Cirrus System 55X Autopilot User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-7P/N 13772-005 5-7
Altitude Correction
Normal Static Source: Standby Altimeter
• 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
12 9 5 0 -11 -24 -38 -50 -61
5000
14 10 6 0 -13 -28 -44 -58 -71
10000
16 12 7 0 -16 -33 -51 -68 -82
15000
19 14 8 0 -18 -39 -60 -80 -97
20000
23 17 9 0 -21 -46 -71 -95 -114
25000
27 20 11 0 -26 -55 -85 -112 -136
50%
S.L
21 0 -14 -21 -30 -46 -66
5000 24 0 -16 -25 -35 -54 -77
10000 28 0 -18 -29 -41 -63 -90
100%
S.L 22 6 -1 -9 -19 -30
5000 25 7 -1 -10 -22 -34
10000 29 8 -2 -12 -25 -40
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English