• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:57来源:蓝天飞行翻译 作者:航空
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

 4. Procedure
_________
 (Ref. Fig. 409/TASK 71-73-49-991-308) Subtask 71-73-49-420-060
 A. Installation of the Forward Oil Sump Drain Tube
 (1) Remove the protective covers from the fitting in the forward oil sump and the drain tubes.

 (2) Connect the forward oil sump drain tube (20) to the fitting in the forward oil sump. Do not torque the coupling nut at this time.

 (3) Connect the drain tube (20) to the manifold oil drain tube. Do not torque the coupling nut at this time.

 (4) Attach the drain tube (20) to the bracket on the fan case with the clamp (5), the bolt (10), and the nut (15).

 (5) Make sure that the forward oil sump drain tube (20) aligned correctly on the engine.

 (6) TORQUE the nut (15) to between 20 and 25 lbf.in (0.22 and 0.28 m.daN).

 (7) Torque the drain tube coupling nuts. CAUTION : USE A SECOND WRENCH TO HOLD THE FITTINGS WHEN YOU


_______ LOOSEN/TIGHTEN THE TUBE COUPLING NUTS. THIS PREVENTS DAMAGE TO THE TUBES.
 (a) TORQUE the drain tube (20) coupling nuts to between 200 and 250 lbf.in (2.26 and 2.82 m.daN).
 F 『 EEFF : ALL E Page 46971-73-49
 E E Feb 01/00 ERE
ECES E 5. Close-up

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


________ Subtask 71-73-49-410-061
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR


 (3) Remove the warning notice(s).


 F 『 EEFF : ALL E Page 47071-73-49
 E E Feb 01/00 ERE
ECES E

 F  『
 E  C F M  E
 E  E


 E 56-5B E E E TASK 71-73-49-000-049

 Removal of the Reservoir to Manifold Hydraulic Oil Drain Tube
 1. Reason for the Job

__________________
 Self Explanatory


 2. Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific container 1 l (0.25 USgal) No specific protective covers No specific warning notice
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 71-73-49-991-309 Fig. 410
 3. Job Set-up
__________ Subtask 71-73-49-941-062
 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.

 (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.
 F 『 EEFF : ALL E Page 47171-73-49
 E E Feb 01/00 ERE
ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


 (b) Put a warning notice to tell persons not to energize the FADEC 1(2).
 Subtask 71-73-49-010-062
 B. Open the fan cowl doors: (Ref. TASK 71-13-00-010-040)
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 4. Procedure
_________
 (Ref. Fig. 410/TASK 71-73-49-991-309) Subtask 71-73-49-020-061
 A. Removal of the Reservoir to Manifold Hydraulic Oil Drain Tube
 (1) Put a container 1 l (0.25 USgal) below the drain mast to catch any hydraulic oil remaining in the tube.

 (2) Disconnect the reservoir to manifold hydraulic oil drain tube (5) from the drain manifold module and let the fluid drain into the container.

 (3) Disconnect the drain tube (5) from the drain reservoir module.

 (4) Remove the drain tube (5) from the engine.

 (5) Put protective covers on the drain manifold module, the drain reservoir module, and the drain tube (5).

 (6) Remove the container from below the drain mast.


 F 『 EEFF : ALL E Page 47271-73-49
 E E Feb 01/00 ERE
ECES E F 『 E C F M E E E E 56-5B E

 

 Reservoir to Manifold Hydraulic Oil Drain Tube Figure 410/TASK 71-73-49-991-309
 
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 动力装置 POWER PLANT 2(123)