2H2E, 2 hydraulic systems with 2 electric backups
Green system is no.1 and Yellow system is no.3 at 5000 psi
32
By the Green system EMP’s or the auxiliary hydraulic pump
Yellow system EDP’s or the EMP’s as aux source
EHA’s and EBHA’s in chapter 27 items and LEHGS in chapter 32
2x solenoids and a manual lockup pull ring on EDP are available for declutching
No.5 flap boat fairing
",Fuel Hyd heat exchanger located in no.1 and 4 pylons
De-clutches both engine no.1 EDP’s together
",The EDP DISC indication must be cleared by an OMS test
Case drain hydraulic fluid
A pressure vessel containing a metal bellows with Helium gas at 2600 PSI on one side and hydraulic fluid at the other side
"Cut the locking wire, undo the screw and turn the valve head emergency device with a spanner to allow dissipation of the high px helium"
Green sys no.2 pylon and yellow at no.3 pylon
Green
yellow
2x pylon 2(green) and 2x pylon 3(yellow)
"Gnd source, 4x EMP’s and cargo door aux pump"
LEHGS
Local Electrical Hydraulic Generation System
8 EHA’s and 6 or 8 EBHA dependant on mod state
High jet 5
",2 fully independent (no PTU) systems at 5000psi (green and yellow system).
Local electro hydraulic generation units. Flight controls via EHA and EBHA braking and NWS through LEHGS (local electro hydraulic generation system).
"2 modes (auto and manual, HSMU managed) auto cargo door (green), Body wheel steering (yellow). Active mode has priority. (note, only one pump operates)"
At rear of hydraulic pylons. (2G and 3Y)
Each engine has fire shut off valve upstream of EDP’s.
"Hydraulic system monitor unit (1 for green system, 1 for yellow system). In MEC (not CPIOM function) totally independent of each other."
ENG 1 and 4 pylons.
"In ENG 2 and 3 pylons, 2 per system"
","Main = EDPs, AUX = EMPs and back is via LEHGS, EBHAs and EHAs"
"Cannot, no EMPs if HSMUs fail"
AIR/HYD heat exchanger located in flap track fairing #5
FUEL/HYD heat exchanger located in outboard pylons
"Signals form HSMU, no back up"
), Odd flt # is pump A, Even flt # is pump B"
"Only PUMP A (green, cargo door ops)"
","‘ON’ illuminated in P/B on maint panel, SD will show filled green arrow for pump in operation (not connected line as this is shown when man)"
"HSMU-G is DC BUS 1 and DC GND SVC BUS, HSMU-Y is DC BUS 1 and DC BUS 2"
Each EDP has a dedicated Px switch that will illuminate a PB fault light and Indication on SD HYD page (all via HSMUs) (PX transducer can carry out function as back up)
","2 accumulators, L/H (green) in L/H WLG wheel well and R/H (yellow) in R/H WLG wheel well. Cannot be serviced on aircraft (will only hold px for 4 seconds)"
"Primary – via dedicated engine (#1 green) (#4 yellow) via RASC, Second – Pneumatic px (via central manifold), Third – Manual/ground cart (via central manifold)"
Switches at GSP (elec) or sprung P/B depress valve at reservoir
Fluid temperature (reservoir temp sensor)
",Movable index on ECAM SD and sys quantity indicator at GSP
"ECAM SD, GSP reservoir indication test and sight glass at reservoir (degrees C/degrees F)"
"Display white with an amber cross at fixed position (20degrees, 45.2 litres)"
",Electrical and mechanical clog indicators
",Class 4 message which will become class 1 fault after 700 hours
"Mechanical clogging indicator only, not elec monitored"
Return filters
"12 total, 4 EMP, 4 Air/HYD heat EXCH (EDP), 2 flap PCU, 1 slat PCU, 1 THS"
"Fans are installed downstream of each dual matrix heat exchanger (therefore 2 fans), the fans are driven by hydraulic motors and electrically controlled"
If electrical power is lost or system is de-energised the fans will run as the solenoid is energised to stop the fans
"Operation will de clutch EDP A and B for particular engine, cannot re-clutch in flight,only manually with engine shut down"
"2, (x1 depressurise, x1 declutch)"
"HYD panel P/Bs, fire switch and EECs"
Pull ring on each EDP assembly
By using a dedicated function in the OMS (ENG pump DISC indication clear)
Would just de pressurise that particular EDP
"At reset port on EDP, check ‘ON’"
HSMU will inhibit during flight
Gives priority to essential users when hyd pressure is low Mechanical spring loaded valve that will shut off supply to WLG at 3200 PSI
","Other green system users are not supplied, solenoid ports pressure to cargo doors only"
(over speed, over temp and phase imbalance)","Each hydraulic system has 1xMCPU in main avionics, MCPU will control 1xMSU"
",Near EMPs in pylons number 2 and 3
If ambient temp is greater than 75 degrees class 1 message is triggered by FWS (to protect against hot air leakage damage from heat exchanger bellows)
"There are 4 in total, 1 Main Leak Measurement Valve (MLMV) and 3 identical LMVs, When MLMV energised flow is directed to 3 LMVs and main sys isolated, LMVs will direct flow to areas of aircraft when energised, operated remotely via OMS, used to monitor flow rate to find internal leaks"
Sprung closed
"Onside (green to AC bus 1 & 2, yellow to AC bus 3 & 4) and green has Ground Service for cargo door operations."
"Green - cargo door, Yellow - Body Wheel Steering"
"From no.1 engine air via RASC, the pneumatic system or from an external source via the GSP"
",The needle will point to 0 in the centre of the green area
3
"With the EMP’s in pylons 2 or 3, there is 1 per EMP"
They live just inside the entry door to the main avionics bay from the fwd cargo bay. There is 1 per system
At least 2 ground powers