A320 Unreliable Speed What are the causes and steps to take? (MADE EASY)

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  • Опубликовано: 19 фев 2021
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    Let's dive in detail how do we pilots manage unreliable speed indications on the airbus A320.
    Watch the updated version here. • A320 Unreliable Speed ...
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Комментарии • 35

  • @Captain_SQ
    @Captain_SQ  3 года назад +1

    Watch the updated video here : ruclips.net/video/tNY8AFOWOYY/видео.html

  • @umutgulmez83
    @umutgulmez83 10 месяцев назад +1

    Great video, thanx Cap

  • @jrajesh88
    @jrajesh88 Год назад +1

    Very useful captain... thank you so much

  • @KRISHNA_VARMA
    @KRISHNA_VARMA Год назад +4

    Hello captain. Lets say we are in FL350, we observe speed discrepancies between pfd’s. What shall we do ? Because we are in steady flight and its not affecting our safe conduct of flight?

    • @Captain_SQ
      @Captain_SQ  Год назад +3

      Skip the memory items and open the QRH to determine the faulty speed indication.

  • @franciscojavierf
    @franciscojavierf Год назад +1

    Why go around f3 to f1?

  • @Acarsfault
    @Acarsfault 3 года назад +1

    Isn’t better to gravity extend lnd gear down after flap 3 (like in a double hydraulic failure) ?

    • @Captain_SQ
      @Captain_SQ  3 года назад

      Hi Acarsfault, in the case of Double hydraulic failure, it depends on what failure it is. If you get Green and Blue Hydraulic failure, you would have selected Gear down at 200 kts (much earlier) if you want more stabiliser control as you only have one elevator. So in this case, would you require to be a direct law much earlier or later on approach? Normal Airbus procedures will be Flaps 1, Flaps 2, Gear Down then Flaps and/or Flaps Full. You would change the sequence if the failure procedure require you to do so. Hope this helps.

    • @matthendricks9666
      @matthendricks9666 2 года назад +1

      Captain SQ did not undertand your question. You only do Flaps 1,2,3...approach speed ...then gear down in 2 abnormals. G+Y Hydraulic failure and stabilizer jam. Why? Because you have no movable stabilizer and the trimming is done by elevators only. As soon as you put the gear down the elevators stop their autotrim. " Use manual pitch trim"....but there is no manual pitch trim any more because the trim wheel addresses the stabilizer and not the elevators. For any other abnormal this is not necessary.

  • @retardaviation5179
    @retardaviation5179 2 года назад +2

    For what reason the landing gear is exteded by the gravity ? thanks for the de video.

    • @tomstravels520
      @tomstravels520 Год назад +4

      Because the LGCIU (Landing Gear Computer) needs data from the ADR to determine if its safe to lower the gear

    • @Captain_SQ
      @Captain_SQ  Год назад +1

      Great answer.

  • @eugeniocoschignano2356
    @eugeniocoschignano2356 Год назад +1

    Hi Captain question pls: if you're flying and you have this ECAM: IR 1 fault, what do you do ? Thank you

    • @Captain_SQ
      @Captain_SQ  Год назад +1

      Good question. AtT HDG SWTG to CAPT 3 and ATC/XPDR to System 2. You can follow the ECAM actions.

    • @eugeniocoschignano2356
      @eugeniocoschignano2356 Год назад

      @@Captain_SQ many thanks so switching Captain 3 due to failure of 1, ok clear, so for example if there was ir 2 fault it was set up fo 2 the switching. Is that right ? And when is the moment that might be used recovery in att mode?

  • @100NUMARALIADAMMM
    @100NUMARALIADAMMM 2 года назад +1

    When below fl250 and buss shown fast when u hold the pitch 5 and climb. So buss tells u that are fast. İn order to fix this u have a 2 choice. İncrease pitch or decrease power. So then u found yourself as stall and protection is initiating.

    • @Captain_SQ
      @Captain_SQ  2 года назад +3

      You don't have protection when you have the BUSS activated.

    • @100NUMARALIADAMMM
      @100NUMARALIADAMMM 2 года назад

      @@Captain_SQ are you sure? How can ı find this info? Fcom? Afm? Where?

    • @Captain_SQ
      @Captain_SQ  2 года назад +2

      @@100NUMARALIADAMMM in older aircrafts,to activate the BUSS, you will have to switch off all 3 ADRs, that would bring you to alternate law and then direct law.

  • @Nam-uf5oq
    @Nam-uf5oq 2 года назад +1

    Why not use speedbreak when using BUSS, capt ?

    • @Captain_SQ
      @Captain_SQ  2 года назад +1

      we might stall the aircraft.

  • @miaomiao6914
    @miaomiao6914 3 года назад

    one question:
    why should we use BAKUP RADIO NAV by QRH?

    • @Captain_SQ
      @Captain_SQ  3 года назад

      Do you mean for this particular failure?

    • @miaomiao6914
      @miaomiao6914 3 года назад

      @@Captain_SQ Yeah. Some A320 have this procedure to use BACKUP NAV in the QRH ALL ADR OFF PROC.

    • @Captain_SQ
      @Captain_SQ  3 года назад +1

      BACK UP NAV is normally used if you get a dual FM failure. I guess it depends on your aircraft serial number. Back up NAV is for flight planning and the NAV you select on your RMP is for manual tuning.

  • @tomstravels520
    @tomstravels520 3 года назад

    How old is this as the BUSS can now be fitted as a push button?

    • @Captain_SQ
      @Captain_SQ  3 года назад

      You are right Thomas, newer MSN aircrafts have been fitted with the BUSS pushbutton located next to the PFD.

    • @ssinja
      @ssinja 3 года назад

      You are lucky to fly new aircraft.Even many old version of A320/330 do not have BUSS too.

  • @tomstravels520
    @tomstravels520 3 года назад +1

    Pilots of AF447 should have paid attention to this

    • @Muthana500
      @Muthana500 3 года назад

      Af447 A330 was not fitted with the Buss system....

    • @tomstravels520
      @tomstravels520 3 года назад +1

      @@Muthana500 I was referring to the memory items and pitch/power settings. I know it didn’t have BUSS installed