(d)
Tighten the clamp screws (36) of the backshell (35). Make sure that the cable is firmly clamped in the backshell (35).
(e)
Safety the clamp screws (36) and the backshell (35) with lockwire.
(f)
Install the new O-ring (30) on the connector (34).
(g)
Put the connector (34) in position in the hole in RIB15.
(h)
Get access through the opening 540KB(640KB) to RIB15.
(i)
Install the washer (31) and the nut (32) on the connector (34).
(j)
TORQUE the nut to between 0.84 and 0.92 m.daN (74.33 and 81.41 lbf.in).
(k)
Safety the nut (32) with the anti-rotation plate (41), the bolts
(42)
and the nuts (40).
(l)
Apply SEALANTS (Material No. 09-001) around the connector (34) to seal it to the rear spar.
(m)
Remove the blanking cap and connect the plug connector (33) to the connector (34).
(n)
Clean the plug connector (33) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(o)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the plug connector (33).
(p)
Get access through the opening 540JB(640JB).
(q)
Put the cable for the connector (34) in position.
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(r)
Attach the harness 14QT1(14QT2) to the structure with the cable-ties (1).
(s)
Get access through the opening 540BB(640BB) to RIB7.
(t)
Identify the cable ends for the connector 4040VC1(4040VC2) (34).
(u) Use a crimping tool to crimp the connector pins on the wires of R the connector (34) (Ref. ESPM 203222).
(v)
Insert the connector pins into the connector (34) (Ref. WL 912840).
(w)
Tighten the clamp screws (36) of the backshell (35). Make sure that the cable is firmly clamped in the backshell (35).
(x)
Safety the clamp screws (36) and the backshell (35) with lockwire.
(y)
Remove the blanking cap and apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-013) to the threads of the connector (34).
(z)
Install the O-ring (30) on the connector (34). (aa) Put the connector (34) in position in the hole on the rear spar. (ab) Get access through the opening 574BB(674BB) to the rear spar. (ac) Install the washer (31) and the nut (32) on the connector (34). (ad) TORQUE the nut (32) to between 1.16 and 1.27 m.daN (102.65 and
112.38 lbf.in). (ae) Safety the nut (32) with MISCELLANEOUS (Material No. 19-010). (af) Apply SEALANTS (Material No. 09-001) around the connector (34) to
seal it to the rear spar. (ag) Remove the blanking cap and connect the plug connector (33) to
the connector (34). (ah) Get access through the opening 540BB(640BB). (ai) Remove the bolts (4) and the P clips (3) and put the cable (for
the connector (34)) in position.
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(aj) Attach the harness to the structure with the P clips (3), the bolts (4) and the cable-ties (1).
R **ON A/C 106-149, 229-299, 401-499,
Subtask 28-42-43-420-095-A R B. Installation of the Wing-Tank Inner-Cell Group B Harness 14QT1 (14QT2)
(1)
Install the harness 14QT1 (14QT2) between RIB 1 and RIB 2 as follows:
(a)
Get access through the opening 540AB(640AB) and find the string at the conduit end.
(b)
Use the string to carefully pull the harness 14QT1(14QT2) through the conduit until all the cables come into view.
(c)
Remove and discard the string and the tape from the harness.
(2)
Install the harness 14QT1 (14QT2) between RIB 2 and RIB 3 as follows: (Ref. Fig. 403A/TASK 28-42-43-991-006-A, 404/TASK 28-42-43-991-007)
(a) Identify the cable ends for the fuel probe 24QT1(24QT2).
(b) Use a crimping tool to crimp the correct color terminal connector R (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 24QT1(24QT2).
(d)
Put the cable for the fuel probe 24QT1(24QT2) in position.
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