A320 - Single Engine Failure Procedure at or above V1

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  • Опубликовано: 28 сен 2024

Комментарии • 15

  • @flammflamm2582
    @flammflamm2582 7 лет назад

    Hello I am acutally a 16years old swiss and I really like to listen to this Videos. Your are the only one I know making these sort of Videos. Thank you for your hard work.

    • @poh
      @poh  7 лет назад

      +Flamm Flamm Thank you!

  • @carlossalgado4009
    @carlossalgado4009 6 лет назад +1

    Good job, thank you for sharing your knowledge.

    • @poh
      @poh  6 лет назад

      You're welcome!

  • @rustomirani6938
    @rustomirani6938 5 лет назад +3

    Sir, I like your videos very much and appreciate the effort you put in.
    Can you pls make videos on Normal Procedures for people who are doing their Type Rating

    • @poh
      @poh  5 лет назад

      I don't want to do that because normal procedures vary from company to company! And its not very explainable on a video. But will plan!

  • @wilhelm12jwl
    @wilhelm12jwl 5 лет назад

    Sir thanks for the video 😀 In case of failure after V1 what is the correct usage of the fuel cross feed? The Ecam will only tell you to check for imbalance. Another question sir for the secondary failure, under the electrical we usually start the APU to reduce the load on the working engine. But must we also use the APU for bleed air for the packs? Thank you sir

    • @poh
      @poh  5 лет назад

      The point is, just after take off there is not gonna be that much imbalance so that's fine and you shall be landing back immediately max withing 30 minutes, so the cross feed largely is played out. Yes you must use the APU bleed.

    • @y2k538
      @y2k538 5 лет назад

      APU bleed is to be used only if eng 2 is shutdown and xbleed is selected to shut psn

    • @poh
      @poh  5 лет назад

      APU BLEED is to be used in case of ANY ENG failure, because it'll reduce the load on one engine. Whichever side has failed that side will be provided with APU bleed automatically because APU has priority over the Engine to supply bleed.

  • @mitalisaini6754
    @mitalisaini6754 5 лет назад

    Hi sir,
    Pls make a MCDU tutorial vid
    Regards

  • @AbidAli-xx2mx
    @AbidAli-xx2mx 6 лет назад

    what will be engine response in case of ECU channel A and B failure in flight.

    • @poh
      @poh  6 лет назад

      The following consequences happens:
      ‐ Affected engine start is lost
      ‐ Autothrust control is lost
      ‐ Thrust reverser on the affected engine is lost
      ‐ When idle is selected, only approach idle is available
      ‐ Bleed corrections on N1 limit are lost.