(28)
Tighten the nut (14).
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(29)
Remove the blanking caps from the electrical connectors and the receptacles.
(30)
Make sure that the electrical connectors are clean and in the correct condition.
(31)
Connect the electrical connectors (40),(41),(15). Subtask 29-11-41-861-050
C.
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). Subtask 29-11-41-865-052
D.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1701GK, 1702GK, 1831GQ, 1832GQ.
Subtask 29-11-41-710-050
E. Test of the Reservoir
(1)
Do an operational test of the low level warning (Ref. TASK 29-31-00-710-001).
(2)
Do an operational test of the low air pressure warning (Ref. TASK 29-34-00-710-001).
(3)
Make sure that the level of fluid in the reservoir of the Green hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).
(4)
Pressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-002).
(5)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(6)
On the ECAM control panel on the center pedestal, push the HYD pushbutton. Make sure that the HYD page on the ECAM lower DU comes on.
(7)
Make sure that the two reservoir contents gages (one on the reservoir and one on the ground service panel of the Green system) show the same contents and agree with the ECAM contents indication.
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(8)
Examine the reservoir and the pipe connections and make sure that there are no leaks.
(9)
Apply leak detector SPECIAL MATERIALS (Material No. 05-004) to the reservoir and air pipe connections and make sure that there are no leaks.
(10)
Pressurize the Green hydraulic system (Ref. TASK 29-10-00-863-001).
(11)
Keep the Green hydraulic system pressurized for 5 minutes to let the hydraulic system bleed.
(12)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
5. Close-up
________ Subtask 29-11-41-860-051
A. Put the aircraft back to the serviceable condition.
(1)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002) .
(2)
De-energize the aircraft electrical circuit (Ref. TASK 24-41-00-862-002).
(3)
Make sure that the fluid level in the reservoir of the Green hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).
(4)
Connect the isolation coupling of the Power Transfer Unit (PTU) (Ref. TASK 29-23-00-860-002).
(5)
Remove the container.
(6)
Remove the access platform.
(7)
Remove the warning notice from the cockpit and from the ground service panel of the Green hydraulic system.
(8)
Make sure that the work area is clean and clear of tool(s) and other items.
(9)
Close the main doors of the main gear (Ref. TASK 32-12-00-410-001).
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TASK 29-11-41-000-002
Removal of the Quantity Indicator of the Green Hydraulic Reservoir
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
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 caps
No specific blanking plug
No specific circuit breaker(s) safety clip(s)
No specific container
No specific plastic bag
No specific warning notices
No specific access platform 2.6 m (8 ft. 6 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-680-001 Drainage of the Reservoir of the Green Hydraulic
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