X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 03 Apr 2010 20:03:42 -0400 Message-ID: X-Original-Return-Path: Received: from web112115.mail.gq1.yahoo.com ([67.195.22.93] verified) by logan.com (CommuniGate Pro SMTP 5.3.5) with SMTP id 4193693 for lml@lancaironline.net; Fri, 02 Apr 2010 15:58:47 -0400 Received-SPF: none receiver=logan.com; client-ip=67.195.22.93; envelope-from=starliteaviation@yahoo.com Received: (qmail 66765 invoked by uid 60001); 2 Apr 2010 19:58:12 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=Message-ID:X-YMail-OSG:Received:X-Mailer:Date:From:Subject:To:MIME-Version:Content-Type; b=Pc29nr3tn/REHuPeBiCu8bL4IvBtXfNLVHSxXk8diUpP2Ealp4nZvDU14OLI0AMFNI9KaZBiuPn+4RhKjXH10D2kU8eMKClvMK3dl9T1KQZcw/4vNQFkJKCJ4xJ1oBsmTNRM/R9VUWQTxL/iLj+/RQqOtiwMBvjoMHcSVurbBLs=; X-Original-Message-ID: <689661.65370.qm@web112115.mail.gq1.yahoo.com> X-YMail-OSG: Zqwb0ncVM1n.0XEzMQrQVeDhAHniY8yUcMXdU.ienPE1CyB xxj7EzzxEyOxXq2V8q._Dvac5.auKthp5A61Pr3SHSnnQNczzUKsD0IBgtKQ CPh5M9X1h8SbHD2HZ769EHQSDaksCfCx_V4aA1Grs2ifIepbYYakCxQKRyph DT0V0olpphgOM98Fjv2sgCJNFz6uVptcZ1ykkMAI_cE6R3jTIna_oDINMouJ g36tWaaubGc0cSp2bHpNWKzx2COC3Nv_k5ZS3_Zi7CITzbIHVuR0ryFeb6mc N_APQlapSTv66QFpceNNgm3k- Received: from [76.178.110.123] by web112115.mail.gq1.yahoo.com via HTTP; Fri, 02 Apr 2010 12:58:12 PDT X-Mailer: YahooMailClassic/10.0.8 YahooMailWebService/0.8.100.260964 X-Original-Date: Fri, 2 Apr 2010 12:58:12 -0700 (PDT) From: Chris Alberti Subject: 4P Air Conditioning X-Original-To: Lancair Mailing List MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-1690357359-1270238292=:65370" --0-1690357359-1270238292=:65370 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable The unit with the P51 style scoop has been installed on our Glasair 3 here = in Yuma, AZ. for over 2 years and has never failed=A0to deliver. We fly thi= s aircraft over 130 hours a year and because of the AC we can fly any day i= n the summer. This was the prototype for all Glasair's since the manufactur= er=A0had never sold=A0one anywhere else. Before the install, we did our fli= ght test and recorded our power, altitude, temperature, and speed settings = etc. After the install we ran the same test and found the no noticeable dif= ference in speed.=A0We thought=A0there had to be some loss of speed but we = really couldn't find any. A Lancair Legacy installed the same system and al= so found no measurable loss in airspeed. Because these aircraft are similar= in speed, roughly 220 knots, we wondered if the the loss isn't measurable = until you get to greater airspeed's.=20 =A0 We bought a 4P with the same system already installed because of the except= ional performance of this system and it cruises just as fast as the one wit= hout the system. I have heard owners of 4P's say they have noticed 2 to 6 k= nots of loss in airspeed but have never heard of anyone losing 10 to 20 kno= ts or more.=20 =A0 Our suggestion is to do your own flight test with your airplane since no tw= o 4P's are the same and all are prototypes. Also, you didn't mention your p= ower, altitude, temp,=A0airspeed's, and the way you fly your particular air= craft so it is hard to determine what kind of cruise speed you are indicati= ng.=20 =A0 One last thought. If you really think you are at a big loss in airspeed my = suggestion is to take the scoop off and see what the difference really is. = This way you will have an apples to apples comparison before you invest the= time and money into a new system. Also, be aware of cutting holes into the= bottom of the fuselage since this may decrease the structural strength of = the airframe. Fly Safe,=20 Christopher J. Alberti=20 President/CEO=20 Starlite Aviation Technologies LLC=20 1963 S. 39th Drive=20 Yuma, Arizona 85364=20 Phone: 928-581-2383=20 Fax: 928-329-6488=20 Email: starliteaviation@yahoo.com=20 Web Site: www.starliteat.com This message contains confidential information only for the use of the addr= essee(s). If you are not the addressee, or the person responsible for deliv= ering it to the addressee, you are hereby notified that reading, disseminat= ing, distributing or copying this message is strictly prohibited. If you ha= ve received this message by mistake, please notify us, by replying to the s= ender, and delete the original message immediately thereafter.=0A=0A=0A = --0-1690357359-1270238292=:65370 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
The unit with the P51 style scoop has be= en installed on our Glasair 3 here in Yuma, AZ. for over 2 years and has ne= ver failed to deliver. We fly this aircraft over 130 hours a year and = because of the AC we can fly any day in the summer. This was the prototype = for all Glasair's since the manufacturer had never sold&n= bsp;one anywhere else. Before the install, we did our flight test and recor= ded our power, altitude, temperature, and speed settings etc. After the ins= tall we ran the same test and found the no noticeable difference in speed.&= nbsp;We thought there had to be some loss of speed but we really could= n't find any. A Lancair Legacy installed the same system and also found no = measurable loss in airspeed. Because these aircraft are similar in speed, r= oughly 220 knots, we wondered if the the loss isn't measurable until you ge= t to greater airspeed's.
 
We bought a 4P with the same system already installed because of the e= xceptional performance of this system and it cruises just as fast as the on= e without the system. I have heard owners of 4P's say they have noticed 2 t= o 6 knots of loss in airspeed but have never heard of anyone losing 10 to 2= 0 knots or more.
 
Our suggestion is to do your own flight test with your airplane since = no two 4P's are the same and all are prototypes. Also, you didn't mention y= our power, altitude, temp, airspeed's, and the way you fly your partic= ular aircraft so it is hard to determine what kind of cruise speed you are = indicating.
 
One last thought. If you really think you are at a big loss in airspee= d my suggestion is to take the scoop off and see what the difference really= is. This way you will have an apples to apples comparison before you inves= t the time and money into a new system. Also, be aware of cutting holes int= o the bottom of the fuselage since this may decrease the structural strengt= h of the airframe.

Fly Safe,

Christopher J. Alberti
President/CE= O
Starlite Aviation Technologies LLC
1963 S. 39th Drive
Yuma, A= rizona 85364
Phone: 928-581-2383
Fax: 928-329-6488
Email: sta= rliteaviation@yahoo.com
Web Site: www.starliteat.com

This message contains confidential = information only for the use of the addressee(s). If you are not the addres= see, or the person responsible for delivering it to the addressee, you are = hereby notified that reading, disseminating, distributing or copying this m= essage is strictly prohibited. If you have received this message by mistake= , please notify us, by replying to the sender, and delete the original mess= age immediately thereafter.

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