B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
 1EFF : ALL 1 57-41-00Page 651 1 1 May 01/04R 1 1 1CES 1

 C. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-84-62-000-001 Removal of the Slat Tracks 5 thru 12
 27-84-62-400-001 Installation of the Slat Tracks 5 thru 12
 27-84-64-000-001 Removal of the No. 2 Slat
 27-84-64-400-002 Installation of the No. 2 Slat
 27-84-65-000-001 Removal of the No. 3 Slat
 27-84-65-400-002 Installation of the No. 3 Slat
 27-84-66-000-001 Removal of the No. 4 Slat
 27-84-66-400-002 Installation of the No. 4 Slat
 27-84-67-000-001 Removal of the No. 5 Slat
 27-84-67-400-002 Installation of the No. 5 Slat
 NTM 57-41-02 PART 6
 ASRM 574000 (for corrective action)

R 57-41-00-991-021 Fig. 611
R 57-41-00-991-022 Fig. 612
 3. Job Set-up
__________
R (Ref. Fig. 611/TASK 57-41-00-991-021, 612/TASK 57-41-00-991-022)
 Subtask 57-41-00-941-059
 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 57-41-00-860-064
 B. Aircraft Maintenance Configuration
 (1)
 Remove the No. 2 slat (Ref. TASK 27-84-64-000-001), the No. 3 slat (Ref. TASK 27-84-65-000-001), the No. 4 slat (Ref. TASK 27-84-66-000-001) and the No. 5 slat (Ref. TASK 27-84-67-000-001).

 (2)
 Remove the slat tracks 5 thru 12 (Ref. TASK 27-84-62-000-001).

 Access Panels, Wing Lower Leading Edge - Track Ribs 5-12 R Figure 611/TASK 57-41-00-991-021
 1EFF : ALL 1 57-41-00Page 653 1 1 May 01/04 1 1 1CES 1

 Forward Upper Roller Pin Holes, Track Ribs 5-12 - Location and Detail R Figure 612/TASK 57-41-00-991-022
 1EFF : ALL 1 57-41-00Page 654 1 1 May 01/04 1 1 1CES 1

 Subtask 57-41-00-865-066

 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 Subtask 57-41-00-010-051
 D. Get Access R (Ref. Fig. 611/TASK 57-41-00-991-021)
 (1)
 Put the adjustable access platform in position below the applicable wing leading edge, zone 522(622).

 (2)
 Remove the applicable access panels:

 -
for the left wing, remove 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB

 -
for the right wing, remove 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB.

 4. Procedure
_________
 Subtask 57-41-00-110-060
 A. Preparation for Inspection R (Ref. Fig. 612/TASK 57-41-00-991-022)
 (1) At the leading edge forward upper roller pin holes, track ribs 5-12:
 (a) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the structure in the area of the bush flanges.
 Subtask 57-41-00-280-051
 B. Inspection
 (1) Do a special detailed inspection of the outer wing fixed leading-edge forward upper roller-pin holes (ribs 5 thru 12) (Ref. NTM 57-41-02 PART 6).
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 574000) 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
________
 Subtask 57-41-00-410-051

 A. Close Access R (Ref. Fig. 611/TASK 57-41-00-991-021)
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panels:

 -
for the left wing, install 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB

 -
for the right wing, install 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB.
　
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