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Target
Fuel Flow
Pressure
Altitude
Target
Fuel Flow
Pressure
Altitude
Target Fuel
Flow
0 27.1 7000 21.4 14,000 17.5
1000 26.2 8000 20.5 15,000 16.9
2000 25.1 9000 19.9 16,000 16.7
3000 24.3 10,000 19.5 17,000 16.2
4000 23.6 11,000 18.8 17,500 16.1
5000 22.8 12,000 18.4
6000 22.1 13,000 17.9
June 2007
Information Manual 4-17
Cirrus Design Section 4
SR22 Normal Procedures
Takeoff
Power Check: Check full-throttle engine operation early in takeoff run.
The engine should run smoothly and turn approximately 2700 RPM.
All engine parameters should read in the green. Discontinue takeoff at
any sign of rough operation or sluggish acceleration. Make a thorough
full-throttle static runup before attempting another takeoff.
For takeoff over a gravel surface, advance Power Lever slowly. This
allows the airplane to start rolling before high RPM is developed, and
gravel will be blown behind the propeller rather than pulled into it.
Flap Settings: Normal and short field takeoffs are accomplished with
flaps set at 50%. Takeoffs using 0% are permissible, however, no
performance data is available for takeoffs in the flaps up configuration.
Takeoffs with 100% flaps are not approved.
Soft or rough field takeoffs are performed with 50% flaps by lifting the
airplane off the ground as soon as practical in a tail-low attitude. If no
obstacles are ahead, the airplane should be leveled off immediately to
accelerate to a higher climb speed.
Takeoffs into strong crosswinds normally are performed with the
minimum flap setting (0% or 50%) necessary for the field length, to
minimize the drift angle immediately after takeoff. With the ailerons
partially deflected into the wind, accelerate the airplane to a speed
slightly higher than normal, and then with authority, rotate to prevent
possibly settling back to the runway while drifting. When clear of the
ground, make a coordinated turn into the wind to correct for drift.
• Note •
Fuel BOOST should be left ON during takeoff and for climb as
required for vapor suppression with hot or warm fuel.
Normal Takeoff
1. Brakes....................................RELEASE (Steer with Rudder Only)
2. Power Lever ........................................................FULL FORWARD
3. Engine Parameters ............................................................ CHECK
4. Elevator Control ........................ ROTATE Smoothly at 70-73 KIAS
5. At 80 KIAS, Flaps.......................................................................UP
June 2007
4-18 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Short Field Takeoff
1. Flaps ........................................................................................50%
2. Brakes ..................................................................................HOLD
3. Power Lever ........................................................FULL FORWARD
4. Mixture .....................................................................................SET
5. Engine Parameters ............................................................ CHECK
6. Brakes ....................................RELEASE (Steer with Rudder Only)
7. Elevator Control ............................. ROTATE Smoothly at 70 KIAS
8. Airspeed at Obstacle..........................................................78 KIAS
Climb
Normal climbs are performed flaps UP (0%) and full power at speeds 5
to 10 knots higher than best rate-of-climb speeds. These higher
speeds give the best combination of performance, visibility and engine
cooling.
For maximum rate of climb, use the best rate-of-climb speeds shown
in the rate-of-climb chart in Section 5. If an obstruction dictates the use
of a steep climb angle, the best angle-of-climb speed should be used.
Climbs at speeds lower than the best rate-of-climb speed should be of
short duration to avoid engine-cooling problems.
1. Climb Power .............................................................................SET
2. Flaps ................................................................................Verify UP
3. Mixture ..............................................LEAN as required for altitude
4. Engine Parameters ............................................................ CHECK
5. Fuel Pump................................................................................OFF
• Note •
The Fuel Pump may be used for vapor suppression during
climb. Fuel BOOST should be left ON above 6000 feet
pressure altitude if takeoff was made with hot or warm fuel.
June 2007
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(30)
