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R  (c) Install the new tab washer (4) and the new nut (3).
 (d) TORQUE the nut (3) to between 1.2 and 1.5 m.daN (106.19 and 132.74 lbf.in). Make sure that you can safety the nut (3) with the tab washer (4).
 (e) Safety the nut (3) with the tab washer (4).
 (f) Apply a bead of SEALANTS (Material No. 09-016) to the nut (3), the tab washer (4) and the adjacent slat structure. Make sure that the sealant does not go onto the internal surfaces of the spherical bearing (5).
 Subtask 57-46-21-410-050
 C. Preparation for Test
 (1) Install the applicable No. 5 slat (Ref. TASK 27-84-67-400-002).
 (2) Make sure that the work area is clean and clear of tool(s) and other items.

 

 Subtask 57-46-21-865-052
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 57-46-21-710-050
 E. Test
 (1) Do an operational test of the slat system (Ref. TASK 27-84-00-710-001).
 5. Close-up
________ Subtask 57-46-21-942-050
 A. Removal of Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the warning notice(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 

 TRAILING EDGE AND TRAILING EDGE DEVICES - 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
 The trailing edge is aft of the rear spar of the wing box, between the wing root and the wing tip. The trailing edge has a fixed structure and eight movable control surfaces.
 2. Component Location
__________________
 The fixed structure (Ref. 57-51-00) is between RIB1 and RIB27. It has attachments for the movable control surfaces and their drive mechanisms. The control surfaces are:
 -
the inboard (double-slotted) flap (Ref. 57-52-00)

 -
the outboard (double-slotted) flap (Ref. 57-53-00)

 -
the aileron (Ref. 57-60-00)

 -
the spoilers 1 thru 5 (Ref. 57-70-00 thru 57-75-00).

 3. Description
___________
 A. Trailing Edge Structure
 The main components of the trailing edge structure are:
 -
the overwing and underwing panels

 -
the fixed shroud and shroud box

 -
the rear false spar.
 The fixed structure also has attachments for the:

 

 -main landing gear (Ref 57-26-00)
 -movable control surfaces
 -engine pylon (Ref 57-26-00).

 Trailing Edge and Trailing Edge Devices
 Figure 001

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-50-00Page 2 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  Trailing Edge and Trailing Edge Devices 
R  Figure 001A
 1EFF :  301-399,  1  57-50-00 Page 3 
1  1  May 01/04
 1  1
 1CES  1

 

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,

 B. Trailing Edge Devices
 There are eight trailing edge devices which are movable control surfaces. They are:
 -inboard flap (Ref. 57-51-00)
 - outboard flap (Ref. 57-52-00)

 -an aileron (Ref. 57-60-00)

 -five spoilers (Ref. 57-70-00).
 The inboard flap and the outboard flap are of the fowler type. Each flap
 is attached to two carriages. There is an interconnecting strut between
 the flaps (Ref. 27-51-00).

 **ON A/C 301-399,
 B. Trailing edge devices
 There are eight trailing edge devices which are movable control surfaces. They are:
 -
the inboard (double-slotted) flap

 -
the outboard (double-slotted) flap

 -
the aileron

 -
the spoilers 1 thru 5.

 The trailing edge devices are connected to brackets installed on the fixed structure. The inboard and outboard flaps are a 'double-slotted' type, with in-set tabs to increase the control surface area. The flaps are connected together by an interconnecting strut and a 'Z' coupling.

 TRAILING EDGE - DESCRIPTION AND OPERATION
_________________________________________
 1. General
_______
 The trailing edge structure is aft of the rear spar between the wing root
 and the wing tip.
 2. Component Location
　
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