SW 1380 one passenger dead: Uncontained engine failure and emergency landing at PHL
#166
Join Date: Sep 2005
Posts: 1,028
As Boeing and McD grew their respective aircraft into various stretched versions (737-200, DC-9-30, DC-9-50, MD80) that were made possible by increasingly more powerful variants of the Pratt&Whitney JT8D, that 107% threshold was exceeded. Rather that have the manufacturers design and install a system to aircraft that were already in production, they took advantage of the increased power of the -9, -5, and -17 versions of the engine, eliminated the 107% requirement, and redefined the reg in terms of a minimum climb gradient percentage--which the aircraft with the newer engines could easily meet. Once the high-bypass engines like the CFM-56 started appearing in the mid-1980s on the 737-300 and onward, that trend continued, so still no need for a fuel dump system.
These days, about the only thing that has a fuel dump system are the original 707, DC-8, 727, as well as some 757s, and other twins that are capable of long-haul flying, where the spread between max takeoff weight and max landing weight is higher.
#167
Join Date: Sep 2005
Posts: 1,028
The aircraft will get the damaged repaired, and a new engine, pylon, and cowling, and will eventually return to service, probably under a different registration number. While there was a fatality onboard the aircraft, that in and of itself doesn't warrant writing the aircraft off if it still some lifespan left. Decisions like this are based on numbers, not emotion. The LGA aircraft that was floated up to ALB for dismantling was due to the damage being beyond economical repair (busted keel beam, IIRC). The damage to the aircraft in PHL is far less severe...
Last edited by OPNLguy; Apr 18, 2018 at 11:40 am
#168
Join Date: May 2005
Posts: 4,872
The aircraft will get the damaged repaired, and a new engine, pylon, and cowling, and will eventually return to service, probably under a different registration number. While there was a fatality onboard the aircraft, that in and of itself doesn't warrant writing the aircraft if it still some lifespan left. Decisions like this are based on numbers, not emotion. The LGA aircraft that was floated up to ALB for dismantling was due to the damage being beyond economical repair (busted keel beam, IIRC). The damage to the aircraft in PHL is far less severe...
#169
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There is alot of talk about this guy thinking he was going to die. But was that realistic?
I get that in such a situation there is confusion and a lack of information..but I also know that de-compression in and of itself is not terminal to the flight envelope. Engine failure isn't either on multi-engine aircraft. A blown window is not structurally critical to the integrity of the airframe on a 737, particularly when only the glass is destroyed. I know that an emergency descent is standard procedure, and that the aircraft was still under control in that it's not rolling or yawing, or inverted. Had I been on the aircraft, I think I would have been confident in the survivability of the situation even without knowing the nature of the damage to the fuselage provided I sensed that that the aircraft was still under control. At least, as opposed to a situation like Alaska 261 where as a pax it would have been absolutely clear that this would be the end. But then again, who knows what this guy knew about flight and procedures.
I get that in such a situation there is confusion and a lack of information..but I also know that de-compression in and of itself is not terminal to the flight envelope. Engine failure isn't either on multi-engine aircraft. A blown window is not structurally critical to the integrity of the airframe on a 737, particularly when only the glass is destroyed. I know that an emergency descent is standard procedure, and that the aircraft was still under control in that it's not rolling or yawing, or inverted. Had I been on the aircraft, I think I would have been confident in the survivability of the situation even without knowing the nature of the damage to the fuselage provided I sensed that that the aircraft was still under control. At least, as opposed to a situation like Alaska 261 where as a pax it would have been absolutely clear that this would be the end. But then again, who knows what this guy knew about flight and procedures.
#170
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There is alot of talk about this guy thinking he was going to die. But was that realistic?
I get that in such a situation there is confusion and a lack of information..but I also know that de-compression in and of itself is not terminal to the flight envelope. Engine failure isn't either on multi-engine aircraft. A blown window is not structurally critical to the integrity of the airframe on a 737, particularly when only the glass is destroyed. I know that an emergency descent is standard procedure, and that the aircraft was still under control in that it's not rolling or yawing, or inverted. Had I been on the aircraft, I think I would have been confident in the survivability of the situation even without knowing the nature of the damage to the fuselage provided I sensed that that the aircraft was still under control. At least, as opposed to a situation like Alaska 261 where as a pax it would have been absolutely clear that this would be the end. But then again, who knows what this guy knew about flight and procedures.
