5. Close-up
________ Subtask 29-00-00-860-053
A. Put the aircraft back to the serviceable condition.
(1)
On the overhead panel 50VU, lift the guard and set the HYD/LEAK MEASUREMENT VALVES/G P/BSW to on. Make sure that the OFF light goes off.
(2)
Refer to the lower DU of the ECAM (HYD page) and make sure that the solenoid valve has operated correctly (the flow arrow of the Green hydraulic system is colored green and the system name is colored white).
(3)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
(4)
Connect the PTU isolation coupling (Ref. TASK 29-23-00-860-002).
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
(6)
Close the right main door of the main gear (Ref. TASK 32-12-00-410-001).
(7)
Disconnect the ground hydraulic supply from the aircraft ground test connections.
(8)
Install the blanking caps on the ground test connections.
(9)
On the overhead panel 40VU, set the PTU P/BSW to AUTO (the OFF and FAULT lights are not on).
(10)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(11)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 29-00-00-410-052
B. Close the access door 197CB.
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TASK 29-00-00-280-002
Check of the Internal Leakage of the Blue Hydraulic System
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
To make sure that the internal leakage of the system and parts of the system are in limits.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
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 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
29-10-00-864-003 Depressurize the Blue Hydraulic System
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
**ON A/C 001-049, 051-061, 101-105, 201-203,
29-00-00-991-005 Fig. 605
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
29-00-00-991-005-A Fig. 605A
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-061, 101-105, 201-203,
R 29-00-00-991-006 Fig. 606 **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
29-00-00-991-006-A Fig. 606A **ON A/C 001-049, 051-061, 101-105, 201-203,
R 29-00-00-991-007 Fig. 607 **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
29-00-00-991-007-A Fig. 607A **ON A/C 001-049, 051-061, 101-105, 201-203,
R 29-00-00-991-008 Fig. 608 **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
29-00-00-991-008-A **ON A/C ALL Fig. 608A
3. Job Set-up__________ Subtask 29-00-00-010-052 A. Open the access doors 195BB, 197EB.
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B. Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION ------------------------------------------------------ IDENT. LOCATION-------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
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