2000/6000/7000
Aluminium for main and CFRP for upper (aft of frame 26).
GLARE, GRFP, CFRP
QFRP Quartz Fibre Reinforced Plastic
CFRP and Aluminium alloy for the tension strut
Titanium alloy
Fuselage skin fwd upper and shell FR22 to 38 (section13) , upper fwd from FR38 to 46 (section 15), aft upper skin FR 74 to 95 (section 18) (the rest is alloy except for CFRP FR95 to 120) <—— this isn’t what he said!!! so I might be wrong
No
Tailcone, Flap Track, Eng Exhaust and landing gear bogie beams.
Glass Fibre and aluminium
Sandwich and Monolithic
A
3
EBAS PADS OHDS and optionally SCS
EBAS
Auto, and it splits L and R sides
ECB
On GND goes to open (ALL the isolation valves go to open on GND)
4 (L, C, R and APU)
It goes to the relay system
The transfer Px sensor and the pressure sensor…. WTF!!!
By a rod
4
No 2
EBAS
CPIOM-B, EBAS App
Regulated Pressure transducer (Pr). Also closes for over-temp/reverse flow
EBAS, uses Pre-cooler Differential Px Transducer to sense and closes Bleed Valve
OHDU. 1=Loop A, 2=Loop B
2 and 3 <—— page 226
Closed
TBV (and to support TCV)
Closed
The pack reset CB
1 (The other is Hot Stby)
Controls the VCM and heating and ventilation (p.416 412 402 386)
Open( no idea why or how) if one of the TAPRV is shut you only have air from one FCV so the two TASOV open to link the operating flow to the other 2 quadrants of the trim air manifold
Non Pressurised area (Only TASOV and TAV in pressurised area)
Stepper motor
Fwd Cargo L/H side (Triangle )
Just 1
OVERHEAT COND FANS RESET button
VCS via VCM
2 (3 for -900)
Normal from ACP(Automatic Control Partition) Backup from DPSM (Differential Pressure Sensor Module)
3 EPP. (The partitions are Automatic Control Partition (ACP), the Safety and Override Partition (SOP) and the Emergency Pressurization Partition (EPP) )
CPIOM-B, AGS App, calculates Flow Demand
Mixer Unit
4 HP fans, 8 HEPA Filters (+2 optional)
CPIOM-B, VCS App and VCM Fwd (left fans) and Aft (right fans)
1 motor per door, 2 doors per AGU. RAID (inlet) is 1 door, 2 motors
To prevent freezing of condenser and provides assistance to TCV if full open and mixer temp too low.
In each wing root
Open to provide Trim Air to the other 2 quadrants normally served by the closed TAPRV
FCV 2 and 3, via TAPRVs
Trim Air Drive Device (TADD) In Fwd Cargo, Left Triangle (sidewall)
CPOIM-B, VCS App, and VCM Fwd and Aft
VCM Aft (they are in the aft bulkhead)
CPOIM-B, CPCS App, OCSMs (ACP to EPP), Outflow Valves
ECAM SD “CAB PRESS” page
To supply cold air from the mixer unit to cool the Fwd Cargo
VCM Fwd
CPIOM-B, using VCS App, VCM Fwd and TCS App, TADD for trim Trim.
Via an In-Line Duct Heater that heats LP Recirc Manifold Air, controlled by CPIOM-B, VCS App, VCM Aft Back-up.
Outboard Engines, via both WAIV. Inboard Engines can be used as alternate via X-Bleed ducting
28VDC for AICU, 115VAC for Heater elements
5 IPCU, 5 IPDU. 3 for Water/Waste, 2 for Floor Panel Heating
OCSMs are 2 and 4 they have 2 ports extra sensor OCM are 1 and 3
VCM fwd was the answer maybe
CPIOM B VSC App
VCM AFT
LP air manifold.
(On ground, during static or low speed operation, an additional inlet flap in the bottom of the belly fairing and a fan assembly are needed to provide sufficient airflow to the condenser. The Ram Air Channel Actuator (RACA) opens this ground air inlet flap in the air channel and the fan assembly, consisting of two fans, draws the ambient air through each condenser.)
With Nitrogen. Individual charging of accumulators with service lines, vent line as well to remove px .
Galden. Own service fill line before pump
Controller behind accumulator in the belly fairing.
CPIOM A
Bulk Cargo Heater Switch ( B2 & B4 VCS app controls can bus via VCM AFT)
COOL G p/b sw on vent panel and SCS reset switches.
The overboard and inboard valves.
When Flow or Temp is low (CED sensor)
Pneumatic air
FDAC. 1 —> L. 2 —> R.
VCM AFT
p/b AV EXTRACT to OVRD.
AVS
both detectors go to AICU 1 and AICU 2
AICU’s
Outboard engines by outer antice valves. Alternate is 2 and 3 via inner antice valves
CYClone nozzle
AICU to vlv solenoid then HP3 muscle air to Close
regulate the air to 74 psi (Alliance Engine is 100 psi)
All of them do. 1st is taken for regulation then 2 if 1 fails. Then 3 if 2 fails
No1 windscreen=1, No2 and sliding is 3.
2 power levels on the windscreen and 1 level for the sliding and fixed.
Total 5 IPCU’s (ipdu’s are married) 3 for Water ice protect. And 2 for floor panel heating.
it is SPDB 7 and 8 115vac and 28vdc.
7 and 8 in fwd and aft cargo others throughout MD.
in upper avionics.
partially open
Titanium Alloy
4 EBAS OHDS SCS PADS!
CPIOM B (AGS)
4 HP fans total and 9 LP’s throughout U/D (he said 8 but 9 (with 10 as an option) is what is think too)
Open
in the FWD cargo
Bulk CC Extraction isolation valve, Bulk CC supply isolation valve and bulk CC and T shape Isolation Valve
VCM AFT
VCS reset 1 and 2
AVS overboard vlv not open on ground.
2 AFT CC Supply VLV’s (trim air) and you have the 1 shared extract bulk cargo fan isolation valve. And you have the 1 Bulk and ‘T’ shape isolation valve. So four valves all together I'm not counting the dedicated Bulk supply valve from HEATER. So 4 in total for the sys. 3 supply isolation valves if they want that ! and only 1 Bulk extraction valve that every fucker shares.
2 supply valve the post Heater supply/iso and the T shape supply/iso . plus the share Extract fan iso.