MaydayMayday
Member
- Joined
- Aug 31, 2020
- Messages
- 19
When watching Mike Busch do his engine presentations he talks about recommended max CHT temperatures he say Max 400 F or 380 F in the tightly cowled engines like the Cirrus (or something like that).
Does anyone know what is the difference in design between the cooling baffle design of the Cirrus Continental engine verses another airplane that has the same Continental engine?
Thanks for the information.
Does anyone know what is the difference in design between the cooling baffle design of the Cirrus Continental engine verses another airplane that has the same Continental engine?
Thanks for the information.