(4)
Lubricate the new O-ring (3) with HYDRAULIC FLUIDS (Material No. 02-003).
(5)
Put the new O-ring (3) in position on the temperature transmitter (2).
(6)
Install the temperature transmitter (2) to the filter head (4).
(7)
TORQUE the temperature transmitter (2) to between 4.0 and 4.5 m.daN
(29.49 and 33.18 lbf.ft).
(8)
Install the bonding jumper (7) together with the washer (6) and the nut (5) (Ref. TASK 20-28-00-912-004).
(9)
Remove the blanking cap from the electrical connector (1).
(10) Make sure that the electrical connectors are clean and in the correct
condition.
(11)
Connect the electrical connector (1). Subtask 29-33-11-865-053
B.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2701GJ, 2702GJ
Subtask 29-33-11-790-051
C. Leak Test of the Hydraulic Connections
(1)
Remove the warning notices from the ground service panel and from the overhead panel.
(2)
Pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).
(3)
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
(4)
Examine the temperature transmitter connection and make sure that there are no leaks.
Subtask 29-33-11-860-053
D. Test of the Temperature Transmitter
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(3)
On the ECAM control panel on the center pedestal push the HYD pushbutton. Make sure the the HYD page on the system (lower) display comes on.
(4)
Make sure that the ECAM system shows no overtemperature.
(5)
Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
5. Close-up
________ Subtask 29-33-11-860-059
A. Put the aircraft back to the serviceable condition.
(1)
Make sure that the fluid level in the reservoir of the Blue hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001).
(2)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(3)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
(4)
Remove the container from below the temperature transmitter.
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
(6)
Close the access panel 197FB.
TASK 29-33-11-000-003
Removal of the Temperature Transmitter (3381GR)
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
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 cap No specific blanking plugs No specific circuit breaker(s) safety clip(s) No specific container No specific warning notices
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 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU) 29-33-11-991-001 Fig. 401
3. Job Set-up
__________
Subtask 29-33-11-865-054
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/HYD POWER/Y 3803GX N30 121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG 3700GD Q37 123VU Y HYD/ELEC/PUMP 3802GX AB06
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