(2)
 Depressurize the applicable hydraulic reservoirs (Ref. TASK 29-14-00-614-001).

 (3)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 Subtask 27-81-00-942-058
 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 barriers.

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 27-81-00Page 525 1 1 Aug 01/05R 1 1 1CES 1

 TASK 27-81-00-710-003
 Operational Test of the Wing-Tip Brake and the Pressure-Off Brake with the Engine Driven Pumps 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 TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
 CAUTION : IF THE THRUST REVERSER COWLS ARE OPEN, MAKE SURE THAT THE HALF DOORS

_______ OF THE THRUST REVERSER ARE RETRACTED BEFORE YOU EXTEND THE SLATS. IF THE DOORS ARE EXTENDED, YOU CAN CAUSE DAMAGE TO THE SLATS AND HALF DOORS WHEN THE SLATS EXTEND.
 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 safety barriers No specific warning notices
 1EFF : ALL 1 27-81-00Page 526 1 1 May 01/04R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-38-00-710-001
24-41-00-861-002
24-41-00-862-002
27-51-00-750-001
27-80-00-869-004
29-10-00-863-001 29-10-00-863-002 29-10-00-863-003
29-10-00-864-001 29-10-00-864-002 29-10-00-864-003 29-14-00-614-001 31-32-00-860-006
71-00-00-710-003 71-00-00-710-004 71-00-00-710-027 71-00-00-710-028
3. Job Set-up
__________ Subtask 27-81-00-941-058
 A. Safety Precautions
Operational Test of the Battery Charge Limiter (BCL), (without the CFDS)Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerAutomatic Integrity Test of the Slat and Flap Control ComputersReset of the Wing Tip Brake (WTB) of the Slat System on the GroundPressurize the Green Hydraulic SystemPressurize the Yellow Hydraulic SystemPressurize the Blue Hydraulic System with a Ground Power SupplyDepressurize the Green Hydraulic SystemDepressurize the Yellow Hydraulic SystemDepressurize the Blue Hydraulic SystemDepressurization of the Hydraulic ReservoirsProcedure to Get Access to the SYSTEM REPORT/TEST F/CTL PageEngine Automatic StartEngine Manual StartEngine ShutdownEngine Shutdown
 (1)
 Put the safety barriers in position.

 (2)
 Put the warning notices in postion to tell persons that the slat and flap systems are in operation.

 1EFF : ALL 1 27-81-00Page 527 1 1 May 01/04R 1 1 1CES 1

 Subtask 27-81-00-860-058
 B. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Make sure that the aircraft batteries are fully charged (Ref. TASK 24-38-00-710-001).

 (3)
 Get access to the SYSTEM REPORT/TEST (F/CTL) page on the MCDU (Ref. TASK 31-32-00-860-006).

 (4)
 Do the automatic integrity test of the two SFCC's, which includes Slat and Flap BITE tests of the two computers (Ref. TASK 27-51-00-750-001).

 (5)
 Make sure that the Wing Tip Brakes (WTBs) are not set (Ref. TASK 27-80-00-869-004).

 Subtask 27-81-00-865-067
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
　
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