NOTE : Measure the dimension L above the applicable slat track.
____
-------------------------------------------------------------------------------| TRACK | DIMENSION L | MAXIMUM ADJUSTMENT BECAUSE OF | | NOS. | | LOCKING PLATE INSTALLATION | -------------------------------------------------------------------------------| 11 and 12 | 2.75 mm (0.1082 in.) | + 0.25 mm (0.01 in.) - 0.25 mm (0.01 in.)| -------------------------------------------------------------------------------
(7) Install the locking plates (33) and (57) and the nuts (34) and (58).
1EFF : ALL 1 27-84-67Page 420 1 1 Nov 01/03R 1 1 1CES 1
(8)
TORQUE the nuts (35) and (47) to between 1.95 and 2.2 m.daN (14.38 and 16.22 lbf.ft).
(9)
Safety the nuts (35) and (47) with the new cotter pins (27).
(10)
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).
(11)
Manually extend the slats to the fully extended position.
(12)
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).
(13)
Apply SEALANTS (Material No. 09-001) to:
-
the nuts (26), (31), (35), (43), (44), (45), (46) and (47)
-
the bolt heads (18), (22), (32), (48), (49), (54), (55) and (56)
-
the locking plates (33) and (57).
(14)
Remove the BLOCK-SLAT GAPPING from the No. 9 slat track.
Subtask 27-84-67-820-058
E. Adjustment of the Stop-Bolt
(1)
Examine the hold-down pad-head for wear. The maximium wear limit is 1 mm (0.0393 in.) or an overall head thickness of 2.5 mm (0.0984 in.). Replace the hold-down pad if the head is worn more than these specified limits.
(2)
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).
(3)
Manually retract the slats to the datum zero position.
(4)
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).
(5)
Turn the stop-bolt (70) until it touches the hold-down pad (73).
(6)
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).
1EFF : ALL 1 27-84-67Page 421 1 1 Nov 01/03R 1 1 1CES 1
(7)
Manually extend the slats to the fully extended position.
(8)
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).
(9)
Measure the dimension Q under the head of the stop-bolt (70).
(10)
Remove the stop-bolt (70).
(11)
The value of dimension R is between 0.20 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 (71) and the washer
(72) that you must install.
(12)
Install the washers (71) and (72) to give the correct dimension R.
(13)
Install and tighten the stop-bolt (70).
(14)
Safety the stop-bolt (70) to the hold-down bracket (73) 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 27-84-67-820-059
F. Closing-Plate Clearance
(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 mm (0.1968 in.) +/- 2 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 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.
R **ON A/C 051-051,
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱8(149)
