(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 access panel is removed:
-
for 6214CM, panel 573BB
-
for 6220CM, panel 575BB
-
for 6264CM, panel 673BB
-
for 6270CM, panel 675BB.
(5)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on a flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the removed component.
Subtask 27-54-45-865-076
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
_________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 404/TASK 27-54-45-991-003) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 404A/TASK 27-54-45-991-003-A)
**ON A/C ALL
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 27-54-45-420-069
A. Preparation for Installation
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Do one of the steps that follow:
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(a)
Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines.
- or
(b)
Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.
Subtask 27-54-45-420-056
B. Installation of the Torque Shafts 6214CM(6264CM)/6220CM(6270CM)
(1)
Put the retaining ring (54) temporarily in position on the shaft of the universal joint (53).
(2)
Install the universal joint (53) and attach it with the pin (55) and the retaining ring (54).
(3)
Install the torque shaft (52).
(4)
Install the applicable steady bearing (56) (Ref. TASK 27-54-44-400-002):
-
FOR 6214CM
install the steady bearing 6215CM
-
FOR 6220CM
install the steady bearing 6219CM
-
FOR 6264CM
install the steady bearing 6265CM
-
FOR 6270CM
install the steady bearing 6269CM.
(5)
Make sure that:
-you cannot see the spline engagement groove on the torque shaft
(52) at the movable joints
-the dimension A is a minimum of 6.5 mm (0.2559 in.) total shaft end float at the movable joints.
(6)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-400-003).
1EFF : ALL 1 27-54-45Page 488 1 1 May 01/00R 1 1 1CES 1
Subtask 27-54-45-865-078
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-54-45-710-056
D. Operational Test of the Flap System
(1)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(2)
Retract the flaps fully (Ref. TASK 27-50-00-866-009).
(3)
Do an operational test of the flap system (Ref. TASK 27-54-00-710-001). Make sure that the operation of the torque shafts is satisfactory.
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