C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-62-000-003 Removal of the Leading Edge Panels 2 and 5 on the
Outboard Flap 27-54-62-400-003 Installation of the Leading Edge Panels 2 and 5 on
the Outboard Flap 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4
NTM 57-53-09 PART 9
ASRM 575300 (for corrective action)
**ON A/C 001-049, 051-056,
57-53-00-991-012 Fig. 611
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
57-53-00-991-012-A Fig. 611A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 672 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
3. Job Set-up
__________ Subtask 57-53-00-941-098
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 57-53-00-860-129
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.
**ON A/C 001-049, 051-056,
Subtask 57-53-00-010-095
C. Get Access
(Ref. Fig. 611/TASK 57-53-00-991-012)
(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 the outboard flap leading edge panel 2 at zone 532(632) (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 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 673 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap
Figure 611/TASK 57-53-00-991-012
R 1EFF : 001-049, 051-056, 1 57-53-00Page 674 1 1 May 01/05 1 1 1CES 1
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-53-00-010-095-A
C. Get Access (Ref. Fig. 611A/TASK 57-53-00-991-012-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(s) 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. 611/TASK 57-53-00-991-012)
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 611A/TASK 57-53-00-991-012-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 675 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap
Figure 611A/TASK 57-53-00-991-012-A12 (SHEET 1)
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 676 1401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap
Figure 611A/TASK 57-53-00-991-012-A22 (SHEET 2)
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 677 1401-499, 1Aug 01/05 1 1 1CES 1 Subtask 57-53-00-280-069
A. Inspection
(1) Do a special detailed inspection (Ref. NTM 57-53-09 PART 9), internally of:
-
the internal support at track 3
-
the RIB 6
-
the fitting at the front spar
-
the internal doubler.
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.
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