曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

maintenance has been accomplished. Review your flight plan and
compute weight and balance.
• 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.
3
1
5
6
7
8
9 10
11
12
13
4
2
SR22_FM04_1454
Figure 4-1
Walk-Around
Revision A5
4-6 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
Preflight Walk-Around
1. Cabin
a. Required Documents................................................ On Board
b. Avionics Power Switch.......................................................OFF
c. Bat 2 Master Switch ........................................................... ON
d. PFD - Serials 0435 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
Revision A8
P/N 13772-001 4-7
Cirrus Design Section 4
SR22 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. Aileron Gap Seal .........................................................Security
d. Hinges, actuation arm, bolts, and cotter pins ................Secure
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：CIRRUS DESIGN SR22西銳22飛行員操作手冊和飛機飛行手冊(30)