(c)
 Move the fairing (with a hand force of between 23 kg (51 lb) and 27 kg (60 lb)) to the right. Do not move the straight edge.

 (d)
 Measure the distance between the straight edge and the fairing to get dimension Y.

 (e)
 Compare the dimension Y with the maximum values in table 601.

 ----------------------------------------------------------------| Fairing | Track 2 | Track 3 | Track 4 | |--------------|---------------|---------------|---------------| | Dimension Y | 11.4 mm | 4.8 mm | 4.0 | | | (0.449 in.) | (0.189 in.) | (0.158 in.) | ----------------------------------------------------------------
Table 601
 (f) If dimension Y is not correct: 1 Remove the applicable fairing (Ref. TASK 57-55-11-000-001).
_ 2 Refer to the applicable CMM procedure (Ref. CMM 575512) or
_ (Ref. CMM 575513) or (Ref. CMM 575514), and replace worn or damaged components.
 3 Install the applicable serviceable fairing (Ref. TASK 57-55-
_
 11-400-001).

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-11Page 606 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  **ON A/C 301-399, 
R  Subtask 57-55-11-220-060-A 
R  A. Check of the Flap Track Fairing Lateral Movement 
R  (1) Measure the lateral movement of each movable fairing as follows: 
R  (a) Move the fairing (with a hand force of between 23 kg (51 lb) and 
R  27 kg (60 lb)) to the left. 
R  (b) Put a straight edge in a vertical position against the flap 
R  trailing edge adjacent to the fairing. Make sure you do not move 
R  the straight edge. 
R  (c) Move the fairing (with a hand force of between 23 kg (51 lb) and 
R  27 kg (60 lb)) to the right. Do not move the straight edge. 
R  (d) Measure the distance between the straight edge and the fairing to 
R  get dimension Y. 
R  (e) Compare the dimension Y with the maximum values in table 601. 
R  ----------------------------------------------------------------
R  | Fairing | Track 2 | Track 3 | Track 4 | 
R  |--------------|---------------|---------------|---------------| 
R  | Dimension Y | 11.4 mm | 4.8 mm | 4.0 | 
R  | | (0.449 in.) | (0.189 in.) | (0.158 in.) | 
R  ----------------------------------------------------------------
R  Table 601 
R  (f) If dimension Y is not correct: 
R  1 Remove the applicable fairing (Ref. TASK 57-55-11-000-001)._ 
R  2 Refer to the applicable CMM procedure (Ref. CMM 575515) or_ 
R  (Ref. CMM 575516) or (Ref. CMM 575517), and replace worn or 
R  damaged components. 
R  3 Install the applicable serviceable fairing (Ref. TASK 57-55-_ 
R  11-400-001).

R **ON A/C ALL
 5. Close-up
________
 Subtask 57-55-11-865-067

 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 57-55-11-860-068
 B. Aircraft Configuration
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Retract the flaps (Ref. TASK 27-50-00-866-009).
 Subtask 57-55-11-942-059

 C. Removal of Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the warning notice(s).

 (3)
 Remove the safety barriers.

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 MISCELLANEOUS (EG : DRAINS) - DESCRIPTION AND OPERATION
_______________________________________________________ _______
1. General
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 001)
 **ON A/C 301-399,

 (Ref. Fig. 001A)
 **ON A/C ALL

 Liquid from the trailing edge flows into the flap track fairings. Liquid from the slat track 9 flows into the outer fairing. The liquid which collects in the fairings flows out through drain-holes in the lower surface of the fairing.

 Drains in the L/E and T/E Devices
 Figure 001

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-59-00Page 2 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  Drains in the T/E Devices 
R  Figure 001A
 1EFF :  301-399,  1  57-59-00 Page 3 
1  1  May 01/04
 1  1
 1CES  1

 MISCELLANEOUS (EG : DRAINS) - INSPECTION/CHECK
　
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