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O-540 question

Chad Meeks

Active member
I'll start with Happy Thanksgiving!

I'm a Continental guy, but I've seen a few guys build an aircraft engine utilizing an O-540 lower end with a GTSIO io-520/550 top end. That sounds impressive.

My question is, if I wanted to build an engine like this, what model O-540 lower end would I use, and would that be a large or small journal crank?

Like I said above, I've only had, and still run Continental engines For 30 years. I've always loved the E-225 with the IO-520 top end.
 
There were a few "lyconentals" built back in the racing days, pretty sure they were on narrow deck cases, mainly 4 cylinder based, they ran ok, lots of work to build up such of an engine.
Keep in mind that GTSIO heads are the worst flowing for naturally aspirated/ carbureted applications.
The E225 with 520 jugs is the great match up if tuned and say blueprinted, 12:1 forged pistons, cam timing advanced to 114° lobe center, other little tricks, why reinvent the wheel?
 
John, I appreciate your feedback. I recently (within the past 2 months now) saw a video of an o-540 with the GTSIO cylinder inverted and installed... they guy who owned it stated it was "rank". So, that kinda peaked my interest in building one.
 
For the effort and cost to add 5% displacement I would opt to add 7.4% and build a Lycoming 580. You get the longer lycoming stroke and an even larger 5.319 bore vs 5.25 Continental. Better flowing cylinders and you can purchase new loaded for $1,900 each. I’m sure the case needs to be opened up, the stud pattern is unknown to me.

Some bore and stroke figures for comparison:

Bore x Stroke

Lycoming
540
5-1/8 x 4-3/8

580
5.319 x 4-3/8

Continental
520
5-1/4 x 4

550
5-1/4 x 4-1/4
 
For the effort and cost to add 5% displacement I would opt to add 7.4% and build a Lycoming 580. You get the longer lycoming stroke and an even larger 5.319 bore vs 5.25 Continental. Better flowing cylinders and you can purchase new loaded for $1,900 each. I’m sure the case needs to be opened up, the stud pattern is unknown to me.

Some bore and stroke figures for comparison:

Bore x Stroke

Lycoming
540
5-1/8 x 4-3/8

580
5.319 x 4-3/8

Continental
520
5-1/4 x 4

550
5-1/4 x 4-1/4
Wow, that's interesting.. Slidin Gator, I appreciate the feedback
 
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