Christen's instructions have you weld the pickup on the back of the oil sump. This creates a potential problem in that the IO-360-A series engine has a long oil sump, and the oil pickup for positive g flight will be at the back of the sump. If you put the nose down in a steep dive, then pull the power to idle at high speed, the discing drag from the prop will cause the oil to move to the front of the oil sump. The oil pickup will now be sucking air, and the oil pressure will go to zero. If you have a non-aerobatic constant speed prop the prop will go to fine pitch. High airspeed and fine pitch leads to high rpm. My engine hit almost 4,000 rpm. I scrapped the prop and had the engine opened up for inspection. This was a very expensive lesson.
After
my event, I talked to my engine overhauler, and a local aerobatic Pitts pilot. Both were aware of other similar incidents with Christen inverted oil systems on IO-360-A series Lycomings. Based on the recommendation of my engine overhaul shop, I switched to an inverted oil pickup from
Raven Aircraft. It is compatible with the Christen boss welded on the back of the oil sump, but the Raven pickup is longer, and it puts the oil pickup towards the middle of the oil sump, so it is much less likely to be sucking air if the oil has run to the front of the sump.
My recommendation is to put the oil pickup boss on the back of the oil sump, but to replace the Christen pickup with one from Raven Aircraft.