Cirrus SR22T User Manual

Cirrus Design Section 3A
SR22T Abnormal Procedures
P/N 13772-005 3A-19P/N 13772-005 3A-19
Flight Control System
Electric Trim/Autopilot Failure
1. Airplane Control..........................................MAINTAIN MANUALLY
2. Autopilot (if engaged).................................................DISENGAGE
If Problem Is Not Corrected:
3. Circuit Breakers ........................................... PULL AS REQUIRED
•PITCH TRIM
•ROLL TRIM
•YAW SERVO
•AP SERVOS
4. Power Lever ........................................................... AS REQUIRED
5. Control Yoke..................................MANUALLY HOLD PRESSURE
6. Land as soon as practical.
Amplification
Any failure or malfunction of the electric trim or autopilot can be over-
ridden by use of the control yoke. If runaway trim is the problem, de-
energize the circuit by pulling the appropriate circuit breakers and land
as soon as conditions permit.
Flap System Exceedance
FLAPS Caution
1. Airspeed...........................................................................REDUCE
or
1. Flaps .............................................................................. RETRACT
Amplification
Flaps are extended beyond airspeed limitations.
Flaps at 100%, airspeed greater than 115 KIAS for 5 seconds or more,
OR
Flaps at 50%, airspeed greater than 155 KIAS for 5 seconds or more.
FLAPS
Original Issue

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