X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml Date: Fri, 11 Aug 2006 20:21:12 -0400 Message-ID: X-Original-Return-Path: Received: from [70.62.14.124] (HELO server1.USTEK) by logan.com (CommuniGate Pro SMTP 5.1c.2) with ESMTP id 1318278 for lml@lancaironline.net; Fri, 11 Aug 2006 10:11:23 -0400 Received-SPF: none receiver=logan.com; client-ip=70.62.14.124; envelope-from=lancair@USTEK.COM Subject: RE: [LML] Re: Wing Twist and EI observations MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----_=_NextPart_001_01C6BD50.23007F0A" Content-class: urn:content-classes:message X-Original-Date: Fri, 11 Aug 2006 10:12:10 -0400 X-MimeOLE: Produced By Microsoft Exchange V6.5 X-Original-Message-ID: X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: [LML] Re: Wing Twist and EI observations Thread-Index: Aca8qN8q5rShSUAbR4yigOcscFsIrgApM/57 References: From: "Lancair" X-Original-To: "Lancair Mailing List" This is a multi-part message in MIME format. ------_=_NextPart_001_01C6BD50.23007F0A Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Scott, =20 I have the Cont TSIO550 with LightSpeed, so is most of what you wrote = applicable? Seems like it, except I believe that Klaus does not have a = rear crank pickup for my engine. As it is, I have his circuit board in = the front end where it is oh so close to the AC pully system and the = yet-to-be- de-iced prop. The Simpsons vary widely: at idle (Chelton = says 1050 rmp) the LSE readout varies from 650 to 1000. I have three of = the units in the panel so I do not have to switch from one to the other = - there is always a display of firing angle, RPM, and MP. I get to = watch all three dance at the same time.=20 =20 Still working on a very low oil pressure problem. Pressure tested the = gauge and it is correct. Startup is 45-50 psi, idle at 1,000 shows 40 = psi at 110 F, 35 at 120 F, 30 at 130 F, 25 at 140 F. In cruise it = stays at about 22 psi and 185-190 F. On landing and pulled back to idle = pressure dromps quickly to 5 psi and if I do not goose it quickly, down = to 2 psi! To get back to the hanger or for another TO I have to keep = the RPM at 1,000 and ride the brakes. =20 =20 I screwed the pressure controller all the way in and got no change. I = pulled it and gave it the old evil-eye (no obstruction seen), put it = back, and no change. Ron Munson at Performance said that they had no = problems on testing so it leaves me scratching my head. Today we'll = pull the aux oil pump out of the system, cap the ends, and see what = happens. =20 =20 Robert M. Simon ES-P N301ES =20 ________________________________ From: Lancair Mailing List on behalf of Sky2high@aol.com Sent: Thu 8/10/2006 2:13 PM To: Lancair Mailing List Subject: [LML] Re: Wing Twist and EI observations In a message dated 8/10/2006 11:57:25 A.M. Central Standard Time, = lancair@USTEK.COM writes: =09 I am still flying off hours and playing at low altitudes, but running = way lean of peak at 12k ft I am burning 15.5 gph and seeing about 205 kt = TAS. These investigation hours are a mix of fun and frustration. The = EI readouts are all over the map and do not agree with the RPM and MAP = displayed on the Grand Rapids EIS. If the firing angle readout is = correct we are at 40 degrees on take off, 32 degrees when cruising ROP = but that drops off as we go LOP - and that seems strange. Could anyone = enlighten me on this?=20 Robert, =20 You are using Light Speed EI, right? And a Lycoming engine, right? If = it is a Continental engine or not LSE, ignore most of this e-mail. =20 Otherwise, remember that the timing is tied to power as represented by = RPM and MAP. At idle (lo MAP, lo RPM), the timing would be quite = advanced (35-38 DBTDC). At takeoff power (hi MAP, hi RPM), timing = advance is minimal, i.e. 25 DBTDC. As power declines by an increase in = altitude (lower MAP) and cruise RPM (2300-2500), the advance should = increase towards 35 or so DBTDC. If running LOP causes a reduction in = RPM or MAP, the advance should increase a bit further. Reduce all the = timing numbers by 5 degrees if the compression ratio (CR) is greater = than 8.7:1. =20 If mag hole timing sensors are being used along with a hi CR, the = sensors are offset and the indicator readouts are 5 degrees higher than = actual. However, if a big engine (6-cyl, >200 HP) is being used, the = very accurate crank sensor should be installed. Once again, if a hi CR, = the sensor magnets imbedded in the flywheel are offset by 5 degrees and = the timing indications are accurately reported.=20 =20 In my airplane, the MAP and RPM are low by .5" and 60, respectively as = against those displayed by VM instrumentation. There is no damping of = the display so the numbers can jump around quite a bit. =20 Finally, if the above doesn't explain what you are seeing, re-check the = actual timing with a timing light. If that is good, check the wiring and = connections. The display is a Simpson volt meter showing hundredths of = volts. The selector switch not only connects the appropriate source, = but adjusts the display decimal point location. =20 Good Luck, =20 Scott Krueger AKA Grayhawk Lancair N92EX IO320 SB 89/96 Aurora, IL (KARR) Abnegate Exigencies! ------_=_NextPart_001_01C6BD50.23007F0A Content-Type: application/ms-tnef; name="winmail.dat" Content-Transfer-Encoding: base64 eJ8+IgsOAQaQCAAEAAAAAAABAAEAAQeQBgAIAAAA5AQAAAAAAADoAAEIgAcAGAAAAElQTS5NaWNy b3NvZnQgTWFpbC5Ob3RlADEIAQ2ABAACAAAAAgACAAEEgAEALQAAAFJFOiBbTE1MXSBSZTogV2lu ZyBUd2lzdCBhbmQgRUkgb2JzZXJ2YXRpb25zAM8OAQWAAwAOAAAA1gcIAAsACgAMAAoABQAVAQEg gAMADgAAANYHCAALAAoADAAKAAUAFQEBCYABACEAAAAyRkFDOEUyODNCMTUxMTRGOUJBREM3RDEx Q0JDNjFFNgBkBwEDkAYARBwAADgAAAADADYAAAAAAEAAOQAKfwAjUL3GAR4APQABAAAABQAAAFJF OiAAAAAAAgFHAAEAAAAsAAAAYz1VUzthPSA7cD1VU1RFSztsPVNFUlZFUjEtMDYwODExMTQxMjEw Wi00MgAeAEkAAQAAACkAAABbTE1MXSBSZTogV2luZyBUd2lzdCBhbmQgRUkgb2JzZXJ2YXRpb25z AAAAAEAATgCAVXyjqLzGAR4AWgABAAAAFQAAAExhbmNhaXIgTWFpbGluZyBMaXN0AAAAAAIBWwAB 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