(2)
Put the access platform in position at Zone 326.
R (3) Remove the access panels 325EL, 325DL, 325ER, 325DR (Ref. TASK 55-33-R 13-000-001).
(4)
Remove the rudder support strut (Ref. TASK 55-36-48-000-001).
(5)
Remove the hinge arm fitting (Ref. TASK 55-36-41-000-001).
4. Procedure
_________
Subtask 55-46-11-020-050
A. Remove the rudder hinge bearing No. 6.
(Ref. Fig. 401/TASK 55-46-11-991-001)
(1)
Release both tabs of the retaining ring (3).
(2)
Remove the ring nut (4) with the TOOL SET - R/I RUDDER BEARING NO. 6.
(3)
Remove the bearing (2).
Rudder Hinge Bearing No. 6
Figure 401/TASK 55-46-11-991-001
1EFF : ALL 1 55-46-11 Page 404
1 1 Feb 01/98
1 1
1CES 1
TASK 55-46-11-400-001
Installation of Rudder Hinge Bearing No.6
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS
_______ ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
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 nonmetallic scraper No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) 98D55307528000 1 TOOL SET - R/I RUDDER BEARING NO. 6
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-21-00-720-002 Functional Test of the Rudder Mechanical Control 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 55-33-13-000-001 Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-400-001 Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-36-41-000-001 Removal of the Hinge Arm Fittings No. 1 thru No. 7 55-36-41-400-001 Installation of the Hinge Arm Fittings No. 1 thru No.
7
55-36-48-000-001 Removal of the Rudder Support Strut
55-36-48-400-001 Installation of the Rudder Support Strut
55-46-11-991-001 Fig. 401
3. Job Set-up
__________
Subtask 55-46-11-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure the warning notice is in position in the cockpit to tell persons not to operate the flight controls.
(2)
Make sure that hydraulic systems are depressurized
(Ref. TASK 29-00-00-864-001).
(3)
Make sure that the access platform is in position at Zone 326.
(4)
Make sure that the access panels 325EL, 325DL, 325ER, and 325DR are removed (Ref. TASK 55-33-13-000-001).
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