CPIOM G for air/ground (LGERS) (also ADIRU for altitude px etc) but NONE run it. They are all LRUs
Aft cargo fwd of T shape
FAP and the PWIP
100%
Heating and disinfection control unit, pump, inhibition of scaling module, water heater (air<10oC or water <6oC).
Switch on the LWSACD (Lavatory Water Supply-Assembly Control-Device)
On the GND and up to 16000ft
Toilet assembly MPI for toilets and GWDU MPI for galleys waste disposal— I think! MCI (Motor Control) does vac blowers
By 2 electric compressors or ground connection
Heater, Circulation Pump, De-Scaling Unit, Heating & Disinfection Control Unit (HDCU)
Aft Cargo, R/H sidewall
Manual shut-off valve
Via LWSACD
FAP or PWIP
Switch on service door gives inhibit signal to MCI for Vac Gen
Below 16,000 ft or if altitude signals are lost
Set to operate as if below 16,000 ft
Multi Purpose Interface (MPI)
Motor Controller Interface (MCI)
5000 psi
4 EDP 2 EMP
A
Check HP accumulator via ATA 32 LEHGS
GND SRVC panel and from reservoir
GSP, ECAM HYD page, OMS report reservoir level, sight glass on reservoir
HP Filters, Return Filters and Case drain filters (reservoir filter is mechanical only and not ellectrically monitored)
Return filter
Turn the reset on the EDP body
Cargo doors are operating the pump
The Inner manifold (the other manifolds are Belly and outer)
Case drain line (the other lines are return line and pressure line)
Cargo door ops or Body Gear Steering
MCPU
HSMU
Reservoir T by HSMU
The HP manifold. 1 PX transmitter (it also has 3 px switches)
Manually with valve on reservoir or electrically via remote depressurisation switch on ground service panel
5000 psi
Case Drain return line to the reservoir
HSMU, using Fan Isolation Valve
CDLCU
Up to 120s (then flash for 5s)
Cabin Pressure and slide armed
Above 60knots and 24000 to 28000 feet
CFRP
LDC
Open the door handle and use switches inside
8 hours
In the arming lever
Aircraft pressured still (>2.5mb)
Green light in panel
DSMCU---> HSMU
It has counterweight springs (2) and a door uplock
3
DSMCU
Autonomous Standby Power Supply Unit (ASPSU)
M1
Px equalisation valve
LDC
Press the manual inflation button
M3 and M1 extension
Push OK button for 3s
Door closed and locked or from FAP Maintenance P/B
Make sure they are all lowered
2. 1 inside and 1 outside
Pitch Attitude Sensor (PAS) in upper AV bay sends signal to LDC
Mechanical Coding Pins, specific order to that location.
Door Sill latches NOT in the UP position
system 1
System 2
DC ESS
DC2
Green
To prevent large fluid loss
selector valves for doors , selector valves for gear
3 cut-out valves (stop supply and connect to return line) 5 vent valves (actuators to return line)
Bypass valves
Behind Captain
5
On the lock link
BLG
To provide wheels down attitude
Rearward
Outer door
Door Bypass Valve
After each full extension and retraction.(Landing Gear Control Indication System sys1 and 2)
SEPDC and SSPC
Using the SEPDC
CPOIM-G, LGERS app
LGRDC 4A/B (also does WLG)
Green
3 per unlock, NUA (1) and EUA (2)
Inner, Centre and Outer. (Auxiliary is mechanically driven by Inner)
Door Selector Valves, Landing Gear Selector Valves.
Cut-Out Valves, Vent Valves
Door Bypass Valves
5 green arrows
Timer. 63 secs to all gears down and locked.
Electric power, Hydraulics, Handle
Remove Maintenance Panel, Simulate gear extended on Pros switches
Normal, Alternate, Ultimate and Emergency (Parking uses HP Accumulators)
BLG Alternate system px. Upper Lowest HP Acc, Lower L/R Px to brakes
CPOIM-G, BCS app
Normal braking available (CPOIM/IRDC), Gear extended, 3 Secs upon retraction.
2, Comfort and Performance
Electronic Control Module (ECU) on each LEHGS
When EBCU gets Park Brake discrete and PRIM Logic (Ground Spoilers deployed or on ground, <15 its, min 1 Eng running)
CPOIM-G, WSCS App
No Green Hyd Px or HP accumulator Px low
Yellow
Comfort and Performance(in use pump on all time).
The ARV
A/c in flight, shock extended, no faults , Autobrake armed.L/g lever set to up . CPIOM and IRDC in control .
per WLG X2 ABSELV’S and x2 ASV’s
EBCU and HYD PWR by LEHGS/HP ACCUM.
EBPTU on the Capts pedals and NBPTU on the F/o’s
)and PBSELV
the L/G used are the BLG 4000psi and WLG(to sdy)1740psi
part of the NORM system and QTY 2
Qty 1 purpose to refill LEHGS
x2
EBPTU
CPIOM fails or ANTI skid sw to off !
Auto- less 30kts on taxi out, on GND. Manual via OMS,CMS test.
1700psi
BCS is in CPIOM G Side 1 is G1&G3 side 2 is G2&G4
Emergency braking is by EBCU and Rudder pedals EBPTU
4000psi
BWS LVDT must be in locked position.
Conventional, EHA, EBHA
Backup Control Module (BCM)
None
CPIOM-C (x2) and Flight Control Data Concentrator (FCDC) app
DC ESS Bus
Pedals via Pedal Feel Transducer Unit (x2)
Sidestick input - provides co-ordinated turn
PRIM and SEC can do Direct Law (SEC can only compute Direct)
NZ Vertical Accel (4), NY Lateral Accel (4), NZ LAF Verfical Accel for LAF (6) and Rate Gyros (6)
2 feedbacks, one to each channel
Active and Damping
Loss of hydraulics, Mode Select Valve (MSV) closed, damping restrictor limits flow between chambers
4. Hydraulic, Retracted, Blocking, Maintenance
Maintenance mode, operated via key, manually opens blocking valves
Electronic Module
5. Hydraulic Active, Retracted, Electric Active, Blocking, Maintenance
Solenoid valve closed, EM controls motor speed/direction
Solenoid valve open, servo valve controls movement
Inboard Aileron (conventional PCU), Outboard Elevator (Conventional PCU) & both Rudders (Upper EBHA)
Pitch Trim Switches
3, Green sys, Yellow sys & Electric (if installed)
OMS
On the ground it is inhibited unless Hyd power is supplied to a/c
Via Sidestick Transducer and Damping Units (SSTDU) - 14 potentiometers
Pedal Transducer Units (2)
Pull lever up to “Arm” auto speedbrake, Push lever down and move rearwards to manually extend
CPOIM-C, Flight Control Data Concentrator (FCDC)
Electronic Module on each PCU
5, Hyd Active, Retracted, Elect Active, Blocking, Maintenance
Use maintenance key to manually operate blocking valves
Yellow motor from Pitch Trim switches
PRIM and SEC (SEC can ONLY compute Direct Law)
PTA = Ailerons and Spoilers 6-8, ATA = Inner and Mid Ailerons
Amber X is due to position feedback loss, amber box is due to control loss
Reset CB for Slat 1/2, Flap 1/2
They both operate (if not on ground) but at half speed
2, 3 or Full
Auto reset when torque reduced, but pop-out indicators have to me manually reset on ground.