-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notices
No specific access platform 4.0 m (13 ft. 1 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-080-002 Removal of the Flap/Slat Control-Lever Locking Tool
(98D27803000000) R 57-51-37-960-001 Replacement of the Lower Trailing Edge Access Panel R Seals
57-51-37-991-003 Fig. 401
3. Job Set-up
__________
Subtask 57-51-37-941-053
A. Safety Precautions
(1)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed on the flap/slat control lever.
(2)
Make sure that the warning notices are in position in the cockpit to tell persons not to operate the flaps or slats.
(3) Make sure that the safety barriers are in position.
Subtask 57-51-37-860-050
B. Aircraft Maintenance Configuration
(1) Make sure that the access platform is in position below the applicable zone 573(673).
4. Procedure
_________
Subtask 57-51-37-420-050
A. Preparation for Installation
(1)
Clean the component interfaces and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
If the access panel seal is damaged, replace it (Ref. TASK 57-51-37-960-001).
Subtask 57-51-37-420-051
B. Installation of the Access Panels
(Ref. Fig. 401/TASK 57-51-37-991-003)
(1)
Install the access panel 573AB(673AB) (6) as follows:
(a)
Put the access panel (6) in position and attach it with two of the outer camloc fasteners (5).
(b)
Set the access panel (6) so that dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 in.) along the full length of the panel. Try and set the clearance as near as possible to 2.0 mm (0.0787 in.).
(c)
Attach the access panel (6) to the wing with the remaining camloc fasteners (5).
(d)
Fill the clearance between the access panel (6) and the trailing edge of the wing skin with SEALANTS (Material No. 09-016).
(2)
Install the access panel 573BB(673BB) (4) as follows:
(a)
Put the access panel (4) in position and attach it with two of the outer camloc fasteners (3).
(b)
Set the access panel (4) so that dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 in.) along the full length of the panel. Try and set the clearance as near as possible to 2.0 mm (0.0787 in.).
(c)
Attach the access panel (4) to the wing with the remaining camloc fasteners (3).
(d)
Fill the clearance between the access panel (4) and the trailing edge of the wing skin with SEALANTS (Material No. 09-016).
(3)
Install the access panel 573CB(673CB) (2) as follows:
(a) Put the access panel (2) in position and attach it with two of the outer camloc fasteners (1).
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(b)
Set the access panel (2) so that:
