I am a Pilot in Indigo, type rated on the A320. Every once in a while I go through all these videos along with the FCOM. What a beautiful explanation, short, crisp, to the point. Very useful for all the aspiring pilots out there.
great video..keep it up...but i haven't clearly understood the purpose of generator on right side. Does it only supply when generator on left fails or in addition to this there is any special task assigned to it?
Nice video but there is case also if all generator losts include emergency generator then your battery 1 will supply the AC essential via static inverter and battery 2 will supply dc essential. You should cover that too.
Hey! i often see all your videos and learn so much from them before i flip through the books. i noticed something and wanted to bring it to your notice. this is regarding Electrical Source Priorities. as per me it is ON SIDE GENERATOR EXTERNAL POWER APU OFF SIDE GENERATOR RAT OR EMER GEN BATTRIES. Please correct me if i m wrong.
Wonderful video again! Question though, nowhere in the FCOM does it actually explain what AC or DC ESS SHED buses are. I can’t seem to find a solid explanation online either, could you help?
It doesn't, but they are designed for less important components of the aircraft so that they can be shed to reduce load when aircraft is in troubled electrical situation such as batteries supplying which is a limited source!
Amazing videos, thank you very much. Do you have any video where you explain how to read circuit diagrams, and logic diagrams for electrical and other systems?
@@poh Thanks a lot for your reply! Well I just meant how to read the different symbols on the circuit diagrams and what they mean. For example the normal electrical configuration diagram
if GEN1 fails with APU and GEN2 running, APU has priority to power AC BUS 1 over GEN2. BUS power Priority is, By the corresponding Generator [GEN 1(2)] (onside GEN) By External Power [EXT PWR] By the APU Generator [APU GEN] Or by the other Generator [GEN 2(1)] (offside GEN)
If TR1 fails (i.e. in turn DC 1 fails), why does the ESS TR has to come in picture to supply the DC ESS?? I mean why can't the DC ESS be supplied by the DC 2 BUSS??
Those day generator and csd is separated...today csd is combined with generator and become IDG..the primary function is generate electrical power by variable input from engine,and constant out put which is 115v 400hz
+Ishwar Vyas An aircraft uses AC power which normally comes from a generator that has 3 seperate windings inside it. This gives 3 seperate outputs (or phases) from the one generator. If one was to measure the voltage between a single one of these phases and ground you would get 115volts. If you were to measure the voltage directly between 2 of the three phases you would get 200volts.
I am a Pilot in Indigo, type rated on the A320. Every once in a while I go through all these videos along with the FCOM. What a beautiful explanation, short, crisp, to the point. Very useful for all the aspiring pilots out there.
Thank you
Great video man, I like how you explain , btw who do you fly for?
Thank you! Air India!
I've previously studied the system, but didn't understand the difference between the TR and the Static inverter until i saw this video
thanks
+s3oodi1 You're welcome 🙂
Great video. really broke it down to were I can actually understand the system. thank you!
Thank you
Holy Crap . What a fantastic explanation. Thank you so much.
You're welcome! Thank you!
Thank you very much captain. Very nicely explained.
You’re videos are just great
Thanks heaps and keep up doing good job,
For lazy ppl like me,these are great refresher.
Thank you!
brilliantly explained, thank you Capt
Thank you
awesome video u shared very good information thanx alot ...greetings from turkey
Thank you!
Thanks for the awesome course!!
great video..keep it up...but i haven't clearly understood the purpose of generator on right side. Does it only supply when generator on left fails or in addition to this there is any special task assigned to it?
It supplies the right side in normal conditions but is capable of supplying the whole system as well during failure of the left generator.
Excellent video
that was a great video. thanks a lot!!!
Welcome
Nice video but there is case also if all generator losts include emergency generator then your battery 1 will supply the AC essential via static inverter and battery 2 will supply dc essential. You should cover that too.
Too long a video it becomes too much to sustain for everyone.
Great explanation. How about if one engine run, and EXT PWR is ON, is that EXT PWR take over one side of the system or take over all the system?
Thank you! And it takes one side of the system!
Hey! i often see all your videos and learn so much from them before i flip through the books. i noticed something and wanted to bring it to your notice.
this is regarding Electrical Source Priorities. as per me it is
ON SIDE GENERATOR
EXTERNAL POWER
APU
OFF SIDE GENERATOR
RAT OR EMER GEN
BATTRIES.
