No alcohol or methanol. I understand that the use of methanol treated fuel is not allowed in any of the car gas STC's. I'm under the belief that is the main culprit in the delamination of fuel bladders.
So bottom line, for me, the advantages of a ponk conversion are outweighed by the down sides.
Well said. Your operation has clearly defined your logical powerplant choice. Have you had any issues with mogas effecting your bladder tanks? I suspect the lower compression of the STC'd PPonk would allow it to run OK on mogas ......
That's for a 2400 rpm engine. Low pitch 15.0* High pitch 29,4*In an old thread Dave Calkins mentioned running a 90" McCauley C2A34C204 on his 180, I'm interested in the pull gained over an 88" McCauley 203. How much did the low pitch stop have to be changed to get the 90" to swing at 2600 rpm?
In an old thread Dave Calkins mentioned running a 90" McCauley C2A34C204 on his 180, I'm interested in the pull gained over an 88" McCauley 203. How much did the low pitch stop have to be changed to get the 90" to swing at 2600 rpm?
Upping engine displacement in a 180 isn’t much different than doing it in a Cub. The biggest advantage is rate of climb and the heavier the plane the bigger the advantage. Since my primary mission was flying family and friends to and from a 1000’ strip with 100’ trees on the end, additional clearance over those trees in unfavorable winds was what I was looking for.
I’ve told this story before but the first time my wife rode in the plane after the Pponk-C401 3-blade upgrade we weren’t even at 1000’ off of Lake Hood strip yet and she said that was the best money I’d ever spent on an airplane. And to further qualify, the Pponk replaced a 100 hour factory reman and 88” seaplane prop, so not a weak or worn out engine. There’s no replacement for displacement.
I know other guys with 180K and the O-470-U have changed the pitch stop to allow that engine to spin up to 2600 with the 90". I'm just curious how much the low stop has to be changed.
Haven't tried it but I bet it would fly hundreds of pounds over gross where I suspect with the O-470 it wouldn't get on step (which is actually a safety benefit making it impossible for someone to fly with a stupid load).
Back in the 90's I flew a 206 down to Wipline for refurbishing, installation of their copilot door, 4000 amphibs and an IO-550. They told me during flight testing they were able to get their testbed 206, with 4000 straight floats, in the air with such a load they were unable to fly it out of ground effect. We latter installed Wip 4000 straight floats on our 206 and were amazed at the ability of that aircraft to climb up on step when HEAVY, something the 3430's would never do. The takeoff run was amazingly long. We joked you needed a Six Pack License to carry five passengers in that airplane (speed boat).Depends more on the floats than the engine. At 3190# a 470 works but a 520 works better.
Back in the 90's I flew a 206 down to Wipline for refurbishing, installation of their copilot door, 4000 amphibs and an IO-550. They told me during flight testing they were able to get their testbed 206, with 4000 straight floats, in the air with such a load they were unable to fly it out of ground effect. We latter installed Wip 4000 straight floats on our 206 and were amazed at the ability of that aircraft to climb up on step when HEAVY, something the 3430's would never do. The takeoff run was amazingly long. We joked you needed a Six Pack License to carry five passengers in that airplane (speed boat).
Actually, those floats will fly out of the water nicely at 3800. I flew 185s at 3350 on late PeeKay 3500s, and EDO 3430s out of the Fairbanks float pond. Then I was handed the keys to an IO 550 206 on Wip 4000 straight floats. I cursed them for a while, till I figured out to get them to fly….on the step, a hard shove on a rudder, and the thing would come unstuck. Felt awkward, but after a few more trials, that thing would come out of the water at 3800 pounds all up, within a 100 feet or a little more of where those 185s launched, at 3350. And it’d climb away.
A great working airplane, that one.
MTV
Should be (but probably not anymore) an easy field approval as your 180 is approved by the TCDS for a O-470-K. I understand there are very minor differences between a K and an L. I've been told it's the tack drive but, in all honesty, I never validated that. I believe Continental allows in the field changes to engine model designations. You may have to call them as it now appears all links to that service letter take you to a dead end. You could then convert the O-470-L to an O-470-K and bolt it in (kind of). Do you currently have an O-470-A/O-470-J in it?I have a question that I thought would be easy to find an answer for.. How can I legally put an O470-L in my 1955 C180? Been searching quite a bit and maybe it's not complicated, but I haven't seen a solution. The title of this thread is perfect for my question..
Thanks.
I have a question that I thought would be easy to find an answer for.. How can I legally put an O470-L in my 1955 C180? Been searching quite a bit and maybe it's not complicated, but I haven't seen a solution. The title of this thread is perfect for my question..
Thanks.
This is from the TC E-273. It does not appear to be a direct bolt in exchange.The original -J is in it, running well for now, and I have a nice low time L ready to install.
I'm curious about this "Scootair STC",View attachment 4363
I did the Scootair STC and changed my O470J to an O470R. It actually wasn't that hard!
Agreed. You also need to use the J induction system for the carb to line up with the existing airbox so you can still use the original lower cowl. I do know of several 180's where these part swaps were all done with a K engine and only a logbook entry using the term "per the TCDS". I guess the argument is the parts changes are all "minor", with the only major change being the welding of the four stud exhausts flanges. Not saying this is "legal" just saying those aircraft are still flying 40 years later. Lots of differing opinions on even installing an O-470-K, using all the associated K parts, (engine mount, air box, exhaust, lower cowl) in a 53 through 55 without FAA approval due to serial number.I'm pretty sure though that it must be installed as per the factory K installation--
later engine mount, single exhaust, etc).
If you're gonna run your existing dual exhaust (by installing 4 bolt flanges),
and existing engine mount (by installing the crankcase legs from the J onto the L),
you might need a field approval.
Sounds like your conversion was done the way I did my original O-470-J to an O-470-R. It was easy to do things the right way back in the day when you could get field approvals easily. Now a days one gets punished with delays and rejections when one tries to dot all the I's and cross all the T's.Nothing was said about changing the induction system or oil pan.