Though a mid-air explosion would be a scenario that fits the most of the circumstances that we know about now, I have a few issues with that article.
Fundamentally, if the fuselage skin over the SATCOM area cracked
and ruptured over such a small area, I believe it would cause rapid decompression, but shouldn't be violent enough for a plane to blow up (See the Southwest 737 Classics).
As I've said before in a previous posts. Fuselages are designed to arrest crack growth in order to prevent complete loss of structural integrity in an emergency situation. Yes, there are certain areas of the fuselage that are more dangerous to have fatigue cracks that rapture than others due to the loads involved over the area (ie. in the forward or aft pressure bulkheads, or in the wing-body join area), but where the SATCOM antenna is, up top in the constant contour section of the fuselage, is one of the least dangerous. These are probably some of the least stressed areas of the fuselage, and you want it to fail there if it ever fails, as that poses the minimal risk to the aircraft's structural integrity.
In any rate, the skin, stringers, frames, and other fuselage structures are designed together to limit crack propagation. Once a crack is found, once a doubler plate is properly installed, then you're good to go.
At the end of the service life of a commercial airplane, you have no idea the number of doublers and triplers that are installed all over the place, in order to fix cracks that were found.
That's on a main power bus (can't take out the whole bus but can begin a linear fire) and, most importantly, broadcasts the aircraft auto-telemetry. Blowing that out would give you a scenario where you may be able to fly for a distance but you could have serious power and comms issues.
It should still fly for a while, at least long enough time needed to reach South Vietnam and land somewhere. I don't know if the reports of the plane heading out to Malacca Strait are still valid, but if so, they are wayyyy off course for an emergency landing.
Doesn't that have to do with all 777 being warned of the same issue that was suppose to go into affect next month
It's most of the 777 models, but it looks like this doesn't include the 200ER (the model of the missing plane) or the 2F.
Possibly so. It doesn't seem limited to the SATCOM link if
this is the directive in question, it refers to potential weakness in panels that have had "scribe lines" applied, etchings that guide painting/decaling of the aircraft.
I'm not an aircraft painter, maybe someone is and they can help us out with the detail
EDIT: Like so many other things about this that I still don't quite understand... given that this directive is in plane sight (hurr hurr) on the FAA site, the papers in most countries are aware of it... why isn't it more of an issue on the wider news in general? Maybe it's a liability thing, Boeing would sue their asses if it turned out to be a hijacking but they'd cast aspersions on the design?
It's only in areas of lap joints, butt joints and cargo door hinges. This directive doesn't look like it applies to the acreage of the skin panels themselves. I'm pretty sure there's no lap joints on the top of the 777 fuselage where the SATCOM would sit, and so this directive wouldn't apply to that area.
I'm not sure how the painting process would cause a scribe line anyways. I've seen planes being painted and I can't think of anything in the process that would cause a scribe line in those specific areas. Generally (at least from the factory), a few base coats are applied, and then the actual decals and liveries are applied over the base coat. The base coat should protect the aluminum from scribed or etched lines, and I just don't see the minimal bump from another coat of paint from a livery foreground be any sort of significant stress concentrator.
Also,
here's an article that I think helps clarify the directive.