(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
Subtask 57-52-00-865-060
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
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page 613 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 57-52-00-010-055
D. Get Access
(1) Put the access platform below the applicable wing trailing edge at the pylon, zone 581(681).
4. Procedure
_________ (Ref. Fig. 603/TASK 57-52-00-991-003) 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 57-52-00-280-050
A. Inspection
(1) Do a special detailed inspection of the internal support bracket of the pylon aft fairing LH/RH (Ref. NTM 57-52-10 PART 9).
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.
5. Close-up
________ Subtask 57-52-00-914-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 57-52-00-865-061
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page 614 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Internal Support Bracket of Pylon Aft Fairing - Inboard Flap
Figure 603/TASK 57-52-00-991-003
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page 615 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 57-52-00-860-082
C. Aircraft Maintenance Configuration
(1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(2) Retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-52-00-942-055
D. Removal of Equipment
(1)
Remove the access platform(s).
(2)
Remove the warning notice(s).
(3)
Remove the safety barriers.
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page 616 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 57-52-00-200-004
Detailed Visual Inspection of Inboard Flap, End Rib including Roller and Interconnecting Strut Attachment Bracket LH/RH
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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.
1. Reason for the Job
__________________
Refer to the MPD TASK: 575211-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
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