R 1. Push in the two brake pedals on On the panel 400VU, the brake yellow
R the CAPT or F/O side. pressure triple indicator shows the
R left and right side pressure values.
R The pistons related to the Yellow
R hydraulic system are extended.
R 2. Release the brake pedals. The triple indicator shows that the
R pressure supplied to the brakes
R decreases to zero.
R The pistons related to the Yellow
R hydraulic system are retracted.
R 3. Slowly push the brake pedals on On the panel 400VU:
R the CAPT or F/O side. - the pressure supplied to the brakes
R increases in proportion to the
R pressure you put on the pedals,
R - the pressure shown at full pedal
R movement is between 2400 psi (165
R bar) and 2700 psi (185 bar).
R 4. Release the brake pedals.
Subtask 32-43-00-710-055
B. Test of the Hydraulic System
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
Pressurize the Green hydraulic system (Ref. TASK 29-23-00-863-001).
2.
Fully push in the CAPT brake pedals until they touch the stop.
3.
On the panel 402VU, set the A/SKID & N/W STRG switch to OFF.
4.
On the panel 402VU, set the A/SKID & N/W STRG switch to ON.
5.
Release the brake pedals.
Subtask 32-43-00-860-054On the panel 400VU, the tripleindicator shows no pressure indications.
The triple indicator shows the value ofthe Yellow pressure. You can hear the single chime. On the upper ECAM display unit the BRAKES A/SKID N/WS OFF indication comes into view.
The pressure indication on the tripleindicator goes to zero. On the upper ECAM display unit the BRAKES A/SKID N/WS OFF indication goes out of view.
C. Aircraft Maintenance Configuration
(1)
Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-864-001).
(2)
On the panel 110VU, put the PARK BRK control switch at ON.
(3)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
1EFF : ALL 1 32-43-00Page 507 1 1 Aug 01/05 1 1 1CES 1
5. Close-up
________ Subtask 32-43-00-942-058
A. Removal of Equipment
(1)
Remove the warning notice(s).
(2)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 32-43-00Page 508 1 1 Aug 01/05 1 1 1CES 1
HYDRAULIC RESERVOIR - BRAKE CONTROL (2624GM) - REMOVAL/INSTALLATION
___________________________________________________________________ TASK 32-43-11-000-001 Removal of the Brake Control Hydraulic Reservoir
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 plugs No specific bleed hose No specific warning notice No specific FILLER ADAPTOR TMH DI43-32-00 No specific access platform 2.0 m (6 ft. 7 in.) No specific container 5 l (1.3208 USgal)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 32-43-11-991-001 Fig. 401
3. Job Set-up
__________ Subtask 32-43-11-861-050
A. Energize the ground service network (Ref. TASK 24-42-00-861-001). Subtask 32-43-11-941-051
B. Safety precaution
(1) In the cockpit, put a warning notice in position to tell persons not to operate the brake pedals.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-43-11Page 401 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1 Subtask 32-43-11-010-050
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