R 1EFF : 106-149, 229-299, 401-499, 1 28-42-43Page 436 1 1 Aug 01/05 1 1 1CES 1

 (8) Install the harness 13QT1 (13QT2) between RIB 6 and RIB 7 as follows:
 (a)
 Get access through the opening 540BB(640BB) to RIB6 and RIB7.

 (b)
 Carefully pull the string from the cable for the connector 4039VC1(4039VC2) (34) until the cable comes into view at the end of the conduit.

 (c)
 Remove and discard the tape and the string from the harness 13QT1(13QT2).

 (d) Use a crimping tool to crimp the wires to the connector pins of R the connector (34) (Ref. ESPM 203222).
 (e)
 Insert the connector pins into the connector (34) (Ref. WL 912840).

 (f)
 Tighten the clamp screws (36) of the backshell (35). Make sure that the cable is firmly clamped in the backshell (35).

 (g)
 Safety the clamp screws (36) and the backshell (35) with MISCELLANEOUS (Material No. 19-010).

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

 (9) Install the harness on the rear spar between RIB 6 and RIB 7 as follows: (Ref. Fig. 404/TASK 28-42-43-991-007, 405/TASK 28-42-43-991-009)
 (a)
 Install the new O-ring (30) on the connector (34).

 (b)
 Put the connector (34) in position in the hole in the rear spar.

 (c)
 Get access through the opening 574BB(674BB) to the rear spar.

 (d)
 Install the washer (31) and the nut (32) on the connector (34).

 (e)
 TORQUE the nut (32) to between 1.16 and 1.27 m.daN (102.65 and

 112.38 lbf.in).
 (f)
 Use a lint-free cloth to remove unwanted adhesive from the connector (34) and the nut (32).

 (g)
 Safety the nut (32) with MISCELLANEOUS (Material No. 19-010).

R 1EFF : 106-149, 229-299, 401-499, 1 28-42-43Page 437 1 1 Aug 01/05 1 1 1CES 1

 (h)
 Apply SEALANTS (Material No. 09-001) around the connector (34) to seal it to the rear spar.

 (i)
 Remove the blanking cap and connect the plug connector (33) to the connector (34).

 (j)
 Get access through the opening 540BB(640BB) to RIB6 and RIB7.

 (k)
 Put the cable for the connector 4039VC1(4039VC2) (34) in position.

 (l)
 Attach the harness to the structure with the P clip (3), the bolt

 (4) and the cable-ties (1). R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 28-42-43-865-067
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1QJ, 1QP, 2QP, 3QP, 4QP, 1QT, 2QT, 8QT, 31QA, 32QA.
 Subtask 28-42-43-740-056
 D. Test
 (1)
 Do a status report (BITE) of the fuel-quantity indicating system (Ref. TASK 28-42-00-740-001).

 (2)
 Do a functional (BITE) test of the fuel-tank level-sensing system (Ref. TASK 28-46-00-740-001).

 5. Close-up
________
 Subtask 28-42-43-410-062

 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the HOOK-COVER (RIB 2 SURGE DOORS) and let the door 540AZ (640AZ) carefully close.

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-43Page 438 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 (3) Install the applicable access panels (Ref. TASK 57-27-11-400-001) and (Ref. TASK 57-27-11-400-002): FOR 13QT1
 -install 540AB, 540BB, 540DB, 540GB, 540JB, 540KB, 574BB FOR 13QT2
 -install 640AB, 640BB, 640DB, 640GB, 640JB, 640KB, 674BB. Subtask 28-42-43-650-051
 B. Fuel Configuration
 (1) Refuel, defuel or transfer fuel as necessary (Ref. TASK 12-11-28-650-003), (Ref. TASK 28-25-00-650-001) or (Ref. TASK 28-25-00-869-001).
 Subtask 28-42-43-942-053
 C. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-43Page 439 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 28-42-43-000-007

 Removal of the Wing-Tank Inner-Cell Group B Harness 14QT1(14QT2)
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油5(94)