They were on fire just as they reached V1.
Plane was fully loaded with 38,000 LB of fuel for 12 hour flight to hawaii. Worst case scenario.
Pilots did the heroic thing - they tried to take off instead at 160 MPH to minimize collateral damage (highway and warehouses at the end of the runway) and crash and die somewhere else, instead of go beyond the runway at that speed. Accelerating a fully loaded jet plane at ground level beyond the runway has obvious consequences. They had one choice.
Instead, they clipped the UPS factory because they were so low, they tried to clear it but did not. Plane then hit the ground port wing down, shearing it off entirely, smearing a fireball of jet fuel across half a mile (not an exaggeration) before the plane flipped. Crew were likely dead by before this, footage shows the cockpit being slammed into the ground like a mousetrap by the flip once the port wing was gone and gravity took the starboard wing over.
Physics took over. Plane flipped and rolled upon loss of port wing, smearing a rolling fireball of the remaining fuel load from the starboard wing for another half a mile.
Louisville is now a firestorm as a result.
Respect to the flight crew; rest in peace, they made the best they could out of a really shitty scenario. They flew it all the way down.
Footage:
https://x.com/osinttechnical/status/1985845987684855969?s=46
https://x.com/faytuksnetwork/status/1985849267152699741?s=46
https://x.com/faytuksnetwork/status/1985848132500885995?s=46
https://x.com/faytuksnetwork/status/1985843126934614297?s=46
Do runways have some sort of barrier between them and the next "important" thing. It seems like that would be prudent both for cases like this, and breaking failures following landings.
Many airports have this problem. The recent korean air disaster which echos this is another example. BTW, this is why most airports, if possible, point out to sea...
Older airports might have EMAS [1] retrofitted at the ends to help stop planes, but that's designed more for a landing plane not stopping quickly enough (like [2]) - not a plane trying to get airborne as in this case.
[1] https://en.wikipedia.org/wiki/Engineered_materials_arrestor_... [2] https://en.wikipedia.org/wiki/Southwest_Airlines_Flight_1248
I think pilot training is playing a factor. A normal rotation kills too much energy. One engine can climb when you have some airspeed and get clean, but if you lose too much energy on rotation, the inefficiency of the AoA for the rest of the short flight means that engine can no longer buy you any up. I've seen too many single-engine planes going down while trying to pitch up the whole way down.
So, less aggressive single-engine rotations and energy absorbers at the ends of runways that can't get longer. This seems like the kind of thing where we do it because it removes a significant cause of people dying.
Just watched this angle a few more times: https://x.com/BNONews/status/1985845907191889930
Another crash video shows the aircraft clearly descending before colliding with anything. It manages to go up a bit, so it's fast enough to get airborne. The normal looking rotation kills too much energy. The plane is then too inefficient to maintain speed. AoA goes up while energy goes down. Power available goes negative and then it's over.
Yes, it did get airborne for a few seconds but from the video below, it looks like the left wing was damaged by the fire and could not provide enough lift, then the right wing rolled the plane to the left causing the crash.
https://bsky.app/profile/shipwreck75.bsky.social/post/3m4tvh...
The wings and aerodynamics don't really care if air or air with combustion are flowing around them.
Roll is a consequence of the loss of control due to low speed and the yaw of the good engines. Speed up, rudder works, plane might maintain positive climb.
Not saying it's what happened here, but if the heat is intense enough to deform the wing / control surfaces, it matters.
I'm skeptical whether pilots can realistically make this kind of decision, given that they have no more than a few seconds to make it, and in cases such as this based on very incomplete information about the state of their aircraft.
Some do. Here is what it looks like when an overshooting plane utilizes such a barrier: https://www.youtube.com/watch?v=zW71FrX8t_g
179 dead.
Consider the possibility that gigantic flying aluminum tubes filled with tons of flammable fuel hurtling around at hundreds of kilometers per hour comprise a dilemma that has no trivial answers. Even defining what "important thing" means at any given instant is not straightforward.
