(7)
 Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003) as follows: - on the torque shaft inboard of the removed component - on the torque shaft outboard of the removed component.

 Subtask 27-84-49-865-050
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,
 (Ref. Fig. 401/TASK 27-84-49-991-001)
R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 27-84-49-991-001-A)R **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 slat actuators may be moist with this separated oil as they are not hermetically sealed units. However, any 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 27-84-49-420-052
 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)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (4)
 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.

 (5) If the TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12) are installed, remove one TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12) and install the applicable actuator before you remove the other TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12).

 Subtask 27-84-49-420-050
 B. Installation of the Type B Actuators
 (1)
 Apply a layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-018) to the shanks of the bolts (9).

 (2)
 Install the actuator (7) and attach it with the washers (8) and the bolts (9).

 (3)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the washers (8) and the bolts (9).

 Subtask 27-84-49-820-051
 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 rigging gage touches the track stop and the lower forward roller.

 (3)
 If necessary, turn the actuator drive to adjust the slat.

 Subtask 27-84-49-410-051
 D. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable torque shaft (3):

 (a) (Ref. TASK 27-84-45-400-007)
 -
FOR 6027CM
 install the torque shaft 6028CM

 -
FOR 6029CM
 install the torque shaft 6028CM

 -
FOR 6035CM
 install the torque shaft 6036CM

 -
FOR 6039CM
 install the torque shaft 6038CM

 -
FOR 6045CM
 install the torque shaft 6044CM

 -
FOR 6077CM
 install the torque shaft 6078CM

 1EFF : ALL 1 27-84-49Page 415 1 1 Nov 01/01R 1 1 1CES 1

R

R
R

-
FOR 6079CM
 install the torque shaft 6078CM

 -
FOR 6085CM
 install the torque shaft 6086CM

 -
FOR 6089CM
 install the torque shaft 6088CM

 -
FOR 6095CM
 install the torque shaft 6094CM.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(26)