53-53-11Page 402
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
(Ref. Fig. 401/TASK 53-53-11-991-001) Subtask 53-53-11-020-050
A. Removal:
(1)
Remove the nut (5), the screw (2) and the washer (3).
(2)
Remove the bonding straps (4).
(3)
Remove and discard the cotter pins (11).
(4)
Remove the nuts (12) and the washers (10).
(5)
Identify each support strut (1).
(6)
Remove the bolts (9), the washers (8) and the support strut (1).
(7)
Remove the bushes (6) and (7).
EFF : ALL
53-53-11Page 403
Horizontal Support Struts
Figure 401/TASK 53-53-11-991-001
EFF : ALL 53-53-11 Page 404
Feb 01/98
CES
TASK 53-53-11-400-001
Installation of the Horizontal Support Struts between STA3531/FR74 and STA3655/FR77
NOTE : The installation of one support strut is given. The procedure is the
____ same for the other support struts.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
cotter pins 53-53-04 01 -040
EFF : ALL
53-53-11Page 405
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage
R and in the Wings (this does not include the tanks)-29-10-00-864-001 Depressurize the Green Hydraulic System 29-10-00-864-002 Depressurize the Yellow Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound 53-53-11-991-001 Fig. 401
3. Job Set-up
__________
Subtask 53-53-11-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft is in the same configuration as for the removal task.
(2)
Make sure that the warning notice is in position to tell persons not to move the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______ BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
Subtask 53-53-11-864-053
B. Make sure that the Green, Yellow and Blue hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-00-864-003).
EFF : ALL
53-53-11Page 406
Subtask 53-53-11-865-052
C. 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/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
R 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 R 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 R 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 R
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