Cirrus SR22T User Manual

24 of 30 P/N 13772-135
Section 9 Cirrus Design
Supplements SR22 / SR22T
Low Pitch Protection Limits
Engagement Limit: ................................................................ -15.5°
Maximum Stick Force attained at:......................................... -20.5°
Disengagement Threshold (Zero Stick Force) ...................... -10.5°
High Airspeed Mode
To protect against an overspeed condition, the High Airspeed Mode
uses engagement limits, thresholds, and stick forces similar to those
used for the pitch and roll modes, but is instead triggered by airspeed
and controlled by pitch attitude. When the aircraft reaches the ESP
engagement limit, the system commands the pitch servo to apply a
supplemental stick force back toward the nominal airspeed range.
• Note •
For turbocharged equipped aircraft, V
ne
reduces above
17,500 ft PA to follow a Mach limit of 0.42.
At high altitudes Mach number determines the threshold.
Nose Down Pitch Angle
-0° -10° -15° -20° -25° -5°
Nose Up Supplemental Stick Force
Always Protected
Only Protected after cross-
ing turn-on threshold
SR22_FM09_3426
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