A320飞机维护手册 AMM HYDRAULIC POWER 液压3(95)

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 Most of the components of the system are installed in the Yellow hydraulic compartment in the RH belly fairing, forward of the main gear compartment. The system is kept physically apart from the other two systems where possible. The system is hydraulically isolated from the other two systems. It is not possible for fluid to go from one system to another. The system operates at a nominal pressure of 3000 psi (206 bar). The Engine-driven Pump (EDP) can supply 140 l/min (37 US gal/min) at 196 bar (2854 psi) at its usual operating speed. The return part of the system is pressurized to 50 psi (3.5 bar). It is possible to pressurize the HP system from any of three different sources: - the Engine Driven Pump (EDP), - the Power Transfer Unit (PTU), - the ground supply connections. - the Yellow electric pump (Ref. 29-24-00) - the hand pump for the operation of the cargo doors (Ref. 29-24-00/52-36-00)
 Operation of the system is usually automatic, but the crew can control parts of the system from the flight compartment if required.
 The Electronic Centralized Aircraft Monitoring (ECAM) system monitors the condition of the system all of the time. When a fault occurs, or if the crew select it, system information is shown in the flight compartment. 
R  **ON A/C 401-499, 
R R R R R  The Yellow hydraulic system is one of the three systems which supply the aircraft with hydraulic power. It supplies: - the cargo doors, - the alternate and parking brake systems, - the right-hand (No. 2) engine thrust reverser,

 

R  - some of the flight controls, 
R  - the Power Transfer Unit (PTU), 
R  - the Nosewheel Steering. 
R 
R  Most of the components of the system are installed in the Yellow hydraulic 
R  compartment in the RH belly fairing, forward of the main gear compartment. 
R  The system is kept physically apart from the other two systems where 
R  possible. The system is hydraulically isolated from the other two systems. 
R  It is not possible for fluid to go from one system to another. The system 
R  operates at a nominal pressure of 3000 psi (206 bar). The Engine-driven Pump 
R  (EDP) can supply 140 l/min (37 US gal/min) at 196 bar (2854 psi) at its 
R  usual operating speed. The return part of the system is pressurized to 50 
R  psi (3.5 bar). It is possible to pressurize the HP system from any of three 
R  different sources: 
R  - the Engine Driven Pump (EDP), 
R  - the Power Transfer Unit (PTU), 
R  - the ground supply connections. 
R  - the Yellow electric pump (Ref. 29-24-00) 
R  - the hand pump for the operation of the cargo doors (Ref. 
R  29-24-00/52-36-00) 
R 
R  Operation of the system is usually automatic, but the crew can control parts 
R  of the system from the flight compartment if required. 
R 
R  The Electronic Centralized Aircraft Monitoring (ECAM) system monitors the 
R  condition of the system all of the time. When a fault occurs, or if the crew 
R  select it, system information is shown in the flight compartment. 
R  **ON A/C ALL
 2. Component Location__________________
 **ON A/C 001-049, 051-058, 101-101,
 (Ref. Fig. 001) 
R  **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 001A)
 **ON A/C ALL
 (Ref. Fig. 002) 

R 1EFF : ALL 1 29-13-00Page 2 1 1 Aug 01/05 1 1 1CES 1

 Component Location Figure 001 
R 1EFF : 1 1 1CES  001-049, 051-058, 101-101,  1 111 29-13-00 Page 3 Aug 01/05

 

R Yellow Hydraulic System - Component Location Figure 001A
R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 29-13-00Page 4 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

R Yellow Hydraulic System Equipment at FR46 and FR47 - Component Location -
R  (Sheet 1)
 Figure 002
 1EFF :  ALL  1  29-13-00 Page 5 
1  1  Aug 01/05
 1  1
 1CES  1

 

 **ON A/C 001-049, 051-058, 101-101,
 (Ref. Fig. 003)

R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 003A)
 **ON A/C ALL
R (Ref. Fig. 004, 005, 006, 007, 008, 009)
 **ON A/C 001-049, 051-058, 101-101,
 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
 | | | | DOOR | REF. -------------------------------------------------------------------------------3000GQ RSVR-Y 196 196BB 29-13-41 3002GM FILTER-RSVR RETURN,Y 196 196BB 29-13-44 3006GM GND CNCTR-SELF SEALING, Y SUCTION 198 198CB 29-10-00 3008GM GND CNCTR-SELF SEALING, Y DELIVERY 198 198CB 29-10-00 3010GM COMPENSATED SLIDE-SUCTION, Y 641 674AB 29-13-47 3017GM CHECK VALVE-ELEC PUMP CASE DRAIN, Y 196 196BB 29-10-00 3018GM CHECK VALVE-PTU SUCTION, Y 197 197EB 29-10-00 3019GM CHECK VALVE-PTU RETURN, Y 146 744 29-10-00 3020GM CHECK VALVE-PTU CASE DRAIN, Y 146 744 29-10-00 3022GM CHECK VALVE-HP MANIFOLD RETURN, Y 196 196BB 29-10-00 3024GM CHECK VALVE-BRK RETURN, Y 146 744 29-10-00 3030GD PUMP-Y, ENG 2 445 447AL 29-13-51 3041GM CHECK VALVE-ENG 2 PUMP CASE DRAIN, Y 413 447AL 29-13-37 3046GD VALVE-Y PUMP FIRE, ENG 2 674 674AB 29-13-52 3048GM FILTER-HP, Y 196 196BB 29-13-45 3050GM CHECK VALVE-ENG 2 PUMP DELIVERY, Y 423 196BB 29-13-36 3056GM CHECK VALVE-FWD CARGO DOOR RETURN, Y 146 734 29-10-00 3058GM CHECK VALVE-BRK SYS, Y 148 744 29-10-00 3059GM CHECK VALVE-HP FILTER, Y 196 196BB 29-10-00 3063GM RELIEF VALVE-HP, Y 196 196BB 29-13-32 3064GM PRIORITY VALVE-Y 147 734 29-13-33 3067GM RELIEF VALVE-BRK SYS, Y 148 744 29-10-00 3070GM ACCU-Y PWR 196 196BB 29-13-42 3071GM VALVE-NITROGEN CHARGING, Y PWR ACCU 196 196BB 29-20-00 3072GM PRESS GAGE-Y POWER ACCU 196 196BB 29-13-21
　
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