Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Fri, 09 Jan 2004 13:20:56 -0500 Message-ID: X-Original-Return-Path: Received: from imo-m02.mx.aol.com ([64.12.136.5] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2925027 for lml@lancaironline.net; Fri, 09 Jan 2004 12:26:42 -0500 Received: from Sky2high@aol.com by imo-m02.mx.aol.com (mail_out_v36_r4.8.) id q.110.2ce5a286 (30960) for ; Fri, 9 Jan 2004 12:26:38 -0500 (EST) From: Sky2high@aol.com X-Original-Message-ID: <110.2ce5a286.2d303e4e@aol.com> X-Original-Date: Fri, 9 Jan 2004 12:26:38 EST Subject: Re: [LML] Re: Piller Point Fuel Sensor X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="-----------------------------1073669198" X-Mailer: 9.0 for Windows sub 370 -------------------------------1073669198 Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable
In a message dated 1/9/2004 10:29:53 AM Central Standard Time,=20 gary21sn@hotmail.com writes:
It would seem the line from the fuel pump to the header tank will hav= e=20 fuel in it because of header tank slosh back from taxi, turns, climb and=20 turbulence, etc. unless a check valve is in the line. =20
Rob, et al,
 
Hmmmm...
 
Let me describe my setup and experience.
 
1. Automatic "header full" system keeps the header tank between 8.25 an= d 9=20 gallons at all times.  Lower level sensor must remain at the lower leve= l=20 for about 15 seconds before the pumps are started (avoiding start/stop cycle= s in=20 turbulence).  This assures me of about 1 hour flight time in case of=20 complete power failure, etc.  Indicators show the header full and anoth= er=20 for "timer running."
 
2. Both pumps (located in the stub wings) are simultaneously=20 engergized.  There are check valves at each header entry point for= a=20 variety of safety reasons - siphoning, negative pressure, etc.  The win= gs=20 are emptied evenly meaning that lateral trim does not change thru the flight= =20 unless I throw the passenger out. 
 
3. Each pump has its' own pullable breaker and manual on/off=20 switch.  This allows for non-automatic operation.  There is no fue= l=20 selector for KISS.
 
4. VM EPI 800 fuel probes are in all three tanks. They are very=20 accurate.  All tanks produce a warning (I have annunciator lights) when= =20 they are below 4 gallons.  I would be gasping for air if the header fal= ls=20 below 4 gallons (ask the Don about this).  The Gallons indicator shows=20= zero=20 (by design) when below 2 gallons.  There is a fuel totalizer runni= ng=20 off the fuel flow sensor, generally 2-3% high, that is another low fuel warn= ing=20 source.
 
5.  The automatic system is manually turned off when the header do= es=20 not refill after dropping to 8 gallons and the wings have been zero for a wh= ile.=20 This probably means the pumps are running "dry" for no more than 15-20=20 minutes.  Slosh, etc. probably means the pumps are not really dry for t= hat=20 length of time.  I have flown in this condition about ten tim= es=20 (including the Kitty Hawk to Dayton race leg, 10 minutes before=20 crossing the finish line) and the pumps are still working.  The wings h= ave=20 been emptied in level flight with not much more than a cup of fuel remaining= in=20 each wing as later measured on the ground.
 
6.  The panel is placarded "Do Not Take Off With Less Th= an 8=20 Gallons In The Header."  There is no experience maneuvering when t= he=20 header contained less than 4 gallons, although the header is throughly=20 baffled. 
 
In flight I cannot hear the pitch of the pumps change when thay run dry= =20 because of their stub wing location - perhaps you can hear them as they are=20 under the seat.  Maybe you could hook up an aural sensor switched into=20= the=20 audio panel or use a stethoscope, checking heart rate and pump pitch, w= hen=20 you think the wings are dry.
 
Scott Krueger=20 AKA Grayhawk
Sky2high@aol.com
II-P N92EX IO320 Aurora, IL=20 (KARR)

"...as we know, there are known knowns; there are things we kn= ow=20 we know. We also know there are known unknowns; that is to say we know there= are=20 some things we do not know. But there are also unknown unknowns - the ones w= e=20 don't know we don't know." D. Rumsfeld
-------------------------------1073669198 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit In a message dated 1/9/2004 10:29:53 AM Central Standard Time, gary21sn@hotmail.com writes: It would seem the line from the fuel pump to the header tank will have fuel in it because of header tank slosh back from taxi, turns, climb and turbulence, etc. unless a check valve is in the line. Rob, et al, Hmmmm... Let me describe my setup and experience. 1. Automatic "header full" system keeps the header tank between 8.25 and 9 gallons at all times. Lower level sensor must remain at the lower level for about 15 seconds before the pumps are started (avoiding start/stop cycles in turbulence). This assures me of about 1 hour flight time in case of complete power failure, etc. Indicators show the header full and another for "timer running." 2. Both pumps (located in the stub wings) are simultaneously engergized. There are check valves at each header entry point for a variety of safety reasons - siphoning, negative pressure, etc. The wings are emptied evenly meaning that lateral trim does not change thru the flight unless I throw the passenger out. 3. Each pump has its' own pullable breaker and manual on/off switch. This allows for non-automatic operation. There is no fuel selector for KISS. 4. VM EPI 800 fuel probes are in all three tanks. They are very accurate. All tanks produce a warning (I have annunciator lights) when they are below 4 gallons. I would be gasping for air if the header falls below 4 gallons (ask the Don about this). The Gallons indicator shows zero (by design) when below 2 gallons. There is a fuel totalizer running off the fuel flow sensor, generally 2-3% high, that is another low fuel warning source. 5. The automatic system is manually turned off when the header does not refill after dropping to 8 gallons and the wings have been zero for a while. This probably means the pumps are running "dry" for no more than 15-20 minutes. Slosh, etc. probably means the pumps are not really dry for that length of time. I have flown in this condition about ten times (including the Kitty Hawk to Dayton race leg, 10 minutes before crossing the finish line) and the pumps are still working. The wings have been emptied in level flight with not much more than a cup of fuel remaining in each wing as later measured on the ground. 6. The panel is placarded "Do Not Take Off With Less Than 8 Gallons In The Header." There is no experience maneuvering when the header contained less than 4 gallons, although the header is throughly baffled. In flight I cannot hear the pitch of the pumps change when thay run dry because of their stub wing location - perhaps you can hear them as they are under the seat. Maybe you could hook up an aural sensor switched into the audio panel or use a stethoscope, checking heart rate and pump pitch, when you think the wings are dry. Scott Krueger AKA Grayhawk Sky2high@aol.com II-P N92EX IO320 Aurora, IL (KARR) "...as we know, there are known knowns; there are things we know we know. We also know there are known unknowns; that is to say we know there are some things we do not know. But there are also unknown unknowns - the ones we don't know we don't know." D. Rumsfeld -------------------------------1073669198--