It's called pencil whipped annuals.He dumped the hopper… then BOTH wings came off? He didn’t even pull up that hard. Something else happened here.
He dumped the hopper… then BOTH wings came off? He didn’t even pull up that hard. Something else happened here.
Same for a PBY4-2 about same time frame.....There was a C-130 20 or so years ago that did the exact same thing. Although the outcome was not as favorable as this one.
Same for a PBY4-2 about same time frame.....
I guess only the logbooks went to the mechanic, not the plane.It's called pencil whipped annuals.
I don't use any streaming services other than youtube or Netflix and I've never seen this movie (obviously I don't have kids). Where might one find these movies online?
My man, let me introduce you to a slippery slope of sloth via justwatch.comI don't use any streaming services other than youtube or Netflix and I've never seen this movie (obviously I don't have kids). Where might one find these movies online?
20 years as a Flight Engineer. F/R/T models.That was a C-130A that started life with Aeroproduct three blade props that didn't have a synchrophaser function. There was a harmonic resonance issue with them that wasn't understood for a while. I doubt many here have ever seen a three blade Electra/P-3 or C-130. That's why they went to a four blade Hamilton Standard prop with a synchrophaser, it kept the RPM synched but it also matched the props angle. Seeing one completely out of phase in flight is pretty rare, and apparently it worked. I might've worked on some of that stuff.
Weakened spar. These photos were shared on the Facebook group with the original video.
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To my slightly trained eye, it looks like a fatigue failure of the built up aluminum extrusions surrounding the wing attach bolt. The “tree rings” are a sign of relative displacement of the metal. The fatigue crack probably originated at the edge of that bolt hole (where the stress concentration factor is the highest) and worked it’s way through the metal over many years. There’s also corrosion on the bolt and in the hole which certainly wasn’t helping matters.
This is a somewhat similar failure mode to the Embry-Riddle Piper Arrow, though different spar design. The AD resulting from that accident forces the removal of the wing attach bolts and inspecting the spar cap bolt holes with an eddy-current machine. Eddy current likely would have found this crack as well.
Aluminum has a finite life. Every flight is a cycle. You only get so many cycles / hours before you have to replace parts and start over.