Hi, I would like to thank you so much for the time you spent making these great videos. I haven’t been flying the Airbus for 2 years now, I miss it a lot, and thanks to your clear explanations, it helps me to remain in the game and moreover, I have learnt more things, giving me a better understanding of this complex aircraft. I think I will feel more confortable when sitting again in the cockpit (hopefully soon). So again, a big thank you sir 🙏
I have a question actually - what is written below "Ref ldg dist" in B+Y row.... I tryed to make a notes somehow and wonder if is it kind of an F - word what refers to situation that in case of B+Y hyd failure, besides discomfort related to that situation we just got in, we don't have a bigger issue? Thanks for effort I really appreciate that - amazing lectures love it !
One query... in case of flight ailerons flight computer priority..... ELAC2 then ELAC1... then made me a little confused bcz fcom says for ailerons ELAC1 then ELAC2... while for elevators that's correct ELAC2 then ELAC1... this may be just the aircraft version or may be ELAC standard difference
Watched a few videos. Really liked them. While discussing System Failures, towards the end, what is written below "REF LDG DIST 1200 m" for B+Y Hyd Failure? Looks like *EPSI*. What does it mean? Or what did you intend to convey?
To honor the British instructors, i would like to share a poem which i was told during OPC to simplify Dual Hydraulic failures: Green and Yellow? You won´t stop this fellow, Green and Blue? You are flying in a poo, Yellow and blue? No problem for you...
@@airbuswhatsitdoingnow320 2 systems. green and yellow. On A350 both engines power both systems so if you loose an engine there is no loss of hydraulics. Then some of the ckntrol surfaces have their own mini hydraulic systems independent of the main and use an Electro Hydrostatic Actuator that just requires electrical power to operate. Some other controls are mixture of conventional and EHA and called EHBA. So even if all hydraulic pumps fail or even loss of hydraulic fluid, the plane can still fly
Very well explained. Your channel is a real boon to all A320 pilots. Thank you for contributing
That’s great to hear. Thank you for taking the time to feedback. Stay safe 👍
Hi, I would like to thank you so much for the time you spent making these great videos. I haven’t been flying the Airbus for 2 years now, I miss it a lot, and thanks to your clear explanations, it helps me to remain in the game and moreover, I have learnt more things, giving me a better understanding of this complex aircraft. I think I will feel more confortable when sitting again in the cockpit (hopefully soon). So again, a big thank you sir 🙏
Im pleased your enjoying the content. Welcome tot he channel
Thank you for the time to make the diagrams, much appreciated along with the your great explanations.
Thanks a lot for the good recap 👌
Love to watch your videos! Thanks for all your effort.
Glad you like them!
I went through Hydraulic, extremely informative and well explained. Thanks a million for your efforts and sharing all the information
You're very welcome
really good briefings.Thank you very much.
I Appreciate the feedback
Thank you for your effort and tips to increase learning of the systems.
My pleasure! thank you for the feedback
Thanks for the effort captain
You're welcome!
Another cracking aid to memoir
Thanks, I hope your enjoying the content
Very nice :)
I have a question actually - what is written below "Ref ldg dist" in B+Y row.... I tryed to make a notes somehow and wonder if is it kind of an F - word what refers to situation that in case of B+Y hyd failure, besides discomfort related to that situation we just got in, we don't have a bigger issue? Thanks for effort I really appreciate that - amazing lectures love it !
Let me take a look
Hi. Why is the fuel penalty greater for a yellow hydraulic failure compared to a Green and yellow failure?
sorry for the late response. id need to review that. Bear with me please
One query... in case of flight ailerons flight computer priority..... ELAC2 then ELAC1... then made me a little confused bcz fcom says for ailerons ELAC1 then ELAC2... while for elevators that's correct ELAC2 then ELAC1... this may be just the aircraft version or may be ELAC standard difference
Hi just a quick question why only hyd B+Y lo pr gives u normal law the rest of dua failure gives us alternate law
Hi thanks for the question. When the Green +1 goes we get Alton law as the green is the primary system 👌
@@airbuswhatsitdoingnow320 great thank you very much really appreciate it 🫡
Watched a few videos. Really liked them. While discussing System Failures, towards the end, what is written below "REF LDG DIST 1200 m" for B+Y Hyd Failure? Looks like *EPSI*. What does it mean? Or what did you intend to convey?
*EASY* apologies for my poor handwriting!
To honor the British instructors, i would like to share a poem which i was told during OPC to simplify Dual Hydraulic failures:
Green and Yellow?
You won´t stop this fellow,
Green and Blue?
You are flying in a poo,
Yellow and blue?
No problem for you...
Have you ever looked at the hydraulic system of the A380/A350 to see how advanced it is?
I haven't
@@airbuswhatsitdoingnow320 2 systems. green and yellow. On A350 both engines power both systems so if you loose an engine there is no loss of hydraulics. Then some of the ckntrol surfaces have their own mini hydraulic systems independent of the main and use an Electro Hydrostatic Actuator that just requires electrical power to operate. Some other controls are mixture of conventional and EHA and called EHBA. So even if all hydraulic pumps fail or even loss of hydraulic fluid, the plane can still fly
@@tomstravels520 it’s the future