Subtask 27-84-66-820-055
D. Adjustment of the Slat
(1)
Install the BLOCK-SLAT GAPPING (98D27804020000) at the No. 9 slat track.
(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 ADAPTOR-DRIVE, SLAT (AND FLAP) (98D27804001000) to retract the slats until they are approximately 50.80 mm (2.0000 in.) +/- 6.35 mm (0.2500 in.) from the BLOCK-SLAT GAPPING.
(4)
Use the BAR-TURNING (98D27804011000) to slowly, retract the slats until the BLOCK-SLAT GAPPING touches the bottom roller at the No. 9 slat track.
(5)
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).
(6)
Adjust the eccentric bushes (22) and (44) at the Nos. 9 and 10 slat tracks to get dimension L. Refer to the table that follows.
NOTE : Measure the dimension L above the applicable slat track.
____
-------------------------------------------------------------------------------| TRACK | DIMENSION L | MAXIMUM ADJUSTMENT BECAUSE OF | | NOS. | | LOCKING PLATE INSTALLATION | -------------------------------------------------------------------------------| 9 | 4.00 mm (0.1575 in.) | +0.25 mm (0.01 in.) -0.25 mm (0.01 in.) | | 10 | 3.50 mm (0.1377 in.) | +0.25 mm (0.01 in.) -0.25 mm (0.01 in.) | -------------------------------------------------------------------------------
(7)
Install the locking plates (18) and (41) and the nuts (19) and (42).
(8)
TORQUE the nuts (31) and (45) to between 1.95 and 2.2 m.daN (14.38 and 16.22 lbf.ft).
(9)
Safety the nuts (31) and (45) with the new cotter pins (25).
(10) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM (FIN 6060CM) (Ref. TASK 27-50-00-000-003).
1EFF : ALL 1 27-84-66Page 416 1 1 Nov 01/03R 1 1 1CES 1
(11)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully extend the slats.
(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 special materials:
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.
(a) Apply SEALANTS (Material No. 09-001) to:
-
the nuts (24), (27), (31), (47), (49), (53), (54) and (45)
-
the bolt heads (20), (21), (30), (39), (40), (43), (51) and
(52)
-
the locking plates (18) and (41).
(14) Remove the BLOCK-SLAT GAPPING from the No. 9 slat track.
Subtask 27-84-66-820-056
E. Adjustment of the Stop-Bolt
(1)
Examine the hold-down pad-head for wear. The maximium wear limit is
1.0 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 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).
1EFF : ALL 1 27-84-66Page 417 1 1 Nov 01/03R 1 1 1CES 1
(5)
Turn the stop-bolt (63) until it touches the hold-down pad.
(6)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft 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 (63).
(10)
Remove the stop-bolt (63).
(11)
The value of dimension S is between 0.2 mm (0.0078 in.) and 0.25 mm (0.0098 in.). Subtract the dimension S from the dimension R. The difference is the total thickness of the washers (64) and the washer
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(142)
