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• Note •
Throughout the walk-around: check all hinges, hinge pins, and
bolts for security; check skin for damage, condition, and
evidence of delamination; check all control surfaces for proper
movement and excessive free play; check area around liquid
reservoirs and lines for evidence of leaking.
In cold weather, remove all frost, ice, or snow from fuselage,
wing, stabilizers and control surfaces. Ensure that control
surfaces are free of internal ice or debris. Check that wheel
fairings are free of snow and ice accumulation. Check that
pitot probe warms within 30 seconds of setting Pitot Heat to
ON.
SR20_FM04_1001
2
4
13
12
11
9 10
8
7
6
5
1
3
Figure 4-1
Walk-Around
March 2010
4-6 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
Preflight Walk-Around
1. Cabin
a. Required Documents................................................ On Board
b. Avionics Power Switch.......................................................OFF
c. Bat 2 Master Switch ........................................................... ON
d. PFD - Serials 1337 and subsequent with PFD.......... Verify On
e. Avionics Cooling Fan ....................................................Audible
f. Voltmeter ................................................................23-25 Volts
g. Flap Position Light ........................................................... OUT
h. Bat 1 Master Switch............................................................ ON
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. Wing/Fuselage Fairing....................................................Check
March 2010
Information Manual 4-7
Cirrus Design Section 4
SR20 Normal Procedures
d. COM 2 Antenna (underside) ...........Condition and Attachment
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
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(26)
