Return-Path: Received: from S1.cableone.net ([24.116.0.227] verified) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 726199 for flyrotary@lancaironline.net; Sat, 12 Feb 2005 11:04:18 -0500 Received-SPF: pass receiver=logan.com; client-ip=24.116.0.227; envelope-from=crayd@cableone.net Received: from chuckathlon (unverified [24.117.230.176]) by S1.cableone.net (CableOne SMTP Service S1) with ESMTP id 10174620 for multiple; Sat, 12 Feb 2005 09:06:49 -0700 Return-Path: From: "Chuck" To: "'Rotary motors in aircraft'" , Subject: RE: [FlyRotary] 1 step forward, 2 steps back... Date: Sat, 12 Feb 2005 09:03:43 -0700 Message-ID: <000001c5111c$6def6850$e401a8c0@chuckathlon> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.3416 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2739.300 X-IP-stats: No info recorded yet X-External-IP: 24.117.230.176 X-Abuse-Info: Send abuse complaints to abuse@cableone.net -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of David Staten Sent: Saturday, February 12, 2005 3:33 AM To: Rotary motors in aircraft Subject: [FlyRotary] 1 step forward, 2 steps back...=20 Well here goes an update on Chris's velocity project.. This past=20 wednesday, EAA Chapter 12 had an open house/meeting that we had at the=20 hangar out at EFD (Ellington Houston,TX) and we had the opportunity to=20 meet a few new prospective members as well as show off the Velo (and our hangar mate's Vari Eze rebuild/refurb). Made some new shop tables that=20 are heavy duty, and able to hold 2 or 3 engines worth of parts if=20 needed, and mounted most of our bench tools on one as a work station for anticipated fab work. We had a nice turnout.. maybe 15-20 peeps max and=20 I managed to get a few newbies to attend (ones a cherry PP the other is=20 a wannabe)... anyways... =20 After then meeting, and obligatory beer session (I mean.. bull session.. yea.. really).. Chris, myself and a newbie named Drake went after=20 mounting the engine mount to the firewall using AN hardware. I ended up=20 with some AN6-30 on the top of the CCI mount and on the bottom some=20 AN6-37A. The A suffix denotes no "hole" on the end of the shank so I=20 took one of my nuts (5 total) and sacrificed it to make a jig for=20 drilling the two -37A bolts to accept cotter pins. Once that was=20 accomplished, we went to fitting the lower longer bolts. I have to=20 mention it is an EXTREMELY tight fit due to the proximity of the gear=20 saddle to the lower engine mount bolts. This meant we spent a lot of=20 time just trying to get the bolt ON the nut in close quarters. After=20 getting it on there we discovered that the holes were just a little too=20 far up to allow a cotter pin to safety the castellated AN nuts, so with=20 SWMBO waiting patiently at home, we called it quits at about 2330 that=20 night. That same night I made use of a very graciously loaned 600 ft/lb=20 torque wrench that an aircraft part/tool house loaned me and=20 removed/reinstalled the "Nut From Hell" and ensured it was TRULY at 350=20 ft/lb. Fast forward to tonight.. after all my social obligations were concluded I ended up running into Drake online, and we went back out to the hangar tonight to try and re-fit the mount. Rather than re-drill the bolts, we=20 added some large fender washers to the assembly that increased the=20 thickness of the assembly. This time we were able to get the AN bolts=20 installed top and bottom and passed a small strip of safety wire though=20 each to ensure that the holes were aligned and able to be pinned later=20 with cotter pins. On a side note, we discovered that hot-glueing the nut to a box end wrench helped tremendously with threading the nut in close=20 quarters. =20 Next step was to place the engine ON the mount for a dry fit. We placed=20 it on the CCI mount plate and went to fit a stock oil pan to the bottom=20 and discovered that the oil regulater splash guard would not be able to=20 stay. Took it off with a cut-off wheel and then placed the pan/engine on the mount with 4 of the 21 bolts placed to ensure it didnt pull off/fall off the mount. The next chore was the removal of the pilot bearing. We=20 had tried removal from several approaches without success.. The Harbor=20 Freight pilot bearing puller is a smidge too large to go into the=20 bearing hole... finally I re-read the RD1-B install manual and it=20 mentioned that a dremel has been used in the past for stubborn ones. I=20 ended up extracting the individual needles with a scalpel and=20 needlenose pliers, collapsed the inner race and yanked it out, then=20 ended up using a dremel to gouge the outer race, then collapsed IT as=20 well.. Infortunately this gouged the inside of the bearing channel in=20 the process, so I drum sanded rough spots until it was finger smooth.=20 The PSRU pilot shaft was able to fit in without difficulty. =20 At this point, I wanted to dry-fit the PSRU on... if nothing more than=20 to give Chris a picture or two to gloat over.. but right around here is=20 where things came to a screeching halt. The damper plate did not match=20 up to the flex plate that we had. The bolt hole diameter was a smidge=20 larger on the flex plate than on the damper plate. Looking back.. I want to say that we have a 1992 flex plate that came with the couterweight I=20 bought.. and while I left the install manual at the hangar, I believe it calls for an 86-91 auto flex plate. So.. it WASNT going to fit.. At that point I decided to call it a night/morning... and post a few pics of all the excitement. Oh well.. back to ebay for a flex plate....=20 somewhere..somehow. =20 Dave Staten =20