Please correct me if i m wrong.
Yes that's correct.
Hello Sir,
Your videos are really heplful. I had a small question.
Is there a need to buy a personal Ipad before going for A320 type rating?
Not really
awesome video bro , keep it up!!
Thank you!
Great job buddy. You have a new subscriber
Thank you!
GEAR ……electrical priorities, easy to remember…
Nice and informative video. Thanks
You're welcome!
Great commentary and well put video. Keep it up. 5 stars!
+Neville A Thank you!
Wonderful video again! Question though, nowhere in the FCOM does it actually explain what AC or DC ESS SHED buses are. I can’t seem to find a solid explanation online either, could you help?
It doesn't, but they are designed for less important components of the aircraft so that they can be shed to reduce load when aircraft is in troubled electrical situation such as batteries supplying which is a limited source!
Planes Over Head Thanks a bunch!!
Superb explanation
Thank you!
Thank you thank you thank you thank you 600 times
Amazing videos, thank you very much. Do you have any video where you explain how to read circuit diagrams, and logic diagrams for electrical and other systems?
Which one do you want? I'll make one
@@poh Thanks a lot for your reply! Well I just meant how to read the different symbols on the circuit diagrams and what they mean. For example the normal electrical configuration diagram
I studying for CPL & in technical general we have electricals is it going to be helpful there?
Not really
Thank you Captain 😊
You're welcome!
Great video, Thank you so much
+Abdulaziz Sabir You're welcome.
so helpfull..thank you.
You're welcome!
if GEN1 fails with APU and GEN2 running, APU has priority to power AC BUS 1 over GEN2.
BUS power Priority is,
By the corresponding Generator [GEN 1(2)] (onside GEN)
By External Power [EXT PWR]
By the APU Generator [APU GEN]
Or by the other Generator [GEN 2(1)] (offside GEN)
Yes that's correct! 👍🏼 onside gen, external, APU, offside gen, RAT, BAT
Great material and video, I just wish you speak a little slower. Keep up the good work and thanks for sharing!
Thank you, I will
have you ever flown from VOMM? if so what sid do you use
Depends to where you are going to. Based on the direction! Whyb though?
flight simmer dont know where to fly from vomm
always wanted to talk to a real indian pilot
what are those little knobs and buttons on a320 pedestal nxt to radio?
Very nice, useful info
+NANDA KISHORE Thank you
very nice, thank you for the good work.
+ayyowazup Welcome! :)
Navrya chi byaco
+Tushar Gawali ??
And this is similar for all A320 family aircrafts? A318/19/21 ?
Yes pretty much, very minute differences but shouldn't bother much!
i want to ask about the loads on ESS DC and ESS AC buses
thanks
Its no more in the FCOM! so pilots don't need to know this.
If TR1 fails (i.e. in turn DC 1 fails), why does the ESS TR has to come in picture to supply the DC ESS?? I mean why can't the DC ESS be supplied by the DC 2 BUSS??
The idea is to use ESS TR as an additional TR back up, rather than relying only on one TR (TR 2).
@@poh Thanks a lot sir. I understood it now 😃
Question: What is the difference between an IDG and a CSD?
+Neville A I don't think there is much difference in them.
Those day generator and csd is separated...today csd is combined with generator and become IDG..the primary function is generate electrical power by variable input from engine,and constant out put which is 115v 400hz
Priority logic u can use GEARB ..
GEN
EXTERNAL
APU
RAT
BAT
Thank you
V good
Sir, What about static inverter
What what about static inverter?
Why 400Hz frequency use in Aircraft?
To reduce the amount of iron, and thus weight, required, and
To keep the efficiency of motors and alternators acceptable.
@@poh Thanks sir
Well explained 👍🏼👍🏼👌🏼 could you please share the file?
I don't have the file anymore.
Virtual bus bar function??
Where is that?
what does 115/200v denotes
+Ishwar Vyas An aircraft uses AC power which normally comes from a generator that has 3 seperate windings inside it. This gives 3 seperate outputs (or phases) from the one generator. If one was to measure the voltage between a single one of these phases and ground you would get 115volts. If you were to measure the voltage directly between 2 of the three phases you would get 200volts.
Very 1988.
Okay!
flight simmer dont know where to fly from vomm
VOMM? Chennai aa
can i have your email?
Its at the end of the video. Anyway it is planesoverhead@hotmail.com