(3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the slat/flap control lever (Ref. TASK 27-00-00-480-002). ________
5. Close-Up
Subtask 27-80-00-860-053
A. Aircraft Maintenance Configuration
(1)
Depressurize the Blue hydraulic system
(Ref. TASK 29-10-00-864-003).
(2)
On the ECAM control panel, set the control/brightness controls to OFF.
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-80-00-942-057
B. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 27-80-00Page 204 1 1 Aug 01/05R 1 1 1CES 1
TASK 27-80-00-866-007
Manual Extension of the Slats
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.
R
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific pneumatic right-angle wrench No specific safety barriers No specific warning notice No specific access platform 1.8 m (5 ft. 11 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804011000 1 BAR-TURNING
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 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
27-80-00-866-008 Manual Retraction of the Slats
R 27-84-45-000-005 Removal of the Torque Shaft 6012CM(6062CM) 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page 27-80-00-991-004 Fig. 201
3. Job Set-up
__________
Subtask 27-80-00-941-059
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position on the panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-80-00-860-060
B. Aircraft Maintenance Configuration
(1)
Make sure that the slats are fully retracted (Ref. TASK 27-80-00-866-005).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
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