You also don't particularly want it to be catastrophically effective as there are real world cases where planes have clipped the fence and then NOT gone on to crash, or at least to crash in a fairly controlled manner with the majority onboard surviving. Hitting a brick wall at 180mph is going to have a 0% survival rate.
Ha, Jeju Air Flight 2216 smashed into a barrier on the second landing attempt in Muan last year [0], and people commented "How could there be a barrier at the end of the runway, so obviously stupid, irresponsible", etc.
Now a plane does not smash into a barrier at the end of the runway and people suggest putting barriers at the end of the runway.
Don't mean to attack parent post, but may I suggest that
a) hordes of experts have thought long and hard about these issues, and it is unlikely that you can encounter this for the first time as a lay person and come up with a solution that has eluded the best engineers for decades ("why don't they attach a parachute to the plane?"), and
b) we are very close to an optimum in commercial aviation, and there are few if any unambiguous ("Pareto") improvements, but rather just tradeoffs. For example: You leave cockpit doors open, terrorists come in and commandeer the plane to turn it into a weapon. You lock the cockpit doors closed, and suicidal pilots lock out the rest of the crew and commandeer the plane to turn it into a weapon of mass-murder-suicide.
There are no easy answers.
[0] https://en.wikipedia.org/wiki/Jeju_Air_Flight_2216
ETA: In 2007 an A320 overran a runway in Brazil and crashed into a gas station, killing 187 pax & crew + 12 on the ground. https://en.wikipedia.org/wiki/TAM_Airlines_Flight_3054
As far as the rest of my comment - watch the videos that I linked.
After V1 you must be able to take off on only the remaining engines. If that's not possible you must reduce weight until it is possible or you're not allowed to start takeoff at all.
This is why in very warm weather and higher altitude airports (lower performance) sometimes cargo/luggage or even some passengers are left behind, while in colder weather all seats could be used.
More specifically, V1 is the max speed at which you're about to take off, but you can still abort from. They hit that max speed and realized there was a major problem that hypothetically, they could have slowed down from, but realistically was not possible. They had no choice.
When the plane reaches V1, pilots take the hand off the throttle: they're committed to takeoff, even if an engine fails. It is better to take off and fix the problem or land again, than to smash into whatever is beyond the end of the runway.
Surely uncertainty about the situation contributes to defaulting to committing, but what if it's a passenger plane and at V1 pilots know they've lost power? Wouldn't veering into highway at 30 mph be weighted against certain, big loss of life?
Edit: I now see that this has been partially answered by uncle comment
The margin is for example that the plane must not just be able to fly, but also reach a minimum climb gradient to clear obstacles with a bit of safety margin. There is also an allowance for the time it takes from calling abort to actually hitting the brakes. And for example headwind is part of the calculation (it makes the takeoff distance shorter) but only 50% of the headwind is used in the calculations.
But all of those margins are not for the crew to use, the crew must just execute the procedure exactly as trained which means at V1 you're committed to continue the takeoff. And before V1 in case of an engine failure you have to hit the brakes to make sure you can stop before the end of the runway.
Between V1, Rotate and V2, there’s like a 2-3kts difference (between each of them).
I am not familiar what the procedure is if you have dual-engine failure at or above V1.
As I understand it, there is a low speed regime, under 80 knots, where are you stop for basically anything.
Then there is a high speed regime, where you only stop for serious issues, because you now have so much kinetic energy that stopping the plane, while still possible, will involve risk. (i.e. fire from overheated brakes.)
At a certain point, called V1, there’s no longer enough room to stop, no matter what your problem is. You’re either getting airborne or you’re crashing into whatever is ant the end of the runway. In general, getting airborne is the safer option, while obviously still not risk free.
