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-No pre-flight check? -Forced takeoff -Power failure (both engines failed, highly unlikely) -Flaps not extended -Landing gear still deployed -Nose pitched up Numerous questions and observations, very difficult to pinpoint the cause, but this is undoubtedly a deeply tragic event

110,055 просмотров • 1 год назад •via X (Twitter)

Комментарии: 11

Фото профиля Indian Rafale Slayer
Indian Rafale Slayer1 год назад

As expected indian pilots 🤡

Фото профиля American Stories Network
American Stories Network1 год назад

Only the strong survive. 💪 Who will conquer the challenges and rise to the top? Tune in and find out! #SurvivingMann #UltimateCompetitor #NavySEALs #SpecOps #TacticalTraining

Фото профиля AmnaH
AmnaH1 год назад

Pilot error mainly that’s what other pilots and aviation analysts are saying.

Фото профиля Vanta Logik
Vanta Logik1 год назад

Black box. The flight recorder anyone? Can someone please find that and show its revealings to all the aviation experts online?

Фото профиля سلیم عام شہری
سلیم عام شہری1 год назад

Now indians will understand the meaning of the center of gravity 😎💥 #planecrash #Ahmedabad

Фото профиля الحمدللہ @
الحمدللہ @1 год назад

Seems Pilot error more than any other cause

Фото профиля carpe diem
carpe diem1 год назад

Landing great still down coz it was on take off segment. Nose pitch up because even in crash landing the aim is always to touch the rear end of plane and main wheels. Something is seriously wrong with these Boeings

Фото профиля Ahmed
Ahmed1 год назад

So the "Real Question" is, Indian govt will blame Pakistan for hijacking the plane or smthg? Or will they accept it as a technical failure or pilot's mistake?

Фото профиля Adil
Adil1 год назад

Involvement of Pakistan?

Фото профиля Maaz Ul Haq 🇵🇰
Maaz Ul Haq 🇵🇰1 год назад

Seems like the pilot was not in his senses

Фото профиля The Curious Philanthropist 🇵🇰🍁
The Curious Philanthropist 🇵🇰🍁1 год назад

Perfect case study of corruption + incompetence + negligence.

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AIR INDIA 787 ‘thoughts’ I’m surprised nobody, even the experts) have mentioned this… The 787 Dreamliner (all variants) has an ‘Air Ground Sensing’ system that opens the Main Gear doors immediately upon leaving the runway and prior to the (Flight Deck) Lever being moved manually to the ‘up’ position. I’ve witnessed this literally hundreds of times when filming The 787 and it’s clear on the footage attached: upon rotate, about one second from wheels off ground, the main Gear Doors open. Then, around three to four seconds (pilot discretion) Positive Rate is called/agreed and the Gear Lever is moved to the UP position. On a side note, the 787 is quite prone to brake malfunction, mostly down to the electric brake system that can fail from time to time on a single (or more) wheel. If the wheels are not retracted within a given amount of time due to a wheel continuing to spin, the gear doors will close back-up until the wheel(s) stop spinning and the gear is recycled at which time the doors will re-open and the gear will retract fully. This is the takeoff/gear-up procedure with all 787s. This is quite clearly not the case when observing the CCTV footage of the doomed Air India jet. I think it’s quite evident there was some kind of (electrical?) malfunction with the system(s). The question of the Flap (takeoff) Setting is still a mystery as, with poor quality footage, it’s difficult to completely confirm whether the flaps were extended or not. In my personal opinion they were not extended. There was a CNN reporter right next to one of the wings on the ground. Although it was heavily charred, it would’ve been clear to see if they were extended or not 🤷🏼‍♂️ Also, as for possible (engine) ingestion/failure, whether by birds or other FOD, there is no evidence of engine Compressor Stall, which is very clear to see in many videos online when it does happen with bird strikes, especially at rotate power/speed. The engine(s) will ‘pop’ flames out of the back. What is evident, is that the Jet uses all of the available runway, which is clear by the amount of dust being kicked-up on rotate. The Jet never seems to reach the optimal takeoff angle, right from the rotate point it appears to struggle, which would suggest either engine power issues or, as mentioned, the lack of lift from the Flaps/Slats. Witness accounts say there was a distinct lack of engine noise coming from the jet, which backs-up some theories of engine failure. You would expect, even with a lack of Flap setting the pilot would be able to increase to max (TOGA) power to give them some chance of climbing or at least gaining enough altitude to get themselves back to the airfield or to a safer (crash) landing zone. That ‘power up’ would be evident with black exhaust from the engines, but that didn’t happen - at all. You’ll see/hear from the (second part) footage I’ve filmed, that the engine sound is very evident at this height and that this climb-out is too Standard Operating Procedures. Personally I find it hard to believe the NFP would make such a rookie mistake as to raise the flaps (push and move the staggered lever) as opposed to the gear lever which is a simple up-down motion. The two levers are also in completely different positions: Gear lever on the facing panel and flap lever (with many settings) next to the throttles. Plus this is such a basic procedure that even the most rookie pilot wouldn’t make this mistake 🤷🏼‍♂️ Again, this is just my opinion and observations based on visual and actual experiences. The CVR and FDR will deliver the final evidence.

BIG JET TV

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Francisco Cunha

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A preventable tragedy On This Day in 1967: Stockport air disaster (England). A British Midland C-4 [G-ALHG] crashes in Stockport, 72 of 84 aboard die. On a go-around, crew lost control after 2 engines failed. Investigation traced the issues to a known - but never addressed - design issue in the fuel system. More details here by ASN (video is from British Pathé) PROBABLE CAUSE: "The immediate cause of the accident was loss of power of both engines on the starboard side, resulting in control problems which prevented the pilot from maintaining height on the available power with one propeller windmilling. The loss of power of the first engine was due to fuel starvation due to inadvertent fuel transfer in flight. The loss of power of the second engine was due either to fuel starvation resulting from inadvertent fuel transfer in flight or to misidentification by the crew of which engine had failed followed by failure to restore power in time to the engine misidentified as having failed. Contributory causes of the accident were: (a) The design of the fuel valves and location in the cockpit of their actuating levers, so that a failure by the pilot correctly to position the lever by an amount so small as to be easy to do and difficult to recognize would result in inadvertent fuel transfer on a scale sufficient to involve the risk after a long flight of a tank expected to contain sufficient fuel being in fact empty. (b) Failure of those responsible for the design of the fuel system or the fuel valves to warn users that failure by a small amount to place the actuating levers in the proper position would result in inadvertent fuel transfer on a scale involving this risk after a long flight. (c) Failure of British Midland's air crew or engineers to recognize the possibility of inadvertent fuel transfer in the air from the evidence available in previous incidents in flight and contained in the fuel logs. (d) Failure of other operators of Argonauts who had learned by experience of the possibility of inadvertent fuel transfer in flight to inform the Air Registration Board, the Directorate of Flight Safety of the Board of Trade or its predecessors, or the United Kingdom Flight Safety Committee of the facts which they had learned so that these might be communicated to other operators of Argonauts and other aircraft equipped with similar systems and fuel cocks."

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