• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-22 07:03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

 Remove and discard the string and the tape from the harness.


 (5) Install the harness 14QT1 (14QT2) between RIB 8 and RIB 9 as follows: (Ref. Fig. 404/TASK 28-42-43-991-007, 406/TASK 28-42-43-991-011, 407/TASK 28-42-43-991-010)
 (a)
 Identify the cable ends for the the sensor 25QJ1(25QJ2).

 (b)
 Connect the cable to the sensor 25QJ1(25QJ2) with the screws (20).

 (c)
 Put the cable in the clamp (22) and tighten the screws (21).

 (d)
 Put the cable for the sensor 25QJ1(25QJ2) in position.

 (e)
 Make a coil of the unwanted cable and attach the harness to the structure with the cable-ties (1).


 1EFF : 001-049, 051-099, 101-105, 151-199, 1 28-42-43Page 463 1201-228, 1Aug 01/05 1 1 1CES 1 (f) Identify the cable ends for the fuel probe 30QT1(30QT2).


 (g) Use a crimping tool to crimp the correct color terminal R connectors (2) to the color identified wires (Ref. ESPM 203222).
 (h)
 Connect the terminal connectors (2) to the terminal block of the fuel probe 30QT1(30QT2).

 (i)
 Put the cables for the fuel probe 30QT1(30QT2) in position.

 (j)
 Attach the harness 14QT1(14QT2) to the structure with the cable-ties (1).

 (k)
 Get access through the opening 540GB(640GB) to RIB13 and find the string at the end of the conduit.

 (l)
 Use the string to carefully pull the harness through the conduit until the cables come into view.

 (m)
 Remove and discard the string and the tape from the harness.


 (6) Install the harness 14QT1 (14QT2) between RIB 12 and RIB 13 as follows: (Ref. Fig. 404/TASK 28-42-43-991-007, 405/TASK 28-42-43-991-009)
 (a)
 Identify the cable ends of the sensor 26QJ1(26QJ2) and connect them to the terminals of the sensor with the screws (20).

 (b)
 Put the cables in position in the clamp (22) and tighten the screws (21).

 (c)
 Put the cables for the sensor 26QJ1(26QJ2) in position.

 (d)
 Make a coil of the unwanted cable and attach it to the structure with the cable-ties (1).

 (e)
 Get access through the opening 540HB(640HB) to RIB13 and find the string at the end of the conduit.

 (f)
 Use the string to carefully pull the harness through the conduit until it comes into view.

 (g)
 Remove and discard the string and the tape from the harness.


 1EFF : 001-049, 051-099, 101-105, 151-199, 1 28-42-43Page 464 1201-228, 1Aug 01/05 1 1 1CES 1


 (7) Install the harness 14QT1 (14QT2) between RIB 13 and RIB 14 as follows: (Ref. Fig. 407/TASK 28-42-43-991-010)
 (a) Identify the cable end for the fuel probe 32QT1(32QT2).
 (b) Use a crimping tool to crimp the correct color terminal R connectors (2) to the color identified wires (Ref. ESPM 203222).
 (c)
 Connect the terminal connectors (2) to the terminals of the terminal block of the fuel probe 32QT1(32QT2).

 (d)
 Put the cables for the fuel probe 32QT1(32QT2) in position.

 (e)
 Attach the harness 14QT1(14QT2) to the fuel probe 32QT1(32QT2) body and the structure with the cable-ties (1).

 (f)
 Get access through the opening 540JB(640JB) to RIB14 and RIB15 and find the string at the end of the conduit.

 (g)
 Use the string to carefully pull the harness 14QT1(14QT2) through the conduit until it comes into view.

 (h)
 Remove and discard the string and the tape from the harness.


 (8) Install the harness 14QT1 (14QT2) between RIB 14 and RIB 15 as follows: (Ref. Fig. 404/TASK 28-42-43-991-007, 405/TASK 28-42-43-991-009, 406/TASK 28-42-43-991-011)
 (a)
 Identify the cable ends for the sensor 27QJ1(27QJ2). Connect them to the terminals of the sensor and tighten the screws (20).

 (b)
 Put each cable in its clamp (22) and tighten the screws (21).

 (c)
 Put the cable for the sensor 27QJ1(27QJ2) in position.

 (d)
 Make a coil of the unwanted cable and attach the harness to the structure with the cable-ties (1).

 (e)
 Remove the nuts (40), the bolts (42), the anti-rotation plate

 (41)
 and the connector 4046VC1(4046VC2) (34).

 (f)
 Remove the nut (32) and the washer (31) from the connector (34).

 (g)
 Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-013) to the threads of the connector (34).


 1EFF : 001-049, 051-099, 101-105, 151-199, 1 28-42-43Page 465 1201-228, 1Aug 01/05 1 1 1CES 1


 (9) Install the harness 14QT1 (14QT2) between RIB 15 and RIB 16 as follows: (Ref. Fig. 404/TASK 28-42-43-991-007, 405/TASK 28-42-43-991-009)
 
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 FUEL 燃油5(103)