(5)
 Make sure that the access platforms are in position at zone 334 and/or zone 344.

 Subtask 55-13-11-865-055

 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20 122VU LIGHTING/LOGO/L 2LY V03 122VU LIGHTING/LOGO/R 1LY V02 
R  Subtask 55-13-11-914-050 
R  C. Apply Sealants 
R R  (1) Apply SEALANTS (Material No. 09-005) to the mating surfaces of the panels. 
R R  (2) Apply separator agent SPECIAL MATERIALS (Material No. 05-013) along the mating surfaces of skin shells and the trailing edge ribs.
 4. Procedure_________
R  (Ref. Fig. 401/TASK 55-13-11-991-001) 
Subtask 55-13-11-420-050 
R  A. Install Access Panels 
R  (1) Install the upper trailing-edge access-panels.
 (a) Put the panel (4) in position. 
R  (b) Wet Install the screws (1), (2) and (3) with SEALANTS (Material No. 09-005). 
R R  (c) Torque the abovementioned screws to between 25 and 35 lbf.in (0.28 and 0.39 m.daN).

R  (d) Install the washers (11) and the nuts (10).
 NOTE : On access panel 334BT(LH) and/or 344BT(RH) install the____ bolt (26) through the bonding lead (25), the bracket (24), the washer (23) and the nut (22) at two positions. 
R  (2) Install the lower trailing-edge access-panels.
 (a) Put the panel (5) in position. 
R  (b) Wet install the screws (1) and (2) with SEALANTS (Material No. 09-005). 
R R  (c) Torque the abovementioned screws to between 25 and 35 lbf.in (0.28 and 0.39 m.daN). 
R  (3) Install the lower trailing-edge hinged-access-panels.
 (a) Put the access panel (6) in position. 
R  (b) Wet install the screws (7), (8) and (9) with SEALANTS (Material No. 09-005). 
R R  (c) Torque the abovementioned screws to between 25 and 35 lbf.in (0.28 and 0.39 m.daN). 
R  (d) Install the washers (11) and the nuts (10).
 NOTE : On access panel 334DB(LH) and/or 344DB(RH) install the____ bolt (26) through the bonding lead (25), the bracket (24), the washer (23) and the nut (22) at two positions. 
R  (e) Close the panel (6), and wet install the screws (2) with SEALANTS (Material No. 09-005). 
R R  (f) Torque the abovementioned screws to between 25 and 35 lbf.in (0.28 and 0.39 m.daN).
 Subtask 55-13-11-110-051 
R  B. Cleaning
 (1) Clean the gaps around the trailing edge panels with CLEANING AGENTS (Material No. 11-008).

 Subtask 55-13-11-914-051

R  C. Apply Sealants
 (1) Apply SEALANTS (Material No. 09-005) to the gaps along the mating surfaces of the trailing edge panels.
 5. Close-up________
 Subtask 55-13-11-210-051
 A. Visual Inspection
R  (1) Make sure that the work area is clean and clear of tool(s) and other items. 
Subtask 55-13-11-865-052 
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 19CE1, 19CE2, 19CE3, 15CE1, 16CE1, 15CE2, 16CE2, 2LY, 1LY. 
R  Subtask 55-13-11-081-050 
R  C. Remove Locking Devices 
R R  (1) Remove the PIN-SIDE STICK LOCKING from the CAPT and from the F/O side stick controllers. 
R  Subtask 55-13-11-942-050 
R  D. Remove Ground Equipment 
R  (1) Remove the access platform(s). 
R  (2) Remove the warning notice(s).

 TRIMMABLE HORIZONTAL STABILIZER TIPS - DESCRIPTION AND OPERATION
________________________________________________________________
 1. General.________
 A. The tips of the trimmable horizontal stabilizer (THS) are the left-hand (LH) and right-hand (RH) outer fairings.
 2. Description.____________ (Ref. Fig. 001)
 A. THS Tips.
 -The tips are made of light alloy. Ribs, which are made of light alloy, make them stronger. The tips are attached to the leading edge rib 25 and to the upper and lower shells of the spar box. Countersunk screws attach them to these components.
 B. Tip Electrical Bonding.
 -For electrical bonding there are bonding plates of light alloy along the mating surfaces of the tips. Each tip has a static discharger.
　
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