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• Note •
Test stall warning system by applying suction to the stall
warning system inlet and noting the warning horn sounds.
j. Fuel Quantity .................................................................Check
k. Fuel Selector ..............................................Select Fullest Tank
l. Flaps.................................................... 100%, Check Light ON
m. Oil Annunciator .................................................................... 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. Wing/Fuselage Fairing....................................................Check
d. COM 2 Antenna (underside)........... Condition and Attachment
March 2010
Information Manual 4-7
Cirrus Design Section 4
SR20 Normal Procedures
e. Baggage Door ........................................... Closed and Secure
f. Static Button ..............................................Check for Blockage
g. 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. 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
(Continued on following page)
March 2010
4-8 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
c. Fuel Drains (2 underside) ............................Drain and Sample
d. Wheel Fairings...................... Security, Accumulation of Debris
e. Tire ............................................Condition, Inflation, and Wear
• Note •
Serials 1005 through 1592 after Service Bulletin SB 2X-32-14
and airplane serials 1593 and subsequent: Clean and inspect
temperature indicator installed to piston housing. If indicator
center is black, the brake assembly has been overheated. The
brake linings must be inspected and O-rings replaced.
f. Wheel and Brakes ....... Fluid Leaks, Evidence of Overheating,
General Condition, and Security.
g. Chocks and Tiedown Ropes........................................Remove
h. Cabin Air Vent..................................................... Unobstructed
8. Nose, Right Side
a. Cowling.................................................... Attachments Secure
b. Exhaust Pipe ....................Condition, Security, and Clearance
c. Transponder Antenna (underside) .. Condition and Attachment
d. Gascolator (underside) ............. Drain for 3 seconds, SAMPLE
9. Nose gear, Propeller, and Spinner
• WARNING •
Keep clear of propeller rotation plane. Do not allow others to
approach propeller.
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 1148-126(25)
