Пікірлер

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  @MrHumbleGuy-yl6lk6 күн бұрын

  Jesus loves you all, AMEN!!

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  @sasidharankoduvazhanoor4465Ай бұрын

  Very very intrested to study

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  @AnubhabGhosh2006Ай бұрын

  7:06 that does not seem dimensionally correct

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  @christopherjofficialАй бұрын

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

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  @zlatimirzdravkov89402 ай бұрын

  Thanks

• 
  @desiadams67082 ай бұрын

  Airframe

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  @lukebristow85582 ай бұрын

  This is wonderful stuff and much appreciated

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  @andremarais27062 ай бұрын

  The buttons do not work.

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  @wagilini972315 күн бұрын

  It seems to be a recording of an interactive lesson, so the buttons are pressed automatically.

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  @altezzadella68653 ай бұрын

  a330

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  @altezzadella68653 ай бұрын

  dhl611😢

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  @shyamprasad71923 ай бұрын

  Dgca exam

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  @user-zd9oi6eq8j3 ай бұрын

  What class is this from?

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  @luisrnandezc3 ай бұрын

  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.

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  @user-ft3gl7ln4i3 ай бұрын

  Thank you

• 
  @MasteringMoney123 ай бұрын

  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.

• 
  @samspade86124 ай бұрын

  Excellent video!

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  @Training313-ng9yt4 ай бұрын

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

• 
  @AidanFay-wu9ob4 ай бұрын

  Amazing resource

• 
  @garimakhatri84804 ай бұрын

  Damn perfectly explained

• 
  @farminky4 ай бұрын

  It would be great to see some new content

• 
  @nanh73504 ай бұрын

  l need this folder powerpoint or pdf, please

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  @nanh73504 ай бұрын

  thank you

• 
  @alex4588975 ай бұрын

  Thank you for this high quality content!

• 
  @aviationworldbyvishakh82285 ай бұрын

  No content ..only important points cover😠

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  @aviationworldbyvishakh82285 ай бұрын

  Video important parts missed..not covering al

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  @cruz_marquez_5 ай бұрын

  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 🙂

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  @echadmiyodea5 ай бұрын

  I love these videos.

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  @annedejong10406 ай бұрын

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

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  @MotmedGaming6 ай бұрын

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

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  @Gearz-3656 ай бұрын

  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

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  @2oopb7 ай бұрын

  thank god for this.

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  @MotmedGaming7 ай бұрын

  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".

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  @MotmedGaming7 ай бұрын

  Why is #39 not available?

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  @heikoolivaliberjen61647 ай бұрын

  Nice video, thanks :)

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  @marcmaillet30448 ай бұрын

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

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  @user-ne5zv6ve8q8 ай бұрын

  Mr.J79Engine 1967-2023

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  @mateuszmista7388 ай бұрын

  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?

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  @oscarrincon21052 ай бұрын

  Not for sonic & supersonic flow. On converging & diverging nozzles, a supersonic flow experiences the opposite effect that a subsonic flow does.

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  @filakyle36638 ай бұрын

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

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  @donanzy12748 ай бұрын

  I love you

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  @soroushrezazadeh83008 ай бұрын

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

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  @musicosaxial5 ай бұрын

  According to my understanding, EPR is measured at two points n1 and n2 as the density reduces the pressure on the intake fan commonly denoted ad 'n1' will be less and as we know that exhaust gases pressure at constant rise in throttle is at speed of Mach 1.which is at point'n2' So in simple words n1 reducing and n2 constant so EPR reduces.

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  @CJWJR9 ай бұрын

  The narrator sounds like Sean Connery.

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  @muhammedbekirkabasakal57889 ай бұрын

  that video really helped. ty so much dudes.

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  @tausifkhan55019 ай бұрын

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

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  @edcew82369 ай бұрын

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

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  @b43xoit9 ай бұрын

  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.

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  @b43xoit9 ай бұрын

  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?

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  @shikuux10 ай бұрын

  ty sm!

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  @MecxKeseito-cv6hp10 ай бұрын

  Great edition really appreciate it

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  @Botwins10 ай бұрын

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

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  @thomasgebrecherkos48222 күн бұрын

  You Can read Del Crane or Aviation maintenance technician handbook ( PowerPlant)

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  @khurramhanif974710 ай бұрын

  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

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  @MotmedGaming7 ай бұрын

  It is not the same as ground level, just slightly lower but the effects of hypoxia (low oxygen) are not yet substantial, so it is considered a safe amount of oxygen supply