(2)
Make sure that the PARKING BRK control switch is set to OFF (released) before you do the reactivation.
4. Procedure
_________
Subtask 32-42-00-440-052
A. Reactivation after Deactivation without Removal of the Brake R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 402/TASK 32-42-00-991-002)
1EFF : ALL 1 32-42-00Page 414 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
(Ref. Fig. 402A/TASK 32-42-00-991-002-A)
**ON A/C ALL
(1)
Cut and remove the lockwire that attaches the two knurled sleeves (1) and (4).
(2)
Remove the self-adhesive fabric tape from the sleeves (1) and (4).
(3)
Connect the sleeves (1) and (4) to the half couplings (2) and (3).
(4) Bleed the brake unit (Ref. TASK 32-43-00-870-002).
Subtask 32-42-00-440-053
B. Reactivation after Deactivation with Removal of the Brake R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 402/TASK 32-42-00-991-002)
**ON A/C 301-399,
(Ref. Fig. 402A/TASK 32-42-00-991-002-A)
**ON A/C ALL
(1)
Remove the wheel of the related main landing gear (Ref. TASK 32-41-11-000-006).
(2)
Cut and remove the lockwire that attaches:
-
the two knurled sleeves (4) and (12),
-
the electrical connector (9) of the brake temperature sensor.
(3)
Install the brake unit (3) (Ref. TASK 32-42-27-400-001).
1EFF : ALL 1 32-42-00Page 415 1 1 Aug 01/05 1 1 1CES 1 Subtask 32-42-00-710-064
C. test
(1)
Do the Operational Test of the Normal Braking System (Ref. TASK 32-42-00-710-001).
(2)
Do an Operational Test of the Alternate Braking System (Ref. TASK 32-43-00-710-001).
(3)
During these tests, make sure that there are no leaks on the hydraulic connections.
5. Close-up
________ Subtask 32-42-00-860-072
A. Put the aircraft back to its initial configuration.
(1)
Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-10-00-864-001) and (Ref. TASK 29-10-00-864-002).
(2)
Make sure that the level of the fluid in the Green and Yellow hydraulic reservoirs is correct. Add some fluid if it is necessary (Ref. TASK 12-12-29-611-001).
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(4)
Remove the warning notice(s).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-42-00Page 416 1 1 May 01/04R 1 1 1CES 1
TASK 32-42-00-040-002
Deactivation of the Normal Braking - With disconnection of the Green Hydraulic Supply
1. Reason for the Job
__________________
Refer to the MMEL TASK: 32-42-02
Normal Braking - Green Brake System
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific self-adhesive fabric tape
No specific temporary placard
No specific vinyl hose
No specific warning notice(s)
No specific container 5 l (1.3208 USgal)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific corrosion resistant steel lockwire dia 0.8 mm
R Material No. 02-003 F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
1EFF : ALL 1 32-42-00Page 417 1 1 Feb 01/05 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 29-10-00-864-001 Depressurize the Green Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump 32-42-00-991-004 Fig. 403
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