Mailing List flyrotary@lancaironline.net Message #59893
From: Scott Emery <shipchief@aol.com>
Subject: Re: [FlyRotary] Re: Airworthiness Cert issued....followed by blown enigne
Date: Sat, 15 Jun 2013 00:19:27 -0700
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
The fitting is a parallel thread swivel elbow with a lock nut & seal ring washer. Spendy bugger.
Looking in the exhaust ports I see scratches and impacted ? Aluminum? On the rotor face near the seals. On one rotor tip I think I can see the end of a seal (chunk out of rotor tip @ edge) rote faces are shiney clean like detonation but engine has about 5 hours since overhaul

Sent from my iPhone

On Jun 14, 2013, at 7:47 PM, Kelly Troyer <keltro@gmail.com> wrote:




On Fri, Jun 14, 2013 at 9:27 PM, Mark Steitle <msteitle@gmail.com> wrote:
Sorry for the bad news, but good thing it happened on the ground.  

As for the possibility of detonation, it doesn't sound like it to me.  If it was detonation, I would expect to find a broken apex seal or two.  Sounds like maybe an o-ring blew.  It could have even been a defective iron.  Pictures would help.  

Mark


On Fri, Jun 14, 2013 at 7:38 PM, <shipchief@aol.com> wrote:
N89SE received it's Airworthiness Certificate June 13, 2013! Yay!
So I put the covers on it an pulled it out of the hangar for a start up and taxi test.
I have not run it this year while finishing the airframe.
So I started it up, a bit behind the curve on the EC-2, chasing the mixture around etc, then settled in to a nice smooth high idle and taxi'd down to the far end of the runway where I ran it up to 4400 +RPM, checked the water & oil temps, (158 & 167) pulled out on the runway, and fed the power to it for a 2 or 3 second burst, to be pulled off to prevent flight.
Well the thing started well enough, I pushed the throttle slowly to about 2/3, and as the plane gained some speed, the CATTO 68x74 prop unloaded a bit and the RPMs went up. The acceleration was profound for about 2 seconds followed by a POP! as or just before I started to pull the throttle back.
Then came the grey smoke as I shut down the fuel pump and glided off the runway to the taxiway.
A few guys came running to help. One asked 'How ya doin'?" Medium I replied. (I'm OK and nothing is burning). Yada Yada, The plane is back @ the hangar, and the oil leak (spew) is a cracked block at the last oil tap fitting on the top gallery, by the distributor pulse counter. (1986 type)
Today I stripped the engine and pulled it off the airframe. Looking in the ports, all the tip seals move and are springy, but I think I detonated it, some damage is visible. Maybe in a previous tethered run (to 40" manifold press), and this time it let go. compression was down (prop pull method) I wonder if detonation under boost will crack the block (end irons)?


What a letdown after your AW certificate.........Curious what type of fitting you have in that oil galley........As I recall from my
1988 13B front housing the side walls may be a little thin after threading.............If a tapered pipe thread fitting was used the 
pressure from the tapered thread can crack the hsg.......I would suggest using straight threaded fittings (US or Metric) with
alum , copper or "O" ring for sealing.............FWIW

--
Kelly Troyer
Dyke Delta_"Eventually"
13B_RD1C_EC2_EM2
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