> >
On Mar 15, 2014, at 7:51 AM, Rogelio Serrano wrote: > .015 in Stainless seem to be the only option... On Mar 15, 2014, at 7:39 AM, John Bouyea wrote: > Thanks for digging up the reference Ken! I'll see what I can do. > > Right off the bat, the existing plans method for constructing our aircraft > with .005 stainless doesn't meet Part 23 requirements in any regard... =-=-=-=-=-=-=-=-=-==-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-= John/Rogelio, IF certifying under FAR 23, and using other than the listed materials, then the fire test is required. Who knows? Perhaps .005" stainless over Fiberfrax is better than .015 stainless. Ken > ?23.1191 > (h) THE FOLLOWING MATERIALS MAY BE USED in firewalls or shrouds "WITHOUT > BEING TESTED" as required by this section: -------------------------------------------------------- ------------------------------------- > (1) Stainless steel sheet, 0.015 inch thick. > (2) Mild steel sheet (coated with aluminum or otherwise protected against > corrosion) 0.018 inch thick. > (3) Terne plate, 0.018 inch thick. > (4) Monel metal, 0.018 inch thick. > (5) Steel or copper base alloy firewall fittings. > (6) Titanium sheet, 0.016 inch thick.