3. Job Set-up
__________
Subtask 57-53-00-941-073
A. Safety Precautions
(1) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2) Put the safety barriers in position.
Subtask 57-53-00-860-119
B. Aircraft Maintenance Configuration
(1)
Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.
Subtask 57-53-00-865-099
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
Subtask 57-53-00-010-069
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633). (Ref. Fig. 619/TASK 57-53-00-991-020)
(2)
Remove the access panel 533AT (633AT) and the flaptrack 4 fairing 533CB (633CB) (Ref. TASK 57-55-11-000-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A627 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap - Inspection
Figure 619/TASK 57-53-00-991-020
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 57-53-00Page A628 1201-214, 1May 01/05 1 1 1CES 1
(3)
Remove the outboard flap leading edge panel 5 (Ref. TASK 27-54-62-000-003).
(4)
Remove and discard the cover from the RH inspection hole on the front spar.
(5) Make sure that the inspection hole is clear of unwanted material. R **ON A/C 106-149, 215-299, 401-499,
Subtask 57-53-00-010-069-A
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633). (Ref. Fig. 619A/TASK 57-53-00-991-020-A)
(2)
Remove the access panel 533AT (633AT) and the flaptrack 4 fairing 533CB (633CB) (Ref. TASK 57-55-11-000-001).
(3)
Remove and discard the cover(s) from the applicable inspection hole(s) on the front spar.
(4)
Make sure that the applicable inspection hole(s) is clear of unwanted material.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
(Ref. Fig. 619/TASK 57-53-00-991-020) R **ON A/C 106-149, 215-299, 401-499,
(Ref. Fig. 619A/TASK 57-53-00-991-020-A)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A629 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap - Inspection
Figure 619A/TASK 57-53-00-991-020-A12 (SHEET 1)
R 1EFF : 106-149, 215-299, 401-499, 1 57-53-00Page A630 1 1 Aug 01/05 1 1 1CES 1
Outboard Flap - Inspection
Figure 619A/TASK 57-53-00-991-020-A22 (SHEET 2)
R 1EFF : 106-149, 215-299, 401-499, 1 57-53-00Page A631 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 57-53-00-280-058
A. Inspection
(1) Do a special detailed inspection (Ref. NTM 57-53-13 PART 9) of:
-
the RIB14
-
the fitting assembly
-
the pendulum support
-
the attachment structure.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
5. Close-up
________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
Subtask 57-53-00-410-068
A. Close Access
(Ref. Fig. 619/TASK 57-53-00-991-020)
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
use BONDING AND ADHESIVE COMPOUNDS (Material No. 08-061A) cut to the correct dimensions, to make a new cover for the RH inspection hole.
(3)
Install the new cover on the RH inspection hole.
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