Cirrus SR22T User Manual

P/N 13772-143 3 of 6
Cirrus Design Section 9
SR22 / SR22T Supplements
Section 3 - Emergency Procedures
Aircraft Serials with Avidyne PFD/MFD Avionics
ALT 1 Failure (Alt 1 Light Steady)
Steady illumination indicates failure of alternator 1. Attempt to restore
alternator. If alternator cannot be restored, it will be necessary to divert
the flight to land within one hour.
Loads on Main Buses, Non-essential Buses, and Air-conditioning
Buses must be reduced and available equipment on these buses
managed as necessary for flight conditions. Equipment essential for
continued safe flight and landing will be powered by Alternator 2 and
Battery 2 through the Essential Buses. However, depending upon
flight conditions, additional equipment is required.
For 14 CFR 135 Operations, the load shedding and equipment
management in the following procedure will provide at least one-hour
operating time on aircraft with a fully charged, 13.6 amp-hour battery
(available from Cirrus Design Spare Parts Sales) in good condition for
equipment required for emergency operation under 14 CFR 135.163(f)
and meets the requirements of that paragraph.
• Note •
Circuit breakers that “PULL” should only be pulled and not
reset.
1. ALT 1 Master Switch ................................................................OFF
2. Alternator 1 Circuit Breaker .................................Check and Reset
3. ALT 1 Master Switch ..................................................................ON
If alternator does not reset
4. ALT 1 Master Switch ................................................................OFF
5. Notify ATC of Alternator Failure and that transponder may be
switched off depending upon flight conditions.
6. Autopilot ...........................................................................ENGAGE
Use of autopilot will reduce work load and provide trim function.
Expect a slight pitch change when autopilot is disengaged.
7. NAV Lights .................................................................................ON
Continued on following page.
Revision 02: 01-06-10

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