(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 27-51-00Page 507 1 1 May 01/00R 1 1 1CES 1
TASK 27-51-00-710-001
Operational Test of the Wing Tip Brake and the Pressure Off 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
__________________
Refer to the MPD TASK: 275100-01
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
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-38-00-710-001 Operational Test of the Battery Charge Limiter (BCL), (without the CFDS) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 27-50-00-869-006 Reset of the Wing Tip Brake (WTB) of the Flap System on the Ground 27-51-00-750-001 Automatic Integrity Test of the Slat and Flap Control
Computers
R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
R Power Supply
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REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-10-00-864-003 Depressurize the Blue Hydraulic System
29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
27-51-00-710-003 Operational Test of the Wing Tip Brake and the Pressure Off Brake with the Ground Power Cart (for corrective action)
27-51-00-710-004 Operational Test of the Wing Tip Brake and the Pressure Off Brake with the Engine Driven Pumps (for corrective action)
3. Job Set-up
__________
Subtask 27-51-00-941-050
A. Safety Precautions
(1) Put the safety barriers in position.
R (2) Put the warning notices in position to tell persons that the flap and R slat systems are in operation.
Subtask 27-51-00-860-054
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).
NOTE : If the test shows that the Wing Tip Brakes (WTBs) are set, do____ the Reset of the WTBs of the Flap System on the Ground (Ref. TASK 27-50-00-869-006).
Subtask 27-51-00-865-064
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-51-00-865-065
D. 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/FLP/SYS2 12CV P20 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
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