However, this calculation also assumes that the engine fails in an isolated fashion, and its failure did not affect the other engines. If the failure of the left engine threw off debris that damaged the middle engine then we are now talking about a double engine failure. I’m sure the pilots knew there was a problem with the engine when they made the decision to continue, but it’s possible that problems with the middle engine weren’t apparent yet and that it only started to fail once they were committed.
Obviously, this is just speculation, and we will have to wait for the preliminary report at least.
RIP
This situation (single engine failure at V1) is something that commercial pilots are certified in at every recurrent certification since it’s one of the most difficult you can be in. The crew now need to climb and go around for a landing on one engine while simultaneously running through the engine failure (and also likely fire) checklist. I don’t know if a double engine failure at V1 on a fully loaded 3 engine aircraft is technically survivable or if it’s something that’s trained on. They were put in an incredibly difficult situation just based on what reports we’ve already seen.
It's astonishing that this is a thing. Why aren't we building airports with enough space for a plane to remain on the ground and have plenty of room to decelerate in this situation? I can understand why it can't be retro fitted to existing airports but is it a scenario that's considered at new airports? Just seems like such an absolutely basic safety step.
Airports also grow themselves. Some municipal airports sited for small aircraft extend their runways to handle larger planes.
They were on fire just as they reached V1.
Plane was fully loaded with 38,000 LB of fuel for 12 hour flight to hawaii. Worst case scenario.
Pilots did the heroic thing - they tried to take off instead of accelerate past the runway at ground level at 160 MPH to minimize collateral damage (highway and warehouses at the end of the runway) and crash and die somewhere else.
Instead, they clipped the UPS factory because they were so low, they tried to clear it but did not. Plane then hit the ground port wing down, shearing it off entirely, smearing a fireball of jet fuel across half a mile (not an exaggeration) before the plane flipped. Crew were likely dead by then, footage shows the cockpit being slammed into the ground by the flip once the port wing was gone and gravity took the starboard wing over.
Plane flipped, continued to smear half of the fuel load for another half a mile.
Louisville is now a firestorm as a result.
Footage:
https://x.com/osinttechnical/status/1985845987684855969?s=46
https://x.com/faytuksnetwork/status/1985849267152699741?s=46
https://x.com/faytuksnetwork/status/1985848132500885995?s=46
https://x.com/faytuksnetwork/status/1985843126934614297?s=46
To know this, they would have to know they had lost multiple engines. Clearly this is the case by the end, but it's not clear who realized what at what time.
The NTSB investigation will bring more light.
Excellent edge-case for IFTTT thermostat. Localized air quality alert --> Intake offline.
> Ground observers reported the aircraft had been delayed for about two hours for work on the left hand engine (engine #1), the engine #1 separated during the takeoff run, the center engine emitted streaks of flames, the aircraft impacted a UPS warehouse and ploughed through other facilities before coming to rest in a large plume of fire and smoke.
haunter•11h ago
https://x.com/BNONews/status/1985845907191889930
https://xcancel.com/BNONews/status/1985845907191889930
Edit: just the mp4 https://video.twimg.com/ext_tw_video/1985845862409334784/pu/...
There is an incredible amount of ground damage! Just wow, this is very bad https://files.catbox.moe/3303ob.jpg
toomuchtodo•11h ago
https://www.flightaware.com/live/flight/UPS2976
justsid•11h ago
Jtsummers•10h ago
Flying with two engines and taking off without an engine in a loaded aircraft are two very different things. A lot more thrust is needed during takeoff than after.
andy99•10h ago
justsid•10h ago
[1] https://www.avherald.com/h?article=4dfd50b9&opt=0%20
bobthepanda•8h ago
anonymars•7h ago
https://imgur.com/a/NYlrLYO
https://cdn.discordapp.com/attachments/757091156717862935/14...
