C. Referenced Information
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REFERENCE DESIGNATION
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27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 57-51-37-000-004 Removal of the Access Panels
575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
57-51-37-400-004 Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
R **ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-45-991-001 Fig. 401 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
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R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
27-54-45-991-001-A Fig. 401A
**ON A/C ALL
27-54-45-991-004 Fig. 405
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 401/TASK 27-54-45-991-001) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-54-45-991-001-A)
**ON A/C ALL
Subtask 27-54-45-941-085
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position to tell persons not to operate the flap/slat controls.
Subtask 27-54-45-860-071
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
R (1) Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever on panel 114VU.
(3)
Make sure that the access platform is in the applicable position.
(4)
Make sure that the applicable spoiler is in the 'M' (Maintenance) position (Ref. TASK 27-60-00-866-002).
(5)
Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
R (6) Make sure that the applicable access panels are removed (Ref. TASK R 57-51-37-000-004):
-
for 6218CM, panels 575AB, 575BB
-
for 6268CM, panels 675AB, 675BB.
(7) Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on the flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the removed component.
Subtask 27-54-45-865-083
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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. 405/TASK 27-54-45-991-004)
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 27-54-45-420-071
A. Preparation for Installation
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1)
Clean the parts:
(a) Use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean:
-
the nuts (74) and (76)
-
the bolts (73) and (77)
-
the flanges of the torque shafts (71) and (72)
-
the flange of the universal joint (75).
(2)
Dry the parts: WARNING : USE A PROTECTIVE EYE SHIELD/GOGGLES WHEN YOU USE COMPRESSED
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