Return-Path: Received: from [65.33.87.139] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.8) with HTTP id 2988811 for lml@lancaironline.net; Thu, 12 Feb 2004 08:42:07 -0500 From: "Marvin Kaye" Subject: Re: [LML] Re: Legacy IO550 fuel injection system vent hose/oil mist To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1.8 Date: Thu, 12 Feb 2004 08:42:07 -0500 Message-ID: In-Reply-To: <011201c3f119$772bc720$be316644@S0030046211> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "nkanagy" : I have heard that many (I believe particulary round) engines that operated in cold temperatures used to have a "oil dilution" control that was activated for a determined period of time before engine shut-down. The purpose of this system was to intentionally inject fuel into the oil while the engine was running and lower the oils viscosity. Then, upon startup (some time later and at quite a bit lower engine temp) the oil was not as thick and the would do a better job of lubricating the engine. The fuel would evaporate in a few minutes and exit via the breather, leaving the now warmed up engine to operate with oil at its normal viscocity. If engines used to be equipped with this for intentional use, how could a little bit of vapor cause any harm? > and gums up the belly (the plane's, not mine). My A&P says the tube vents fuel > injection system overload, during priming, and washes some oil off the engine > innards. I suggested routing the hose into the crankcase vent hose, thence > through the oil/air separator. My A&P voiced disapproval of introducing the > fuel (vapors only, I suspect) into the oil by return to the engine. > > I'd appreciate the group's guidance. Wendell Durr > > [ you want a snuffle valve... its a small reservoir with a ball barring > that will flow when inflight but will hold some priming gas on the > ground... photo attached. -Rob ]