AV8ORJWC
Joined: 13 Jul 2006 Posts: 1149 Location: Aurora, Oregon "Home of VANS"
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Posted: Mon Nov 27, 2006 10:46 am Post subject: 2 Tailcone Questions: F-1012B came unpunched, small tear in |
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Removing the obvious (the visible crack) does not remove the adjacent
induced stress which is yet to propagate. Many who have stop drilled
learn that lesson with time on their airframe after a perceived patch
was signed off. You are only cheating the inevitable. Metal has memory,
it does not forget. You are not going to fool it into long term
submission. We resort to Eddy Current and Ultrasonic more often that
people know with our air carrier aircraft.
The use of polarizing lens while watching the bending, drilling or
cutting of Plexiglas/acrylic panel is a real eye opener if you can
excuse the pun. The stresses can go wild. You can watch with dazzling
amazement at the exact moment just before the crack destroys the final
piece.
Replacing it with one (F-1010)that has not been manipulated or masked is
the "No brainer". You can consider it the Golden Panel too. Dip it in
alodine like Tim did and then tell stories about it in hangars, years
from now.
John Cox
#40600
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