(2)
 Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU.

 (3) Fully retract the slats (Ref. TASK 27-80-00-866-005). Subtask 57-40-00-710-050
 C. Test
 (1) Do an operational test of the slat system (Ref. TASK 27-84-00-710-001).
 Subtask 57-40-00-942-050
 D. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 TASK 57-40-00-440-001

 Restoration of the Aircraft for Flight After Damage to Rubber Seal Under Slats
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 Refer to the CDL TASK: 27-7
 Rubber Seal under Slats

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific warning notice
 No specific adjustable access platform 3.5 m (11 ft. 6 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground
 27-80-00-866-005 Retracting the Slats on the Ground
 27-84-00-710-001 Operational Test of the Slat System
 CMM 57-42-21 (for corrective action)
 CMM 57-43-21 (for corrective action)
 CMM 57-44-21 (for corrective action)
 CMM 57-45-21 (for corrective action)
 CMM 57-46-21 (for corrective action)

 3. Job Set-up
__________

 Subtask 57-40-00-941-051
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice in the cockpit to tell persons not to operate the slat controls.

 Subtask 57-40-00-010-051
 B. Get Access
 (1)
 Fully extend the slats (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on panel 114VU.

 (3)
 Put the adjustable access platform in position below the applicable zone 510(610).

 Subtask 57-40-00-865-052
 C. 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
 4. Procedure
_________ Subtask 57-40-00-440-050
 A. Restoration of the Aircraft for Flight After Damage to Rubber Seal Under Slat
 (1) Remove and replace the damaged rubber seal:
 -
for the slat No.1, refer to the Component Maintenance Manual (Ref. CMM 57-42-21)

 -
for the slat No.2, refer to the Component Maintenance Manual (Ref. CMM 57-43-21)

 -
for the slat No.3, refer to the Component Maintenance Manual (Ref. CMM 57-44-21)

 -
for the slat No.4, refer to the Component Maintenance Manual (Ref. CMM 57-45-21)

 -
for the slat No.5, refer to the Component Maintenance Manual (Ref. CMM 57-46-21).

 5. Close-up
________ Subtask 57-40-00-865-053
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 57-40-00-410-051
 B. Close Access
 (1)
 Remove the access platform(s).

 (2)
 Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the slat/flap control lever on panel 114VU.

 (3) Fully retract the slats (Ref. TASK 27-80-00-866-005). Subtask 57-40-00-710-051
 C. Test
　
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