• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-24 08:35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

29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
 after Operation of the PTU R 29-11-49-991-911 Fig. 409 R 29-11-49-991-912 Fig. 410
 FOR FIN 1000EM1
 71-13-00-010-040 Opening of the Fan Cowl Doors

 

 3. Job Set-up
__________ Subtask 29-11-49-860-083
 A. Aircraft Maintenance Configuration
 (1)
 Depressurize the Green hydraulic system (Ref. TASK 29-23-00-864-001).

 (2)
 Depressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-001).

 (3)
 Put warning notice(s) in position to tell persons not to pressurize the Green hydraulic system: - on the ground service panel 197CB.

 (4)
 Put warning notice(s) on the access door 195BB to tell persons not to pressurize the Green hydraulic reservoir.


 Subtask 29-11-49-941-073
 B. Safety Precautions
 (1)
 On the center pedestal, on the ENG panel 115VU:

 -put warning notice(s) to tell persons not to start the engine.

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

 (3)
 Put warning notice(s) in position to tell persons not to pressurize the Green hydraulic system:

 -in the cockpit, on the HYD section of the overhead panel 40VU.

 (4)
 On the overhead maintenance panel 50VU:

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

 (5)
 Put warning notice(s) to tell persons not to energize the FADEC 1(2).

 (6)
 Put a container under the pressure relief valve.


 1EFF : ALL 1 29-11-49Page 458 1 1 Aug 01/05R 1 1 1CES 1


 Subtask 29-11-49-865-059
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34
 Subtask 29-11-49-010-073
 D. Get Access
 (1)
 Open the left fan cowl door: FOR 1000EM1 - open the door 437AL (Ref. TASK 71-13-00-010-040).

 (2)
 Put the access platform in position at the engine.


 4. Procedure
_________ R (Ref. Fig. 409/TASK 29-11-49-991-911, 410/TASK 29-11-49-991-912) Subtask 29-11-49-020-065
 A. Removal of the Pressure-Relief Valve Hose/Tube
 (1) Disconnect the higher pressure relief valve hose/tube (25) from the lower pressure-relief valve tube (20) and let the fluid flow into the container.
 NOTE : Use a second wrench to hold the lower pressure-relief valve
____ tube when you loosen the coupling nut on the higher pressure-relief valve tube.
 (2)
 Disconnect the pressure-relief valve hose/tube (25) from the pressure-relief valve interface.

 (3)
 Remove the bolts (5), the washers (10), the nuts (15) and the clamps

 (20) that attach the pressure-relief valve hose/tube (25) to the engine brackets at flange STA.199(A2).

 (4)
 Remove the pressure-relief valve hose/tube (25) from the engine.

 (5)
 Put protective covers on the pressure-relief valve tube (30), the fitting on the top case drain hose/tube and the pressure-relief valve hose/tube (25).

 (6)
 Disconnect the lower pressure-relief valve tube (30) from the top
 case drain hose/tube and let the fluid flow into the container.

 

 

R  Pressure Relief Valve Hose/Tubes Figure 409/TASK 29-11-49-991-911
 1EFF : 1 1 1CES  ALL  1 111 29-11-49 Page 460 Aug 01/05

 

R  Pressure Relief Valve Hose/Tubes Figure 410/TASK 29-11-49-991-912
 1EFF : 1 1 1CES  ALL  1 111 29-11-49 Page 461 Aug 01/05

 

 NOTE : Use a second wrench to hold the fitting on the case drain tube
____ when you loosen the coupling nut on the pressure-relief valve tube.
 (7) If not done before, disconnect the lower pressure-relief valve tube
 (30) from the higher pressure-relief valve hose/tube (25).
 NOTE : Use a second wrench to hold the lower pressure-relief valve
____
 tube when you loosen the coupling nut on the higher
 pressure-relief valve tube.

 (8)
 Remove the bolt (5), the washer (10), the nut (15) and the clamp (20) that attach the lower pressure-relief valve tube to the engine bracket at flange STA.199(A2).

 (9)
 Remove the bolt (5), the washer (10), the nut (15) and the clamp (20) that attach the lower pressure-relief valve tube to the engine bracket at flange STA.185(B5).
 
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 HYDRAULIC POWER 液压2(110)