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So to answer your question: There was a problem with the DB 605 engine at the time which resulted in piston burn-through at higher boost pressure. I believe the root cause was bearings: Ball bearings had been replaced with roll bearings and the lubrication system was changed accordingly. With more powerful oil pumps the engine suffered from low oil pressure and lack of proper lubrication because of oil foaming.
Here is a transcript of a conversation between Reichsmarschall Göring and representants from Daimler-Benz and Junkers in September 1943:
Source: http://kurfurst.org/Engine/Boostclearances/DB605A_GLmeeting_September1943.html
But F4 has a diffirent engine right? And it was more developed at the time of Stalingrad and was allowed to use 1.42 for a short period.
But which engine has more power f4 1.42 or g2 1.3?
The F-4 turns slightly better than the G-2 but the G-2 does have a slight engine advantage since you won't be flying at WEP for the most part (1200 bhp in the F-4 vs 1300 bhp in the G-2 without WEP). This makes the G-2 a bit better as a "boom-and-zoom" fighter. The G-2 is also more effective at high altitude than the F-4.