• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 16:58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

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2442 *
 engine oil (Ref. 70-30-00)
 Material No. CP2859 *
 corrosion protective additive (Ref. 70-30-00)

 F 『 EEFF : ALL E Page 40972-63-00
 E E Aug 01/05 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E
 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-13-79-610-003 Oil Tank Draining 24-21-51-000-040 Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) 26-12-15-000-042 Removal of the Fan Fire Detectors (4000WD1,4000WD2)
R  29-11-51-000-041 Removal of the Green Engine Pump (1030GK) 71-13-00-010-040 Opening of the Fan Cowl Doors 71-71-43-000-041 Removal of the Drain Manifold Module 71-73-49-000-003 Removal of the Starter Pad Oil Drain Tube 71-73-49-000-004 Removal of the IDG Oil Drain Tube 71-73-49-000-007 Removal of the Fan Case Drain Tubes 71-73-49-000-008 Removal of the Fuel Pump Drain Tubes 71-73-49-000-026 Removal of the Heat Exchanger Drain Tube 71-73-49-000-027 Removal of the Hydro Mechanical Unit (HMU) Drain Tube 71-73-49-000-028 Removal of the Hydraulic Pump Drain Tube 71-73-49-000-029 Removal of the Forward Oil Sump Drain Tube 71-73-49-000-049 Removal of the Reservoir to Manifold Hydraulic Oil
 Drain Tube 72-63-00-860-001 Disengagement/Engagement of the Horizontal Drive
 Shaft
 73-11-10-000-003 Removal of the Fuel Pump and Filter Assembly
 73-21-30-000-001 Removal of the Control Alternator
 77-11-20-000-002 Removal of the N2 Speed Sensor (4001EV).
 78-30-00-481-041 Make the Thrust Reverser Unserviceable for

 Maintenance
 78-36-00-010-040 Opening of the Thrust Reverser Doors
 79-21-10-000-004 Removal of the Lubrication Unit
 80-11-10-000-002 Removal of the Pneumatic Starter
 72-63-00-991-309 Fig. 403
 72-63-00-991-310 Fig. 404
 72-63-00-991-311 Fig. 405
 72-63-00-991-312 Fig. 406
 72-63-00-991-313 Fig. 407
 72-63-00-991-314 Fig. 408

 F 『 EEFF : ALL E Page 41072-63-00
 E E Aug 01/03 E E ECES E 3. Job Set-up

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


__________ Subtask 72-63-00-941-061
 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.

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

 


 Subtask 72-63-00-010-071
 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 72-63-00-040-053

 C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 72-63-00-010-074


 D. Open the thrust reverser doors: (Ref. TASK 78-36-00-010-040)
 FOR 1000EM1
 451AL, 452AR
 FOR 1000EM2
 461AL, 462AR

 F 『 EEFF : ALL E Page 41172-63-00
 E E Aug 01/00 ERE
ECES E E 56-5B E

 F  『
 E  C F M  E
 E  E


 E E

 4. Procedure_________
 (Ref. Fig. 403/TASK 72-63-00-991-309, 404/TASK 72-63-00-991-310, 405/TASK 72-63-00-991-311, 406/TASK 72-63-00-991-312, 407/TASK 72-63-00-991-313, 408/TASK 72-63-00-991-314)
 Subtask 72-63-00-941-062
 A. Put a container under the Accessory Gearbox to collect the remaining fluid from the tubes and control.
 Subtask 72-63-00-010-070
 B. Preparation for the Removal of the AGB CAUTION : USE 2 WRENCHES TO REMOVE OR INSTALL THE TUBE COUPLING NUTS.
_______ ONE WRENCH TO HOLD THE UNION AND ONE TO LOOSEN OR TIGHTEN THE COUPLING NUT. THIS WILL PREVENT DAMAGE TO THE HARDWARE.
 (1) Remove the fan fire detector (Ref. TASK 26-12-15-000-042).

 (2) Remove the drain manifold module (Ref. TASK 71-71-43-000-041).

 (3) Remove the drain tubes under the AGB/TGB as follows:
 
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 ENGINE 发动机 2(135)