• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 18:01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

 (a)
 Apply a coat of the primer. Let it dry for not less than 2 hours and not more than 3 hours.

 (b)
 Apply a coat of the undercoat. Let it dry for not less that 3 hours and not more than 4 hours.

 (c)
 Apply a coat of the top-coat. Let it dry for 24 hours before you touch it.


 NOTE : The paint must dry for 7 days until it becomes resistant
____ to Skydrol.
 1EFF : ALL 1 32-40-00Page 704 1 1 Feb 01/98 1 1 1CES 1 WHEELS - DESCRIPTION AND OPERATION


__________________________________
 1. Component Location
__________________
 A. Main Gear Wheels
 (Ref. Fig. 001)

 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
 | | | | DOOR | REF. -------------------------------------------------------------------------------2649GM WHEEL-MLG, 2 731 32-41-11 2650GM WHEEL-MLG, 4 741 32-41-11 2651GM WHEEL-MLG, 1 731 32-41-11 2652GM WHEEL-MLG, 3 741 32-41-11
 B. Nose Gear Wheels
 (Ref. Fig. 002)

 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
 | | | | DOOR | REF. -------------------------------------------------------------------------------2659GM WHEEL-NLG, 9 711 32-41-12 2660GM WHEEL-NLG, 10 711 32-41-12
 2. Component Description

_____________________
 A. Main Gear Wheel
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 003, 004)
 The wheels consist of two forged half-wheels made of light alloy.
 They are attached together with bolts made of high-tensile steel and
 self-locking nuts.
 An O-ring seal is put between the two half-wheels.
 The wheels are equipped with:

 -taper roller bearings with protective seals,
 -drive keys for the brake rotor disks,
 -six fuse plugs which deflate the tire in the event of excessive brake overheat and thus protect against tire burst because of excessive pressure,
 - one standard inflating valve which you can replace by a valve with an incorporated pressure indicator (PSI type),
 1EFF : ALL 1 32-41-00Page 1 1 1 Aug 01/05 1 1 1CES 1


 Main Gear Wheels - Component Location
 Figure 001
 1EFF :  ALL  1  32-41-00 Page 2 
1  1  Feb 01/98
 1  1
 1CES  1

 

 Nose Gear Wheels - Component Location
 Figure 002
 1EFF :  ALL  1  32-41-00 Page 3 
1  1  Feb 01/98
 1  1
 1CES  1

 

 Main Gear Wheel
 Figure 003

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-41-00Page 4 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1


R  Main Gear Wheel 
R  Figure 003A 
R 1EFF :  301-399,  1  32-41-00 Page 5 
1  1  May 01/04
 1  1
 1CES  1

 

 Main Gear Wheel
 Figure 004

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-41-00Page 6 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 -a provision for installation of a transducer for the Tire Pressure


 Indicating System (optional system). Each wheel is installed on the axle with an axle sleeve. Characteristics:
 -weight: 60.6 kg max.
 -melting point of the fuse plug: . first set, inside keys: 300 deg.C (572.00 deg.F), . second set, on wheel web: 183 deg.C (361.40 deg.F).
 **ON A/C 301-399,
 (Ref. Fig. 003A, 004A)
 The wheels consist of two forged half-wheels made of light alloy.
 They are attached together with bolts made of high-tensile steel and
 self-locking nuts.
 An O-ring seal is put between the two half-wheels.
 The wheels are equipped with:

 -taper roller bearings with protective seals,
 -drive keys for the brake rotor disks,
 -three fuse plugs which deflate the tire in the event of excessive brake overheat and thus protect against tire burst because of excessive pressure,
 - one standard inflating valve which you can replace by a valve with an incorporated pressure indicator (PSI type), - one overpressure relief valve,
 -a provision for installation of a transducer for the Tire Pressure
 Indicating System (optional system). Each wheel is installed on the axle with an axle sleeve which the manufacturer supplies. Characteristics:
 -weight: 87 kg max.
 -melting point of the fuse plug: 183 deg.C (361.40 deg.F).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM LANDING GEAR 起落架6(44)