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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