NOTE : One electrical motor of the parking brake control valve may be
____ inoperative provided both thrust reversers are operative.
NOTE : If the motor, supplied by the HOT BUS 701PP is inoperative, the
____ parking brake valve will not operate if the aircraft is supplied by batteries only.
NOTE : If the motor, supplied by the HOT BUS 701PP is inoperative, the
____ aircraft towing is not allowed if the aircraft is supplied by batteries only.
Subtask 32-45-00-860-055
B. Aircraft Maintenance Configuration
(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
5. Close-up
________ Subtask 32-45-00-942-052
A. Removal of Equipment
(1)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2)
Remove the warning notice(s).
(3) Remove the access platform(s). Subtask 32-45-00-410-051
B. Close Access
(1) Close the right MLG door (Ref. TASK 32-12-00-410-001).
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R Parking Brake Electrical Control Valve 102GG R Figure 401A/TASK 32-45-00-991-002-A
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PARKING/ULTIMATE EMERGENCY BRAKING - ADJUSTMENT/TEST
____________________________________________________ TASK 32-45-00-710-001 Operational Check of the Parking Brake System Using Individual Motors in Turn WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
WARNING : PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR
_______ THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______
OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 324500-01
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice(s)
No specific access platform 2 m (6 ft. 7 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
1EFF : ALL 1 32-45-00Page 501 1 1 May 01/05 1 1 1CES 1
B. 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 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
29-24-00-864-001 Depressurize the Yellow Hydraulic System
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
32-45-00-991-001 Fig. 501
R **ON A/C ALL
3. Job Set-up
__________
Subtask 32-45-00-860-051
A. Aircraft Maintenance Configuration
(1)
On the panel 400VU, make sure that the landing gear control lever is in the DOWN position.
(2)
On the panel 110VU, make sure that the PARKING BRK control-switch is in the OFF position.
(3)
Make sure that the CAPT and F/O brake pedals are released.
(4)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
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Subtask 32-45-00-010-050
B. Get Access
(1) Open the right MLG door (Ref. TASK 32-12-00-010-001).
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