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OldnGrounded
2025-06-15T13:29:00 permalink Post: 11902475 |
World wide grounding of the DC10 fleet after Chicago where maintenance had modified engine removal procedures which led to a wing engine loss taking out hydraulic systems that allowed the slats to retract ..aircraft stalled asymetrically and rolled inverted. Many other aircraft had damaged mounts/bolts not all were reported.
Last edited by OldnGrounded; 15th Jun 2025 at 13:37 . Reason: Typo. to not yo Subjects: Hydraulic Failure (All) Hydraulic Pumps NTSB |
OldnGrounded
2025-06-15T13:34:00 permalink Post: 11902477 |
Trying to keep an open mind, but\x85.
Is no one surprised the lone survivor remembers a bang just before impact, and other things like apparently emergency lights, but has not mentioned the power going from takeoff power to nothing. Even the power change at thrust reduction altitude is often very noticeable in the cabin, so it surprises me nothing about the noise (and startle/panic) of full-power to no-power has been mentioned. I think we are getting into absurd scenarios trying to make the scenario of a simultaneous double engine failure just after liftoff fit, based on perhaps not the best evidence. Subjects: Dual Engine Failure Engine Failure (All) 1 user liked this post. |
OldnGrounded
2025-06-15T19:07:00 permalink Post: 11902731 |
https://en.wikipedia.org/wiki/LATAM_Airlines_Flight_800 Subjects: None |
OldnGrounded
2025-06-15T23:28:00 permalink Post: 11902958 |
Subjects: TCMA (All) |
OldnGrounded
2025-06-15T23:34:00 permalink Post: 11902965 |
Subjects: FADEC |
OldnGrounded
2025-06-15T23:55:00 permalink Post: 11902983 |
Ah, yes. Missed that. Thanks. But I have to assume (I know) that any responsible aviation engineers designing a system that can shut down both (all) engines simultaneously when the airplane is on the ground is going to want to make very sure that the airplane is on the ground.
But I'll check. Subjects: Dual Engine Failure Engine Failure (All) |
OldnGrounded
2025-06-16T00:52:00 permalink Post: 11903015 |
Petition for Time Limited Exemption to 14 CFR 25.901(c) at Amendment level 25-46 and 25-126 and 25.1309{b) at Amendment Level 25-41 and 25-123 for General Electric GEnx-1 B Thrust Control Malfunction Accommodation - 787 787-8, 787-9
https://downloads.regulations.gov/FA...tachment_1.pdf Grant of exemption: https://downloads.regulations.gov/FA...tachment_1.pdf I'll keep looking to find out what they actually did. Subjects: TCMA (Air-ground Logic) TCMA (All) 1 user liked this post. |
OldnGrounded
2025-06-16T01:19:00 permalink Post: 11903028 |
The TCMA patent application is at:
https://patents.google.com/patent/US6704630B2/en
Quite a simple system (not) What gets your attention is the fact that you can continue to operate the aircraft without an MMEL entry when one of the two systems (per EEC) that shadow each other... is unserviceable. As it says: "Typically the aircraft is allowed to operate for a limited period of time with just a single operative processing subsystem." That 787 was not long out of maintenance. I note that, unless I missed it, the patent application doesn't address a mechanism for determining whether an aircraft is actually on the ground. I suppose that will depend on some of those "several other digital inputs."
Via the execution of software package
130
, each of the processing subsystems
20
a
and
20
b
monitors the position of thrust lever
36
, engine power level,
and several other digital inputs provided from the aircraft
via digital ARINC data buses
46
.
I'm still looking for identification of the relevant inputs for TCMA on the GEnx-1B. If anyone has suggestions, please share. Subjects: ARINC TCMA (All) |
OldnGrounded
2025-06-16T01:33:00 permalink Post: 11903033 |
From six paragraphs down in the TCMA patent application.
"​​​​​​ The method of the present invention compares the engine's actual power level with a threshold contour defined by the TCMA software package. When the TCMA software package determines that a thrust control malfunction has occurred, based on the engine's power level exceeding the threshold contour, the engine is shut down by the TCMA circuit." Subjects: TCMA (All) 1 user liked this post. |
OldnGrounded
2025-06-16T01:40:00 permalink Post: 11903037 |
This has just appeared in the Times (of London) which is usually one of the most reliable sources of information in the UK.
