Cirrus SR20 - Airspeeds for Normal Operation

Cirrus Design Section 4
SR20 Normal Procedures
P/N 21399-004 4-3P/N 21399-004 4-3
Introduction
This section provides amplified procedures for normal operation.
Normal procedures associated with optional systems can be found in
Section 9: Log of Supplements.
Airspeeds for Normal Operation
Unless otherwise noted, the following speeds are based on a
maximum weight of 3050 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% ....................................................65-70 KIAS
• Short Field, Flaps 50% ...................................................65 KIAS
• Obstacle Clearance, Flaps 50% .....................................77 KIAS
Enroute Climb, Flaps Up:
• Normal, SL......................................................................96 KIAS
• Normal, 10,000’ ..............................................................92 KIAS
• Best Rate of Climb, SL ...................................................96 KIAS
• Best Rate of Climb, 10,000’............................................92 KIAS
• Best Angle of Climb, SL..................................................83 KIAS
• Best Angle of Climb, 10,000’ ..........................................87 KIAS
Landing Approach:
• Normal Approach, Flaps Up ...........................................88 KIAS
• Normal Approach, Flaps 50%.........................................83 KIAS
• Normal Approach, Flaps 100%.......................................78 KIAS
• Short Field, Flaps 100% .................................................78 KIAS
Go-Around, Flaps 50%:
• Full Power.......................................................................78 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3050 Lb.........................................................................131 KIAS
• 2600 Lb.........................................................................122 KIAS
• 2200 Lb......................................................................... 111 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing .........................................................20 Knots
Revision A1