(2)
Remove the warning notices from the cockpit and the ground service panel.
(3)
Make sure that the fluid level in the Yellow hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001).
(4)
Pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002).
(5)
Examine the connection of the fluid sampling valve (1) and the manifold and make sure that there are no leaks.
(6)
Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
1EFF : ALL 1 29-13-34Page 410 1 1 May 01/04R 1 1 1CES 1
5. Close-up
________ Subtask 29-13-34-860-052
A. Put the aircraft back to the serviceable condition.
(1) Connect the isolation coupling of the power transfer unit (Ref. TASK 29-23-00-860-002).
(2)
Remove the container. Subtask 29-13-34-410-050
B.
Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access panel 196BB.
(3)
Close the access door 198CB. Subtask 29-13-34-865-052
C.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1831GQ, 1832GQ, 3801GX, 3802GX, 3803GX
1EFF : ALL 1 29-13-34Page 411 1 1 May 01/04R 1 1 1CES 1
CHECK VALVE - ENGINE 2 THRUST REVERSER (3010KM2) - REMOVAL/INSTALLATION
_______________________________________________________________________
TASK 29-13-35-000-001
Removal of the Engine 2 Thrust Reverser Check Valve (3010KM2)
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 blanking plug
No specific cloth
R No specific warning notice No specific wrench No specific access platform 1.50 m (4 ft. 11 in.) No specific container 5 l (1.3208 USgal)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
29-24-00-864-001 Depressurize the Yellow Hydraulic System
71-13-00-010-040 Opening of the Fan Cowl Doors
R 78-30-00-040-040 Deactivation of the Thrust Reverser System 29-13-35-991-001 Fig. 401
3. Job Set-up__________
R Subtask 29-13-35-860-050-A
R A. Aircraft Maintenance Configuration
R (1) Depressurize the Yellow hydraulic system (Ref. TASK 29-24-00-864-
R 001).
R (2) Depressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-
R 001).
R (3) Put a warning notice in position to tell persons not to pressurize
R the Yellow hydraulic system:
R - on the ground service panel 198CB.
R (4) Put a warning notice on the access door 195BB to tell persons not to
R pressurize the Yellow hydraulic reservoir.
R (5) Make the thrust reverser system unserviceable (Ref. TASK 78-30-00-
R 040-040).
R Subtask 29-13-35-941-052-A
R B. Safety Precautions
R (1) On the ENG MASTER control panel 115VU:
R - make sure that the ENG 2 switch is in the OFF position
R - put a warning notice to tell persons not to start the engine 2.
R (2) Make sure that the engine 2 shutdown occurred not less than 5 minutes
R before you do this procedure.
R (3) Put a warning notice in position to tell persons not to pressurize
R the Yellow hydraulic system:
R - on the HYD section of the panel 40VU.
R (4) On the ENG section of the panel 50VU:
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