Cirrus DESIGN SR22T User Manual

3A-12 P/N 13772-003
Section 3A Cirrus Design
Abnormal Procedures SR22T
Low Alternator 1 Output
ALT 1 Caution (Failure)
1. ALT 1 Circuit Breaker ..............................................CHECK & SET
2. ALT 1 Master Switch ........................................................... CYCLE
If alternator does not reset (low A1 Current and M1 voltage):
3. ALT 1 Master Switch ................................................................OFF
4. Non-Essential Bus Loads.................................................REDUCE
a. If flight conditions permit, consider shedding the following to
preserve Battery 1:
(1) Air Conditioning,
(2) Landing Light,
(3) Yaw Servo,
(4) Convenience Power (aux items plugged into armrest jack)
5. Continue Flight, avoiding IMC or night flight as able (reduced
power redundancy).
Amplification
• Caution •
Dependant on Battery 1 state (indicated by M1 voltage),
landing light may be weak or inoperative for landing.
Alternator 1 output is low, indicative of alternator failure; will typically
be associated with low M1 voltage, Battery 1 discharge and M BUS 1
Caution message.
ALT 1
Revision 1

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches