Cirrus SR22T User Manual

Cirrus Design Section 9
SR22 / SR22T Supplements
P/N 13772-135 25 of 30
High Airspeed Protection Limits - Below 17,500 ft PA
Engagement Limit:...........................................................200 KIAS
Maximum Stick Force attained at:....................................205 KIAS
Disengagement Threshold (Zero Stick Force) .................190 KIAS
High Airspeed Protection Limits - Above 17,500 ft PA
Engagement Limit:....................................................... Mach 0.419
Maximum Stick Force attained at:................................ Mach 0.430
Disengagement Threshold (Zero Stick Force) ............. Mach 0.399
205
Indicated Airspeed (KIAS)
180 190 195 200 210185
Nose Up Supplemental Stick Force
Always Protected
Only Protected after cross-
ing turn-on threshold
SR22_FM09_3405
Always Protected
Only Protected after cross-
ing turn-on threshold
0.4 0.41 0.42
Mach Number
0.395 0.415 0.425 0.43 0.4350.405
Nose Up Supplemental Stick Force
SR22_FM09_3428
Revision 03: 12-14-10

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots