• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-24 08:55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

 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific warning notice
 No specific access platform 1 m (3 ft. 3 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
30-21-49-000-040 Removal of the Secondary Anti-ice Ducts 30-21-49-000-043 Removal of the Muscle Pressure Tubes and Hoses 30-21-49-000-044 Removal of the Forward Anti-ice Duct 30-21-49-000-045 Removal of the Middle Anti-ice Duct 30-21-49-000-046 Removal of the Top Anti-ice Duct 30-21-49-400-040 Installation of the Secondary Anti-ice Ducts 30-21-49-400-043 Installation of the Muscle Pressure Tubes and Hoses 30-21-49-400-044 Installation of the Forward Anti-ice Duct 30-21-49-400-045 Installation of the Middle Anti-ice Duct 30-21-49-400-046 Installation of the Top Anti-ice Duct 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 30-21-49-991-305 Fig. 601 30-21-49-991-306 Fig. 602
 1EFF : ALL 1 30-21-49Page 606 1 1 Feb 01/99R 1 1 1CES 1


 3. Job Set-up
__________ Subtask 30-21-49-941-081
 A. Safety Precautions
 (1)
 On the center pedestal, on the ENG panel 115VU:

 (a) Put a warning notice to tell persons not to start the engine 1(2)

 (2)
 Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.

 (3)
 On the overhead maintenance panel 50VU:

 (a)
 Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.

 (b)
 Put a warning notice to tell persons not to energize the FADEC 1(2).

 


 Subtask 30-21-49-010-109
 B. Get Access
 (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
 FOR 1000EM1
 437AL 438AR
 FOR 1000EM2
 447AL 448AR

 (2) Put the access platform in position. Subtask 30-21-49-865-077
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU ANTI ICE/ENG/2 1DN2 W10 122VU ANTI ICE/ENG/1 1DN1 X10
 1EFF : ALL 1 30-21-49Page 607 1 1 Feb 01/99R 1 1 1CES 1


 4. Procedure
_________
 (Ref. Fig. 601/TASK 30-21-49-991-305, 602/TASK 30-21-49-991-306) Subtask 30-21-49-210-066
 A. Do a visual inspection of the anti-ice system hoses, tubes and ducts.
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1.
 Examine the muscle pressure line hose assemblies, look for:

 2.
 Examine the fittings on the two ends of the hose, look for:

 

 A. Broken Wire Braids.  Maximum of 3 broken wires per plait. No more than 6 broken wires in an assembly. No more than 6 broken wires in each 1 ft. (0.30 m) of hose. If the damage is more thanthe allowable limits,replace the hose(Ref. TASK 30-21-49-000-043) and (Ref. TASK 30-21-49-400-043).
 B. Cracks.  None permitted.  If cracks are found, replace the hose (Ref. TASK 30-21-49-000-043) and (Ref. TASK 30-21-49-400-043).
 C. Crimps.  None permitted.  Replace the hose assembly (Ref. TASK 30-21-49-000-043) and (Ref. TASK 30-21-49-400-043).
 D. Internal blockage.  None permitted.  If blockage is found remove the blockage or replace the hose (Ref. TASK 30-21-49-000-043) and (Ref. TASK 30-21-49-400-043).
 E. Leakage.  None permitted.  Replace the hose (Ref. TASK 30-21-49-000-043) and (Ref. TASK 30-21-49-400-043).

 1EFF : ALL 1 30-21-49Page 608 1 1 Feb 01/99R 1 1 1CES 1


 Anti-Ice System Tubes, Hoses and Ducts Figure 601/TASK 30-21-49-991-305
 1EFF : 1 1R 1CES  ALL  1 11 1 30-21-49 Page 609 Feb 01/99

 

 Anti-Ice System Tubes, Hoses and Ducts Figure 602/TASK 30-21-49-991-306
 1EFF : 1 1R 1CES  ALL  1 11 1 30-21-49 Page 610 Feb 01/99

 

 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
A. Thread damage.  Damage is permitted if the threads that are good are not reduced by more than one thread.  If the damage is more thanthe allowable limits,replace the hose(Ref. TASK 30-21-49-000-040) and (Ref. TASK 30-21-49-400-040).
 
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 ICE AND RAIN PROTECTION 防冰和排雨1(79)