My guess, thanks
Thanks guys and girls for your responds. The fuel system pumps consist of a jet pump (pri), AC pump (sec), and engine driven pump. My feeling/guess was the engines would continue to run below a max altitude. The EDP by nature should be able to pull fuel out of the fuel lines. I also suspect the eng driven fuel pumps are altitude rated in the event of a motive flow pump failure. While I understand how motive flow (jet pump) works, its purposes in life is just to provide positive fuel VOLUME in the fuel lines. Head pressure to the EDP is the result. The EDP is what regulates fuel pressure to the FCU and VSA.
I knew this was the right forum to ask.
Thanks again and for your help.
LL
Thanks guys and girls for your responds. The fuel system pumps consist of a jet pump (pri), AC pump (sec), and engine driven pump. My feeling/guess was the engines would continue to run below a max altitude. The EDP by nature should be able to pull fuel out of the fuel lines. I also suspect the eng driven fuel pumps are altitude rated in the event of a motive flow pump failure. While I understand how motive flow (jet pump) works, its purposes in life is just to provide positive fuel VOLUME in the fuel lines. Head pressure to the EDP is the result. The EDP is what regulates fuel pressure to the FCU and VSA.
I knew this was the right forum to ask.
Thanks again and for your help.
LL