I get that in such a situation there is confusion and a lack of information..but I also know that de-compression in and of itself is not terminal to the flight envelope. Engine failure isn't either on multi-engine aircraft. A blown window is not structurally critical to the integrity of the airframe on a 737, particularly when only the glass is destroyed. I know that an emergency descent is standard procedure, and that the aircraft was still under control in that it's not rolling or yawing, or inverted. Had I been on the aircraft, I think I would have been confident in the survivability of the situation even without knowing the nature of the damage to the fuselage provided I sensed that that the aircraft was still under control. At least, as opposed to a situation like Alaska 261 where as a pax it would have been absolutely clear that this would be the end. But then again, who knows what this guy knew about flight and procedures.
Practically speaking the most dangerous aspect of this incident was neither the decompression, nor the blown window, but the potential structural damage to the engine pylon and wing spar as well as the hydraulic systems. This could have easily also lead to structural or hydraulic damage to the left main landing gear if the debris had taken a different path.
#171
Join Date: Jul 2006
Location: NYC
Programs: pleb
Posts: 563
There is alot of talk about this guy thinking he was going to die. But was that realistic?
I get that in such a situation there is confusion and a lack of information..but I also know that de-compression in and of itself is not terminal to the flight envelope. Engine failure isn't either on multi-engine aircraft. A blown window is not structurally critical to the integrity of the airframe on a 737, particularly when only the glass is destroyed. I know that an emergency descent is standard procedure, and that the aircraft was still under control in that it's not rolling or yawing, or inverted. Had I been on the aircraft, I think I would have been confident in the survivability of the situation even without knowing the nature of the damage to the fuselage provided I sensed that that the aircraft was still under control. At least, as opposed to a situation like Alaska 261 where as a pax it would have been absolutely clear that this would be the end. But then again, who knows what this guy knew about flight and procedures.
I get that in such a situation there is confusion and a lack of information..but I also know that de-compression in and of itself is not terminal to the flight envelope. Engine failure isn't either on multi-engine aircraft. A blown window is not structurally critical to the integrity of the airframe on a 737, particularly when only the glass is destroyed. I know that an emergency descent is standard procedure, and that the aircraft was still under control in that it's not rolling or yawing, or inverted. Had I been on the aircraft, I think I would have been confident in the survivability of the situation even without knowing the nature of the damage to the fuselage provided I sensed that that the aircraft was still under control. At least, as opposed to a situation like Alaska 261 where as a pax it would have been absolutely clear that this would be the end. But then again, who knows what this guy knew about flight and procedures.
Was there certainty that the aircraft would stay intact, that no further damage would result, that everything needed to land safely would be functioning properly? To these passengers, absolutely not.
#172
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...Sumwalt said the NTSB wants to determine if the affected engine part is subject to a pending FAA airworthiness directive (AD) for certain CFM56-7B engines that would require ultrasonic inspections of certain fan blades. The agency proposed the AD after a Southwest 737 experienced a fan blade failure while flying from New Orleans to Orlando in August 2016...
[politically loaded comment redacted by nsx to prevent reader reaction derailing this very active thread]
Last edited by nsx; Apr 18, 2018 at 12:37 pm
#173
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Just watched the GMA video interview with Facebook live person (via Yahoo), and while he sounds collected now, one would have to believe he thought his time "on this earth" was ending.
#174
Join Date: Mar 2011
Posts: 6,286
I know the government sucks, and works at a snail's pace, and the safety and well-being of the public is LAST in the minds of these federal employees, but is there some reason these incredibly important things have to take YEARS to be implemented?
[politically loaded comment redacted by nsx to prevent reader reaction derailing this very active thread]
[politically loaded comment redacted by nsx to prevent reader reaction derailing this very active thread]
#175
Join Date: May 2004
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That is so simplistic. There's a process to follow involving the manufacturer, the airline, the crew, the passengers, and a bunch of research. Some of these incidents are more obvious than others, but in other cases it simply takes time. They do a lot of simulations and recreations to try to determine and then confirm what actually happened. I've not heard that budgetary issues have held any of those things back, but maybe that's the case. It's also by the way incredibly insulting to say that the "safety and well-being of the public is LAST" in the minds of "these federal employees." Anybody who has any actual experience with the NTSB knows that almost nothing could be further from the truth.
