Posts by user "Musician" [Posts: 88 Total up-votes: 95 Page: 5 of 5]

Musician
July 18, 2025, 05:57:00 GMT
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Post: 11924842
Originally Posted by galaxy flyer
I would guess the OP on this subject is wildly overestimating “survivability”. Any chance off-airport barely controlled impact is gonna be catastrophic. There maybe survivors but that’s just luck.
To clarify, I did not mean to imply that a "miracle" was possible. There was always going to be a high chance (inevitability?) that the fuel would explode, especially with the engines relit.
We're speaking here on the amount of luck available. As it turned out, even crashing into buildings, it sufficed for one passenger to survive. So there's more luck here than with a CFIT from cruise—and some bad luck in not missing the house they crashed into.

Last edited by Musician; 18th July 2025 at 06:46 .

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Musician
July 18, 2025, 06:18:00 GMT
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Post: 11924846
Thank you for your reply, appruser , and apologies fur cutting most of it:
Originally Posted by appruser
Big questions in my mind:
1. If the loss of ADSB corresponds to the E1/E2Fuel Cutoff switches being moved from RUN -> CUTOFF, why is the airspeed declining for the prior 4 seconds?
2. In 4 seconds, why is there only 50ft of altitude gain? that seems odd.
3. To account for only 50ft of alt gain, if we assume the 1st reading is on the runway just before rotation, the intermediate +25ft alt gain is at rotation (Nose up but MLG still on the runway), and the last 4 readings are in the air (nose up an additional 25ft), that means that 1 second or less after lift-off, ADSB was lost - this is before E1/E2 FCO RUN-> CUTOFF.

It's just weird .
1. I don't know that the transponder lost power, because I don't have knowledge which electrical bus it is powered from on the 787. It may well have been powered from the main battery the whole time. The FR24 receiver may have stopped receiving data because it could no longer "see" the aircraft‐‐we know there are issues because it didn't even see the eastern half of the runway.
2. Altitudes are rounded, so this could be close to 75 feet gain‐‐or a gain and decline, if the data covers the top of the trajectory.
3. The first reading is definitely in the air, after rotation. FR24 does not report the altitude when the ADS-B data indicates that the aircraft is on the ground, and their data download confirms that.

The best bet to establish timing is to use rotation as datum, and then match the altitude/time estimates from the CCTV with position/time from the ADS-B and the estimated ground speed of the aircraft.

The fact that the ground speed is declining throughout the data sequence strongly suggests that it begins some time after the point, or at the point, when thrust was lost. And we know that didn't begin to happen until the aircraft was 3 seconds into the air.

Last edited by Musician; 18th July 2025 at 06:38 .

Subjects ADSB  CCTV  FlightRadar24  Fuel (All)  Fuel Cutoff Switches  RUN/CUTOFF

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Musician
July 18, 2025, 06:36:00 GMT
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Post: 11924853
Originally Posted by andihce
[...snip...]
We are not conducting either a criminal trial, or a civil trial here. I would rather call it (perhaps optimistically) a "scientific enquiry". I think the standard to be applied is whatever we (individually or collectively) think is reasonable, is order to fairly reach a meaningful conclusion. The standard for a criminal trial need not apply.
[...snip...]
Inasmuch as a scientific enquiry is based partially on rumors and conducted before all the evidence is in, yes.

The disconnect in the discussion stems partially from some speaking to what is " reasonable " while others talk about what is possible , given that we don't have all of the evidence yet.

For example:
Is it reasonable to assume the switch was defective? No .
Is it possible that it was? Yes .
Could future evidence change what is reasonable? Yes, but it probably won't. Wait and see.

So all of this can be true simultaneously, and if you don't pay attention to the context, that "yes" and "no" clash. (Can we call that a hamster fight? )

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Musician
August 09, 2025, 08:15:00 GMT
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Post: 11935586
Originally Posted by Lookleft
What do you think? BTW they weren't relighting the engine. They were returning the fuel switch to the position that it should have been in.`
And that did relight the engines, as the preliminary report notes.

Subjects Fuel (All)  Fuel Cutoff Switches  Preliminary Report  Relight

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Musician
August 09, 2025, 08:21:00 GMT
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Post: 11935588
Originally Posted by cncpc
The aircraft is said to have reached 600 feet AGL. It couldn't have done that without evidencing positive rate to the PNF.
AI171 reached 600 feet MSL (barometric), which, due to air pressure, temperature and field elevation, turns out to be approximately 200 feet AGL (or above airfield elevation, the ground does not slope a lot there). Watch the CCTV video of AI171 taking off, considering that the wing span is ~200 ft, to see this for yourself.

It is reasonable to think that 3 seconds into that flight is where "positive rate" would've been evident.


Subjects AI171  CCTV

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Musician
October 03, 2025, 06:44:00 GMT
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Post: 11963525
Originally Posted by Chiefttp
This is a Professional Pilots website, not a literary or professional poets website😄
Antoine de Saint-Exup\xe9ry notwithstanding.

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Musician
November 07, 2025, 19:01:00 GMT
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Post: 11984922
Originally Posted by sitigeltfel
This is the Supreme Court Judge, Justice Surya Kant, who has decided the Captain was not to blame.
That's not what it was about.

From the Reuters article:
Nov 7 (Reuters) - India's top court said on Friday that a preliminary report on an Air India crash that killed 260 people in June does not insinuate anything against the captain, but it will hear a plea from the pilot's father on November 10 for an independent probe.
So the question was: did the preliminary report blame the Captain?
I agree with the judge that it did not.

It's a father who wants a court to tell everyone that his son did nothing wrong.
It's understandable, but I'd rather wait for the facts to emerge.

But given this legal climate, I fear the AAIB might withhold the final report, as they're likely to get sued over it if they publish.

Subjects AAIB (All)  Preliminary Report

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Musician
November 28, 2025, 13:41:00 GMT
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Post: 11997203
Originally Posted by LondonSpotter
'it appears to be a broken link - does anyone have the right one?' and then when I googled AI171 multiple failures 48 hours it did finally take me to what appears to be the article.
original source: https://thefederal.com/category/busi...failure-217674
In Part 1, 2 and 3 of The Federal investigation into the Air India 171 crash, we looked at how core network degradation caused multi-component failure, and how the airline has been speeding up extensive D-check of its Dreamliners.
In part 4, we will look into how the Aircraft Accident Investigation Bureau's (AAIB) report mentions a stabilizer trim sensor issue on the previous flight (Al 423 Delhi-Ahmedabad) of the same plane, but does not mention a bigger problem with the stabilizer motor unit.

The Federal has gained access to the Aircraft Health Management (AHM) report that was sent to Boeing at 9.48 am IST (for Flight Al 423) that shows not only was the sensor showing stabilizer position malfunctioning but also the electronic control box that drives one of the tail-trim motors called the horizontal stabilizer electric motor control unit (EMCU). Both were replaced and the plane released for flight.
.
As yet unconfirmed.

Edit: I should probably explain that I posted this so we can reference what The Federal actually wrote, and don't need to discuss secondhand paraphrases of it. As long as it's unconfirmed, I don't believe any of it.

Last edited by Musician; 29th November 2025 at 09:00 .

Subjects AAIB (All)  AI171

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