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)
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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
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Forward Upper Roller Pin Holes, Track Ribs 5-12 - Location and Detail R Figure 612/TASK 57-41-00-991-022
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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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