When I got my L3, there was a fishmouth external splice at the upper left rear longeron. I assumed it was a nicely done repair. Then I noticed it was on the actual fuselage frame drawings! And the only other L3 I have seen close up had the same splice. This is curious - anyone have any idea why this was done? If a design weakness was discovered and remedied, surely the drawings would have been changed. And a weakness would be more like an undersize tube that would be changed to a larger size, not a reinforced joint. I know enough about aircraft design and stress analysis to make this baffling to me, since I can't think of a condition that would warrant such a change.
I have seen splices in random places where the factory simply used up left over tubing, but that is different.
Any ideas?
L3 fuselage question
L3 fuselage question
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Re: L3 fuselage question
Does look like very nice welding!
Re: L3 fuselage question
Nice buildup spot for 5 tubes of equal diameter to join.
Doc - 1T8
1943 O-58B NC47185 (43-26975)
1946 7AC NC2241E - "Dearly Departed"
EAA TC #5453 CAF Life #2782
FAA Senior AME #20969
"Leben ohne Reue"
1943 O-58B NC47185 (43-26975)
1946 7AC NC2241E - "Dearly Departed"
EAA TC #5453 CAF Life #2782
FAA Senior AME #20969
"Leben ohne Reue"