Since you're down there and you probably got the manual out of that Seminole there that's up for sale, see if the guy is interested in trading that project for my 1960 Mercury Panel truck. Last time I checked with a body man in the States he told me not to touch a thing as it is all original and numbers all match. Fewer than 150 ever built in that last year of production for the panel truck. Told me it was worth well over 50k as is. Doug Rupert
-----Original Message----- From: krnet-bounces+drupert=sympatico...@mylist.net [mailto:krnet-bounces+drupert=sympatico...@mylist.net] On Behalf Of Colin & Bev Rainey Sent: Saturday, September 25, 2004 3:59 PM To: KRnet Subject: KR> Seminole John Pickup a Piper Seminole Operating Manual and you will find that max operating G loading is 3.8 positive flaps up & 2.0 positive flaps down and 0 negative. Section 2 in the Limitations Section. All certified aircraft have them published there. If you go over the published weights you then do what Steve Jacobs illustrated and calculate the new limitations, AND then expect to test for ALL new speeds due to the changes that will occur to them due to the higher weight. Colin & Bev Rainey KR2(td) N96TA Sanford, FL crain...@cfl.rr.com http://kr-builder.org/Colin/index.html _______________________________________ to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net please see other KRnet info at http://www.krnet.org/info.html
