22

Oxygen Duration (Precise Flight System)

Oxygen System Usage Duration - A5 Flowmeter

P/N 13728-010 P-i