The tubular-gear Cessnas sometimes had a jackpoint on the gear leg, but that is little help when you want to pull the leg out or replace the retaining bolt.
Heavier retractable singles like the R182 and 210 have a factory-supplied jackpoint that is attached to the main spar with screws, into nutplates in the spar. The Corvalis has small, threaded jackpoints, removed unless needed.
The 172 service manual has stuff like this in it:
A piece of 1x4 padded with rubber. Really? Nothing to prevent it from slipping on the wing, and nothing to prevent the 1x4 from splitting under jacking forces. I made thick plywood, rubber-padded jackpoints, with drilled sockets to prevent sliding off the jack, and screws in the top sticking out a little, arranged to fit into the strut cutout in the wing skin to prevent the wing's sliding off the pad. Worked fine.
We also had jackpads that fit in the main gear "armpit" where the gear meets the fuselage. They were 10-gauge steel sheet (about 3/16") shaped to fit around the gear leg a little to prevent fore-aft slippage, and they lifted at the leg's outer bulkhead casting in the gear box and the leg itself. Good for doing work on wheels and brakes. The airplane with the flat leaf spring gear were easy: a welded-up, tapered U-shaped jackpoint that fit around the leg with a minimum of padding, and it would slide up and wedge itself securely on the leg with jacking pressure. It had a welded-on jackpoint, angled so as to be vertical when on the leg. Had several of those to fit the different leg widths. These things need nice big red flags on them, or you will forget it someday and it will go flying and could kill someone on the ground when it finally falls off. They wedge on tightly enough that you have to tap them loose with a hammer.