In a message dated 00-05-03 03:00:07 EDT, you write:

> It turned out that someone had replaced the fuel line from the
gascolator, 
> mounted on the firewall, to the fuel injection unit with a fuel line
that 
was 
> too large in diameter. This, coupled with the fact that the gascolator
was 
> vented under the top of the cowl caused the engine to quit whenever you 
made 
> a rapid rotation on take off.

I am not familiar with this configuration.  A vented gascolator may be
able 
to introduce an air bubble into the fuel line.  I am also not sure what I 
said that you are disagreeing with.  I stand behind the following:
Gravity 
fed (carb) systems are not subject to vapor locking.  Boost pumps (or any 
fuel pump, for that matter) will not vapor lock as long as the feed to the

pump inlet is gravity feed.  The problem occurs when the pump needs to
lift 
the fuel (not push it).  The suction cannot immediately clear the vapor 
bubble, and in fact agrivates the problem as lower pressure causes more
vapor.

The Ercoupe engine driven pump is higher than the wing tanks, and therefor

subject to vapor lock.  The header tank provides a cushion, and the vapor 
lock condition will clear before the header runs dry, so should be no 
problem.  

Luscombes with fuselage tanks are subject to engine power loss on takeoff 
because the fuel head on climb is minimal and the fuel burn is maximal.
The 
fuel system simply can't deliver enough fuel fast enough due to the 
combination of fuel line size and low pressure.  This may also be an issue

with the Alon, but the Luscombe tank is much further back, so there's more
of 
a head loss.  'Course, it could be just carb ice.  Small Continentals can
ice 
up in a heart beat and lots of folks refuse to acknowledge that.

John
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