Cirrus SR22T User Manual

2-8 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Engine Instrument Markings & Annunciations
The following describes the engine instrument markings. Associated
Warning and Caution Annunciations are shown in capitalized text.
PowerPlant
Instrument
(Range & Units)
Red
Arc/Bar
Yellow
Arc/Bar
Green
Arc/Bar
Yellow
Arc/Bar
Red
Arc/Bar
Lower
Warning
Range
Minimum
Caution
Range
Normal
Range
Maximum
Caution
Range
Upper
Warning
Range
Cylinder Head
Temp erat ur e
(100°F – 500°F)
–– –– 240 – 420 420 – 460
CHT
> 460
CHT
Engine Speed
(0 – 3000 RPM)
–– –– 500 – 2550 –– > 2550
RPM
Exhaust Gas
Temp erat ur e
(1000°F – 1800°F)
–– –– 1000–1800 –– ––
Manifold Pressure
(10 – 40 in.Hg)
–– –– 15.0 - 36.5 36.5 - 37.5 37.5 - 40.0
Oil Pressure
(0 – 100 PSI)
0 – 10 10 – 30
OIL
PRESS
30 – 60 60 – 100 > 100
OIL
PRESS
Oil Temperature
(75°F – 250°F)
–– –– 100 – 240 –– > 240
OIL TEMP
Percent Power
(0 – 100%)
–– –– 0 – 100 –– ––
Turbo ch ar ge r Inl et
Temp erat ur e
(1000°F - 1800°F)
–– –– 1000 –
1750
–– 1750 -1800
TIT
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