I guess it depends. I generally like 40ºF as a point where some preheat is needed but I fly an experimental plane with its experimental engine using 15w40. I was reading an article that talks about using multiweight oil and the advantage it gives (FWIW):
The engine heater and a small cabin heater have been keeping the aircraft warm and ready to go for almost two weeks. Heresy, you say? Leaving a preheater on for this long will corrode the engine, you say? Not necessarily.
www.aopa.org
I've seen that article before, and I've questioned it before. This:
Crankshaft bearings are an excellent example. The crankshaft bearing is supported by the aluminum case, while the crankshaft itself is steel. The clearances for these parts are designed for normal operating temperatures. In extremely cold temperatures, the aluminum case contracts enough to make the bearings too tight and can cause substantial wear and damage upon start-up.
The author is an A&P and should know that the STEEL crankshaft rides in bearing shells that are STEEL and lined with babbit, a soft material that absorbs any grit to keep it from cutting the crank. Those steel shells are semicircular and are precisely made so that their ends butt together when the crankcase bolts are tightened up. It's called "crush." The bearing bores in the case are machined precisely as well, to get the exact crush required. Too loose, and the bearings start to shift around and bad things happen. When the aluminum case gets cold and contracts, those bearings get clamped together more tightly, but they cannot get a smaller ID other than from the cold, and the crank, also cold, accommodates that.
The pistons do indeed get a lot smaller than the cylinder, and clearances increase. Taking off too soon can cause near-seizure and scuffing. Preheating can prevent that. Those big clearances are why there is so much combustion gas blowby when the engine isn't at operating temperature, carrying water vapor and corrosive combustion byproducts into the case, mixing with the oil that is flying around in there, and which will eat the engine if it's not flown long enough to let the heat drive that stuff out of the crankcase breather.
Doing some quick calculations using the coefficients of linear thermal expansion for steel and aluminum, for the bearings I find that at a 40°F temperature drop, the
difference between the contraction of the aluminum case and the steel crankshaft is about .0004 inches. Lycoming's specified bearing-to crank main journal clearance is .0025" minimum, .0055" maximum, or six to nearly 14 times the reduction in clearance, even if the case was able to collapse the steel bearing shells, which it can't.
.0004" is about 1/8th of the thickness of a sheet of paper, or 1/9th the thickness of a human hair.
Oil is definitely a problem. When I taught aircraft systems, one of the classes covered lubricants, and why we have different viscosities.
Before the class I took two each of W80, W100, and 15W50 and put one of each in the freezer. The others went into a pan of water and set on the stove to get them to the boiling point of water, where oil's hot viscosity is measured. I took a cold and a hot of each and poured them over an aluminum plate so they could see how the temperature spread thickened and thinned them. It was really stark with the straight-grades, a lot less with the multigrades.
I asked the students how easy it would be to suck that 80 or 100 up the oil tube from the sump to the pump when the engine was cold. I had those parts there, too. They got the point. Then I told them that the fridge's freezer was only at -10°C (+14°F) and reminded them that we regularly flew down to -25°C (-13°F), and what would those straight-grades look like then? Even at -10°C the 100 was like molasses. At -25°C, even 15W50, without preheating, the engine's life might be measured in a few minutes. It just wouldn't get enough oil, and the bearings would crater. They need a lot more oil than the piston and cylinder due to the far larger loads on them.