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Very very intrested to study

7:06 that does not seem dimensionally correct

I've always been looking for thise CBT ATPL ground school courses. Thanks for uploading them on YT

Thanks

Airframe

This is wonderful stuff and much appreciated

The buttons do not work.

a330

dhl611😢

Dgca exam

What class is this from?

12:20 I get that the AOA is not optimal, but why this would create a stall? The AOA decreases when the compressor rpm are low, which means the AOA is way below the critical value.

Thank you

Thanks I have understand the syllabus from you. Do you have QA bank because I want to start training and read the QA bank before getting to the exams.

Excellent video!

I am very glad to study this lesson. With warm regards, Zokhid Sattarov

Amazing resource

Damn perfectly explained

It would be great to see some new content

l need this folder powerpoint or pdf, please

thank you

Thank you for this high quality content!

No content ..only important points cover😠

Video important parts missed..not covering al

Thank you for these videos! they are clear and structured, I'm about to head in to a job interview to work on engines, and these videos have been by far the best preparation 🙂

I love these videos.

Them used for the IJN armada?! Heard of them B26 earliest too, window makers

09:45 Isn't the center tank normally abbreviated by CTR rather than CRT?

Turbine engines also have accessory drives? I honestly didn't know that. But interesting that it's very similar to the accessory drives of car and truck engines

thank god for this.

09:25 I wonder how the Helios accident coul've happened if there is a aural warning of failed pressurization... EDIT: I just read the report and apparently the alarm sounded at around 12'000ft but was misidentified by the crew as a "take-off configuration warning".

Why is #39 not available?

Nice video, thanks :)

Why not use electrically heated elements in the combustion chamber - no more fuel - and stick an electric generator in the engine.

Mr.J79Engine 1967-2023

hello. video is great , but I have one question. at 5:45, you are saying that as gases goes through divergent passage its velocity is progressively increasing. Shouldn;t velocity decrease and static pressure increase, while gases are going through divergent passage?

just came accros your channel. This is so briliant I had never seen on youtube. Pure aviation and great school. Thank you.

I love you

Hi 09:43 why EPR showed to decrease? Because I think at high altitudes and low density conditions EPR will increase. thank you

The narrator sounds like Sean Connery.

that video really helped. ty so much dudes.

hello sir,please make a video on a combustion drain valves

Hmm. High wing airplanes have struts and those are not for compressive loads. Or is that British vs American English?

What engineering provisions arrange for the free turbine to run at constant rotational speed? Why doesn't it slow down when the load increases? There must be a governor on it, controlling the throttle of the engine.

If a turbine engine is quieter than a piston engine when used as the APU in an airplane, why do cars still run on piston engines?

ty sm!

Great edition really appreciate it

Do you have any reference (like textbook) to read about a/c turbine engine ?

How are you madam can you tell me please that oxygen level of airplane on the 8000feet is same like ground level we can breathe easily please explain little bit

Em.... The nitrogen is above the oil and not as shown. Oops !