jpw
Active Member
I need some help with an issue discovered on a prebuy on an RV-4.
Have detected two large wrinkles with breaks in the firewall/footwell area of the plane.
It appears the previous owner( deceased natural causes) did indeed groundloop the plane.
He repaired and covered over the damage with insulating foam.
The gear and fudelage appear straight and the only manifestation of the accident
is in the area about 5 inches above the lowest point of the footwells-firewall
on either side. The motor mount attach point folded the stainless in about 2 inches. When attempting to repair the stainless cracked about 1-2 inches .
Question , even if it appears stupid is; How critical is this area to the structural
integrity of the craft? My sense is that it should be replaced completely.
The area where the longitudinal frame connects to the firewall is undamaged
and the motor mount is not damaged although it looks like it was welded to
repair some hairline cracks.
Thanks for the help.
JPW
Have detected two large wrinkles with breaks in the firewall/footwell area of the plane.
It appears the previous owner( deceased natural causes) did indeed groundloop the plane.
He repaired and covered over the damage with insulating foam.
The gear and fudelage appear straight and the only manifestation of the accident
is in the area about 5 inches above the lowest point of the footwells-firewall
on either side. The motor mount attach point folded the stainless in about 2 inches. When attempting to repair the stainless cracked about 1-2 inches .
Question , even if it appears stupid is; How critical is this area to the structural
integrity of the craft? My sense is that it should be replaced completely.
The area where the longitudinal frame connects to the firewall is undamaged
and the motor mount is not damaged although it looks like it was welded to
repair some hairline cracks.
Thanks for the help.
JPW