Air India Crash

Only a little bit out there. Taken off without and tried to extend once they realised?
 
There is no way of proving or disproving the RAT deployment. I wish people would stop fixating on this, adamant that it was definitely deployed (or indeed wasn't)

The videos are poor quality and the audio may be indicative, but it may equally be a nearby Air con unit, poor quality microphone artifacts or anything else.
 
There is no way of proving or disproving the RAT deployment. I wish people would stop fixating on this, adamant that it was definitely deployed (or indeed wasn't)

The videos are poor quality and the audio may be indicative, but it may equally be a nearby Air con unit, poor quality microphone artifacts or anything else.

The lack of engine noise when they should be at take-off thrust would need addressing too.
 
Skipped update 4 but 5 is out and seems to indicte RAT deployed and that the landing gear has started to retract


That's what I said before like almost two days ago - RAT was deployed which indicates major system failure

There is no way of proving or disproving the RAT deployment. I wish people would stop fixating on this, adamant that it was definitely deployed (or indeed wasn't)

The videos are poor quality and the audio may be indicative, but it may equally be a nearby Air con unit, poor quality microphone artifacts or anything else.

Yes but you can hear it, the rat makes a very descriptive sound that can clearly be heard in the earliest footage. Personally I've never heard any aircon unit motor that sounds like that

But anyway speculation is boring at this stage; they found the black box which will tell them everything
 
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I'd never heard of a ram air turbine before this incident, from an engineering point of view it's genius, and is one of those things that makes me wonder why I never knew of its existence, or thought of it at all. Makes perfect sense.

I do wonder about the efficiency of it, if the aircraft is flying with the wind it'll be a lot less powerful than against the wind, but that'll be factored in to its design.
 
Definitely a unique case given the 787 hasn't had a fatal crash yet and the potential of a double engine failure (being a very rare situation). Hopefully the flight data recorder will reveal answers to this...
 
APU restart is now at the top of the list thanks to Sully; get some sort of power. So pressing APU as its all going to wrong would put the doors open as it tried to spin up to start.

Remember, it was 23 seconds was rotation to impact. Also the airfield is at 200 feet above sea level and the quoted altitude was also above sea level.
 
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I do wonder about the efficiency of it, if the aircraft is flying with the wind it'll be a lot less powerful than against the wind, but that'll be factored in to its design.

It will produce the same power for any given *airspeed*. The effect of steady wind on an aircraft in flight is only relevant to its movement with respect to the ground.
 
It will produce the same power for any given *airspeed*. The effect of steady wind on an aircraft in flight is only relevant to its movement with respect to the ground.

No mate, just no. The ground speed and the air speed are two very different things, before factoring in things like ambient temperature, air density, velocity, etc.
 
I know exactly what the differences between airspeed (indicated and true) and ground speed are.

Claiming a ram air turbine's power output will vary with wind direction is like saying a plane's stall speed will differ.
 
APU restart is now at the top of the list thanks to Sully; get some sort of power. So pressing APU as its all going to wrong would put the doors open as it tried to spin up to start.

Remember, it was 23 seconds was rotation to impact. Also the airfield is at 200 feet above sea level and the quoted altitude was also above sea level.
APU start on elec loss is automatic on the 787, they wouldn't have even had to press anything.
 
I'd never heard of a ram air turbine before this incident, from an engineering point of view it's genius, and is one of those things that makes me wonder why I never knew of its existence, or thought of it at all. Makes perfect sense.

I do wonder about the efficiency of it, if the aircraft is flying with the wind it'll be a lot less powerful than against the wind, but that'll be factored in to its design.
It's already been stated about how wind direction means nothing, but as for the RAT itself, they're always of a constant-speed variety, meaning their blades can change pitch to maintain the correct speed over a wide range of airspeeds.

This includes the low speed we see in the case of this crash, and indeed the blades would have been at a very broad pitch to maintain speed, leading to the very distinctive noise heard in the video that is being baffling dismissed by many.
 
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Edit:

I had the reply window open as I watched the video and then posted, unaware ThundyCat had posted it previously.
 
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It's already been stated about how wind direction means nothing, but as for the RAT itself, they're always of a constant-speed variety, meaning their blades can change pitch to maintain the correct speed over a wide range of airspeeds.

This includes the low speed we see in the case of this crash, and indeed the blades would have been at a very broad pitch to maintain speed, leading to the very distinctive noise heard in the video that is being baffling dismissed by many.

You mean the blades pitch to maintain the correct angle of attack ;). The CSU maintains the RPM (Speed).
 
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This pilots opinion changed after seeing the raw video of the crash that showed the RAT being deployed. It's deployed automatically for Engine failure, Hydraulic failure or Electrical failure.


Fascinating video.

Not being an expert in this sort of stuff, I can't see how it could be "natural" dual engine failure. I start to wonder if it was a deliberate act that took out the hydraulics and or electrical systems - especially considering what's been going on around that geographical area. A loud bang followed by flickering lights. Sounds to me that they lost systems, and at that height couldn't recover. Also a tad suspicious that it happened just at that moment in time when it was most likely to crash the plane.
 
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Fascinating video.

Not being an expert in this sort of stuff, I can't see how it could be "natural" dual engine failure. I start to wonder if it was a deliberate act that took out the hydraulics and or electrical systems - especially considering what's been going on around that geographical area. A loud bang followed by flickering lights. Sounds to me that they lost systems, and at that height couldn't recover. Also a tad suspicious that it happened just at that moment in time when it was most likely to crash the plane.
Just for the sake of clarity, killing all the electrics or all the hydraulics would not kill the engines. They have a self-driven generator to ensure electronic control of them continues even in the event of a catastrophic failure of the electronics - to the point where even the trust lever position detector is actually powered by this self-driven generator. Continued running of the engines is absolute.

There's an excellent post on PPRuNe which covers in a bit more detail about how various things operate, and appears to be written by a chap who was previously responsible in certifying aircraft types. It concludes as follows:

Now, if I assume the speculation that the RAT deployed is correct, I keep coming up with two potential scenarios that could explain what's known regarding this accident:

1) TCMA activation shutdown the engines, or
2) The fuel cutoff switches were activated.


I literally can come up with no other plausible scenarios. In all due respect to all the pilots on this forum, I really hope it wasn't TCMA. It wouldn't be the first time a mandated 'safety system' has caused an accident (it wouldn't just be Boeing and GE - TCMA was forced by the FAA and EASA to prevent a scenario that had never caused a fatal accident) - and there would be a lot embarrassing questions for all involved. But I personally know many of the people who created, validated, and certified the GEnx-1B TCMA logic - and can't imagine what they would be going through if they missed something (coincidentally, one of them was at my birthday party last weekend and inevitably we ended up talking about what we used to do at Boeing (he's also retired)). Worse, similar TCMA logic is on the GEnx-2B (747-8) - which I was personally responsible for certifying - as well as the GE90-115B and the 737 MAX Leap engine - the consequences of that logic causing this accident would be massive.

As speculated by a few including myself, and it seems more and more are coming round to the same area of conclusion, it's looking most likely to be a catastrophic software failure or pilot suicide.
 
Silly question, but I take it that the plane computer knew the plane was about to fly directly to the UK and would prevent takeoff if the plane hadn't been refuelled sufficiently?
How about this one :eek:
 
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