A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(29)

 2.

-
the MCDU shows the SLAT SYSTEM DATAsubmenu.

-
the MCDU shows the PPU DATA page(s).

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 Subtask 27-84-49-865-055
 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 Subtask 27-84-49-010-052
 E. Get Access
 (1)
 Put an adjustable access platform in position below the applicable torque shaft.

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

 (a) (Ref. TASK 27-84-45-000-006)
 -
FOR 6037CM
 remove the torque shaft FIN 6036CM

 -
FOR 6041CM
 remove the torque shaft FIN 6040CM

 -
FOR 6087CM
 remove the torque shaft FIN 6086CM

 -
FOR 6091CM
 remove the torque shaft FIN 6090CM.

 (b) (Ref. TASK 27-84-45-000-011)
 -
FOR 6033CM
 remove the torque shaft FIN 6032CM

 -
FOR 6083CM
 remove the torque shaft FIN 6082CM.

 (3)
 Remove the applicable torque shaft (1):

 (a) (Ref. TASK 27-84-45-000-012)
 -
FOR 6033CM
 remove the torque shaft FIN 6034CM

 -
FOR 6083CM
 remove the torque shaft FIN 6084CM.

 (b) (Ref. TASK 27-84-45-000-006)
 -
FOR 6037CM
 remove the torque shaft FIN 6038CM

 -
FOR 6041CM

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 remove the torque shaft FIN 6042CM
 -
FOR 6087CM remove the torque shaft FIN 6088CM

 -
FOR 6091CM remove the torque shaft FIN 6092CM.

 (4) Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) 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.
 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)
 **ON A/C ALL
 Subtask 27-84-49-020-051
 A. Removal of the Type B Actuators
 (1)
 Hold the actuator (2) and remove the bolts (4) and the washers (5). Remove the actuator (2).

 (2)
 If you remove both actuators from a slat, install a TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12) (98D27804007000) in each pinnion after each actuator (2) is removed or the slat will extend.

 TASK 27-84-49-400-002
 Installation of the Type B Actuators 6033CM(6083CM)/6037CM(6087CM)/
 6041CM(6091CM)

 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
R R Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice(s)
 98D27804012000 1 GAGE-RIGGING

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
 GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
 Material No. 05-063 USA MIL-A-907E
 NEVERSEEZ NICKEL SPECIAL GRADE (Ref. 20-31-00)

 Material No. 09-018  USA AMS 3267/3
 CORROSION INHIBITING LOW ADHESION SEALANT
 (Ref. 20-31-00)

 Material No. 09-019  USA AMS 3267/3
 LOW ADHESION CORROSION INHIBITING SEALANT
 (Ref. 20-31-00)

 Material No. 11-026  GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)