Cirrus SR22T User Manual

Cirrus Design Section 9
SR22 / SR22T Supplements
P/N 13772-135 23 of 30
Roll Protection Limits:
Engagement Limit:.....................................................................45°
Maximum Stick Force attained at...............................................50°
Disengagement Threshold (Zero Stick Force) ...........................30°
High Pitch Protection Limits
Engagement Limit:................................................................+17.5°
Maximum Stick Force attained at:.........................................+22.5°
Disengagement Threshold (Zero Stick Force): .....................+12.5°
Always Protected
Only Protected after cross-
ing turn-on threshold
Bank Angle
0° 30° 45° 60° 75° 90°15°
Wings Level Supplemental Stick Force
SR22_FM09_3399
Nose Up Pitch Angle
0° 10° 15° 20° 25° 5°
Nose Down Supplemental Stick Force
Always Protected
Only Protected after cross-
ing turn-on threshold
SR22_FM09_3403
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