Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-9P/N 13772-005 2-9
Fuel
* Dynamically changes based on engine parameters.
Electrical
Instrument
(Range & Units)
Red
Arc/Bar
Yellow Arc/
Bar
Green Arc/
Bar
Yellow Arc/
Bar
Red
Arc/Bar
Minimum Minimum
Caution
Range
Normal
Range
Maximum
Caution
Range
Maximum
Fuel Flow
(0 – 45 U.S. Gal./Hr.)
–– –– *See Note –– ––
Fuel Totalizer
(U.S. Gallon)
N < 9
FUEL QTY
9 – 18 > 18 –– ––
Fuel Quantity Gage
(0 – 46 U.S. Gallon)
010 – 1414 – 46–– ––
Instrument
(Range & Units)
Red
Arc/Bar
Yellow
Arc/Bar
Green Arc/
Bar
Yellow
Arc/Bar
Red
Arc/Bar
Minimum Minimum
Caution
Range
Normal
Range
Maximum
Caution
Range
Maximum
Essential Bus Volts
(0 – 36 Volts)
0 – 24.4
ESS BUS
–– 24.5 – 32 –– > 32
ESS BUS
Main Bus 1 Voltage
(0 – 36 Volts)
–– 0 – 24.4
M BUS 1
24.5 – 32 –– > 32
M BUS 1
Main Bus 2 Voltage
(0 – 36 Volts)
–– 0 – 24.4
M BUS 2
24.5 – 32 –– > 32
M BUS 2
Alternator 1 Current
(0 – 100 Amps)
–– –– 2 – 100 0 – 1
ALT 1
––
Alternator 2 Current
(0 – 100 Amps)
–– –– 2 – 100 0 – 1
ALT 2
––
Battery 1 Current
(-59 to 59 Amps)
–– –– -4 – 59 -59 to -5
BATT 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