Cirrus SR22T User Manual

Cirrus Design Section 3A
SR22T Abnormal Procedures
P/N 13772-005 3A-13P/N 13772-005 3A-13
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
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