Source: https://reddit.com/r/flying/comments/1ooms7t/ksdf_accident/n...
rob74•48m ago
In this case however, with the wing already on fire (the engine is below the wing, so flames coming out of it would be visible behind and under the wing, not in front), I'm afraid that even if they had managed to take off, the fuel tank would have exploded or burned through the wing before they would have had a chance to land. Actually, this looks similar to the 2000 Concorde crash...
appreciatorBus•8h ago
dboreham•7h ago
avalys•8h ago
filleduchaos•8h ago
In fact, it being normal almost certainly contributed to the scale of this accident, since a single engine failure during the takeoff roll isn't considered enough of an emergency to reject the takeoff at high speed (past a certain speed, you only abort if the aircraft is literally unflyable - for everything else, you take the aircraft & emergency into the air and figure it out there). The crew wouldn't have had any way to know that one of their engines had not simply failed, but was straight-up gone with their wing on fire to boot.
Jtsummers•8h ago
I don't know about the MD-11 itself, but other aircraft from that time period have sensors to detect and report overheat and fire in various parts of the aircraft, including engines and wings.
appreciatorBus•7h ago
positron26•7h ago
Jtsummers•7h ago
positron26•7h ago
filleduchaos•5h ago
There's also a very big difference between "Engine failure: something has damaged or jammed enough components that the turbines are no longer spinning fast enough to produce thrust or drive the generators" and "Engine failure: the engine is no longer attached to the aircraft, which is why it is no longer producing thrust". However, both things are reported in the cockpit as ENG FAIL.
(Un)fortunately, cockpit warnings prioritise the what (so to speak) and not the how or why. On one hand, this makes decision-making a lot simpler for the crew, but on the other...well, in rare cases the lack of insight can exacerbate a disaster. Depending on when exactly the engine gave out, this poor crew might have been doomed either way, but they might have been able to minimise collateral damage if they knew just how badly crippled the aircraft was. And there was a very similar accident to this one (actually involving the predecessor of the MD-11, the DC-10), American Airlines 191 - one of the engines detached from the aircraft, damaging the leading edge of its wing in the process, causing that wing to stall when the crew slowed down below the stall speed of the damaged wing in a bid to climb. If they could have somehow known about the damage, the accident might have been avoided entirely as the crew might have known to keep their speed up.
eternityforest•1h ago
roryirvine•1h ago
In emergencies, information overload tends to make things worse, not better.
ExoticPearTree•29m ago
And now we have technology that allows for cameras everywhere to give a better situational awareness across all critical aircraft surfaces and systems.
It is going to take a little bit of adjusting to, but it will help improve safety in a tremendous way.
cedilla•13m ago
And how would the cameras even work? Are the pilots supposed to switch between multiple camera feeds, or do we install dozens of screens? And then what, they see lots of black smoke on one camera, does that really tell them that much more than the ENG FIRE alert blaring in the background?
Maybe this could help during stable flight, but in this situation, when the pilots were likely already overloaded and probably had only a few seconds to escape this situation - if it was possible at all - I can't imagine it being helpful.
zuppy•6m ago
Now... not sure how much that is helpful in this kind of emergency, they really didn't have time to do much.
ragazzina•3m ago
What is the difference?
roygbiv2•7h ago
appreciatorBus•7h ago
loeg•7h ago
Freeze frame: https://imgur.com/a/c3h8Qd3
FabHK•6h ago
loeg•6h ago
appreciatorBus•6h ago
CPLX•6h ago
Obviously impossible to tell from some cell phone type videos. Being struck by something is also possible. But it sure does look like an uncontained engine failure.
loeg•6h ago
https://news.ycombinator.com/item?id=45818448
JCM9•42m ago
Scarily there are communities that have ignored such logic and permitted dense residential development right next to an airport.
anonymars•7h ago
https://www.wdrb.com/news/ups-plane-catches-fire-and-explode...
> There is an incredible amount of ground damage!
It's fortunate it wasn't taking off the other direction, towards the adjacent downtown of Louisville (https://www.google.com/maps/place/Louisville+International+A...)
rodface•6h ago
The_President•1h ago