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WOT Climb to 10,000'

David-aviator

Well Known Member
This morning the plan was -

Check CHT in an extended climb.
Check OT same situation.
Measure time to climb.
Carefully approach 200 KTAS on the way down.

With the OAT 78 - max CHT in the climb was 377 using EIS 4000 to measure it.
This engine cools well because it is NOT an IO360 angle valve 200+HP unit. It is a simple standard compression IO360 180 HP.

OT hit 175. I may have to cover the cooler a bit.

Time to climb was 8:23. Not too shabby and also not so good, but decent for this engine/Catto prop combination and no wheel pants. For sure any CS prop will beat it.

I used the GRT Sport EFIS TAS indicator to ease up to 200 knots on decent. The maneuver is always a bit tension filled but the airplane was solid the whole way and the speed advance was very gradual. I did not try any turns or abrupt stick action at that speed, just wanted to see if it was stable. It is. Note: Like most guys doing this stuff, I am no trained test pilot.

Van comments in his Landing the RV article some time back, what makes a difference is practice, practice, practice. He is absolutely right. With just 4.9 hours in the RV-8, i need lots more practice. I can get it on but I don't like the landings even if they don't bounce. I am flairing too high and need to go out and drive it closer to the grass or asphalt.
 
What was your target climb airspeed?

I let the speed build until engine rpm was 2450 or so, IAS was 125 knots and that was the start. IAS decreased in the climb as I tried to maintain power at 2400-2500 rpm.

It's not very scientific but engine cooling was confirmed. Later after a refuel stop, CHT topped out at 390 taking off with a hot engine.
 
IO-360 Angle Valves Ca Run Cool

This engine cools well because it is NOT an IO360 angle valve 200+HP unit. It is a simple standard compression IO360 180 HP.

David,

For the record, angle valve IO-360s can be kept cool just fine as I've documented in this thread:

Nice Numbers

Skylor
RV-8
 
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This engine cools well because it is NOT an IO360 angle valve 200+HP unit. It is a simple standard compression IO360 180 HP.

There are threads on this forum documenting the fact that the 200 hp angle valve engines have more cylinder fin area per horsepower than the 180 hp parallel valve engines and run cooler as a result.
 
Temps

I have the IO-360M1B with C/S prop. My CHT always seems to be in the 370 range, not a lot of variation. At first I had the straight flow through on the oil cooler but added the shutter. The OT always was running about 100 degrees above ambient temp...ie 40 OAT equaled 140 OT. Installing shutter solved the OT temp management issue.
 
You guys with the magic cooling touch need to pay me a visit and help me with my baffles.

Mine look good but apparently are lacking somewhat.

My climb performance is ALWAYS CHT limited.
 
David,

For the record, angle valve IO-360s can be kept cool just fine as I've documented in this thread:

Nice Numbers

Skylor
RV-8


Agreed. I don't believe I've ever seen my CHT's above 350 and that was during engine break in abuse with a questionable plenum. Oil temp is another matter but I still have some plenum work to do.
 
Seven decent landings this morning including 2 at Spirit my previous haunt.

I'm back on the groove with the 8, at least for now, imagined landing at OSH going into 26R at Spirit. :)
 
You guys with the magic cooling touch need to pay me a visit and help me with my baffles.

Mine look good but apparently are lacking somewhat.

My climb performance is ALWAYS CHT limited.

Mine used to be. Devil is in the details. Start a new thread so as not to derail David's; I can share what I did. RV-7, 180HP parallel valve Superior IO-360, vertical draft, 8.5:1 pistons, boringly stock except for dual LSE Plasma III ignitions. Am now only CHT limited on the hottest Sacramento Valley days, and even then never on first flight of the day.
 
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