My own experience is that when the cold start switch is
inappropriately selected and the engine is running at medium-hight rpm -
is that the engine does not stop immediately, but starts to bog down,
sloppy sounding exhaust and then eventually dies. But, then I am using 460
cc/min injectors. I even found that I could fly (keep engine running) with
the cold start on provided I put the manual mixture control maximum lean and it
was still sloppy sounding - if I had 550 cc/min injectors I doubt that it would
have kept running.
My best SWAG given that Tracy found no fault and the
sudden termination of the engine - is either CAS problem or ignition (and it
would have to be an ignition problem that would taken out both sets of spark
producing devices). If CAS then that could account for the sudden stoppage
more so than a misplaced cold start switch in my opinion, but then distant
diagnostics is still an evolving "Art". {:>)
Ed
Sent: Saturday, October 15, 2011 3:32 AM
Subject: [FlyRotary] Re: Bill Eslick's EC2
inspection
Man, I hate that cold start switch ;-)
Dave
Leonard
On Fri, Oct 14, 2011 at 1:02 PM, Tracy <rwstracy@gmail.com> wrote:
Thought the group would like to hear what i found when I
Finally had a chance to closely examine Bill's EC2. I was hoping to
find a definitive reason behind his sudden and complete loss of power on
takeoff on his last flight.
On powering it up on the bench I found both
A and B controllers Working normally. Bill noted in his report that in
the 'Fly The Plane' situation called for in a power failure during
takeoff he had not tried switching to controller B. It does not appear
that it would have done any good this time.
None of the parameters were
set outside the expected range so no sign of data corruption. In fact
the only thing notable about the data downloaded from it was the unusually
smooth programming of the MAP table. Most of the time I find units
returned for updates with choppy looking data in the table indicating a lack
of care or proper methodology in setting it up. A and B controllers had
identical data.
The PCM was also returned with the unit so just in case
the control panel was the cause I substituted it for the bench test panel I
normally use. Thought I saw a problem because the injection pulse width
was so large that it could well have caused engine flooding. This was
caused by the mixture control being set fairly high and the cold start switch
being in the on position. This does not prove anything because that
could easily have happened during removal of the panel from the plane or while
packing it for shipping. When the switch and mixture control was
returned to normal settings the injection pulse width returned to
normal.
Ran the unit on the bench for several hours while heating and
subjecting it to vibration but nothing else turned up.
Tracy -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html
-- David Leonard
Turbo Rotary RV-6 N4VY http://N4VY.RotaryRoster.net http://RotaryRoster.net
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