X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 15 Nov 2008 10:06:56 -0500 Message-ID: X-Original-Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.120] verified) by logan.com (CommuniGate Pro SMTP 5.2.10) with ESMTP id 3301504 for lml@lancaironline.net; Sat, 15 Nov 2008 09:23:08 -0500 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.120; envelope-from=super_chipmunk@roadrunner.com Received: from Laptop ([74.75.176.139]) by cdptpa-omta05.mail.rr.com with SMTP id <20081115142230.CSAB7376.cdptpa-omta05.mail.rr.com@Laptop> for ; Sat, 15 Nov 2008 14:22:30 +0000 X-Original-Message-ID: From: "Bill Wade" X-Original-To: "Lancair Mailing List" References: In-Reply-To: Subject: Re: [LML] Prop Length for 360 X-Original-Date: Sat, 15 Nov 2008 09:22:35 -0500 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Windows Mail 6.0.6001.18000 X-MIMEOLE: Produced By Microsoft MimeOLE V6.0.6001.18049 You wouldn't have any noticeable vibrations if the prop is balanced correctly but that doesn't necessarily mean that there are no problems. My understanding is that engine/prop combinations are tested on specific airframes and the results may not apply to other setups. My Chipmunk was the prototype for a TCM IO-360 engine conversion STC in the sixties. Part of that is a custom Hartzell prop. I was able to get a copy of the test results and it turns out there's a limitation that centers on 2500 RPM due to harmonics that could stress the blades over time. The prop itself runs very smooth- when I had it dynamically balanced it required almost nothing for weights. OTOH my Navion has an STC'd engine conversion that uses a Bonanza FWF IO-550 and McCauley prop. I doubt it was tested in the same manner- probably they just put it on and made sure it didn't tear the airplane apart. There is a recent AD on the prop restricting MP/RPM combinations but that's for all installations not just mine. Go figure. Hope this helps but now you're probably as confused as I am- Bill Wade ----- Original Message ----- From: To: Sent: Saturday, November 15, 2008 7:36 AM Subject: [LML] Prop Length for 360 > I'm in the middle of getting my Hartzell 2 blade prop overhauled for my > Lancair > 360. I got a new hub at 50% discount from Hartzell to eliminate the > recurring > eddy current inspection. The prop shop doing the overhaul has issues with > the > blades and they will not issue the formal 8131 (I think) paperwork for the > overhaul. The problem is the blade length. > > I bought the airplane 3 years ago and it had an overhauled "0" time prop > when > the airplane was built in 2002. The blades are 70" long according to the > prop > shop. They also say that the Hartzell recommends a 72" blade. But > Hartzell > also allows a 68" blade for the Lyc 360. They do not however, recommend a > 70" > blade. > > The question is, since I've had no problems or vibration issues with my > 70" > blades - should I be concerned? I guess Hartzell's recommendation is based > on > some harmonic resonance or some other vibration related things (which are > outside my knowledge). Does my 70" blade length provide cruise or climb > capabilities that are greater or lesser than a 68" prop. > > I'm planning to have the 70" blades reinstalled on the new hub, and the > log > entry will just say the standard overhaul stuff (except the IAW stuff), > and it > will specify "experimental A/C usage only." > > Any thoughts? > > Thanks, > Matt McManus > lnc2 360 > 408 hours total time airplane. > > > > > -- > For archives and unsub > http://mail.lancaironline.net:81/lists/lml/List.html > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > >