A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(130)_航空信息_民用航空_通用航空

(54)

-
the locking plates (28) and (43).

(14) Remove the BLOCK-SLAT GAPPING from the No. 9 slat track.
Subtask 27-84-64-820-056
D. Adjustment of the Stop-Bolt
(Ref. Fig. 404/TASK 27-84-64-991-004)

(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)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the slats.

(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 (67) until it touches the hold-down pad.

1EFF : ALL 1 27-84-64Page 422 1 1 Nov 01/03R 1 1 1CES 1

(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).

(7)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully extend the slats.

(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 R under the head of the stop-bolt (67).

(10)
Remove the stop-bolt (67).

(11)
The value of dimension S is between 0.37 mm (0.0145 in.) and 0.42 mm (0.0165 in.). Subtract the dimension S from the dimension R. The difference is the total thickness of the washers (68) and the washer

(69) that you must install.

(12)
Install the washers (68) and (69) to give the correct dimension S.

(13)
Install and tighten the stop-bolt (67).

(14)
Safety the stop-bolt (67) to the hold-down bracket (70) with lockwire, corrosion resistant steel 0.8 mm (0.032 in) dia.

R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-84-64-820-057
E. Adjustment of the Closing Plate
**ON A/C 001-049, 052-061, 101-105, 201-203,

(Ref. Fig. 401/TASK 27-84-64-991-002) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-84-64-991-002-A)R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,

(Ref. Fig. 402/TASK 27-84-64-991-003, 404/TASK 27-84-64-991-004)
(1)
Install the 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 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 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.
**ON A/C 051-051,
Subtask 27-84-64-820-057-A
E. Adjustment of the Closing Plate (Ref. Fig. 401/TASK 27-84-64-991-002, 402/TASK 27-84-64-991-003, 404/TASK 27-84-64-991-004)
(1)
Install the 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 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 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.

R **ON A/C 001-049, 051-061, 101-105, 201-203,
Subtask 27-84-64-420-053
F. Continue with the Installation Procedure (Ref. Fig. 401/TASK 27-84-64-991-002, 403/TASK 27-84-64-991-001)
(1)
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.