Cirrus System 55X Autopilot User Manual

5-8 P/N 13772-005
Section 5 Cirrus Design
Performance Data SR22T
Altitude Correction
Alternate 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.
•Heater, Defroster, & Vents..................................................................................ON
Flaps Density
Alt
CORRECTION TO BE ADDED - FEET
Alternate Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L
481421406494127164
5000
41016254775109148191
10000
51119295587127172222
15000
613233464102149202261
20000
715274076121176239308
25000
818324890144209284366
50%
S.L
-10 -4 4 11 29 50 80
5000 -12 -4 4 13 33 58 93
10000 -14 -5 5 15 39 68 108
100%
S.L -2 -9 -2 6 15 39
5000 -2 -11 -2 7 17 45
10000 -3 -13 -3 8 20 53
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English