(2)
Make sure that the trailing edge access-panels and the rudder fairings are removed (Ref. TASK 55-33-13-000-001) (Ref. TASK 53-55-12-000-001).
(3)
Make sure that the access platform is in position.
(4)
Make sure that the warning notices are in position in the cockpit to tell persons:
-
not to pressurize the hydraulic systems,
-
not to operate the flight controls.
Subtask 55-36-41-865-053
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 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure_________
Subtask 55-36-41-420-050
A. Install the hinge arm fittings No. 1 thru 5.
(Ref. Fig. 401/TASK 55-36-41-991-001)
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1)
If necessary, remove unwanted sealant from the hinge arm with a nonmetallic scraper.
(2)
Clean the hinge arm with CLEANING AGENTS (Material No. 11-003).
(3)
Do an inspection of the component interface and/or the adjacent area.
1EFF : ALL 1 55-36-41Page 414 1 1 Feb 01/02R 1 1 1CES 1
(4) If necessary, prepare the replacement components (Ref. ASRM 55-36-42-201).
(5) Put the hinge arm fitting (11) and the plate (9) in position and install the Hi-Lock rivets (Ref. ASRM 51-42-11-001).
(6) Put the bonding strap (7) in position and install the screw (8) (Ref. TASK 20-28-00-912-004).
(7) Apply SEALANTS (Material No. 09-016) to the edges of the hinge arm fitting (11).
NOTE : Obey the sealant Manufacturers curing time instructions before____ you apply structure paints.
(8) Apply STRUCTURE PAINTS (Material No. 16-003) to the edges of the hinge arm fitting (11).
(9) If the rudder was removed, install the rudder (Ref. TASK 27-21-41-400-001).
NOTE : Do not install the rudder unless a minimum of six hinge arm____ fittings are installed.
R (10) If the rudder was not removed, you must continue as follows:
R R (a) Make sure that the bushes (4) are in the correct condition (Ref. TASK 27-21-41-200-001).
R (b) If necessary, replace the bushes (4).
R (c) Apply SPECIAL MATERIALS (Material No. 05-002) to the bushes (4) and install the bushes (4).
NOTE : Make sure that the lower bush does not fall out.____
R (d) Install the retaining-plate (3) and the washer (2).
R (e) Apply COMMON GREASE (Material No. 04-004) to the hinge bolt (1).
R (f) Install the hinge bolt (1) and the slotted nut (5).
R (g) Use the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-322-5625) and TORQUE the slotted nut (5) to 3.0 m.daN (22.12 lbf.ft).
R (h) Use the TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 (SL90-313-5625) and install the tab washer (6) at the slotted nut (5).
Subtask 55-36-41-420-053
B. Install the hinge arm fitting at rudder bearing No. 6. (Ref. Fig. 402/TASK 55-36-41-991-002)
(1)
Put the hinge arm fitting (6) and the plate (7) in position and install the Hi-Lock rivets (Ref. ASRM 51-42-11-001).
(2)
Put the bonding strap (4) in position and install the screw (5) (Ref. TASK 20-28-00-912-004).
(3)
Apply SEALANTS (Material No. 09-016) to the edges of the hinge arm fitting (6).
NOTE : Obey the sealant Manufacturers curing time instructions before
____
you apply structure paints.
