AC43-13-1b says "Install drain grommets on the underside of all components, at the lowest point in each fabric panel, when the aircraft is in stored
attitude"
Researching wing grommet placement here I find that the recommended inspection procedure says "open drain grommets at each rib bay trailing edge".
My BC12-D was restored by a well respected professional and he put holes along the very trailing edge of wings and ailerons.
The IA I asked to do this year's annual says this compromises the integrity of the wing and wants to involve a DER. He interprets that grommets must be in the fabric before the trailing edge aluminum.
I like what I have but am willing to put additional seaplane grommets in. I'm curious of other's opinions on this and what you have on your plane. An additional question - because of dihedral would underwing grommets go in at the inboard point of each rib bay to be most effective? My plane has seen very little moisture so I discount any chance of corrosion in my trailing edge aluminum.
Thanks tribe.
attitude"
Researching wing grommet placement here I find that the recommended inspection procedure says "open drain grommets at each rib bay trailing edge".
My BC12-D was restored by a well respected professional and he put holes along the very trailing edge of wings and ailerons.
The IA I asked to do this year's annual says this compromises the integrity of the wing and wants to involve a DER. He interprets that grommets must be in the fabric before the trailing edge aluminum.
I like what I have but am willing to put additional seaplane grommets in. I'm curious of other's opinions on this and what you have on your plane. An additional question - because of dihedral would underwing grommets go in at the inboard point of each rib bay to be most effective? My plane has seen very little moisture so I discount any chance of corrosion in my trailing edge aluminum.
Thanks tribe.
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