B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-013 D TV-53-3507/73 RELEASE AGENT (OBSOLETE USE 05-013A) (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 55-42-13-991-001 Fig. 401
3. Job Set-up
__________
Subtask 55-42-13-865-051
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
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Subtask 55-42-13-860-051
B. Aircraft Maintenance Configuration
(1)
Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(2)
Make sure that the warning notices are position to tell persons not to pressurize the hydraulic systems:
-In the cockpit on the hydraulic section 40VU of the overhead panel,
-On the ground service panels of the hydraulic systems.
(3)
Make sure that the warning notices are in position in the cockpit to tell persons not to operate the flight controls.
(4)
Make sure that the adjustable access platform is in position at the leading edge of the rudder.
4. Procedure
_________
(Ref. Fig. 401/TASK 55-42-13-991-001) Subtask 55-42-13-210-050
A. Preparation for Installation WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(2)
Examine the anchor nuts on the access panel (3) for good condition.
(3)
Do an inspection of the component interface and/or the adjacent area.
(4)
Clean the component interface and/or the adjacent area, with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
(5)
Apply the SPECIAL MATERIALS (Material No. 05-013) to the mating surface of the access panel (3) as necessary.
(6)
Apply the SEALANTS (Material No. 09-005) on the mating surfaces of the rudder leading edge (1) as necessary.
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Subtask 55-42-13-420-050
B. Installation of the Access Panel 326CT at the Rudder Attach Fitting No. 7
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Put the access panel (3) in position at the rudder leading edge (1) and install the screws (2).
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE
_______
SPECIAL MATERIAL.
THIS MATERIAL IS DANGEROUS.
(3) Apply the SEALANTS (Material No. 09-019) into the joints between the access panel (3) and the rudder leading edge (1).
5. Close-up
________ Subtask 55-42-13-860-052
A. Put the aircraft back to the serviceable condition.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(4) Remove the warning notice(s). Subtask 55-42-13-865-052
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