P/N 13999-002 Info Manual 5-13
Cirrus Design Section 5
SR20 Performance Data
Altitude Correction
Alternate Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed
• KCAS = Knots Calibrated Airspeed
Conditions: Example:
• Power for level flight or maximum
continuous, whichever is less.
Flaps..............................................0%
Indicated Airspeed..............120 Knots
• Weight ...................................3000 LB Desired Altitude ................. 12,000 FT
• Heater, Defroster, & Vents.............ON Altitude Correction................... -11 FT
Altitude to Fly..................... 11,989 FT
Flaps Press
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L -9 -10 -10 -11 -10 -7 -1 11 27 51
5000 -10 -11 -12 -12 -12 -9 -1 12 32 59
10000 -12 -13 -14 -14 -14 -10 -1 14 37 69
15000 -14 -15 -16 -17 -16 -12 -1 17 44 80
50%
S.L -11 -15 -18 -21 -22 -19
10000 -13 -18 -21 -24 -26 -22
15000 -15 -20 -25 -28 -30 -26
100%
S.L -20 -20 -20 -20 -18
10000 -23 -24 -23 -23 -21
15000 -27 -27 -27 -26 -25
Figure 5-4
September 2011
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