R 57-51-00-991-010 Fig. 624
3. Job Set-up
__________
Subtask 57-51-00-941-078
A. Safety Precautions
(1)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(2)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(3)
Put the safety barriers in position.
Subtask 57-51-00-865-097
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
Subtask 57-51-00-010-078
C. Get Access
(1)
Put the adjustable access platform below the applicable wing trailing edge, zone 570(670).
(2)
Remove the applicable access panels:
-
for the left wing, remove 573CB, 575AB, 575DB, 575EB, 575GB
-
for the right wing, remove 673CB, 675AB, 675DB, 675EB, 675GB.
(3)
Remove the two inner hinge pins:
-
for spoiler 1 (Ref. TASK 27-64-41-000-001)
-
for spoiler 2 (Ref. TASK 27-64-42-000-001)
-
for spoiler 3 (Ref. TASK 27-64-43-000-001)
-
for spoiler 4 (Ref. TASK 27-64-44-000-001)
-
for spoiler 5 (Ref. TASK 27-64-45-000-001).
4. Procedure
_________
R (Ref. Fig. 624/TASK 57-51-00-991-010)
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 Spoiler Hinge Pins Figure 624/TASK 57-51-00-991-010
1EFF : 1 1 1CES ALL 1 111 57-51-00 Page A646 Nov 01/04
Subtask 57-51-00-110-081
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the area around the inner hinge pins of the spoilers 1 thru 5.
Subtask 57-51-00-240-056
B. Inspection
(1) For each spoiler, do a magnetic inspection of the hinge pins (Ref. NTM 57-51-06 PART 7).
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
Subtask 57-51-00-420-077
C. Install the Hinge Pins
(1) Install the two inner hinge pins:
-
for spoiler 1 (Ref. TASK 27-64-41-400-001)
-
for spolier 2 (Ref. TASK 27-64-42-400-001)
-
for spoiler 3 (Ref. TASK 27-64-43-400-001)
-
for spoiler 4 (Ref. TASK 27-64-44-400-001)
-
for spoiler 5 (Ref. TASK 27-64-45-400-001).
5. Close-up
________ Subtask 57-51-00-410-079
A. Close Access
(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 573CB, 575AB, 575DB, 575EB, 575GB
-
for the right wing, install 673CB, 675AB, 675DB, 675EB, 675GB.
1EFF : ALL 1 57-51-00Page A647 1 1 Nov 01/04R 1 1 1CES 1
Subtask 57-51-00-865-098
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 21CE3, 21CE2.
Subtask 57-51-00-942-078
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