R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 27-84-48-991-001-A)
 **ON A/C ALL
 NOTE : The slat actuators are vented units filled with grease. It is normal
____ for this grease to have some oil separation. The external surfaces of the actuators can be moist with this grease as they are not hermetically sealed units. But separated oil in the units that touches the grease will be changed back during operation. The oil separation will decrease during in-service operation until the lubricant is in a condition that is stable. This is normal and will not cause damage to the units.
 Subtask 27-84-48-420-051
 A. Preparation for Installation
 CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
 GREASE AND ASSEMBLY PASTE DO NOT MIX.

 (1)
 Clean the component interface and/or the adjacent area with MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Do one of the steps that follow:
 CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.

_______
 GREASE AND ASSEMBLY PASTE DO NOT MIX.

 (a)
 Apply a thin layer of SPECIAL MATERIALS (Material No. 05-063) to the actuator output splines.

 - or

 (b)
 Apply a thin layer of COMMON GREASE (Material No. 04-018) to the actuator output splines.

 (4) If two TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 2 AND 3) are installed, remove one TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 2 AND 3) and install the applicable actuator before you remove the other TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 2 AND 3).
 Subtask 27-84-48-420-052
 B. Installation of the Type A Actuators 6013CM(6063CM)/6015CM(6065CM)
 (1)
 Apply a layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the shanks of the bolts (4).

 (2)
 Install the actuator (2) with the washers (5) and the bolts (4).

 (3)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the washers (5) and the bolts (4).

 Subtask 27-84-48-820-051
 C. Dimensional Check
 (1)
 To make sure that the track has not moved, put the GAGE-RIGGING (98D27804012000) between the track stop and the lower forward roller.

 (2)
 Make sure that the GAGE-RIGGING contacts the track stop and the lower forward roller.

 (3)
 If it is necessary to adjust the slat, turn the actuator drive in the applicable direction.

R 1EFF : ALL 1 27-84-48Page 414 1 1 Nov 01/01 1 1 1CES 1 Subtask 27-84-48-410-050

 D. Close Access
 (1)
 Install the applicable torque shaft (1):

 (a) (Ref. TASK 27-84-45-400-006)
 FOR 6013CM

 -
install the torque shaft 6012CM
 FOR 6063CM

 -
install the torque shaft 6062CM.

 (b) (Ref. TASK 27-84-45-400-008)
 FOR 6015CM

 -
install the torque shaft 6016CM
 FOR 6065CM

 -
install the torque shaft 6066CM.

 (2)
 Install the applicable torque shaft (3) (Ref. TASK 27-84-45-400-007): FOR 6013CM

 -
install the torque shaft 6014CM
 FOR 6015CM

 -
install the torque shaft 6014CM
 FOR 6063CM

 -
install the torque shaft 6064CM
 FOR 6065CM

 -
install the torque shaft 6064CM.

 Subtask 27-84-48-865-052
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-48-740-051
 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).

 1EFF : ALL 1 27-84-48Page 415 1 1 May 01/03R 1 1 1CES 1

 (3) Do a check of the slat PPU angles (deg) at the slat/flap control lever position 0 on the MCDU as follows:
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