5. Close-Up
________ Subtask 27-80-00-860-055
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).
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Subtask 27-80-00-865-059
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 14CC1, 14CC2.
Subtask 27-80-00-942-053
C. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the warning notice(s).
(3)
Remove the safety barrier(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 27-80-00-866-008
Manual Retraction of the Slats
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
R
1. Reason for the Job
__________________
To manually retract the slats after they have been manually extended.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific pneumatic right-angle wrench No specific safety barriers No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 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 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001)
27-80-00-866-007 Manual Extension of the Slats
27-84-45-400-006 Installation of the Torque Shaft 6012CM(6062CM)
27-80-00-991-004 Fig. 201
3. Job Set-up
__________
Subtask 27-80-00-941-060
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position on the panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-80-00-860-061
B. Aircraft Maintenance Configuration
(1)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is attached to the flap/slat control lever on the panel 114VU.
(2)
Make sure that the access platform is in position below zone 191,
192.
(3)
Make sure that the torque shaft assy 6012CM (6062CM) is removed and that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is installed inboard of the torque shaft assy.
(4)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(5)
On the MCDU, make sure that the PPU DATA page is shown.
Subtask 27-80-00-865-066
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 R 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 R 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
4. Procedure
_________ (Ref. Fig. 201/TASK 27-80-00-991-004) Subtask 27-80-00-866-059
A. Manual Retraction of the Slats with Pneumatic Wrench WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
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