(43)
and the nuts (45).
(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)
Clean the plug connector (33) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(k)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the plug connector (33).
(l)
Put the cable for the connector 4045VC1(4045VC2) (34) in
position.
(m)
Attach the harness 13QT1(13QT2) to the structure with the
cable-ties (1).
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(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).
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(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 106-149, 229-299, 401-499,
Subtask 28-42-43-420-093-A R B. Installation of the Wing-Tank Inner-Cell Group A Harness 13QT1 (13QT2)
(1) Install the harness 13QT1 (13QT2) between RIB 2 and RIB 3 as follows: (Ref. Fig. 402/TASK 28-42-43-991-004, 403A/TASK 28-42-43-991-006-A, 404/TASK 28-42-43-991-007)
(a)
Get access through the opening 540AB(640AB) and find the string at the end of the conduit.
(b)
Use the string to carefully pull the harness 13QT1(13QT2) through the conduit until it comes into view.
(c)
Remove and discard the string and the tape from the harness 13QT1(13QT2).
(d)
Identify the cable ends for the sensor cadensicon 19QT1(19QT2).
(e)
Install the spacer sleeve (6) on the cable.
(f) Use a crimping tool to crimp each correct color terminal R connector (2) to its color identified wires (Ref. ESPM 203222).
(g)
Connect the terminal connectors (2) to the terminal block of the sensor cadensicon 19QT1(19QT2).
(h)
Put the cable for the sensor cadesicon 19QT1(19QT2) in position.
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(i) Attach the harness 13QT1(13QT2) to the structure with the cable-ties (1).
(2) Install the harness 13QT1 (13QT2) at RIB 2 as follows: (Ref. Fig. 402/TASK 28-42-43-991-004, 403A/TASK 28-42-43-991-006-A)
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