Cirrus System 55X Autopilot User Manual

5-6 P/N 13772-005
Section 5 Cirrus Design
Performance Data SR22T
Altitude Correction
Normal Static Source: Primary Flight Display
• Note •
Add correction to desired altitude to obtain indicated altitude to fly.
Indicated airspeed values assume zero instrument error.
KIAS: Knots Indicated Airspeed.
Conditions:
•Power for level flight or maximum continuous, whichever is less.
•3600 LB
Flaps Density
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L
000000000
5000
000000000
10000
000000000
15000
000000000
20000
000000000
25000
000000000
50%
S.L
9-9-19-22-19-22-28
5000 10 -10 -22 -25 -22 -25 -33
10000 12 -12 -25 -29 -25 -30 -38
100%
S.L 22 -6 -10 -14 -19 -18
5000 25 -7 -12 -16 -22 -21
10000 29 -9 -14 -18 -25 -25
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English