-in the cockpit, on the HYD section of the overhead panel 40VU.

 (4)
 On the overhead maintenance panel 50VU:

 -make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.

 (5)
 Put warning notice(s) to tell persons not to energize the FADEC 1(2).

 (6)
 Put a container below the fluid disconnect panel to collect the hydraulic fluid.

 Subtask 29-13-38-865-050
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG 3700GD Q37 121VU HYDRAULIC/Y HYD/PUMP ENG2/CTL 3701GD Q36
 Subtask 29-13-38-010-051
 D. Get Access
 (1)
 Open the left fan-cowl door 447AL (Ref. TASK 71-13-00-010-040).

 (2)
 Open the access door 195BB.

 (3)
 Put the access platform in position at the engine.

 4. Procedure
_________
 (Ref. Fig. 401/TASK 29-13-38-991-901) Subtask 29-13-38-020-051
 A. Removal of the Engine 2 Pump Suction Self-Sealing Coupling
 (1) Disconnect the suction hose (5) from the self-sealing coupling (15). Drain the hydraulic fluid directly into the container.
 NOTE : Use a second wrench to hold the self-sealing coupling (15)
____ when you loosen the coupling nut on the suction hose.
 (2) Disconnect the self-sealing coupling (15) from the union on the hydraulic pump (10).
 NOTE : Use a second wrench to hold the self-sealing coupling (15)
____
 when you loosen it.

 (3) Install protective covers on the self-sealing coupling (15), the suction hose (5) and the union on the hydraulic pump (10).

 Engine 2 Pump Suction Self-Sealing Coupling
 Figure 401/TASK 29-13-38-991-901
 1EFF :  ALL  1  29-13-38 Page 404 
1  1  Feb 01/98
 1  1
 1CES  1

 TASK 29-13-38-400-041
 Installation of the Engine 2 Pump Suction Self-Sealing Coupling (3672GM)
 WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
 WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
 CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC
_______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific absorbent material
 No specific warning notice(s)
 No specific access platform 1.50 m (4 ft. 11 in.)
 No specific container 5 l (1.3208 USgal)
 No specific Torque Wrench : range 2.00 to 20.00 m.daN

 (15.00
 to 150.00 lbf.ft) No specific Torque Wrench : range 6.00 to 36.00 m.daN

 (50.00 to 260.00 lbf.ft)

 B.
 Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic
 Service Cart 29-13-00-710-002 Operational Test of the Yellow Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector
 29-23-00-863-002  Pressurize the Yellow Hydraulic System from the Green Hydraulic System through the PTU with the Ground Service Cart
 29-24-00-864-001 Depressurize the Yellow Hydraulic System 29-13-38-991-901 Fig. 401 FOR FIN 1000EM2 71-13-00-410-040 Closing of the Fan Cowl Doors
 3. Job Set-up
__________
 Subtask 29-13-38-860-053
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the Yellow hydraulic system is depressurized (Ref. TASK 29-24-00-864-001).

 (2)
 Make sure that the Yellow hydraulic reservoir is depressurized (Ref. TASK 29-14-00-614-001).
　
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