B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 R SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 27-64-42-000-001 Removal of the Spoiler 2 27-64-42-400-001 Installation of the Spoiler 2 27-64-43-000-001 Removal of the Spoiler 3 27-64-43-400-001 Installation of the Spoiler 3 27-64-44-000-001 Removal of the Spoiler 4 27-64-44-400-001 Installation of the Spoiler 4 27-64-45-000-001 Removal of the Spoiler 5 27-64-45-400-001 Installation of the Spoiler 5 NTM 57-70-06 PART 4
R NTM 57-70-06 PART 6 ASRM 577000 (for corrective action) 57-72-00-991-003 Fig. 603
3. Job Set-up
__________
Subtask 57-72-00-941-053
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put warning notices in the cockpit to tell persons not to operate the spoilers.
(3)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-72-00-860-054
B. Aircraft Maintenance Configuration
(1)
Put the access platform below the applicable spoiler:
-
for spoiler 2, zone 583 (683)
-
for spoiler 3, zone 584 (684)
-
for spoiler 4, zone 585 (685)
-
for spoiler 5, zone 586 (686).
(2)
Do a manual extension of the spoilers (Ref. TASK 27-60-00-866-002).
(3)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
R (4) Make sure that the COLLAR-SAFETY, SPOILER is installed on the spoiler servo control.
R (5) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
(6) Disconnect the eye end of the spoiler servo control from the applicable spoiler:
-
for the spoiler 2, (Ref. TASK 27-64-42-000-001)
-
for the spoiler 3, (Ref. TASK 27-64-43-000-001)
-
for the spoiler 4, (Ref. TASK 27-64-44-000-001)
-
for the spoiler 5, (Ref. TASK 27-64-45-000-001).
Subtask 57-72-00-865-054
R C. 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
4. Procedure
_________
(Ref. Fig. 603/TASK 57-72-00-991-003)
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.
Subtask 57-72-00-110-052
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the spoiler center hinge fitting.
Spoiler Inspection Area
Figure 603/TASK 57-72-00-991-003
1EFF : ALL 1 57-72-00 Page 614
1 1 Feb 01/98
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1CES 1
Subtask 57-72-00-280-050
B. Inspection
R (1) Do a special detailed inspection of the center hinge fitting on R spoilers 2, 3, 4 and 5 (Ref. NTM 57-70-06 PART 4) and (Ref. NTM 57-R 70-06 PART 6).
NOTE : If necessary, refer to the ASRM (Ref. ASRM 577000) 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 57-72-00-865-055
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
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