Bob Turner
Well-known member
- Joined
- Apr 4, 2018
- Messages
- 3,998
On that inexpensive Decathlon I posted a while back - the shop spotted corrosion on the leading edges under the fabric, freaked out, and towed the aircraft back to its parking spot.
I found, through a friend, ACA service bulletin 449, which discusses inadequate corrosion prevention coatings on early metal spar wings, and allows quite a bit of leading edge corrosion. They allow 50% of the linear dimension of the leading edge to be speckled with bumps below .030” high. They allow counting only bumps above .010”, so it is fairly liberal.
You can measure bumps quite accurately with a feeler gauge and a short straightedge. Our aircraft came in at 46%, counting all bumpy areas, so we passed. But none of the shops would touch it - service bulletin or no. (one wing 46%; the other at 10%)
Having rebuilt lots of aluminum/fabric wings, leading edge corrosion really doesn’t bother me - except that, at least with Cub wings, it takes decades to have corrosion take over, and usually it happens because of improper storage. So I am doing the inspection myself. What you do not want, obviously, and what ACA addresses, is a "cave-in" or structural failure. Apparently, ACA has investigated, found lots of these problems, and given us guidelines.
Inside the wing there are lots of little areas of extremely light surface corrosion. No pits at all, just little white rings. Nothing to get excited about, except it leads me to believe ACA used the wrong alloy. The spars in these wings are coated with a green substance that looks like epoxy primer, and are pristine.
I found, through a friend, ACA service bulletin 449, which discusses inadequate corrosion prevention coatings on early metal spar wings, and allows quite a bit of leading edge corrosion. They allow 50% of the linear dimension of the leading edge to be speckled with bumps below .030” high. They allow counting only bumps above .010”, so it is fairly liberal.
You can measure bumps quite accurately with a feeler gauge and a short straightedge. Our aircraft came in at 46%, counting all bumpy areas, so we passed. But none of the shops would touch it - service bulletin or no. (one wing 46%; the other at 10%)
Having rebuilt lots of aluminum/fabric wings, leading edge corrosion really doesn’t bother me - except that, at least with Cub wings, it takes decades to have corrosion take over, and usually it happens because of improper storage. So I am doing the inspection myself. What you do not want, obviously, and what ACA addresses, is a "cave-in" or structural failure. Apparently, ACA has investigated, found lots of these problems, and given us guidelines.
Inside the wing there are lots of little areas of extremely light surface corrosion. No pits at all, just little white rings. Nothing to get excited about, except it leads me to believe ACA used the wrong alloy. The spars in these wings are coated with a green substance that looks like epoxy primer, and are pristine.
Last edited: