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Before Starting Engine...............................................................4-10
Starting Engine ..........................................................................4-11
Before Taxiing............................................................................4-13
Taxiing .......................................................................................4-13
Before Takeoff ...........................................................................4-14
Maximum Power Fuel Flow .......................................................4-16
Takeoff.......................................................................................4-17
Normal Takeoff ..........................................................................4-17
Short Field Takeoff ....................................................................4-18
Climb..........................................................................................4-18
Cruise ........................................................................................4-19
Cruise Leaning...........................................................................4-20
Descent......................................................................................4-20
Before Landing ..........................................................................4-20
Landing ......................................................................................4-21
Balked Landing/Go-Around .......................................................4-22
After Landing .............................................................................4-22
Shutdown...................................................................................4-23
Stalls ..........................................................................................4-24
Environmental Considerations ......................................................4-25
Cold Weather Operation ............................................................4-25
Hot Weather Operation..............................................................4-27
Noise Characteristics/Abatement..................................................4-28
Fuel Conservation.........................................................................4-29
Revision A7
4-2 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
Intentionally Left Blank
Revision A7
P/N 13772-001 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.
Revision A5
4-4 P/N 13772-001
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
Revision A5
P/N 13772-001 4-5
Cirrus Design Section 4
SR22 Normal Procedures
Normal Procedures
Preflight Inspection
Before carrying out preflight inspections, ensure that all required
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(29)