#176
Join Date: Sep 2005
Posts: 1,028
How could Philadelphia be the closest vector? Debris was found in Bernville, PA which is probably only 5 miles north of Reading (RDG). Admittedly 5 miles is probably too close to descend 38,000' and the runway is probably short (don't know anything about runway length), but Harrisburg (MDT), Allentown (ABIt's notE), and Lancaster (LNS) are much, much closer than Philadelphia.
I fully admit PHL is the most equipped for emergencies, I'm just wandering why PHL and not the closest airport. Listening to the ATC it was clear they knew people were injured, so I would think the priority would be getting on the ground.
Hats off to the pilot, she sounded cool and collected. I've been in situation where someone died and another time when someone probably should've died. Emergency staff keeping cool and collected isn't that easy even for professionals. If one person died as a result of a triage type situation when 150 people could've died that's a win in my book. I want to be clear I'm not criticizing anyone, just looking for an education.
I fully admit PHL is the most equipped for emergencies, I'm just wandering why PHL and not the closest airport. Listening to the ATC it was clear they knew people were injured, so I would think the priority would be getting on the ground.
Hats off to the pilot, she sounded cool and collected. I've been in situation where someone died and another time when someone probably should've died. Emergency staff keeping cool and collected isn't that easy even for professionals. If one person died as a result of a triage type situation when 150 people could've died that's a win in my book. I want to be clear I'm not criticizing anyone, just looking for an education.
#178
Join Date: Mar 2011
Posts: 6,286
That is so simplistic. There's a process to follow involving the manufacturer, the airline, the crew, the passengers, and a bunch of research. Some of these incidents are more obvious than others, but in other cases it simply takes time. They do a lot of simulations and recreations to try to determine and then confirm what actually happened. I've not heard that budgetary issues have held any of those things back, but maybe that's the case. It's also by the way incredibly insulting to say that the "safety and well-being of the public is LAST" in the minds of "these federal employees." Anybody who has any actual experience with the NTSB knows that almost nothing could be further from the truth.
https://www.reuters.com/article/us-p...-idUSKBN1HP0QK
From the article:
An early review of Tuesday’s failed Southwest engine found preliminary evidence of metal fatigue where a fan blade had broken off, Robert Sumwalt, chairman of the U.S. National Transportation Safety Board (NTSB), told reporters on Tuesday.
In August 2016, a Southwest flight made a safe emergency landing in Pensacola, Florida, after a fan blade separated from the same type of engine, and debris ripped a foot-long hole above the left wing. There too, investigators cited signs of metal fatigue.
“We are very concerned,” the NTSB’s Sumwalt said, referring to the general problem of detecting slow-developing metal fatigue.
“There needs to be proper inspection mechanisms in place to check for this before there’s a catastrophic event.”
Southwest said it was speeding up inspections of all related engines, which it expected to complete within 30 days.
Investigators said they would be examining maintenance records of the airline, which operates one of the world’s largest 737 fleets and has a strong safety record.
The 2016 incident prompted the U.S. Federal Aviation Administration (FAA) to propose ultrasonic inspections of similar fan blades and their replacement if needed.
Sumwalt said the NTSB would review whether the engines involved in Tuesday’s incident might have been subject to that directive, which is not yet finalised.
The U.S. FAA has estimated that checks, originally prompted by a safety bulletin from CFM itself, would require two hours per inspection.
#179
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Why? It's just an arbitrary number. Given one fan blade flying away, the probability of fan blade 13 being the one to disappear is exactly the same as the probability of fan blade 7 (lucky 7!!!) disappearing or any other one of the 24 fan blades -- 1 in 24. It's less than a coincidence... it's superstition, which is an impediment to logic and reasoning.
#180
Join Date: Apr 2005
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Why? It's just an arbitrary number. Given one fan blade flying away, the probability of fan blade 13 being the one to disappear is exactly the same as the probability of fan blade 7 (lucky 7!!!) disappearing or any other one of the 24 fan blades -- 1 in 24. It's less than a coincidence... it's superstition, which is an impediment to logic and reasoning.
13 is lucky in Italy. It was just a number, in most cultures, till it just so happened that the Knights Templar were ambushed on Friday the 13th. Not good to be the main creditor of the French king...