X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 25 May 2011 13:44:38 -0400 Message-ID: X-Original-Return-Path: Received: from ndmsnpf02.ndc.nasa.gov ([198.117.0.122] verified) by logan.com (CommuniGate Pro SMTP 5.4c3j) with ESMTP id 4994209 for lml@lancaironline.net; Wed, 25 May 2011 12:14:48 -0400 Received-SPF: none receiver=logan.com; client-ip=198.117.0.122; envelope-from=michael.s.reinath@nasa.gov Received: from ndjsppt02.ndc.nasa.gov (ndjsppt02.ndc.nasa.gov [198.117.1.101]) by ndmsnpf02.ndc.nasa.gov (Postfix) with ESMTP id 4D2541084EE for ; Wed, 25 May 2011 11:14:15 -0500 (CDT) Received: from ndjshub03.ndc.nasa.gov (ndjshub03-pub.ndc.nasa.gov [198.117.1.33]) by ndjsppt02.ndc.nasa.gov (8.14.4/8.14.4) with ESMTP id p4PGEE2J025089 for ; Wed, 25 May 2011 11:14:15 -0500 Received: from NDJSSCC06.ndc.nasa.gov ([198.117.4.176]) by ndjshub03.ndc.nasa.gov ([10.202.202.162]) with mapi; Wed, 25 May 2011 11:14:14 -0500 From: "Reinath, Michael S. (ARC-AM)" X-Original-To: Lancair Mailing List X-Original-Date: Wed, 25 May 2011 11:14:13 -0500 Subject: RE: Fuel restriction or air part 2 Thread-Topic: Fuel restriction or air part 2 Thread-Index: Acwa9slk8GYQsjHjxUmLVQ1osaaDOg== X-Original-Message-ID: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: user-agent: Microsoft-Entourage/13.8.0.101117 acceptlanguage: en-US Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable MIME-Version: 1.0 X-Proofpoint-Virus-Version: vendor=fsecure engine=2.50.10432:5.4.6813,1.0.148,0.0.0000 definitions=2011-05-25_07:2011-05-25,2011-05-25,1970-01-01 signatures=0 > First of all...thanks to everyone that has tried to help me with my engin= e > surge (fuel related) problem on my normally aspirated Lancair IV. I have > throughly checked and tested everything suggested so far. There are no t= ank > vent issues and a vacuum test of the entire system from the engine driven= fuel > pump back to the tanks proved there is no air getting into the system. I= even > replaced the o rings on the inlet and outlet sides of the electric fuel p= ump > just to be sure. Unfortunately my test flight this morning confirmed tha= t the > issue still remains. >=20 > This is what happened. On a 50 mile cross country where I took off and > climbed to 7,500 I experienced zero issues. I landed took on some fuel a= nd > took off for home. I climbed to 7,500 again and saw that the fuel flow a= nd > fuel pressure gauges were fluctuating. Since this occurrence preferred m= y > engine surge problem in the past I knew it was coming and it did. The en= gine > began surging and continued to do so until I turned on the electric ( bac= k up) > fuel pump. The engine and gauge readings stabilized immediately. >=20 > So this is where I am...I know I do not have any vacuum (air) leaks from = the > tanks through to the engine driven pump, nor do I have any restrictions i= n the > fuel lines or fuel tank vents. I have replaced my engine driven pump. A= ll > symptoms remain. >=20 > Question...if I am at cruise settings and leaned out reading 16GPH on the= fuel > flow and 10PSI on the fuel pressure should this readings rise when I turn= the > electric fuel pump on? My GPH goes from 16 to 21 and my fuel pressure go= es > from 10 to 15 or higher. Berni, I see fuel pressure fluctuations in my LNC2 after a short fuel stop followe= d by a long climb in warm weather. We have talked about this on the LML in th= e past for the LNC2 model. As the fuel lines, and everything else under the cowling, gets heat-soaked during the short stop, vapor bubbles start to for= m in the lines and cause the fuel pressure to fluctuate. Turning the pump on, stabilizes the pressure. If I climb from a cold start to 15,500ft, for example, I have no problem. M= y cooling is fine, so I have no climb restrictions. If I make a short flight to get fuel, with only a quick stop, and then climb to 15,500, I get the pressure fluctuations, in warm weather. They are never bad enough to cause surging, but the pressure will drop from 25psi to around 11-14 psi, and surge back and forth (if I leave the electric pump off). Once I level off, and the area at the back of the cowling begins to cool from the climb, and the heat soaking from the fuel stop, the pressure fluctuations begin to subside. After 10-12 minutes, they are gone. I have insulated the fuel lines, which helped, but it still happens. Maybe your problem is something similar. Mike Reinath LNC2 at 1067 hrs San Jose, CA