(65) that you must install.
(12)
Install the washers (64) and (65) to give the correct dimension S.
(13)
Install and tighten the stop-bolt (63).
(14)
Safety the stop-bolt (63) to the hold-down bracket (66) 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 27-84-66-820-057
F. Adjustment of the Closing-Plate
(1)
Install the slat closing plate (Ref. TASK 27-84-69-400-001).
(2)
Measure the dimension N of the slat lower trailing-edge. The dimension N must be 5.0 mm (0.1968 in.) +/- 2.0 mm (0.0787 in.) at all points along the length of the slat. (Ref. Fig. 404/TASK 27-84-66-991-004)
(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 N 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.
R **ON A/C 051-051,
R Subtask 27-84-66-820-057-A
R F. Adjustment of the Closing-Plate
R (1) Install the slat closing plate (Ref. TASK 27-84-69-400-001).
R (2) Measure the dimension N of the slat lower trailing-edge. The
R dimension N must be 5.0 mm (0.1968 in.) +/- 2.0 mm (0.0787 in.) at
R all points along the length of the slat.
R (Ref. Fig. 404/TASK 27-84-66-991-004)
R (3) The slat lower trailing-edge must not be more than 1.0 mm (0.0393
R in.) into-wind or out-of-wind.
R NOTE : The dimension N and the into-wind and out-of-wind dimensions____
R are not adjustable. If the dimensions you measure are out of
R limits, you must tell the design authority at Airbus
R Industrie.
R (4) Use the GAGE-GO NO GO (SLATS) (98D27804013000) to check the clearance
R is correct between the inboard and outboard buffer blocks and the
R leading edge of the 'D' nose.
R **ON A/C ALL
Subtask 27-84-66-820-058
G. 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 and the Nos. 4 and 5 slats:
(a)
Remove the blanking-covers from the anti-icing ducts.
(b)
Install the flexible tubes (4) with the clamps (5).
(c)
Install the weather seal (2). Make sure that the end of the weather seal (2) is aligned with the slat lower trailing-edge.
(d)
Install the stops (3) and attach them with the screws (1).
(e)
Attach the bonding strap (7) to the bonding tag with the bolt (9), the washer (8) and the nut (6) (Ref. TASK 20-28-00-912-004).
Subtask 27-84-66-860-052
H. Aircraft Maintenance Configuration
(1)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the slats to the zero position.
(2)
Energize the ground service network (Ref. TASK 24-42-00-861-001).
(3)
On the MCDU display, make sure that the PPU DATA page is shown (to monitor the slats PPU position).
(4)
If necessary, use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to move the slat drive shaft until the PPU data (on the MCDU) 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 angle values must agree +/- 1.3 deg.
-
the LH APPU and the RH APPU angles must agree +/- 0.45 deg.
(5)
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).
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱8(143)
