Cirrus DESIGN SR20 - Page 113

Cirrus Design Section 4
SR20 Normal Procedures
P/N 11934-004 4-5
1. Cabin
a. Required Documents.................................................On Board
b. Avionics Power Switch.......................................................OFF
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
k. Fuel Quantity .................................................................Check
l. Fuel Selector ..............................................Select Fullest Tank
m. Flaps.....................................................100%, Check Light ON
n. Oil Annunciator.................................................................... On
o. Bat 1 and 2 Master Switches.............................................OFF
p. Alternate Static Source..............................................NORMAL
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
f. Baggage Door ........................................... Closed and Secure
g. Static Button.............................................. Check for Blockage
h. Parachute Cover........................................ Sealed and Secure
(Continued on following page)
Revision 1