Cirrus SR22T User Manual

P/N 13772-151 21 of 52
Cirrus Design Section 9
SR22T Supplements
8. Left Wing Tip
• WARNING •
Pitot Probe may be HOT.
a. Pitot Probe (underside) .............................. UNOBSTRUCTED
b. Pitot Probe.............................................................. VERY HOT
9. Cabin
a. Fluid Quantity .......................... VERIFY 5 GALLON MINIMUM
b. ICE PROTECT System Switch.......................................... OFF
c. Flaps....................................................................................0%
d. Battery 1 Master Switch ....................................................OFF
e. Avionics Master Switch......................................................OFF
f. Cabin Speaker................................................................... OFF
Ice Formation Determination
Typically, a leading edge with a small radius will collect ice more
quickly than a leading edges with a large radius. To help monitor
possible ice accumulation, a thin metal tab is attached to the outboard
end of the RH and LH stall strips. In some icing conditions this tab may
be the first place that airframe ice accretion is noticeable. Additionally,
refer to other areas of the aircraft, such as the horizontal tail and lower
windscreen, to aid in determining if ice is accreting to the aircraft.
Original Issue: 02-01-13

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