Korean airline emergency landing goes wrong and many killed (3 Viewers)

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It did look like a late touchdown, but what the reason was?

Huh, just went back to watch the video in my post#3, and how about that? The URL has had the video changed so that it no longer shows the actual crash, now it only shows the flaming and smoking wreckage over & over again.
 
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The only issue with a Total Hydraulic failure is that Modern Airliners have at least 2 and usually 3 separate Hydraulic systems, with engine driven Pumps on each engine, and a electric hydraulic pump, and usually a reversible hydraulic pump motor assembly, not to mention the RAT or Ram Air Turbine that can provide a minimum hydraulic and electrical power for emergency use. The only realistic way you can have a total loss of hydraulic power is to lose all of the fluid, and as there are no common lines shared between the systems, and they all have separate reservoirs. It would take a case like the United Airlines Sioux City Iowa crash where the #2 engine fan assembly came off and cut thru all 3 systems lines in the horizontal stabilizer where they are in close proximity on the DC-10. And even then it took over 30 minutes for enough fluid to leak out to make the A/C uncontrollable.

Granted something catastrophic happened, but I do not think it was a total hydraulic system failure. But we will see what the investigation uncovers. But I suspect it will not be this week that we get an answer.
 
fubar57 said:
CBC just reported about a wall that should not have been at the end of the runway. This area is supposed to be free of obstacles to allow for overshooting. The "expert" on CBC said, had this wall not been there, no explosion
Click to expand...
The embankment is 250 meters or 800 feet from the end of the runway. That is a long way from the end of the runway.

The fact that the aircraft was going 150 mph when it hit that embankment is not the fault of the design of the airport.

Aircraft aren't supposed to be going 150 mph on the ground 800 feet from the end of the runway.
 
Here's the runway if anyone is interested, dated Sept. '24

1735528600083.png
 
I just remembered an odd incident from my airline days that could also lead to a full hydraulic failure, but I don't think it would be a factor in this crash.

At one of our smaller out stations that at the time only smaller DC-9's and Convair 580's flew into. Someone contaminated the Hydraulic refilling bowser with hand soap of all things. Apparently the station had 55 gallon drums of both Skydrol hydraulic fluid and the hand soap side by side and as both fluids have a purple color to them they got confused.

The Convair's were not affected as they still used 5606 Hydraulic fluid that is dyed red. The 5 or so DC-9's that were affected were having odd hydraulic issues, and more frequent failures of the seals on hydraulic actuators. The actual biggest complaint by the flight crews was inconsistent braking, and nose gear shimmy at high taxi speeds. We had replaced the shimmy dampers and bled the brakes many times. The actual brakes had also been replaced, and the write ups continued.

The problem was finally discovered several weeks later when one of the A/C developed a pin hole leak in one of the hydraulic lines in the right wheel well. A pin hole in a line under pressure usually results in a fine mist spraying out of the hole. In this case besides the fine mist it looked like a bubble machine was operating in the right wheel well! With purple bubbles coming out of the wheel well with the main gear door opened!

Well we had to conduct fluid sampling of the entire fleet's hydraulic systems after that. And we did find that it was contained to about 5 of the smaller DC-9-10 & DC-9-30 models. All the affected A/C were taken out of service, had there Hydraulic systems drained and flushed. I am not sure what if any of the hydraulic components were changed as most of the work was done at the main Maintenance base. We only performed the work on the 1st DC-9 that the issues was discovered on.

So Hydraulic fluid contamination is also a remote possibility. But I still think that it was not a hydraulic issue as the aircraft looked to still be controllable and was wings level and headed down the runway at the time of the accident. If there was a big issue with the hydraulic systems it would have affected the abilities of the crew to steer the aircraft.

That being said I should also state that I do not have any experience with 737's other than a few small servicing items on older 727-200 & 300 models. And the most modern Boeing products I have worked on are 757 & 747-400 models.
 
Without gear down, no wheel braking, and appears to be neither flaps or spoilers for aero braking, which would have likely forced nose down. Appears to be very long in touchdown, metal on concrete is low friction, and nose high attitude seems strange.
Few reports have mentioned there was a very effective plowed gravel area at runway end, but that would work only with gear down, nose down.
Until NTSB, etc. we're armchair experts, but seems like a lot of bad decisions, system failures, and short runway working together.
 
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