-
FOR 6283CM
 in the RH wing bonding position.
 Do not tighten in this step. Do not apply sealant.

 (5)
 Apply a layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the shanks of the bolts (9).

 (6)
 Put the countersunk washers (10) on the bolts (9), with the
 countersink adjacent to the heads of the bolts.

 (7)
 Install the remaining bolts (9), the washers (11) and the nuts (12).

 (8)
 TORQUE all the nuts (12) in a diagonally opposite sequence to between

 2.8 and 3.0 m.daN (20.64 and 22.12 lbf.ft).

 (9)
 Do an electrical bonding check between the structure and the
 applicable bolt (Ref. TASK 20-28-00-869-002):

 -
FOR 6233CM
 in the LH wing bonding position

 -
FOR 6283CM
 in the RH wing bonding position.

 (10) Seal the bolt (9), the countersunk washer (10), the washers (11) and the nut (12) in the applicable hole (Ref. TASK 20-28-00-912-004):
 -
FOR 6233CM
 in the LH wing bonding position

 -
FOR 6283CM
 in the RH wing bonding position.

R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-54-49Page A426 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (11)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to these remaining items:

 -
the bolts (9

 -
the countersunk washers (10)

 -
the washers (11)

 -
the nuts (12).

 (12)
 Install the universal joint (1) so that the flanges align with the torque shaft (2).

 (13)
 Install the torque shaft (2) (Ref. TASK 27-54-45-400-013):

 -
FOR 6233CM
 install 6232CM

 -
FOR 6283CM
 install 6282CM.

 (14)
 Install the Asymmetry Position Pick-off Unit (APPU) (4) (Ref. TASK 27-51-18-400-001).

 **ON A/C ALL
 Subtask 27-54-49-080-055
R E. Removal of Support Equipment
 (1) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003).
R (2) Remove the clamp that holds the carriage in position.
 (3) Remove the support from the flap trailing edge.
 Subtask 27-54-49-740-067
 F. Do a Check of the Position Pick-Off Units (PPUs) on the Centralized Fault Display System (CFDS)
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Get access to the SYSTEM REPORT/TEST (F/CTL) page on the Multipurpose Control Display Unit (MCDU) (Ref. TASK 31-32-00-860-006).

 (3)
 Do a check of the flap PPU angles (deg) at the slat/flap control lever position FULL on the MCDU as follows:

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:
-push (in) the line key < SFCC
1.
 -
push (in) the NEXT PAGE button.

-
push (in) the line key SYSTEM DATA FLP >.

-
push (in) the line key < PPU.

-write down the APPU and the FPPU angles (deg) shown on the display or push (in) the line key PRINT > to get a print out of the screen.
 -push the line key < RETURN frequently until the CFDS menu page is shown.
 2. De-energize the electrical circuits (Ref. TASK 24-41-00-862-002).
 Subtask 27-54-49-820-065
 G. Adjustment After BITE Test
On the MCDU:
-
the MCDU shows the SFCC 1 menu.

-
the MCDU shows the next page of the SFCC 1 menu.

-
the MCDU shows the SFCC 1 FLAPSYSTEM DATA menu.

-
the MCDU shows the PPU DATA page(s). Refer to Table 1.

 (1)
 Compare the APPU and the FPPU angles (deg) with those that were written down (or printed) before the actuator was removed (Ref. TASK 27-54-49-000-004).

 (2)
 Make sure that the FPPU angle values agree with the values recorded before the actuators were removed (+/- 0.2 deg).

 (3)
 Make sure that the APPU angle values agree with the values recorded before the actuators were removed (+/- 0.2 deg).

 (4)
 Make sure that the APPU/FPPU angles (deg) agree (+/- 1.3 deg).

 (5)
 Make sure that the LH APPU and the RH APPU angles agree (+/- 0.45 deg).
　
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