Re: Engine upgrade
I owned a BC-12D with a non-electric 85 "bolted on". I have no idea how the annuals were signed off, because I never found a 337 or STC in the paperwork. To be honest, I had it annualled that way and just kept my mouth shut, and the IA didn't say anything either. He probably (mistakenly) assumed that an 85 was on the type certificate so that was that.
However I also realize this was probably not exactly up to FAA paperwork standards under the current rules.
As with probably everyone else here, I strongly support the Foundation making an argument for, and applying for a blanket approval, to bolt on an 85 non-electric with the minimum changes and no weight increase. This would allow Mr. Harer to still have a valid, valuable product to sell for the increased weight and avionics capability, but also allow people to get more power without tearing apart the entire front end of the airplane and requiring a new mount and cowl. The Foundation can also offer the FAA that it will bring a lot of "bootleg and barnyard" installations into conformity and thus offer an increase in safety. Perhaps the approval could be written so that existing installations must be inspected and signed off by an IA to conform before being approved under this new arrangement.
I support this type of proposal since it would make sense to the FAA, increase safety, and allow an improvement in aircraft performance without any big downside. AS LONG as the new approval also covers my pre-war Taylorcraft!!!!!!!!
Bill Berle
I owned a BC-12D with a non-electric 85 "bolted on". I have no idea how the annuals were signed off, because I never found a 337 or STC in the paperwork. To be honest, I had it annualled that way and just kept my mouth shut, and the IA didn't say anything either. He probably (mistakenly) assumed that an 85 was on the type certificate so that was that.
However I also realize this was probably not exactly up to FAA paperwork standards under the current rules.
As with probably everyone else here, I strongly support the Foundation making an argument for, and applying for a blanket approval, to bolt on an 85 non-electric with the minimum changes and no weight increase. This would allow Mr. Harer to still have a valid, valuable product to sell for the increased weight and avionics capability, but also allow people to get more power without tearing apart the entire front end of the airplane and requiring a new mount and cowl. The Foundation can also offer the FAA that it will bring a lot of "bootleg and barnyard" installations into conformity and thus offer an increase in safety. Perhaps the approval could be written so that existing installations must be inspected and signed off by an IA to conform before being approved under this new arrangement.
I support this type of proposal since it would make sense to the FAA, increase safety, and allow an improvement in aircraft performance without any big downside. AS LONG as the new approval also covers my pre-war Taylorcraft!!!!!!!!
Bill Berle
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