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R  Subtask 27-84-67-820-059-A 
R  F. Closing-Plate Clearance 
R  (1) Install the slat closing plate (Ref. TASK 27-84-69-400-001). 
R R R  (2) Measure the dimension M of the slat lower trailing-edge. The dimension M must be 5 mm (0.1968 in.) +/- 2 mm (0.0787 in.) at all points along the length of the slat. 
R R  (3) The slat lower trailing-edge must not be more than 1 mm (0.0393 in.) into-wind or out-of-wind. 
R R R R  NOTE : The dimension M and the into-wind and out-of-wind dimensions____ are not adjustable. If the dimensions you measure are out of limits, you must tell the design authority at Airbus Industrie. 
R R R  (4) Use the GAGE-GO NO GO (SLATS) (98D27804013000) to check the clearance is correct between the inboard and outboard buffer blocks and the leading edge of the 'D' nose. 
R  **ON A/C 001-049, 051-061, 101-105, 201-203,
 Subtask 27-84-67-420-053-A
 G. Continue with the Installation Procedure
 (1) At the slat-to-slat interface connection:
 (a) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003).
 (b) Manually extend the slats to the fully extended position.
 (c) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003).
 (d) Remove the blanking covers and connect the flexible tube (4) with the clamps (5).
 (e) Install the weather seal (2). Make sure that the end of the weather seal is aligned with the slat lower trailing-edge.
 (f) Install the stops (3) and attach them with the screws (1). 

R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-84-67Page 423 1 1 May 01/05 1 1 1CES 1

 (g) Attach the bonding strap (7) with the bolt (9), the washer (8) and the nut (6) (Ref. TASK 20-28-00-912-004).
 (2) At the slat-to-track interface connection:
 (a)
 Remove the nut (19) and the washer (20) from the bolt (24).

 (b)
 Install the bonding strap (21), the washer (20) and the nut (19) on the bolt (24) (Ref. TASK 20-28-00-912-004).

 (c) Safety the bolts (24) with MISCELLANEOUS (Material No. 19-010). R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 Subtask 27-84-67-420-053-B
 G. Continue with the Installation Procedure
 (1)
 At the slat-to-slat interface connection:

 (a)
 Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003).

 (b)
 Manually extend the slats to the fully extended position.

 (c)
 Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003).

 (d)
 Remove the blanking covers and connect the flexible tube (4) with the clamps (5).

 (e)
 Install the weather seal (2). Make sure that the end of the weather seal is aligned with the slat lower trailing-edge.

 (f)
 Install the stops (3) and attach them with the screws (1).

 (g)
 Attach the bonding strap (7) with the bolt (9), the washer (8) and the nut (6) (Ref. TASK 20-28-00-912-004).

 

 (2)
 At the slat-to-track interface connection:

 (a)
 Remove the nut (19) and the washer (20) from the bolt (24).

 (b)
 Install the bonding strap (21), the washer (20) and the nut (19) on the bolt (24) (Ref. TASK 20-28-00-912-004).

 (c)
 Safety the bolts (24) with MISCELLANEOUS (Material No. 19-010).

 

 

 **ON A/C ALL
 Subtask 27-84-67-820-060
 H. Seal Adjustment after Adjustment of a New Slat
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 (1)
 Remove the screws (83), the support assembly (84) and the seal (85).

 (2)
 Apply a layer of SEALANTS (Material No. 09-016) to the screws (83).

 (3)
 While the sealant is still wet, install the seal (85) and the support assembly (84) with the screws (83). Tighten the screws by hand.

 (4)
 Adjust the seal (85) to touch the wing tip structure over its full length.
　
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