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SR22_FM04_1454
March 2010
Cirrus Design Section 4
SR22 Normal Procedures
Information Manual 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
• 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. 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
(Continued on following page)
March 2010
4-6 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
f. Baggage Door ........................................... Closed and Secure
g. Static Button ..............................................Check for Blockage
h. Parachute Cover ........................................ Sealed and Secure
3. Empennage
a. Tiedown Rope .............................................................Remove
b. Horizontal and Vertical Stabilizers .............................Condition
• Note •
Verify tape covering the forward and aft inspection holes
located on outboard ends of horizontal stabilizer is installed
and securely attached.
c. Elevator and Tab...............................Condition and Movement
d. Rudder..................................................Freedom of Movement
e. Rudder Trim Tab ...................................Condition and Security
f. Attachment hinges, bolts and cotter pins...................... Secure
4. Right Fuselage
a. Static Button ..............................................Check for Blockage
b. Wing/Fuselage Fairings..................................................Check
c. Door Lock ......................................................................Unlock
5. Right Wing Trailing Edge
a. Flap and Rub Strips (if installed) ..........Condition and Security
b. Aileron and Tab.................................Condition and Movement
c. Aileron Gap Seal .........................................................Security
d. Hinges, actuation arm, bolts, and cotter pins ............... Secure
6. Right Wing Tip
a. Tip...........................................................................Attachment
b. Strobe, Nav Light and Lens ..................Condition and Security
c. Fuel Vent (underside) ......................................... Unobstructed
7. Right Wing Forward and Main Gear
a. Leading Edge and Stall Strips ...................................Condition
b. Fuel Cap .......................................Check Quantity and Secure
c. Fuel Drains (2 underside) ............................Drain and Sample
d. Wheel Fairings...................... Security, Accumulation of Debris
March 2010
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(30)
