Altitude Correction; Normal Static Source - Cirrus DESIGN SR20 Information Manual

Section 5
Performance Data
Conditions:
• Power for level flight or maximum
continuous, whichever is less.
• Weight .................................. 3000 LB
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed
• KCAS = Knots Calibrated Airspeed
Flaps Press
Alt
S.L
5000
0%
10000
15000
S.L
50% 10000
15000
S.L
100% 10000
15000
5-12

Altitude Correction

Normal Static Source

• Note •
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80
-12 -11 -10
-14 -13 -12
-16 -15 -14
-19 -18 -16
-2 -4 -5
-2 -4 -6
-2 -5 -7
-1 -4 -6
-1 -5 -7
-1 -6 -9
Figure 5-3
Example:
Flaps ........................................... 50%
Indicated Airspeed ............... 85 Knots
Desired Altitude.................. 12,000 FT
Altitude Correction .....................-7 FT
Altitude to Fly ..................... 11,993 FT
90 100 120
-9 -8 -5
-11 -9 -6
-12 -11 -7
-14 -12 -8
-6 -5 +2
-7 -6 +2
-8 -7 +2
-7 -5
-8 -6
-9 -6
P/N 13999-002 Info Manual
Cirrus Design
140 160 180
-3 -3 -5
-4 -3 -5
-4 -4 -6
-5 -4 -7
September 2011
SR20
200
-10
-11
-13
-16