X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 2 [X] Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 24 Feb 2007 07:38:58 -0500 Message-ID: X-Original-Return-Path: Received: from mail38c8.megamailservers.com ([69.49.106.188] verified) by logan.com (CommuniGate Pro SMTP 5.1.6) with ESMTPS id 1859656 for lml@lancaironline.net; Sat, 24 Feb 2007 03:27:37 -0500 Received-SPF: none receiver=logan.com; client-ip=69.49.106.188; envelope-from=jhk@clearwire.net X-POP-User: jhk.clearwire.net Received: from hoben59c2e82ed (74-61-137-71.bel.clearwire-dns.net [74.61.137.71]) by mail38c8.megamailservers.com (8.13.6.20060614/8.13.1) with SMTP id l1O7iO3N024883 for ; Sat, 24 Feb 2007 02:44:26 -0500 X-Original-Message-ID: <001901c757e7$9ec94180$6504a8c0@hoben59c2e82ed> From: "James H. Keyworth" X-Original-To: "Lancair Mailing List" Subject: Fuelling & Grounding X-Original-Date: Fri, 23 Feb 2007 23:44:29 -0800 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0015_01C757A4.8F68EDA0" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.3028 Disposition-Notification-To: "James H. Keyworth" X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3028 This is a multi-part message in MIME format. ------=_NextPart_000_0015_01C757A4.8F68EDA0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit After reading all the previous related comments, can I reasonably conclude that the safest method for fuelling a composite aircraft might be to attach the grounding lead from the fuel truck directly to the hinged fuel cap (neck & cap combination), or, in the case of a detaching filler cap, to have an attachment point on the rim of the tank neck itself? If so, would this also work in situations of polishing, sanding, painting, et cetera? JHK Legacy hopeful Still learning ------=_NextPart_000_0015_01C757A4.8F68EDA0 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
After reading all the previous related = comments,=20 can I reasonably conclude that the safest method for fuelling a = composite=20 aircraft might be to attach the grounding lead from the fuel truck = directly to=20 the hinged fuel cap (neck & cap combination), or, in the case of a = detaching=20 filler cap, to have an attachment point on the rim of = the tank neck itself?
 
If so, would this also work = in situations of=20 polishing, sanding, painting, et cetera?
 
JHK
Legacy hopeful
Still = learning
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