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Fuel Conservation.........................................................................4-29
June 2007
4-2 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Intentionally Left Blank
June 2007
Information Manual 4-3
Cirrus Design Section 4
SR22 Normal Procedures
Introduction
This section provides amplified procedures for normal operation.
Normal procedures associated with optional systems can be found in
Section 9.
June 2007
4-4 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Airspeeds for Normal Operation
Unless otherwise noted, the following speeds are based on a
maximum weight of 3400 lb. and may be used for any lesser weight.
However, to achieve the performance specified in Section 5 for takeoff
and landing distance, the speed appropriate to the particular weight
must be used.
Takeoff Rotation:
• Normal, Flaps 50%........................................................70 KIAS
• Obstacle Clearance, Flaps 50%....................................78 KIAS
Enroute Climb, Flaps Up:
• Normal ................................................................. 110-120 KIAS
• Best Rate of Climb, SL ................................................101 KIAS
• Best Rate of Climb, 10,000............................................95 KIAS
• Best Angle of Climb, SL.................................................78 KIAS
• Best Angle of Climb, 10,000 ..........................................82 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) ....................................77 KIAS
Go-Around, Flaps 50%:
• Full Power......................................................................80 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3400 lb.........................................................................133 KIAS
• 2900 lb.........................................................................123 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing ........................................................20 Knots
June 2007
Information Manual 4-5
Cirrus Design Section 4
SR22 Normal Procedures
Normal Procedures
Preflight Inspection
Before carrying out preflight inspections, ensure that all required
maintenance has been accomplished. Review your flight plan and
compute weight and balance.
• Note •
Throughout the walk-around: check all hinges, hinge pins, and
bolts for security; check skin for damage, condition, and
evidence of delamination; check all control surfaces for proper
movement and excessive free play; check area around liquid
reservoirs and lines for evidence of leaking.
In cold weather, remove all frost, ice, or snow from fuselage,
wing, stabilizers and control surfaces. Ensure that control
surfaces are free of internal ice or debris. Check that wheel
fairings are free of snow and ice accumulation. Check that
pitot probe warms within 30 seconds of setting Pitot Heat to
ON.
3
1
5
6
7
8
9 10
11
12
13
4
2
SR22_FM04_1454
Figure 4-1
Walk-Around
June 2007
4-6 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Preflight Walk-Around
1. Cabin
a. Required Documents................................................ On Board
b. Avionics Power Switch.......................................................OFF
c. Bat 2 Master Switch ........................................................... ON
d. PFD - Serials 0435 and subsequent with PFD.......... Verify On
e. Avionics Cooling Fan ....................................................Audible
f. Voltmeter ................................................................23-25 Volts
g. Flap Position Light ........................................................... OUT
h. Bat 1 Master Switch............................................................ ON
i. Lights .............................................................Check Operation
j. Stall Warning .................................................................... Test
• Note •
Test stall warning system by applying suction to the stall
warning system inlet and noting the warning horn sounds.
k. Fuel Quantity .................................................................Check
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(25)
