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Cirrus SR22 - Page 119

Cirrus SR22
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Cirrus Design Section 4
SR22 Normal Procedures
P/N 13772-004 4-5P/N 13772-004 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. Lights............................................................. Check Operation
j. Stall Warning .....................................................................Test
• Note •
Test stall warning system by applying suction to the stall
warning system inlet and noting the warning horn sounds.
k. Fuel Quantity .................................................................Check
l. Fuel Selector ..............................................Select Fullest Tank
m. Flaps.....................................................100%, Check Light ON
n. Bat 1 and 2 Master Switches.............................................OFF
o. Alternate Static Source..............................................NORMAL
p. Circuit Breakers.................................................................... IN
q. Fire Extinguisher ................................. Charged and Available
r. Emergency Egress Hammer ......................................Available
s. 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
f. Baggage Door ........................................... Closed and Secure
g. Static Button.............................................. Check for Blockage
h. Parachute Cover........................................ Sealed and Secure
(Continued on following page)
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