Cirrus DESIGN SR22T User Manual

Cirrus Design Section 4
SR22T Normal Procedures
P/N 13772-003 4-5
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. Oil Annunciator.................................................................... On
q. Bat 1 and 2 Master Switches.............................................OFF
r. Circuit Breakers.................................................................... IN
s. Fire Extinguisher ................................. Charged and Available
t. Emergency Egress Hammer ......................................Available
u. 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 DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches