Just out of curiosity - Airplane Guys

The 737 affair... https://www.moonofalabama.org/2024/01/boeings-737-max-is-still-a-mess.html#more

(I have heard tell that the several sub-assemblies are sometimes fitted with the aid of alignment bars and hammers...as the holes don't line up...well, I have never worked on flying machines, but I have seen some really bad stuff on the ground!

I am recalling the Comet jets, which had serious problems of metal fatigue and cracks....though to be fair, Comet went on to a long and safe life-time.

bummer Dude!

Will be interesting to see what happens Next The FAA and Boeing cooperation has been so so at times " Like dogs watching television "
 
I met my wife while we worked at Hughes Aircraft. Years earlier she had met and chatted with him. She worked "Configuration Management". One of those obscure entities that gobble up defense $. As programs advance and designs mature someone has to keep track of the changes. A very obscure but important part of DoD readiness. A -1 Power Supply may work fine in a -7 radar set but a -7 processor may not work in a -1 radar set. When backward or forward interchangability stops there are rule about issuing new part numbers and new part number series.
HH had many lady friends, they say, and when I was 19 I listened to pillow talk about him. She was at that time "49" and well worth knowing. OTT my lips are sealed!
 
The Comet suffered from being first jet airliner. When losses occurred - planes breaking up in the air - the subsequent investigations led to the realisation that the corners of square windows were stress multipliers leading to metal fatigue and catastrophic failure. Solution was oval windows. And of course all later jet airliners from Boing, M-D, et al have oval windows.
My recollection is slightly different, though only in detail... from reading - this is that the rivet holes were punched, not drilled, such that incipient cracks exceeding a critical growth size were thus formed. One of the fix changes (in addition to oval) was to drill the rivet holes. I have punched lots of aluminum and steel and stainless in sheet metal fab...with the observation that punch dies are almost always "non-ideal", as in phuched up. .................. A GE engineer I worked under in the 1980s, over pizza and beers at the completion of a steam turbine overhaul, said that the alloys developed for the recip engine airframes were not fatigue-compatible with the gas turbine vibration spectrum, at least in his days in that department...circa 1950's..so he said. He told some stuff about the bomb, too...which I have kept to myself, but it was interesting. He must be dead by now... Nice guy. I took his stories as sincere, but a with a grain of salt.

(Jimmy collapses the gear!)
 
No doubt you are correct, but a citation would be helpful. I recall the name of the fellow at GE, and I believe I have some sort of published documentation in library... but it has been a long time. So, Jim did you punch the rivet holes, or is that just what somebody said?
 
On second thought, and after a quick look under rubric "comet airliner crack propagation punched holes"
https://www.thinkreliability.com/case_studies/comet-accidents/
https://www.sciencedirect.com/topics/engineering/de-havilland-comets

"In this case, rivet holes that punctured the skin, which were used to attach the aircraft windows, acted as the “flaw” where cracking could begin. Fatigue cracking caused the crack to grow, and there was nothing to stop the crack from propagating,"

I guess my old pal was telling a true... It made sense at the time...
 
No doubt you are correct, but a citation would be helpful.
Kinda hard to cite a negative, no?

Have I ever "punched" rivet holes? Yes I have, but rarely, and only on non-structural type stuff. Interior panels and such... stuff that doesn't affect structural integrity. Wing/fuselage skins... ribs, stringers and formers... all drilled with precision. That was all well understood back in the comets day also.
 
Countersunk holes are precision holes. Depth of the countersink is critical to a smooth skin. Kinda hard to believe they'd "punch" a hole then use precision tooling to countersink it.


Untitled2.png
 
Kinda hard to cite a negative, no?

Have I ever "punched" rivet holes? Yes I have, but rarely, and only on non-structural type stuff. Interior panels and such... stuff that doesn't affect structural integrity. Wing/fuselage skins... ribs, stringers and formers... all drilled with precision. That was all well understood back in the comets day also.
With burnishing.
 
Interesting!:thumbsup: Thanks VFT.
View attachment 259602


That needle nose put me in mind of the Douglas X-3, first flight October 20, 1952 and featured in an old 1955 Eagle Book of Modern Wonders I've had since I were a kid.

Douglas_X-3_NASA_E-1546.jpg


I know, the resemblance is only superficial, some people eh?
 
1950s aerospace - throw more power at it, it'll work.
Nine year old me was so impressed by that X-3. I mean, WOW.

But looking at Wikipedia, it seems the thing was designed as a Mach 2 plane but never able to achieve Mach 1 in level flight, due to the specified power unit not being available, so they fitted much lower thrust engine instead. But apparently, it gave useful data used later for the Starfighter?
 
Last edited:
Back
Top