Cirrus DESIGN SR22T User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-003 5-9
Altitude Correction
Alternate 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.
• 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
10 25 40 56 87 114 141 169 205
5000
11 29 47 65 100 133 163 196 238
10000
13 34 55 76 117 155 191 229 277
15000
16 39 64 89 138 182 224 268 325
20000
18 47 76 105 162 215 264 317 384
25000
22 55 90 125 193 255 314 377 457
50%
S.L
25 40 55 69 91
5000 29 46 64 81 106
10000 34 54 75 94 123
100%
S.L 28 42 53 62 71
5000 33 49 62 72 83
10000 38 57 72 84 96
Original Issue

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches