GAHorn wrote:There has been years of commentary by very respectable folks who state the oil sump is made of magnesium….and like others, I’ve believed it because it was so-commonly stated by these folks. However, the TCM/Continental Ovhl Manual X30013, page 7, paragraphs 6 and 7 state that the oil sump is Aluminum…and the Crankcase-Cover (Accy cover) is Magnesium.
George,
Airworx Aviation, an FAA authorized repair station, says the sump is magnesium. I don't know what sort of material they use in their
High Velocity Oxygen Fuel (HVOF) coating procedure but I would think, in order to avoid future dissimilar metal corrosion, they would know what the sump is made of.
Note that the overhaul manual also says that the engine mount legs are aluminum. The common understanding is that they are magnesium. Also note that the Continental Overhaul Manual covers not only the O-300 but also the C-125 and C-145 engines. My
guess is that Continental made changes to the metals used in these parts over the years. They may have started production using aluminum but switched to magnesium at some point. The sump on the C-125 may be made of aluminum. Here's why I think this may be the case. Several years ago I found a sump that was sold as a C-145-2 sump.

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By the Sharpie writing on it, it came off of a 1948 C-170, N3914V. Because of some undisclosed corrosion on the mounting flange I was refunded my money on it. Anyway, there are several unusual features on this sump that made me question whether it really was a C-145-2 sump and whether it is magnesium or aluminum:
1.) Both drain plugs are 5/8"-18 rather than the standard 1"-18 plug in the rear. The forward drain plug area is raised which precludes the bottom 3/16" of oil to drain there. Compare this to the picture Richard posted
here.2.) there is no baffle in the intake T. It is not missing; it was never installed.
3.) Note the red paint on the inside. This is Glyptal which we discussed
here. Factory original paint? Who knows.
4.) The IPC says the sump assembly p/n is 530763A1. The "A1" on that part number indicates that it is an assembly number, i.e. there are attaching parts. My sump has "6638" cast into the rear face, not 530763. Floating around the internet is the attached
Continental A&C-Series Aircraft Engines Parts Interchangeability Catalogue. There it says, "Original part number for the C125 (sump) was #6638-Al." According to
Continental this 6638 p/n has been superseded an additional three times. Could one of these supersedures involve a change from aluminum to magnesium?
5.) It did not fizz when I applied a drop of vinegar to it. Magnesium should fizz, aluminum should not.
6.) It weighs just shy of 6 lbs. Anybody have a C-145-2 or O-300 sump for comparison?