**ON A/C 001-049, 051-056,
57-53-00-991-006 Fig. 605
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
57-53-00-991-006-A Fig. 605A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 624 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
3. Job Set-up
__________
Subtask 57-53-00-941-055
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 57-53-00-860-102
B. Aircraft Maintenance Configuration
(1)
Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.
Subtask 57-53-00-865-059
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
**ON A/C 001-049, 051-056,
Subtask 57-53-00-010-054
D. Get Access
(Ref. Fig. 605/TASK 57-53-00-991-006)
(1)
Put the access platform below the applicable wing trailing edge at flap track 3, zone 532 (632).
(2)
Remove the access panel 532AT (632AT) and the flap track 3 fairing 532CB (632CB) (Ref. TASK 57-55-11-000-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 625 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap - Front Splices and Attachment Areas - Inspection
Figure 605/TASK 57-53-00-991-006
R 1EFF : 001-049, 051-056, 1 57-53-00Page 626 1 1 May 01/05 1 1 1CES 1
(3)
Remove the outboard flap leading edge panel 2 (Ref. TASK 27-54-62-000-003).
(4)
Remove and discard the cover from the applicable inspection hole on the front spar.
(5)
Make sure that the applicable inspection holes are clear of unwanted material.
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-53-00-010-054-A
D. Get Access
(Ref. Fig. 605A/TASK 57-53-00-991-006-A)
(1)
Put the access platform below the applicable wing trailing edge at flap track 3, zone 532 (632).
(2)
Remove the access panel 532AT (632AT) and the flap track 3 fairing 532CB (632CB) (Ref. TASK 57-55-11-000-001).
(3)
Remove and discard the cover from the applicable inspection hole on the front spar.
(4)
Make sure that the applicable inspection holes are clear of unwanted material.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
4. Procedure
_________
**ON A/C 001-049, 051-056,
(Ref. Fig. 605/TASK 57-53-00-991-006) R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 605A/TASK 57-53-00-991-006-A)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 627 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap - Front Splices and Attachment Areas - Inspection
Figure 605A/TASK 57-53-00-991-006-A12 (SHEET 1)
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 628 1401-499, 1Aug 01/05 1 1 1CES 1
Outboard Flap - Front Splices and Attachment Areas - Inspection
Figure 605A/TASK 57-53-00-991-006-A22 (SHEET 2)
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 629 1401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
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 57-53-00-280-053
A. Inspection
(1) Do a special detailed inspection of the front spar splices and attachment areas, internally and externally (Ref. NTM 57-53-03 PART 9).
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