Reaching out to the community for some friendly advice on the level of concern and follow-on action.
Background: 1981 M20J (IO-360) went in for annual service with some avionics upgrades early this year. Every item found on the report was approved for repair/fix. A/C flew from MX to home station, about a 4+30 flight with one stop for fuel. One item was a crankshaft seal leaking, removed and replaced the crankshaft seal and prop o-ring—common fix from what I can research, done. After arriving home, I noticed a few streaks on the passenger side windshield, which appeared lubricant-based. Noted and cleaned the windshield as the prop was dry. Fast forward two short flights later, followed by another 4+00 flight, the streaks appeared on the windshield again, prop still dry.
Findings: The spinner was removed yesterday to check for any apparent issues. On removal, there was a random installation of long and short bolts on the spinner and the inner spinner assembly. The aft spinner bulkhead appears to be installed 180° out from the markings of a #1 and #2 on the assembly—minor streaks from the prop and engine crankshaft attachment point. Spinner had a small lubricant (grease) transfer relative to prop #2.
Action: I cleaned streaks and the spinner transfer, reinstalled the proper bolt pattern, and will perform a ground run and flight, then recheck for streaks or lubricant transfers.
Concern: The aft spinner bulkhead is the balancing attachment point for added weight. Can it be rotated 180° without removing the prop? Or does it even matter?