The Ranger engine was an inverted 6-cylinder, so every cylinder was vulnerable to hydraulic lock. It is only the lowest two or three cylinders of a radial engine that have the same exposure.
To clear a hydraulic lock, you pull the motor through by hand, using the propeller. If you feel resistance, you stop. Then you pull the motor through [Bbackwards[/B] which opens the exhaust valve first, letting the oil out through the exhaust system, which is designed to give some oil room to pool and drain.
Electric starters on older aircraft engines had clutches designed in as a way to address hydraulic lock. They were preset to slip at a torque low enough to prevent over-stressing the engine components if hydraulic lock was encountered. Sadly, they often fail to prevent this, so it is important to turn the engine by hand before starting if it has been sitting for any length of time.
The engine cylinders are made of finned, steel barrels, bolted to the block with a great many 3/8" NC studs. The heads are aluminum, and are threaded onto the barrels while very hot. The thread joint is an interference fit, and the barrels are cooled, while the heads are heated to over 500 degrees F. This results in a very tight "shrink" fit. It is so tight, that the bore in the cylinder barrels is finished after the heads are installed. This joint is very strong, and rarely fails. Some of those failures may come from damage from unnoticed hydraulic lock incidents.
Modern aircraft engines are generally horizontally opposed and do not provide an opportunity to hydraulic lock. There are still many radial engines in service.