(22.12 and 26.54 lbf.in).
(16)
Attach the bonding straps (45) to each end of the spoiler with the bolts (44), the washers (47) and the nuts (46) (Ref. TASK 20-28-00-912-004).
Subtask 27-64-44-916-051-A
E. Application of Special Materials
(1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the cotter pins (1), (26), (34), (35) and (49)
-
the locking caps (2), (25), (33), (36) and (50)
-
the nuts (3), (24), (32), (37) and (51)
-
the washers (4), (23), (31), (38) and (52)
-
the hinge pins (6), (29), (41) and (54)
-
the flange of the shaft (21)
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-64-44Page 430 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
-the nuts (27), (43) and (56)
-the bolt (48).
**ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 27-64-44-860-051
F. Aircraft Maintenance Configuration
(1)
Retract spoiler 4 (Ref. TASK 27-60-00-866-002).
(2)
On the servo-control, turn the SPOILER MAINTENANCE KEY (98D27603002000) or the SPOILER MAINTENANCE KEY (98D27603002001) on the maintenance device to the operation position and then remove it.
(3)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap and slat control lever on panel 114VU.
R **ON A/C 151-199, 301-399, 401-499,
Subtask 27-64-44-860-051-A
F. Aircraft Maintenance Configuration
(1)
Retract spoiler 4 (Ref. TASK 27-60-00-866-002).
(2)
On the spoiler servo-control, turn the pointer of the maintenance device to the 'O' (Operation) position.
(3)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap and slat control lever on panel 114VU.
**ON A/C ALL
Subtask 27-64-44-865-052
G. 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
Subtask 27-64-44-820-051
H. Clearance Checks
(1)
Make sure that the clearance 'X' is between 16 mm (0.6299 in.) and 20 mm (0.7874 in.).
(2)
Make sure that the clearance 'Y' is between 0 mm (0.0 in.) and 0.50 mm (0.0196 in.). Adjust the seals if it is necessary.
(3)
Make sure that the clearance 'Z' is between 1.63 mm (0.0641 in.) and
2.82 mm (0.1110 in.). The spoiler and the structure must make a continuous surface. The seal must touch the trailing edge structure along its full length.
(4)
Pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002).
(5)
Adjust the spoiler to give the dimension 'U' between the spoiler and the flap (Ref. TASK 27-64-00-820-001).
Subtask 27-64-44-410-050
J. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the access panels (Ref. TASK 57-51-37-400-004):
-
for the left wing, install 575EB
-
for the right wing, install 675EB.
(3) Remove the access platform(s). Subtask 27-64-44-865-053
K. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 21CE1, 21CE2, 21CE3.
Subtask 27-64-44-710-050
L. Operational Test
(1) Do an operational test of the spoiler (Ref. TASK 27-64-00-710-001).
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5. Close-up
________ Subtask 27-64-44-942-051
A. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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SPOILER 4 - INSPECTION/CHECK
____________________________ TASK 27-64-44-200-001 Inspection/Check of the Spoiler 4 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
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