(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).

 1EFF : 001-049, 052-061, 101-105, 201-203, 1 27-84-63Page 426 1 1 Aug 01/05R 1 1 1CES 1

R  (13) Apply special materials: 
R  WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL_______ 
R  MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. 
R  OBEY THE MANUFACTURERS INSTRUCTIONS. 
R  PUT ON PROTECTIVE CLOTHING. 
R  DO NOT GET THEM IN YOUR MOUTH. 
R  DO NOT SMOKE. 
R  DO NOT BREATHE THE GAS. 
R  THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. 
R  GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 
R  (a) Apply SEALANTS (Material No. 09-001) to: 
R  - the nuts (4), (6), (18), (19), (20), (31), (32) and (42) 
R  - the bolt heads (11), (12), (15), (16), (17), (37), (39) and 
R  (41) 
R  - the locking plates (13) and (38). 
R  (14) Remove the BLOCK-SLAT GAPPING from the No. 9 slat track. 
R  (15) Do a check of the slat lower trailing-edge, dimension L: 
R  (a) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, 
R  installed outboard of the removed torque shaft FIN 6010CM(6060CM) 
R  (Ref. TASK 27-50-00-000-003). 
R  (b) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) 
R  to fully retract the slats. 
R  (c) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 
R  outboard of the removed torque shaft FIN 6010CM(6060CM) 
R  (Ref. TASK 27-50-00-400-003). 
R  (d) Measure the dimension L of the slat lower trailing-edge. The 
R  dimension L must be 5 mm (0.1968 in.) +/- 2 mm (0.0787 in.) at 
R  all points along the length of the slat. 
R  (Ref. Fig. 405/TASK 27-84-63-991-004) 
R  (e) The slat lower trailing-edge must not be more than 1 mm (0.0393 
R  in.) into-wind or out-of-wind. 
R  NOTE : The dimension L and the into-wind and out-of-wind____ 
R  dimensions are not adjustable. If the dimensions you 
R  measure are out of limits, you must tell the design 
R  authority at Airbus Industrie. 

R 1EFF : 001-049, 052-061, 101-105, 201-203, 1 27-84-63Page 427 1 1 May 01/05 1 1 1CES 1

R  (16) Install and adjust the closing plates (9) and (35) (Ref. TASK 27-84-
69-400-001). 
R  **ON A/C 051-051, 
R  Subtask 27-84-63-820-055-B 
R  C. Adjustment of the Slat 
R  (Ref. Fig. 401/TASK 27-84-63-991-001, 402/TASK 27-84-63-991-002, 403/TASK 
R  27-84-63-991-003, 405/TASK 27-84-63-991-004) 
R  (1) Install the BLOCK-SLAT GAPPING (98D27804020000) at the No. 9 slat 
R  track. 
R  (2) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, 
R  installed outboard of the removed torque shaft FIN 6010CM(6060CM) 
R  (Ref. TASK 27-50-00-000-003). 
R  (3) Use the ADAPTOR-DRIVE, SLAT (AND FLAP) to retract the slats until 
R  they are approximately 50.8 mm (2.0000 in.) +/- 6.35 mm (0.2500 in.) 
R  from the BLOCK-SLAT GAPPING. 
R  (4) Use the BAR-TURNING (98D27804011000) to slowly retract the slats 
R  until the BLOCK-SLAT GAPPING touches the bottom roller at the No. 9 
R  slat track. 
R  (5) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 
R  outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 
R  27-50-00-400-003). 
R  (6) Adjust the eccentric bushes (10) and (36) at the No. 1, 2, 3 and 4 
R  slat tracks to get dimension J. Refer to the table that follows. 
R 
R  NOTE : Measure dimension J above the applicable slat track.____ 
R  -------------------------------------------------------------------------------
R  | TRACK | DIMENSION J | MAXIMUM ADJUSTMENT BECAUSE OF | 
R  | NO. | | LOCKING PLATE INSTALLATION | 
R  -------------------------------------------------------------------------------
R  | 1 | 4.75 mm (0.187 in.) | + 0.25 mm (0.01 in.) - 0.25 mm (0.01 in.) | 
R  | 2 | 5.00 mm (0.196 in.) | + 0.25 mm (0.01 in.) - 0.25 mm (0.01 in.) | 
R  | 3 | 6.50 mm (0.255 in.) | + 0.25 mm (0.01 in.) - 0.25 mm (0.01 in.) | 
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(120)