Re: FAA Airworthiness Concern Sheet
I have noticed on some planes the fittings were pretty much covered over with fabric and the metal parts that were exposed were just sprayed with the dope-silver-and paint with the fabric. The dope doesnt stick to the metal parts very long and becomes loose-cracks and can be fkaked off with a pocket knife and sometimes there is rust there. The way I prevent this is to scuff the epoxy primer and paint the fittings,lift handles, step supports, etc. with Aerothane(I use Poly Fiber) before I cover the fuselage,When covering I glue the fabric around the outside the of the fittings making sure that it is completly glued down flat. Then mask off the fittings etc. when I start applying the fabric dope. This way the paint wont peel off and leaves a nice clean surface.Ifaplanewas covered and they had used the fabric materials over the fittings you could just remove the gunk on the fittings-trim the fabric around the fitting and check and clean the fitting and re-prime@ paint the fittings-make a patch as per the covering manuel-mask off the fittings and blend in the patch.By the way Aerothane is an excellent Urethane paint for this-very similar to emron..itis very durable and almost no chemicals will soften it. I clean it sometimes with paint thinner and it doesnt hurt it. Hope this helps
Buell
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Fuselage strut fitting - FAA Airworthiness Concern Sheet (merged)
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Re: FAA Airworthiness Concern Sheet
A Taylorcraft on floats sits quite tail low compared to many other floatplanes.....The tail is still the low point on my plane.....(which obviously is on floats)
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Re: FAA Airworthiness Concern Sheet
IMHO, this should only affect seaplanes. The fitting on a seaplane becomes the lowest point where moisture runs to. I have never seen this as a problem on non float equipped aircraft. They will rot at the tail. I have fixed my fair share of fuselages of all makes and models. The only time I have ever ran into the issue of rot arounf that area was on a Tri-Pacer. The carry thru tube betwwen the attachpoints had rot and had to be repalced.
Mike
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Re: FAA Airworthiness Concern Sheet
Forrest, do you have any knowledge or recollection of the number of Taylorcrafts that suffered strut or strut attch failures? Is the Wiley crash the first one ever, or the fifth???
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Re: FAA Airworthiness Concern Sheet
This morning I posted a suggestion on another thread that may well help address this new Airworthiness Concern in the future. Perhaps Forrest can promote this idea to the FAA engineer if he deems it a good idea:
A relatively simple part, combination of access plate and protective fairing, could make it a lot easier to inspect for existing corrosion and help prevent corrosion in the future.
In addition to allowing full 360 degree inspection access, it would also serve to not trap water next to the fitting, and (if properly sealed to the rabric and struts) it would help prevent water/mud splashing o nto the lower strut attach area.
I'll let Rob determine whether to merge that thread into this one... "mergers and acquisitions" seem to be in fashion nowdays
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Re: FAA Airworthiness Concern Sheet
I don't need praise just patience....... THE DAMN fuselage fitting pulled off the fuselage, IT WAS a RUSTY PIECE OF CRAP.
I will try for the photos tomorrow. We have a two fold thing here, inspect the struts , inspect the attach fitting area. One is now an AD , the other will likely be a SB IMHO.
As to the notifications , YES the FAA sends AD's to owners by regular mail, sometimes they get it before the IA's do. In my case I got it by my AD service within hrs of the issuance. I use ATP-NAV.
The FAA engineer felt this discussion group was the quickest way to get it to owners, I explained to him that only 30% of the registered owners belong to the Type Club or Foundation.
It has always been a problem. faa.gov gets me a lot of info...
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Re: FAA Airworthiness Concern Sheet
Well done, Forrest. You're a Star!
To be fair, there was an FAA Airworthiness Concern notice went out on struts before the Strut Ad was formally issued.:rolleyes2:Originally posted by cpirrmannGood job! This is more like what we should be seeing
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Re: FAA Airworthiness Concern Sheet
Was it the strut that failed or the Fuselage? Tim
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Re: FAA Airworthiness Concern Sheet
Good job! This is more like what we should be seeing. ThanksOriginally posted by Forrest Barber View PostFAA engineer Andrew McAnaul has asked that I get this out to our members ASAP. Here it is for you to return comments. The NTSB is still investigating there is a lot of information and we need more. Comment on this thread is good too! I think I did it... Rob & Robert would be proud of me.
Off for a Flight Review.
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Fuselage strut fitting - FAA Airworthiness Concern Sheet (merged)
FAA engineer Andrew McAnaul has asked that I get this out to our members ASAP. Here it is for you to return comments. The NTSB is still investigating there is a lot of information and we need more. Comment on this thread is good too! I think I did it... Rob & Robert would be proud of me.
Off for a Flight Review.
Service Letter102 (Taylorcraft factory)Attached FilesTags: None
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