"A loss of engine power is emerging as the most likely cause of the crash of the Air India Boeing that killed at least 279 people at Ahmedabad on Thursday. The Boeing 787-8 series appeared to have suffered from lower than normal thrust from its General Electric GEnx engines as it took off and failed to climb more than 450ft before crashing, video and reports from the Indian authorities have indicated.The new information has eclipsed an early focus on the unusual configuration of the aircraft\x92s wing flaps and landing gear." https://www.thetimes.com/world/asia/...rash-vhqw6b7v3 (subscription required to read the article) And it quotes Juan Browne (Blancolirio): \x93There was something terribly wrong with this 787 jet and we need to find out really quickly what went wrong because we\x92ve got a thousand of these operating today and operators need to find out what happened.\x94 Subjects: DGCA GEnx (ALL) Gear Retraction 5 users liked this post. |
OldnGrounded
2025-06-16T02:15:00 permalink Post: 11903057 |
Folks, if an interim report or other official communication from the investigation is released, it will almost certainly come from India's AAIB or at least be posted to its site. So checking there before posting something like that here would be a really good idea.
https://aaib.gov.in/ Admin note: the url is correct, app are the Government allow advertising on their sites! SPlot Subjects: AAIB (All) 2 users liked this post. |
OldnGrounded
2025-06-16T03:41:00 permalink Post: 11903083 |
Please, we really don't need any more snark in this thread. And your snark suggests that you may not understand the implications of the story cited in the posts you quoted.
That the Times reports, clearly based on information from official Indian sources, that loss of thrust in both engines was a key factor in this crash, and that DGCA has ordered urgent inspections of 787s because of preliminary findings of the investigation, is important news from one of the most responsible newspapers anywhere. And Juan Browne's urging quick action and citing the importance to the entire fleet and to aviation generally is also significant. He's a respected aviator many here pay serious attention to. Subjects: DGCA 4 users liked this post. |
OldnGrounded
2025-06-16T03:52:00 permalink Post: 11903086 |
Yes, so do I. But we live now in a world where information from officials who aren't quoted because they aren't authorized to speak, or are authorized but insist on anonymity, is very often the only information available, especially early in an investigation like this one. The fact that this story is in the
Times
gives me a fair amount of confidence that what is being reported really is from official sources. They actually have journalistic standards there.
Subjects: None |
OldnGrounded
2025-06-16T02:15:00 permalink Post: 11903737 |
Folks, if an interim report or other official communication from the investigation is released, it will almost certainly come from India's AAIB or at least be posted to its site. So checking there before posting something like that here would be a really good idea.
https://aaib.gov.in/ Admin note: the url is correct, app are the Government allow advertising on their sites! SPlot Subjects: AAIB (All) |
OldnGrounded
2025-06-16T23:49:00 permalink Post: 11903875 |
https://downloads.regulations.gov/FA...tachment_1.pdf https://downloads.regulations.gov/FA...tachment_1.pdf I haven't yet been successful in finding the details of the solution that would have brought TCMA for that engine into compliance by the 2018 deadline requested and granted. Subjects: TCMA (All) 1 user liked this post. |
OldnGrounded
2025-06-17T02:42:00 permalink Post: 11903927 |
[. . .] In this regard we can recall several instances of double engine failure associated with bird strikes generally involving large birds or large flocks or both. But it seems we have discounted this theory very early in discussion. Why? Because we cant see any birds, or flocks of birds or engine flames/surges or puffs of smokes from the engines which would support this. Really?
[. . .] Edit: I might add, they would have found remains on the runway if this did indeed happen. But we have heard anything from anybody?
The Indian authorities indicated that a bird strike has been ruled out.
Subjects: Bird Strike Dual Engine Failure Engine Failure (All) 2 users liked this post. |
OldnGrounded
2025-06-17T03:02:00 permalink Post: 11903932 |
Back to the subject of the TCMA, in order for the four channels (A and B for engine 1 and A and B for engine 2) to be truly independent, there would have to be, for example, four, separate weight on wheels sensors and two, separate throttle position sensors per throttle. I would be extraordinarily surprised if that's what has been implemented, but will happily stand correct.
Subjects: TCMA (All) Weight on Wheels 2 users liked this post. |
OldnGrounded
2025-06-17T03:34:00 permalink Post: 11903943 |
Thanks. Do we know that these are monitored by TCMA for air/ground state and if so, do we know the logic used to make a determination based on those inputs? Alternatively, do you know where we should be looking for those answers?
Subjects: MLG Tilt TCMA (Air-ground Logic) TCMA (All) 2 users liked this post. |
OldnGrounded
2025-06-17T04:05:00 permalink Post: 11903952 |
Last edited by OldnGrounded; 17th Jun 2025 at 05:06 . Subjects: FAA MEL TCMA (All) |
OldnGrounded
2025-06-17T05:03:00 permalink Post: 11903972 |
Subjects: TCMA (All) |