• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 14:41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

24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector 49-00-00-710-010 Operational Test of the APU (131-9(A)) 52-41-00-010-001 Open the APU Doors for Access 52-41-00-410-001 Close the APU Doors after Access 49-32-13-991-002 Fig. 401
 3. Job Set-up
__________
 Subtask 49-32-13-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Energize the ground service network
 (Ref. TASK 24-42-00-861-001).


 (2)
 On the panel 25VU, make sure that the APU MASTER SW p/bsw is OFF.

 (3)
 Make sure that there is a warning notice in the cockpit to tell persons not to start the APU.

 (4)
 Make sure that hydraulic systems are depressurized
 (Ref. TASK 29-00-00-864-001).


 (5)
 Make sure that the access platform is in position below the APU compartment.

 (6)
 Make sure that the APU access doors are open (Ref. TASK 52-41-00-010-001).

 (7)
 Make sure that the LIGHT SW 11LJ is set to the ON position.

 

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-32-13Page 406 201-210, Aug 01/05
 CES  Subtask 49-32-13-865-055


 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
 4. Procedure
_________
 (Ref. Fig. 401/TASK 49-32-13-991-002) Subtask 49-32-13-420-051
 A. Installation of the Flow Divider
 CAUTION : YOU MUST USE TWO WRENCHES AND HOLD THE COMPONENT WHEN YOU

_______ REMOVE/INSTALL THE PIPE COUPLINGS AND/OR UNIONS. THIS PREVENTS DAMAGE TO THE COMPONENT.
 CAUTION : -YOU MUST NOT INCREASE THE TIGHTENING TORQUE MORE THAN THE
_______ MAXIMUM VALUE. -APPLY ALL TIGHTENING TORQUES WITH A TORQUE WRENCH OR A CALIBRATED SCREWDRIVER.
 (1)
 Remove the blanking caps from the flow divider (1).

 (2)
 Clean the component interface and/or the adjacent area.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Lubricate the new O-rings (3) with OILS (Material No. 03-002).

 (5)
 Install the new O-ring (3) on the union (7).

 (6)
 Install the union (7) into the solenoid on side nearest the master key.

 (7)
 TORQUE the union (7) to 1.59 m.daN (11.72 lbf.ft)

 (8)
 Install the nut (2), the O-ring (3) and the retainer ring (4) on the flow divider (1).

 

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-32-13Page 407 201-210, Aug 01/05
 CES


 (9) Install the flow divider (1) into the solenoid (9) on the side furthest from the master key.
 (10)
 Put the flow divider (1) and solenoid (9) in position on the APU.

 (11)
 Install the clamp (10) and the bolt (12).

 (12)
 TORQUE the bolt (12) to 0.57 m.daN (50.44 lbf.in).

 (13)
 Remove the blanking plugs from the disconnected line ends.

 (14)
 Connect the secondary manifold fuel pipe (8) to the union (7).

 (15)
 Loosely connect the primary manifold fuel pipe (14) to the flow divider (1).

 (16)
 Loosely connect the main fuel feed pipe (15) to the flow divider (1).

 (17)
 Hold the flow divider (1) in position and tighten the nut (2).

 (18)
 TORQUE the nut (2) to 1.14 m.daN (100.88 lbf.in).

 (19)
 Tighten the primary manifold fuel pipe (14).

 (20)
 TORQUE the primary manifold fuel pipe (14) to 1.14 m.daN (100.88 lbf.in).

 (21)
 Tighten the main fuel feed pipe (15) and the secondary manifold fuel pipe (8).

 (22)
 TORQUE the secondary manifold fuel pipe (8) and main fuel feed pipe

 (15) to 1.14 m.daN (100.88 lbf.in).

 (23)
 Install the bonding lead (6) on the solenoid (9) with the bolt (16) and the nut (5).

 (24)
 Remove the blanking caps from the electrical connectors.

 (25)
 Connect the electrical connector (12) to the solenoid. Subtask 49-32-13-865-056


 
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 机载辅助动力 AIRBORNE AUXILIARY POWER4(56)