Return-Path: Received: from [207.30.237.27] (account ) by logan.com (CommuniGate Pro WebUser 4.0b7) with HTTP id 1733783 for ; Sun, 15 Sep 2002 12:16:58 -0400 From: "Marvin Kaye" Subject: Re: 320: negative Flaps, current for starting / battery To: lml X-Mailer: CommuniGate Pro Web Mailer v.4.0b7 Date: Sun, 15 Sep 2002 12:16:58 -0400 Message-ID: In-Reply-To: MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Bernhard Saneke" : I just sold my 235 that gave me so much fun and bought a flying 320! On my first flight with the 320 I had a hard landing without any damage but I am in the process to get a solution why it happend. I think that the flaps are the problem as they are adjusted to be in neutral position (trailing edge of the flaps is at same level as fuselage / nomal airfoil contour) if they are in the most upward position! That means that they travel 42 degrees downward. In my opinion and compared to the 235 this is wrong. With the 235 flaps in most upward position ment negative flaps of 7 degrees up, and vice versa that means that downward travel is 35 degrees, which is producing much less drag. In my opinion the down flaps at 42 Degrees produced too much drag and almost destroyed any lift. And that is what happend on my first landing: approaching with about 95 mph I pulled back the throttle and the aircraft stopped flying almost immediately. (It just fell down) Discussing this with the preowner, he states that according to the blueprints the flaps are adjusted correctly, that means that negative flaps means flaps in neutral airfoil position (trailing edge of the flaps is at same level as fuselage) What is the right answer now? In my opinion the wing of the 320 is the same as for the 235. So negative flaps means really negative! (up from neutral) That means that correct down position is 35 degrees from neutral which produces lift and drag (42 degrees down seem so produce only drag, but little to no lift) Second question: the 320 has the battery placed directly behing right seat, which gives the aircraft rear center of gravity positions which makes the aircraft very unstable (there are so many reports about this fact in the internet). I want to move the battery forward of the firewall but have very little space there, so I am afraid to be able to find a battery that fits in there. (most of the room between motor and firewall is occupied by the mufflers that are mandytory in Germany.) My question is: what is the least size for the battery. Is a 32 Ah nattery sufficient? what about 24 Ah? I have an IO 320 engine, full IFR panel and electrical gyros. What is the highest current in ampere the battery has to supply to start the engine? Thanks for your answers! Regards, Bernhard, D-ESTL, Germany