(a)
 Move the torque limiter away from the torque shaft (2).

 (b)
 Put the universal joint (3) into the torque limiter.

 (c)
 Turn the universal joint (3) until the bolt holes are aligned.

 (d)
 Install the torque limiter on the torque shaft (2).

 (e)
 Remove the universal joint (3).

 (3)
 Put a countersunk washer (10) on a bolt (9), with the countersink
 adjacent to the head of the bolt.

 (4)
 Install the bolt (9), with the countersunk washer (10), washer (12) and the nut (13) in the applicable hole (Ref. TASK 20-28-00-912-004):

 -
FOR 6211CM
 in the LH wing bonding position

 -
FOR 6261CM
 in the RH wing bonding position.

 NOTE : 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 these remaining items:

 -the shanks of the bolts (9) and (14).

 (6)
 Put the countersunk washers (10) and (15) on the bolts (9) and (14). Make sure that countersink is adjacent to the heads of the bolts.

 (7)
 Install the longer bolt (14) through the lever stop (11), the
 structure and the actuator assembly.

 (8)
 Install the washer (7) and the nut (8) on the longer bolt (14). Do
 not tighten in this step.

 (9)
 Install the remaining bolts (9) through the actuator assembly and the structure.

 (10)
 Install a washer (12) and a nut (13) on each of the bolts (9).

 (11)
 TORQUE all the nuts (8) and (13) in a diagonally opposite sequence to between 2.8 and 3.0 m.daN (20.64 and 22.12 lbf.ft).

R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-54-49Page 472 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (12)
 Do an electrical bonding check between the structure and the applicable bolt (Ref. TASK 20-28-00-869-002):

 -
FOR 6211CM
 in the LH wing bonding position

 -
FOR 6261CM
 in the RH wing bonding position.

 (13)
 Seal the bolt (9), the countersunk washer (10), the washer (12) and the nut (13) installed in the applicable hole (Ref. TASK 20-28-00-912-004):

 -
FOR 6211CM
 in the LH wing bonding position

 -
FOR 6261CM
 in the RH wing bonding position.

 (14)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to these remaining items:

 -
the bolts (9) and (14

 -
the washers (7), (10), (12) and (15)

 -
the nuts (8) and (13).

 (15)
 Install the universal joint (3) and the torque shaft (4) (Ref. TASK 27-54-45-400-005):

 -
FOR 6211CM
 install 6210CM

 -
FOR 6261CM
 install 6260CM.

 **ON A/C ALL
 Subtask 27-54-49-080-053
R D. Removal of Support Equipment
 (1)
 Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the torque shafts (1) and (6) (Ref. TASK 27-50-00-000-003).

 (3)
 Remove the support from the flap trailing edge.

R (2) Remove the clamp that holds the carriage in position.

 Subtask 27-54-49-740-062
 E. 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.
　
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