• 热门标签

当前位置: 主页 > 航空资料 > 飞行资料 >

时间:2010-10-20 17:01来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Cirrus Design Section 4
SR22 Normal Procedures
Information Manual 4-7
e. Tire ............................................Condition, Inflation, and Wear
• Caution •
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 Orings
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. Vortex Generator .......................................................Condition
b. Cowling.....................................................Attachments Secure
c. Exhaust Pipe ....................Condition, Security, and Clearance
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.
a. Tow Bar .......................................................Remove and Stow
b. Strut...........................................................................Condition
c. Wheel Fairing ....................... Security, Accumulation of Debris
d. Wheel and Tire ..........................Condition, Inflation, and Wear
e. Propeller ........................... Condition (indentations, nicks, etc.)
f. Spinner ............................... Condition, Security, and Oil Leaks
g. Air Inlets ..............................................................Unobstructed
h. Alternator...................................................................Condition
10. Nose, Left Side
a. Landing Light.............................................................Condition
b. Engine Oil.........Check 6-8 quarts, Leaks, Cap & Door Secure
c. Cowling.....................................................Attachments Secure
(Continued on following page)
March 2010
4-8 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
d. External Power .....................................................Door Secure
e. Vortex Generator .......................................................Condition
f. Exhaust Pipe(s) .................Condition, Security, and Clearance
11. Left Main Gear and Forward Wing
a. Wheel fairings....................... Security, Accumulation of Debris
b. Tire ............................................Condition, Inflation, and Wear
• Caution •
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 Orings
replaced.
c. Wheel and Brakes ....... Fluid Leaks, Evidence of Overheating,
General Condition, and Security.
d. Chocks and Tiedown Ropes........................................Remove
e. Fuel Drains (2 underside) ............................Drain and Sample
f. Cabin Air Vent..................................................... Unobstructed
g. Fuel Cap .......................................Check Quantity and Secure
h. Leading Edge and Stall Strips ...................................Condition
12. Left Wing Tip
a. Fuel Vent (underside) ......................................... Unobstructed
b. Pitot Mast (underside) .................Cover Removed, Tube Clear
c. Strobe, Nav Light and Lens ..................Condition and Security
d. Tip ..........................................................................Attachment
13. Left Wing Trailing Edge
a. Flap And Rub Strips (If installed)..........Condition and Security
b. Aileron ..................................................Freedom of movement
c. Aileron Gap Seal .........................................................Security
d. Hinges, actuation arm, bolts, and cotter pins ............... Secure
March 2010
Cirrus Design Section 4
SR22 Normal Procedures
Information Manual 4-9
Before Starting Engine
1. Preflight Inspection ...................................................COMPLETED
• WARNING •
Ensure that the airplane is properly loaded and within the
AFM’s weight and balance limitations prior to takeoff.
2. Weight and Balance............................................Verify within limits
3. Emergency Equipment ................................................ON BOARD
4. Passengers ..................................................................... BRIEFED
• Note •
Ensure all the passengers have been fully briefed on smoking,
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(31)