(2)
Make sure that the warning notice is in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-058
B. Aircraft Maintenance Configuration
(1)
Make sure that the slats are retracted fully (Ref. TASK 27-80-00-866-005).
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is attached to the flap/slat control lever on panel 114VU.
R (3) Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.
(4) Make sure that the aircraft is in the same configuration as at the end of the removal task.
R (5) Make sure that the access platform is in position below the applicable access panel 521EB(621EB).
R R R R (6) Make sure that the applicable access panels have been removed: - for 6016CM(6066CM), panels 521EB, 621EB - for 6020CM(6070CM), panels 521GB, 621GB.
(7) Make sure that the applicable steady bearing has been removed (Ref. TASK 27-84-44-000-002).
Subtask 27-84-45-865-080
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure_________
R R (Ref. Fig. 402/TASK 27-84-45-991-002)
Subtask 27-84-45-420-078
R A. Preparation for Installation
R R CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______ GREASE AND ASSEMBLY PASTE DO NOT MIX.
R R (1) Clean the component interface and/or the adjacent area with 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.
R (4) Do one of the steps that follow:
R R CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______ GREASE AND ASSEMBLY PASTE DO NOT MIX.
R R R R (a) Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines. - or
R R R (b) Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.
Subtask 27-84-45-420-058
B. Installation of the Torque Shafts
(1) Install the shaft (45) in the steady bearing (46) and install the applicable steady bearing (46) (Ref. TASK 27-84-44-400-002): - FOR 6018CM install the steady bearing 6017CM - FOR 6068CM install the steady bearing 6067CM.
R (2) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003): - from the torque shaft, inboard of the applicable component - from the torque shaft, outboard of the applicable component.
Subtask 27-84-45-865-100
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-710-059
D. Test
(1) The operational test of the slat power-transmission system is contained in the installation of the steady bearing (Ref. TASK 27-84-44-000-002).
5. Close-up
________ R (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-410-061
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the access panels:
-for 6016CM, install 521EB, 621EB
-for 6020CM, install 521GB, 621GB.
Subtask 27-84-45-942-057
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
TASK 27-84-45-000-009
R Removal of the Torque Shaft 6022CM(6072CM)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
