Cirrus DESIGN SR20 Information Manual

5-12 P/N 13999-002 Info Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-3
Altitude Correction
Normal 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 ........................................... 50%
Indicated Airspeed ............... 85 Knots
• Weight .................................. 3000 LB Desired Altitude..................12,000 FT
Altitude Correction .....................-7 FT
Altitude to Fly .....................11,993 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 -12-11-10-9-8-5-3-3-5-10
5000 -14 -13 -12 -11 -9 -6 -4 -3 -5 -11
10000 -16 -15 -14 -12 -11 -7 -4 -4 -6 -13
15000 -19 -18 -16 -14 -12 -8 -5 -4 -7 -16
50%
S.L -2 -4 -5 -6 -5 +2
10000 -2 -4 -6 -7 -6 +2
15000 -2 -5 -7 -8 -7 +2
100%
S.L -1 -4 -6 -7 -5
10000 -1 -5 -7 -8 -6
15000 -1 -6 -9 -9 -6
September 2011

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English