(11)
The value of dimension R is between 0.2 mm (0.0078 in.) and 0.25 mm (0.0098 in.). Subtract the dimension R from the dimension Q. The difference is the total thickness of the washers (66) and the washer
(67) that you must install.
(12)
Install the washers (66) and (67) to give the correct dimension R.
(13)
Install and tighten the stop-bolt (65).
1EFF : ALL 1 27-84-65Page 417 1 1 Nov 01/03R 1 1 1CES 1
(14) Safety the stop-bolt (65) to the hold-down bracket (68) with MISCELLANEOUS (Material No. 19-010).
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-84-65-820-057
E. Adjustment of the Closing Plate
(1)
Install the slat closing plate (Ref. TASK 27-84-69-400-001).
(2)
Measure the dimension M of the slat lower trailing-edge. The dimension M must be 5.0 mm (0.1968 in.) +/- 2.0 mm (0.0787 in.) at all points along the length of the slat.
(3)
The slat lower trailing-edge must not be more than 1.0 mm (0.0393 in.) into-wind or out-of-wind.
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.
(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.
**ON A/C 051-051,
Subtask 27-84-65-820-057-A
E. Adjustment of the Closing Plate
(1)
Install the slat closing plate (Ref. TASK 27-84-69-400-001).
(2)
Measure the dimension M of the slat lower trailing-edge. The dimension M must be 5.0 mm (0.1968 in.) +/- 2.0 mm (0.0787 in.) at all points along the length of the slat.
(3)
The slat lower trailing-edge must not be more than 1.0 mm (0.0393 in.) into-wind or out-of-wind.
NOTE : The dimension M and the into-wind and out-of-wind dimensions
____ are not adjustable. If the dimensions you measure are out of
R R 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 ALL
Subtask 27-84-65-820-058
F. Slat-to-Slat Interface Adjustment
(1) 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).
(2) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully extend the slats.
(3) 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).
(4) At the interface of the Nos. 3 and 4 slats only:
(a) Remove the blanking-covers from the anti-icing ducts.
(b) Install the flexible tube (4) with the clamps (5).
(5) At the interface of the Nos. 2 and 3 slats and the Nos. 3 and 4 slats:
(a) Install the weather seal (2). Make sure that the end of the weather seal is aligned with the slat lower-trailing-edge.
(b) Install the stops (3) and attach them with the screws (1).
(c) Attach the bonding strap (7) with the bolt (9), the washer (8) and the nut (6) (Ref. TASK 20-28-00-912-004).
Subtask 27-84-65-860-052
G. Aircraft Maintenance Configuration
(1)
Install the applicable telescopic duct (Ref. TASK 30-11-41-400-001).
(2)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the slats.
(3)
Energize the ground service network (Ref. TASK 24-42-00-862-001).
(4)
On the MCDU display, make sure that the PPU DATA page is shown (to monitor the slats PPU position).
(5)
If necessary, use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to move the slat drive shaft until the PPU data shows the same values as recorded in Para. 3.B.:
-
the FPPU angle value must agree +/- 0.1 deg.
-
the APPU angle value must agree +/- 0.1 deg.
-
the FPPU and APPU angles must agree +/- 1.3 deg.
-
the LH APPU and the RH APPU angles must agree +/- 0.45 deg.
(6)
De-energize the ground service network (Ref. TASK 24-42-00-862-001).
(7)
Remove the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) from the slat drive shaft.
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