Cirrus SR22T User Manual

Cirrus Design Section 9
SR22 / SR22T Supplements
P/N 13772-135 3 of 30
6. The Autopilot may not be engaged beyond the Engagement
Limits. If the Autopilot is engaged beyond the command limits (up
to engagement limits) it will be rolled or pitched to within the
command limits and an altitude loss of 1000 feet or more can be
expected while attitude is established in the selected mode.
7. The Autopilot and Flight Director will not command pitch or roll
beyond the Command Limits.
8. Use of VNAV is not supported during an approach with a teardrop
course reversal. VNAV will be disabled at the beginning of the
teardrop.
9. For aircraft with optional USP, If Stall Warning is inoperative,
Autopilot Underspeed Protection will not be provided in Altitude
Critical Modes (ALT, GS, GP, TO and GA)
Axis Autopilot Engagement Limit
Pitch ± 30°
Roll ± 75°
Axis Autopilot Command Limit
FD Pitch Command Limits +20°, -15°
FD Roll Command Limits ± 25°
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