Material No. 11-026 GB DEF-STAN 68-148/1 R SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-81-42-000-001 Removal of the PPU Adaptor Plate 6048CM(6098CM) 27-81-42-400-001 Installation of the PPU Adaptor Plate 6048CM(6098CM) 27-84-45-991-001 Fig. 401
R 27-84-45-991-002 Fig. 402
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-84-45-991-001)
Subtask 27-84-45-941-077
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 slat controls.
Subtask 27-84-45-860-063
B. Aircraft Maintenance Configuration
R (1) Make sure that the access platform is in position below the R applicable zone 522(622).
(2) Make sure that the adapter plate of the PPU has been removed (Ref. TASK 27-81-42-000-001).
Subtask 27-84-45-865-095
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 (Ref. Fig. 402/TASK 27-84-45-991-002)
R
Subtask 27-84-45-420-087
R A. Preparation for Installation
R CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______
R GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1) Clean the component interface and /or the adjacent area with a
R MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS
R (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 CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______
R GREASE AND ASSEMBLY PASTE DO NOT MIX.
R (a) Apply a thin layer of COMMON GREASE (Material No. 04-022) to the
R torque shaft splines.
R
R - or
R (b) Apply a thin layer of COMMON GREASE (Material No. 04-018) to the
R torque shaft splines.
R
Subtask 27-84-45-420-063
R B. Installation of the Torque Shaft 6046CM(6069CM)
(1) Install the shaft (47).
(2) Install the PPU adaptor plate (Ref. TASK 27-81-42-400-001).
(3) Make sure that:
R - you cannot see the spline engagement groove at the movable joint
R - the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable
R joint.
Subtask 27-84-45-710-062
C. Test
(1) The operational test of the slat power-transmission system is contained in the installation of the PPU adaptor plate (Ref. TASK 27-81-42-400-001).
5. Close-up
________ Subtask 27-84-45-865-096
A. Make sure that this(these) circuit breaker(s) is(are) closed:
5CV, 7CV.
Subtask 27-84-45-942-062
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.
1EFF : ALL 1 27-84-45Page A422 1 1 Feb 01/00R 1 1 1CES 1
ACTUATOR ASSY - TYPE A (6013CM,6015CM,6063CM,6065CM) - REMOVAL/INSTALLATION
___________________________________________________________________________
TASK 27-84-48-000-001
R Removal of the Type A Actuators 6013CM(6063CM)/6015CM(6065CM)
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
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(17)
