Return-Path: Received: from interlock.halnet.com ([206.61.34.3]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with SMTP id AAA2006 for ; Tue, 6 Oct 1998 08:36:33 -0400 Received: by interlock.halnet.com id HAA22346 (InterLock SMTP Gateway 3.0 for lancair.list@olsusa.com); Tue, 6 Oct 1998 07:36:25 -0500 Received: by interlock.halnet.com (Internal Mail Agent-1); Tue, 6 Oct 1998 07:36:25 -0500 Message-Id: <43AEA19B4857D111B57600805F193CE2020CEFA4@LONEXCH002> From: Michael Holland To: "'lancair.list@olsusa.com'" Cc: "'jenspeter@get2net.dk'" Subject: First Flight G-PJMT Date: Tue, 6 Oct 1998 13:35:42 +0100 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Folks, Just to let you know that Lancair 320 G-PJMT made its maiden flight from Exeter Airport, England on 27th September 1998 with Don Goetz in command. Between the 27th and 30th September we put over 5 hours on her including 15 landings and a flight of over 2 hours duration. This was a requirement of our PFA ( equivalent of the EAA ) prior to considering an application for a full permit. Our CAA ( FAA) test pilot also wished to check it out during this period and he gave it a clean bill of health. Don believes she is a good example of the model and was complimentary of its handling characteristics, speed, and comparatively low noise and vibration levels for this type. As you can see from the weight she is not light and soundproofing, 2 AP servos plus a wiring system to allow HOTAS electric's operation from both sides but not simultaneously all added to this. However, at gross weight and 2450 x 25" we were still seeing about 185 knots. G-MT was an original FB Kit number 263 and was delivered in October 1992. Work started on November 1st 1992 after we had extended our garage to allow us to fit both wings on at once. Subsequent extensions were made later in the project to allow the engine to be mounted and the forward hinging canopy to open up. Along the way we were informed by our PFA that we would have to fit the Mk II tail and we traded our original for the first series slow build carbon fibre version. Some details are as follows. Empty Weight: 1219 lbs. Engine: IO 320 D1B Propeller: MT 6V Constant Speed Hotas Grips: Operating Flaps, Aileron and elevator trims, PTT, Altitude hold and A/P disconnect Avionics: Narco Mk 12D Navcom with DME readout in GS/Localiser Dial Narco DME Skyforce GPS and moving map S-Tec Model 50 Autopilot VM 1000 Engine Management and fuel/temp gauges Anyone building in or visiting UK are welcome to view at Exeter and discuss any issues regarding their projects with myself or my Father who was the real builder of G-MT. Appreciate the contributions and advice on some of the later issues we encountered through this forum. Will continue to monitor and post any useful contributions we might have as we build on our hours. Regards, Michael Holland........