Cirrus SR22T User Manual

Cirrus Design Section 4
SR22T Normal Procedures
P/N 13772-005 4-5P/N 13772-005 4-5
c. Bat 2 Master Switch ...........................................................ON
d. PFD ........................................................................... Verify On
e. Essential Bus Voltage............................................. 23-25 Volts
f. Flap Position Light ........................................................... OUT
g. Bat 1 Master Switch ............................................................ON
h. Avionics Cooling Fan.................................................... Audible
i. Oxygen Masks/Cannulas and Hoses .............Check Condition
j. Oxygen System ...................................................................ON
(1) Quantity........Verify adequate supply for flight with reserve
(2) Flow ................................... Check flowmeter on all masks
(3) Oxygen System...........................................................OFF
k. Lights............................................................. Check Operation
l. Stall Warning .....................................................................Test
• Note •
Test stall warning system by applying suction to the stall
warning system inlet and noting the warning horn sounds.
m. Fuel Quantity .................................................................Check
n. Fuel Selector ..............................................Select Fullest Tank
o. Flaps.....................................................100%, Check Light ON
p. Bat 1 and 2 Master Switches............................................. OFF
q. Circuit Breakers.................................................................... IN
r. Fire Extinguisher ................................. Charged and Available
s. Emergency Egress Hammer ......................................Available
t. CAPS Handle .....................................................Pin Removed
2. Left Fuselage
a. Door Lock ...................................................................... Unlock
b. COM 1 Antenna (top) ......................Condition and Attachment
c. Transponder Antenna (underside)...Condition and Attachment
d. Wing/Fuselage Fairing....................................................Check
e. COM 2 Antenna (underside) ...........Condition and Attachment
(Continued on following page)
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