I will come bach on NWWW asap

stopped here:
http://avianascenery.blogspot.com/
Glad to hear your back to developing
Now about the electrical system.
The aircraft is powered by four sources, each operating individually and at various stages of flight. The first one ofcourse is the EPU (or GPU for Ground Power Unit), which is connected to aircraft while stationary with the engines turned off. The EPU would officially be classified as "Ground Service Equipment" as it's not part of the aircraft and in most cases feautures the logo of the service company or the airport. The next powerplant is the APU. It's turned on when the aircraft is nearing the pushback to prepare for the release of the EPU and to start the next source, the main generators in the engines. The APU-design is different from previous Airbus aircraft (specifically the A320-family) wchich feautued an intake beteeth the Tail and the opening to the rear. The APU on this aircraft feautures a design similar to that on the Boeing 777, thus a bigger intake near the rudder with the intake facing the direction of flight (thanks to Roel who noted this to me).
The APU should on it's turn give enough "electricity" (because we all know that word isn't a meausurable unit or anything, though this Honeywell HGT1700 produces 1,268 kW) to start the main generators located in the engines. This is supposed to be a smooth transition, however I've noticed on older Airbus models (specifically the A320-family aircraft) that the transistion tends to be rather crued with a cabin light-out of about a second on the switch between APU and main generators. I have however never flown on an A350 so I can't say if the same things tends to happen on the A350.
The last official source (but not a generator) are the batteries. They where supposed to be Lithium-Ion instead of conventional Nickel-cadmium batteries. However in light of the Boeing 787s Lithium-Ion batteries catching fire, which lead to the grounding of the 787 fleet in January 2013, Airbus decided that for the time being the A350 would receive Nickel-cadmium batteries. This does not mean that the idea of Lithium-Ion batteries has been whipped of the charts, Airbus is still testing the batteries that where intended to be fitted in the aircraft (and this is one of the reasons why the aircraft are still being tested at Toulouse) and Airbus will probably retro-fit existing A350s as soon as the Lithium-Ion batteries enter service with aircraft still in production. The Batteries are, just like on other commercial jetliners, primarilly ment for emergency use in case the main generators (or the APU) fails. In this case the system will reduce the electrical use of the aircraft to a bare minimum, control surfaces and primary flight instruments. Now I don't know what exactly happens in that scenario but I would assume it's similar to the Boeing systems in which only the Captains primary flight instruments stay on.
The final resource for power is the RAT (Ram Air Turbine). It's to be used in extreme emergencies, when the batteries will not contain enough energy to reach the nearest airport. The RAT is a simple device that can be deployed in flight at speed. It simply is a windmill type of construction that comes out of the main fusalage. Through the airflow around the aircraft it then generates electricity to power the cockpit and the flight control sufaces, however it is not a comfortable way of flying since the pilots will then only have the bare minimum of their instruments. The RAT has proven itself as a life saver in the Air Transat 236 incident, where an Airbus A330-200 glides for more then 130 Miles with the RAT as it's lifeline.
On the the 3D representation. The model will feature three of these systems, namely the GPU/EPU, the APU and the RAT. The other systems are not vissible.
The GPU/EPU
It still needs the wire to the aircraft, which I need to remodel.
The RAT
Finally I need to model the APU, however I hope to gain some details on how that looks when Airbus gives me some information.
