Return-Path: Received: from imo12.mx.aol.com ([198.81.17.2]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 16 Mar 1999 01:56:01 -0500 Received: from Sky2high@aol.com by imo12.mx.aol.com (IMOv19.3) id kASNa01925 for ; Tue, 16 Mar 1999 01:57:54 -0500 (EST) From: Sky2high@aol.com Message-ID: <87442b25.36ee00f2@aol.com> Date: Tue, 16 Mar 1999 01:57:54 EST To: lancair.list@olsusa.com Subject: Major Alterations X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Marv, There is no reference to FAR43 in the appellate court statement. In any event, as I stated in my article: One must LOG the changes one makes, along with their effects and any tests/checks to verify the change. This logging is necessary to satisfy a variety of FAR requirements. One should then write to the FAA, outlining the changes, claiming that they are "minor" by the definitions listed in 91.23 and asking for a written reply. In my district, most will be considered minor and a "major" would, at the very worst, require some fly off time to be recorded in your logs. The resultant reply from the FAA is considered the "Experimental aircraft 337" form and should also be filed with your logs. The FAA would probably not require "recertification" of a change to the fuel delivery system in an EXPERIMENTAL aircraft. Why do this? So that one does NOT leave the determination of a change as major or minor and whether recertification is required, up to an insurance company lawyer or an uninformed judge. If Mr. Davenport had such a reply document from the FAA, his insurance company could not have used the court to interpret FAAese and wiggle out of its duties to pay. Scott Krueger N92EX [Scott... from section II in the decision in question: [2] Davenport argues that the series of modifications he made to his aircraft's fuel system did not constitute a "major change" because the fuel system at the time of the crash was in the same configuration as at the time of the initial certification. We reject this argument. Common sense dictates that altering the method of delivering fuel to the engine of an aircraft has an obvious and substantial effect on the "reliability, operational characteristics, or other characteristics affecting the airworthiness of the [aircraft]." 14 C.F.R. S 21.93(a)."2" [note: this "2" ref's a footnote] The fact that Davenport made repeated changes to the fuel system did not remedy his failure to notify the FAA prior to making each change. Each change Davenport made to the fuel system was major, and each change therefore required FAA notification under the operating limitation. [Here is footnote "2"] "2" Indeed, in an analogous regulation applying to the maintenance and repair of non-experimental aircraft, the FAA has defined major alterations as including "[c]hanges to the basic design of the fuel . . . system[ ]." 14 C.F.R. S 43 app. (a)(1)(xii). ]