(2)
Examine the interface of the structure and the PPU adaptor plate (1) for damage, cracks and corrosion.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Do an inspection of the component interface and/or the adjacent area. Subtask 27-81-42-420-052
B. Installation of the PPU Adaptor
(1)
Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the interface of the structure and the PPU adaptor plate (1).
(2)
Apply a layer of SPECIAL MATERIALS (Material No. 05-002C) to the interface of the structure and the locking ring (6).
(3)
Apply COMMON GREASE (Material No. 04-022) to the splines on the slat torque-shaft.
(4)
Put the PPU adaptor plate (1) and the locking ring (6) in the correct position on the structure and the torque shaft.
(5)
Install the bolts (8) and the nuts (4).
(6)
Install the pin (5) and safety it with the retaining ring (7).
(7)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the nuts (4) and the heads of the bolts (8).
(8)
Turn the cover plate (3) clockwise to cover the nuts (4) then tighten the screws (2).
(9)
Install the APPU (Ref. TASK 27-81-18-400-001).
5. Close-up
________ Subtask 27-81-42-410-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the applicable access panel:
-
FOR 6048CM
install 522UB
-
FOR 6098CM
install 622UB.
Subtask 27-81-42-942-051
B. Removal of Equipment
(1)
Remove the warning notice(s).
(2)
Remove the access platform(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
BRAKE - WING TIP (WTB) (35CV,36CV) - REMOVAL/INSTALLATION
_________________________________________________________
TASK 27-81-51-000-001
Removal of the Slat Wing-Tip Brake
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
_______ GEAR.
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific blanking caps No specific blanking plugs No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice(s) No specific access platform 4 m (13 ft. 1 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-80-00-866-005 Retracting the Slats on the Ground 27-84-45-000-006 Removal of the Torque Shafts
6014CM(6064CM)/6028CM(6078CM)/6036CM(6086CM)/
6038CM(6088CM)/6040CM(6090CM)/6042CM(6092CM)/6044CM(6
094CM) 29-10-00-864-001 Depressurize the Green Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 27-81-51-991-001 Fig. 401
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(76)
