I am the culprit. A coworker who is a member on this forum sent this thread to me.
This aircraft suffered a bird strike. The aircraft had an air interupt and proceeded to land at Austin TX. if I recall. This was about 10 years ago. I have no idea what kind of bird, it was dead and smelly. The airline parked the aircraft at the old TWA air cargo ramp on the other side of the field.
When my crew arrived that afternoon we were dumped off at that remote spot and left. We were told not to leave the aircraft and they would check on us from time to time and gave us a radio to contact them on. The company gave us instructions to do a temporary repair so they could move the aircraft to a repair facility. We showed up with tools and materials to do just that. For some reason I also threw some titanium sheet in the box of materials I took along. The damage was that the skin under the patch was lifted up into a scoop shape. The bird had depressed the skin forward of the patch, sheared the rivets in the lap and pulled the skin up. I bet it made a **** of a racket.
By 6pm the radio died. We no longer had contact with the guys at the terminal. Then shift change came and we were forgotten. We had a cordless drill, and some cherry max rivets and some metal. I had brought all the technical data and we had an inspector with us. The skin panel that was damaged was either chem milled, or had a bonded doubler so the panel was pretty thick. In most areas on the 80 the skin is a minimum of .050" thick, and add the chem mill or bonded doubler and it gets thick really quick. I did not have any aluminum with me that would have been thick enough to do a straight normal type srm repair. But if you considered using a material substitution chart and the srm for temporary repairs I did have the parts to do a decent enough job to put the aircraft back into revenue service. So, we took our box of band aides, titanium and our cordless tools and went to work. At about 4 AM we finished putting that repair on by flashlight. Since they forgot about us and we had the time and materials to do a repair to return the aircraft to service that is what we did.
The repair has no chamfer because the titanium is much thinner than the aluminum it replaced. There are two sheets because of the thickness at the lap.
The repair is still on the aircraft because the damage is right over top of the EPC panel which is the main electrical panel for the entire aircraft and it would have to be removed to do the kind of repair that you would normally see. It is just not cost effective to do.
My crew flew with the line crew to DFW where the aircraft was returned to service, the PR-1422 we sealed the patch with streaked all over the place by the time we landed. It was since then resealed, although that is sloppy as well.
So, while it is not pretty it is an airworthy repair and it has been inspected over and over again. That aircraft will go to the bone yard with that repair still attached. That repair does have additional inspection requirements.
Sometimes you just have to do what you can.
Ray