- RELIEF VALVE-HP, Y (3063GM)

 - FILTER-RSVR RETURN, Y (3002GM)

 - FILTER-HP, Y (3048GM)

 - CHECK VALVE-HP FILTER, Y (3059GM)

 - CHECK VALVE-HP MANIFOLD RETURN, Y (3022GM) R - RELIEF VALVE-BRK SYS, Y (3067GM)
 - SDAC-1 (1WV1)

 - SDAC-2 (1WV2)

 - VALVE-Y PUMP FIRE, ENG 2 (3046GD)

 - internal leakage

 - wiring

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  temperature sensor
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power AMM 29-00-00-280-003 Check of the Internal Leakage of the Yellow Hydraulic System
 AMM 29-00-00-280-006  Check of the Green or Yellow Hydraulic System after Operation in a Possible Cavitation Condition of the Engine Pump
 AMM 29-00-00-910-003 General Removal and Installation Procedure of the Check Valves in the Hydraulic Systems AMM 29-10-00-710-001 Operational Test of the Hydraulic Fire Shut-Off Valves AMM 29-13-14-000-001 Removal of the HP Manifold of the Yellow Hydraulic System
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-13-00∞∞∞∞∞∞∞∞∞∞Page 209
 Feb 01/01 CES

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 29-13-14-400-001 Installation of the HP Manifold of the Yellow Hydraulic System AMM 29-13-32-000-001 Removal of the Pressure Relief Valve of the Yellow Hydraulic System (3063GM) AMM 29-13-32-400-001 Installation of the Pressure Relief Valve of the Yellow Hydraulic System (3063GM) AMM 29-13-43-610-040 Servicing of the Engine Pump Case-Drain Filter
 (3084GM) AMM 29-13-44-610-001 Servicing of the LP-Filter (3002GM) AMM 29-13-45-610-001 Servicing of the HP-Filter (3048GM) AMM 29-13-52-000-001 Removal of the Engine Pump Fire-Valve (3046GD) AMM 29-13-52-400-001 Installation of the Engine Pump Fire-Valve (3046GD) AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
 Electric Pump AMM 29-24-00-864-001 Depressurize the Yellow Hydraulic System AMM 29-24-21-000-001 Removal of the Yellow E-Pump Check Valve (3083GM) AMM 29-24-21-400-001 Installation of the Yellow E-Pump Check Valve
 (3083GM) AMM 29-33-11-000-003 Removal of the Temperature Transmitter (3381GR) AMM 29-33-11-400-003 Installation of the Temperature Transmitter (3381GR) AMM 31-50-00-710-001 Ground Scanning of the Central Warning System AMM 31-55-34-000-001 Removal of the SDAC (1WV1,1WV2) AMM 31-55-34-400-001 Installation of the SDAC (1WV1,1WV2) AMM 31-60-00-860-001 EIS Start Procedure
R  AMM 32-44-15-000-001 Removal of the Pressure Relief Valve 3067GM
R  AMM 32-44-15-400-001 Installation of the Pressure Relief Valve 3067GM ASM 29-13/01 ASM 29-33/01
 3. Fault Confirmation
__________________

 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG  3700GD Q37
 B. Test

 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
 BEFORE YOU START A TASK ON OR NEAR:

 - THE FLIGHT CONTROLS

 - THE FLIGHT CONTROL SURFACES

 - THE LANDING GEAR AND THE RELATED DOORS

 - COMPONENTS THAT MOVE.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-13-00∞∞∞∞∞∞∞∞∞∞Page 210
 Feb 01/01 CES WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE

_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

 (2) Pressurize the Yellow hydraulic system with the electric pump (Ref. AMM TASK 29-24-00-863-001).
　
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