Cirrus DESIGN SR22T Pilot Operating Handbook page 127

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Cirrus Design
SR22T
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
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
P/N 13772-003
Original Issue
• Note •
(Continued on following page)
Section 4
Normal Procedures
4-5

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