R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-53-00-010-056-A
D. Get Access (Ref. Fig. 607A/TASK 57-53-00-991-008-A)
(1) Put the access platform below the applicable wing trailing edge at flap track 3, zone 532(632).
(2) Remove the access panel 532AT (632AT) and the flap track 3 fairing 532CB (632CB) (Ref. TASK 57-55-11-000-001).
(3) Remove and discard the cover from the applicable inspection hole(s) on the front spar.
(4) Make sure that the inspection hole(s) are 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, 051-056,
(Ref. Fig. 607/TASK 57-53-00-991-008)
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 607A/TASK 57-53-00-991-008-A)
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.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 646 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 57-53-00-280-054
A. Inspection
(1) Do a special detailed inspection (Ref. NTM 57-53-09 PART 9), internally and externally of:
-
the support at track 3
-
the inboard and outboard faces of RIB5
-
the fitting assembly
-
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, 051-056,
Subtask 57-53-00-410-055
A. Close Access
(Ref. Fig. 607/TASK 57-53-00-991-008)
(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 LH inspection hole.
(3)
Install the new cover on the LH inspection hole.
(4)
Install the leading edge panel 2 (Ref. TASK 27-54-62-400-003).
(5)
Install the flap track 3 fairing 532CB (632CB) and the access panel 532AT (632AT) (Ref. TASK 57-55-11-400-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 647 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap
Figure 607A/TASK 57-53-00-991-008-A12 (SHEET 1)
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 648 1401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap
Figure 607A/TASK 57-53-00-991-008-A22 (SHEET 2)
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 649 1401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-53-00-410-055-A
A. Close Access
(Ref. Fig. 607A/TASK 57-53-00-991-008-A)
(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(s) for the applicable inspection hole(s).
(3)
Install the new cover(s) on the LH inspection hole(s).
(4)
Install the flap track 3 fairing 532CB (632CB) and the access panel 532AT (632AT) (Ref. TASK 57-55-11-400-001).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-53-00-865-064
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-53-00-860-107
C. Aircraft Maintenance Configuration
(1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(2) Retract the flaps fully (Ref. TASK 27-50-00-866-009).
Subtask 57-53-00-942-056
D. Removal of Equipment
(1)
Remove the warning notice(s).
(2)
Remove the access platform(s).
(3)
Remove the safety barriers.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 650 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼4(79)
