Having the deepest respect and personal knowledge of GASSITT's uncanny abilities with Rotax 912 engines (an opinion shared by Lockwood who sends him parts to repair) I too am pondering his excellent original questions concerning climb angle and time versus oil pump output pressure.
As a rough estimate, the engine's oil pump pressure output, under wings-level, straight-ahead-vectored, positive G loading, should be adequate up to AT LEAST 45 degrees of pitch (.707 G at that angle) with no lube problem. This is also about the same point that the carbs would start to "unport" and falter; long before the oil pump output pressure would drop below that required to maintain adequate lubrication in the journals.
In this latter case, combustion would cease, and, in all likelihood, so would the engine along with the mechanical oil pump, but if the engine isn't turning, no oiling is necessary. I've not tested the airspeed required to rotate a flamed-out 912 up to the point the oil pump will rotate fast enough to deliver normal-range pressure, nor am I about to investigate this situation. Observing the severity with which a 912 stops at shutdown, I'm thinking I'd have to install a mach-meter to run such a test!
Assuming positive Gs are maintained, light aerobatic maneuvers have always been a no-sweat issue with a 912, so it's obvious to me that a whole lot more details concerning the conditions of flight at the time of the alleged "blow-up" are needed before any conclusions can be drawn. Something here is just too fishy for fact-finding.
Anyhooo, WELCOME ABOARD GASSITT! I often wondered why you hadn't joined us earlier; I'm awfully glad to see you in this forum and, after your initial experience with us today, I sincerely hope you aren't rethinking the wisdom of your decision!
I'm personally delighted that the Desert Fox Squadron's personal Engine Guru, "Doctor" (I like to call him that) GASSITT, is now on board...operators are standing by!!!
"E.T."
Desert Fox 6
(Opposing Solo)