_________
(Ref. Fig. 401/TASK 55-36-48-991-001) Subtask 55-36-48-020-050
A. Remove the Rudder Support Strut
(1)
Install the FIXTURE - VERT. STABILIZER/RUDDER (98D27207508000).
(2)
Remove and discard the cotter pins (2).
(3)
Remove the lockwashers (5) and remove the nuts (4) with a groove nut wrench.
(4)
Remove the washers (3), the bolts (1) and the rudder support strut (9).
Rudder Support Strut
Figure 401/TASK 55-36-48-991-001
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TASK 55-36-48-400-001
Installation of the Rudder Support Strut
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific safety wire MS 20995-C25
98D27207508000 1 FIXTURE - VERT. STABILIZER/RUDDER
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
cotter pin 27-21-04 15A-240
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-21-00-710-001 29-00-00-864-001
R 55-33-13-010-002 R R R 55-33-13-410-002 R R
55-36-48-991-001
3. Job Set-up
__________ Operational Test of the Centering Spring RodPut the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BRFig. 401
R Subtask 55-36-48-860-050-A
R A. Aircraft Maintenance Configuration
R (1) Make sure that the Green, Blue and/or Yellow hydraulic system is(are)
R depressurized (Ref. TASK 29-00-00-864-001).
R (2) Make sure that the vertical and horizontal stabilizer are safe.
R (3) Make sure that the access panel 325DL is open (Ref. TASK 55-33-13-
R 010-002).
R (4) Make sure that the access panels 325EL, 325ER and 325DR are removed R (Ref. TASK 55-33-13-010-002). R (5) Make sure that the warning notice is in position in the cockpit to
R tell persons not to operate the flight controls. R (6) Make sure that the access platform is in position.
Subtask 55-36-48-865-051
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/FAC2/28VDC 5CC2 M19 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
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